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https://brilliant.org/problems/thats-all/
[ "# That's all?\n\nGeometry Level 2\n\nThe two larger angles of an isosceles triangle have a combined measure of $135^\\circ$. If this triangle has a perpendicular height of $2\\text{ m}$, find the length of its base in meters.\n\nIf the latter can be expressed in the form $a\\sqrt { b } -c$, where $a,b$ and $c$ are positive integers with $b$ square-free, write your answer as $a\\times b\\times c$.\n\n×" ]
[ null ]
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https://www.wired.com/2014/07/whats-the-difference-between-work-and-potential-energy/
[ "What's the Difference Between Work and Potential Energy?\n\nThe Work Energy Principle is one of the big ideas in introductory physics courses. It’s so big that the textbook presentation can get a little confusing – but it doesn’t have to be that way. How Do Textbooks Introduce the Work-Energy Principle? I haven’t looked in all the introductory textbooks, but it seems like they […]\n\nThe Work Energy Principle is one of the big ideas in introductory physics courses. It's so big that the textbook presentation can get a little confusing - but it doesn't have to be that way.\n\nHow Do Textbooks Introduce the Work-Energy Principle?\n\nI haven't looked in all the introductory textbooks, but it seems like they all follow a similar style. Oh, this is for the algebra-based physics course. That means no integration, no dot products.\n\nHere is how they do it (roughly).\n\nConservation of Energy. Many texts start off with some type of statement like \"energy is neither created nor destroyed\".\n\nTypes of Energy. There are many different types of energy: kinetic, potential, thermal energy, chemical energy.\n\nDefinition of Work. Work is defined as the ability to change energy. I know that sound silly, but sometimes textbooks make a circular definition like that. They then go on to define work in some way. Usually, it will look something like this:", null, "Just so you know, that's a fine definition of work.\n\nNon-Conservative Work. This is the part that most textbooks strive for. This is the version of the work-energy principle.", null, "Non-conservative work is a work that depends on the path. Conservative work is path independent. A great example of non-conservative work is the work done by friction. Suppose I push a block along a surface with friction from point A to point B along the two paths shown.", null, "The work done along path 2 will be greater than path 1. However, if this was work done by gravity (no friction) then the work done along the two paths would only depend on the starting and ending points. Gravity is conservative, friction is non-conservative. Why does this matter? Well, it turns out that for any conservative forces (like gravity, springs, electrostatic) you could make that work a potential instead of a \"work done by\". That's usually how a textbook explains it - perhaps it's not the best description.\n\nSpecial Cases. What about special cases where the work (non-conservative work) done is zero? In these cases, we can just say there is constant energy. Pick any two points in space and the following would be true:", null, "This isn't wrong, but it is just for the special case where the work is zero.\n\nA Different Approach\n\nWhy do we need a different approach? I think the above presentation is a little bit disjointed and confusing. Here is the way I present it in class. First, two notes. My views on work-energy are heavily influenced by the Matter and Interactions textbook (which I think is awesome). Second, it can cause a small problem when your approach isn't the same as the textbook.\n\nWhat is energy? Energy is just a way to view the world. The work-energy principle is a mathematical tool that works very well at predicting and explaining real world phenomena. That's it. The work-energy principle is just something that works (pun intended).\n\nThe simplest version of the work-energy principle is for a single point particle. The above definition of work is still fine, but in the case of a point particle the work-energy principle is:", null, "That's it. A point particle can only have kinetic energy. Note: in Matter and Interactions, this would be W = ΔE where is the energy of a particle. This version is different in that it includes an energy definition that works at relativistic speeds also.\n\nIt's all about the system. If you want a potential energy, you need to pick a system that includes more than just a mass. Let's consider a ball released from rest near the surface of the Earth that falls a distance h.\n\nIf I choose a system just consisting of the ball (which is sort of like a point mass) then I can look at the work done on this ball as it falls. What forces are acting on the ball? Just the gravitational force (mg). Since the gravitation force is in the same direction as the displacement, the angle between these two is zero. I can write:", null, "From here, you could solve for the velocity at the bottom position. Not too difficult.\n\nWhat if I change my system to include both the ball AND the Earth? In that case, I can subtract the work done by the gravitational force from both sides of the equation. I would get this:", null, "Algebraically, this is the same equation as before. However, this says that there is no work done on the system and instead we have a change in gravitational potential energy (U). The change in potential is then defined as the negative of the work done by that force. This is technically the gravitational potential energy of the ball-Earth system. In the end, you would get the same expression as before (with the system of just the point particle).\n\nBe careful. You can't have work done by gravity AND a change in gravitational potential energy. You have to do it one way or the other.\n\nThis means that the most important step in solving work-energy problems is choosing a system. For internal forces (like gravity) in a system, you will have a potential energy term.\n\nWhat about those special cases of conservation of energy? Yes, they can be useful at times - but you have to be careful to realize that they are just special cases.\n\nSummary\n\nAs I read over this post, it seems like I am that guy from Spinal Tap that tries to explain why his amplifier is better because the dial goes to 11. Yes, it might seem like I am basically saying the same thing as the textbooks. Let me emphasize the key points:\n\n• If you are talking about work but not a system, you are missing something.\n• You can do just about all of the basic problems in intro physics by picking a point particle as your system and having all the forces on that particle do work. You don't even need potential energy.\n• If you try to use energy = constant for some situation, be very careful. This is only true for some cases (not always true)." ]
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https://masaka.luxiarweddingphoto.com/building-estimate-xls/
[ "", null, "building estimate xls - Masaka.luxiarweddingphoto.com\n\n# Building Estimate Xls\n\nfree estimating software building remodeling .\n\nfree construction estimating spreadsheet for building and .\n\n001 construction estimating spreadsheet free expenses excel .\n\nfree construction cost estimating spreadsheet expenses excel .\n\nbuilding cost estimator spreadsheet magdalene project org .\n\n016 free construction cost estimate excel template in india .\n\nhouse building cost estimator spreadsheet home building cost .\n\nfree construction estimate templates collections .\n\nconstruction estimate spreadsheet excel house costs building .\n\nhow to estimate a construction project fine homebuilding .\n\nfree residential construction cost estimator magdalene .\n\n015 construction cost tracking spreadsheet house expenses .\n\nhow to estimate a construction project fine homebuilding .\n\nfile estimating spreadsheet png wikimedia commons .\n\n003 building construction estimate spreadsheet excel .\n\nhome construction cost estimate spreadsheet template new .\n\nnew home construction cost spreadsheet magdalene project org .\n\nhouse construction costing spreadsheet sheet excel building .\n\nhome construction estimating spreadsheet excel template cost .\n\nhome building cost estimate spreadsheet x residential .\n\nbuilding schedule template excel construction expenses .\n\nestimated construction cost spreadsheet construction cost .\n\nbuilding cost estimator spreadsheet islamopedia se .\n\nexcel estimating spreadsheet magdalene project org .\n\nresidential construction cost estimator excel software .\n\n010 house construction budget worksheet fantastic new .\n\nhome buildingost estimate spreadsheetonstruction expenses .\n\nconstruction cost estimating spreadsheet construction cost .\n\ndetailed construction cost estimate spreadsheet house .\n\nhome construction cost estimate spreadsheet estimating india .\n\nconstruction estimating spreadsheet template beautiful free .\n\nhome building cost breakdown spreadsheet best of residential .\n\nhome building budget template house construction estimate .\n\nconstruction cost estimate te template excel residential tor .\n\nresidential construction cost estimator excel estimate .\n\nresidential construction cost estimator residential .\n\nconstruction estimating excel spreadsheet building estimate .\n\nexcavation estimating spreadsheet horoscopul org .\n\nconstruction estimating spreadsheete xls building estimate .\n\nconstruction cost estimate template spreadsheet free .\n\nresidential construction cost estimator excel philippines .\n\nconstruction cost estimate home sheet template xls india .\n\nhome building cost estimate spreadsheet home building cost .\n\nexcel template home construction estimating spreadsheet new .\n\nresidential construction cost estimator muramasa info .\n\ncost estimate template in format software estimation xls .\n\nexcel spreadsheet for construction estimating .\n\nfree rehab repair cost estimator house flipping spreadsheet .\n\ncost estimate sheet bicibague co .\n\ndetailed construction cost estimate spreadsheet construction .\n\ncost estimate spreadsheet template of construction bid .\n\nbuilding cost estimator spreadsheet magdalene project org .\n\n005 template ideas construction cost estimate spreadsheet .\n\nbuilding construction material estimate spreadsheet excel .\n\ncost estimate spreadsheet extension renovation .\n\nresidential construction cost estimator excel breakdown .\n\nresidential construction budget template excel free format .\n\nconstruction estimating spreadsheet excel report templates .\n\ncost estimate sheet linkefa co .\n\nother size s home construction estimating spreadsheet cost .\n\nfree construction cost estimate template project excel .\n\nconstruction estimating software _ free cost estimate .\n\nspreadsheet example of home building cost estimate .\n\nconstruction cost estimate spreadsheet tagua .\n\nresidential construction budget template excel free .\n\nhome building estimate spreadsheet beautiful house flipping .\n\nuda construction estimating templates light commercial .\n\nhow to estimate construction projects shawnvandyke com .\n\nhouse construction costing spreadsheet residential .\n\nit project estimation template project estimation document .\n\nconstruction cost estimate spreadsheet template umbrello co .\n\n19 free estimate templates pdf doc xls free premium .\n\nconstruction estimate templates work estimate free template .\n\nconstruction cost estimate template xls templates .\n\nconstruction cost spreadsheet template building costing estimate .\n\ndetailed construction cost estimate spreadsheet building ." ]
[ null, "https://mc.yandex.ru/watch/65499823", null ]
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https://bodheeprep.com/base-system-advance
[ "Bodhee Prep-Online CAT Coaching | Online CAT Preparation | CAT Online Courses\n\n10% OFF on all CAT Courses. Discount code: BODHEE10. Valid till 31st May Enroll Now\n| Best Online CAT PreparationFor Enquiry CALL @ +91-95189-40261", null, "### Addition, Subtraction and Multiplication in different bases\n\nThe process of addition, subtraction and multiplication in bases other than 10 might sound difficult because we haven’t done much practice of it during our school days. But the process is exactly same as we do in decimal system.\n\nLet us see the process of addition of two numbers in decimal system, and then we will extend the logic to add two numbers in bases other than 10.\n\nSay, we have to add 368 to 437 i.e", null, "We start from right and add the unit digits, i.e. 8 + 7 = 15. Then we write 5 at the unit digit of the final answer and carry over the number 1 to next column of ten’s digits. We repeat the same process till the end.\n\nThe entire logic lies on the answer of the question that why did we carry over 1 and kept 5 at the unit place? The logic is, 15 can be written as 10+5 or $1 \\times 10 + 5$ (read 1 time 10 plus 5). So we kept 5 at the unit place and carried over 1.\n\n(If the sum was say 47, it would have been written as $4 \\times 10 + 7$, so we would have kept 7 at unit place and carried over the number 4).\n\nHence the logic is, whenever the sum is greater than the base, we divide the sum by the base, keep the remainder and carry over the quotient.\n\nExample: Calculate (456)7 + (234)7\n\nSolution:", null, "The addition of unit digits (6 and 4) is 10, which is more than 7, and would be written as $1 \\times 7 + 3$. The quotient is 1 and the remainder of 3. The Remainder is kept at the units place of the answer and the quotient gets carried over to the ten’s place. The process is repeated till the end.\n\nSimilarly, the process of subtraction and multiplication is same as explained above. Let us take few worked out examples.\n\nExample: Calculate  ${\\left( {54} \\right)_8} \\times {\\left( {36} \\right)_8}$\n\nSolution:\n\nFirst we multiple 6 with 4 = 24\n\n24 = 3$\\times$8 + 0, so the remainder 0 will be written at the unit place of the answer and 3 will be carried over to next column (ten’s digits column)", null, "Next, we multiply 6 with 5 and add 3 (carry) = 33. Again, 33 = 4$\\times$8 + 1 = (41)8. The Process till now looks like:", null, "Similarly, 3 multiplied by 4 = 12 = 1$\\times$8 + 4, so 4 is written in units place and 1 is carried over. Finally 3 multiplied by 5 + 1 (carry) = 16 = 2$\\times$8 +0 = (20)8. The process till now looks like:", null, "The last step is to add the two rows in base 8 to get the final answer which is equal to (2450)8\n\nExample: Calculate (753)9 – (476)9\n\nSolution:\n\nThe unit digits of the given numbers are 3 and 6, as 3 < 6 (we can’t subtract 6 from 3), we will take 1 carry from ten’s digit of the first number i.e 5 and the new ten’s place digit of the first number will become 4. As we are working in base 9, the weight-age of 1 carry is 9.  So 3 + 1 (carry) = 3 + 9 = 12.\n\nNow, 12 – 6 = 6 is the unit digit of the answer.\n\nSimilarly moving to the next column, the new ten’s digit of first number is 4 and ten’s digit of second number is 7, again we will repeat the same concept of carry as above. The final answer is illustrated below.", null, "Therefore, (753)9 – (476)9 = (266)9\n\n### Converting number from base x to base y, none of x and y is equal to 10\n\nThe standard approach is to convert the number in base x to the number in base 10 and then again convert this number in base 10 to the number in base y. i.e.\n\n(number)x ————–> (number)10 —————> (number)y\n\nThe process is repetitive and tedious if the number is large. However if the base y is some power of x, then the conversion is easy.\n\nExample: Convert (10011110101)2 to base 4.\n\nSolution:\n\nNote that 22 = 4, also the digits used in base 4 are 0, 1, 2, and 3.\n\nThe conversions of these digits in base 4 to base 2 are as follow:\n\n(0)4 = (00)2\n\n(1)4 = (01)2\n\n(2)4 = (10)2\n\n(3)4 = (10)2\n\nTo convert (10011110101)2 into base 4, we write the digits in pairs starting from the right hand side. i.e.\n\n(10011110101)2 = (01   00   11   11   01   01)2\n\nNow substituting the above conversion from base 2 to base 4 we get\n\n(10011110101)2 = (1 0 3  3 1 1)4\n\nSimilarly, if we have to convert (2322310)4 into base 2, it can easily be done by substitution as we did in the above problem, i.e.\n\n(2322310)4 = (10 11 10 10 11 01 00)2\n\nThe logic can be extended to base 8 also by using the following substitution:\n\n Binary Octal 000 0 001 1 010 2 011 3 100 4 101 5 110 6 111 7\n\nExample: convert (100010101010100011110)2 into base 8.\n\nSolution:\n\nGrouping digits of the number in groups of three from the right hand side we get (100  010  101  010  100  011  110)2\n\nNow substituting each group of digits with the corresponding equivalence in base 8 we get:\n\n(100  010  101  010  100  011  110)2 = (4 2 5 2 4 3 6)8\n\n### Important results related to divisibility rules in different bases\n\n1. If the sum of all the digits of a number in base x is divisible by x-1, then the number itself is divisible by x-1.\n\nExample:  Is (343626)9 divisible by 8?\n\nSolution:\n\nThe sum of digits = 3 + 4 + 3 + 6 + 2 + 6 = 24. As 24 is divisible by 8, the number (343626)9 is also divisible by 8.\n\n1. If a number in base x has even number of digits, and the number is a palindrome i.e. the digits equidistant from each end are the same, then the number is divisible by x+1.\n\nExample: (234432)7 is a six digit palindrome number and by the above result, it is divisible by 7+1 = 8.\n\nClick here to get one day FREE trial of full online CAT course\n\nFREE CAT Quant Practice Problems\n\nOnline CAT Quant Course\n\n### [PDF] CAT 2021 Question Paper (slot 1, 2 & 3) with Solutions\n\nCAT 2021 question paper PDF is available on this page. The page has the CAT 2021 question paper PDFs of all the three slots. There\n\n### All About CAT Mock Test Series\n\nTable of Content for CAT Mock Tests Ideal number of CAT Mock Test Series How many CAT mocks should one write What is the right\n\n### [PDF] CAT 2020 Question Paper (slot 1,2 &3) with Solution\n\nCAT 2020 question paper threw a number of surprises. Not only was there a change in exam pattern but also the difficulty level of almost\n\n### BIG change in CAT 2020 Paper Pattern\n\nAnnounced changes in CAT 2020 Pattern As we march towards the end of the year 2020, there is another unexpected turn in the sorry saga\n\n##### CAT Online Courses\n\nFREE CAT Prep Whatsapp Group" ]
[ null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%20800%20456'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%2089%20110'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%2089%20126'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%2078%2093'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%2078%2093'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%20132%20154'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%2089%20102'%3E%3C/svg%3E", null ]
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http://survo.fi/help/qu1_03.html
[ "#", null, "Help System (web edition)\n\n```TABTEST <table_of_frequencies>,L\nperforms various tests for independence etc. by simulation\nfor a two-dimensional table of frequencies. The table is\ngiven in edit field in the form used by the TAB operations.\nThe table can be also given in a simpler form without any labels:\nTABLE TEST / Example (An empty line indicates the end of the table.)\n7 2 0\n3 1 5\n\nDifferent assumptions about the stochastic structure of the table are\ndetermined by a FIX specification with following alternatives:\nFIX=Fisher Both row and column margins fixed (exact test)\nFIX=RC Both row and column margins fixed\nFIX=C Column margins (vertical sums) fixed\nFIX=R Row margins (horizontal sums) fixed\nFIX=N No fixed margins, only the grand total fixed\nFIX=F(i,j) Element of row i and column j fixed\nFIX=FIT Goodness of fit test for an n x 2 table\n\nThe test statistics used in simulation is selected by a TEST specification:\nTEST=X^2 is the common Pearson's chi-square statistics: sum of (O-E)^2/E .\nTEST=G^2 is the likelihood statistics: sum of -2*O*log(O/E) .\nTEST=PROB is the probability of the simulated table. The unknown\nmargin probabilities are replaced by simulated relative\nfrequencies. We call this `Probability statistics'.\nIn case FIX=Fisher, TEST=PROB is always selected.\nIn other cases TEST=X^2 is default.\n\nMaximum number of replicates is given by SIMUMAX (default 10000000).\nThe seed number of the random number generator (either 'rand' or 'urand')\nis given by RAND (default RAND=rand(12345). See RAND? .\nThe process may be interrupted by pressing any key.\n\nThe results are displayed after each 100 replicates as a table of the form\nN P Confidence interval (level=0.95)\n# of replicates Estimate of P lower limit\ns.e. Standard error upper limit\n\nThe confidence level for P is set by CONF=p (0.8<p<1). Default is CONF=0.95\nThe two-way table is also saved as a matrix by using the specification\nMATRIX=<name_of_a_matrix_file> , say, MATRIX=T .\nThis matrix can be analyzed further, for example, by the sucro command\n/X2\nwhich computes various derived tables as matrices such as the expected\nfrequencies and decomposition of the X^2 statistics in cells and\nmargins.\n\n........................................................................\nExample:\nTABLE T / This 2x2 table is tested with default settings.\n7 2\n1 4\n\nTABTEST T,CUR+1\n\nG = Goodness of fit test for an n x 2 table" ]
[ null, "http://survo.fi/survologo1.gif", null ]
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https://paramountestimating.com/7-steps-to-a-successful-roofing-job/
[ "# 7 Steps To A Successful Roofing Job\n\nUnderbidding is a common problem faced by the Roofing Industry nowadays. Most contractors not only underbid the job but undercut their profits as well. One of the major reasons behind this is that the roofer’s price by the number of squares instead of pricing by the time it takes them to get the job done which leads to them underestimating their overhead. Unprofessional bids are another mistake that the roofers make. There is a 90% chance of you underbidding a roofing job if you are unsure about roofing business pricing strategies.\nThe good news is you can always learn how to price and bid roofing jobs and attain a profit.\n\nFor effective pricing on the roofing job you need to follow this process:\n\n### 1. Properly understand the scope of your work\n\nInspecting the Roof\n\nDetermine the existing condition of the roof. If the flashings can’t be reused, then make sure to factor replacement flashings into your material costs. Identify all the unusual roof features, the condition, and the number of the valleys and all the damaged areas. Note down the number and condition of the vent stacks, eaves, and ridges. Also, determine whether the roof requires a complete tear-off and whether the existing materials can’t be used or not.\n\nChecking the Building Codes\n\nCheck the building codes to determine whether the existing layers can be shingled over and if the building codes allow another layer then make sure that the shingles are in good condition to support another layer. If another layer can’t be added that make sure to factor removal costs into the total estimate. Also determine which materials and colors are restricted by the Building Codes.\n\n### 2. Get the accurate measurements of the Roof\n\nCalculating the flat area of the Roof\n\nStand on the ground and measure the exterior of the house. Use these measurements to calculate the total area of the house. Then you need to divide the area of the home by 100 to find out the total number of squares. 1 square is usually covered by 3 shingles. Most of the residential roof are however pitched and we need to factor in the Roof Pitch into our calculations.\n\nDetermining the Pitch of the Roof\n\nThe roof pitch is the steepness or the slope of the roof that is created by the rafter. It is a measurement of how much the roof rises as compared to the horizontal measurement of the roof, also called the horizontal run of the roof.\n\nA ratio of 6:13 means that the roof rises 6 feet for every 13 feet of the horizontal length of the roof. The roof pitch can be either low, medium, or high. You need the measure the pitch of the house’s roof. Low pitch roofs have a ratio of 5:12 or less. Medium pitch roofs are in the ratio 6:12 or 9:12. High pitch roofs have a ratio of 10:12 to 12:12.\n\nDetermine the Roof Pitch Multiplier\n\nThe Roof Pitch multiplier is a number that is multiplied by the square foot area of the sloped roof to produce the actual surface area of the roof. A roof pitch multiplier chart is used to find out the pitch multiplier to which the ground level squares of the house’s roof, that is calculated, is multiplied to. Low pitch roofs are multiplied by a factor of 1.15 to 1.25. Medium pitch roofs are multiplied by a factor of 1.24 to 1.4. And a factor of 1.4 to 1.7 is used for high roof pitches.\n\n### 3. Estimating Material Costs\n\nDetermine the Materials Needed\n\nAfter you have the measurements of the roof, you will need to determine the type and the quantity of the required materials. List these materials down and calculate the total cost of materials. The material’s list usually includes Shingles, Nails, Flashing, Underlayment, Moisture Barriers, and Dumpsters for Shingle Removal.\n\nCalculating the Material Costs\n\nFor estimating the total number of shingles required, you will use the square footage of your house you just calculated above. The total number of squares will tell you how many shingles will be needed to cover the entire roof. Underlayment is another vital roofing material that is placed underneath the shingles and acts as a second line of defense against water damage to the roof. Once you have the total square footage of the roof you can use it to estimate the amount of underlayment. One roll of underlayment covers 4 squares. So by dividing the total number of squares by 4, we can find out the total number of underlayment required. Since Nails are sold by the pound, you will require 2 and a half pounds for each square. The most common roofing material is asphalt shingles but solar tiles, metal roofing, and rubber slate are also used. Contact your supplier to get the square footage cost of the roofing material you are using. Sum up the cost of all the materials you are using to get the total cost.\n\n### 4. Estimating the Labor Costs\n\nFor estimating the labor costs you need to first determine the labor hours, which are the hours the job will take, and then multiply it by the total number of employees on the job. Now you will need to work out the hourly labor cost. The hourly labor cost will include both the worker’s wage along with the taxes and worker’s compensation. Once you have the labor hours and the hourly wage, you will calculate the total labor cost by multiplying the labor hours with the hourly wage.\n\n### 5. Estimating the Overhead Costs\n\nOverhead costs include the costs for uniforms, accounting, rent, insurance and tools. For your business to be profitable, the price you charge must include the cost for all of these.\n\n### 6. Determining the Total Cost and Adding Markup\n\nAdd all the costs you just estimated in order to get the breakeven cost the roofing job requires. Add a markup into your total cost so that you can profit from the services you are providing. Markup is usually expressed as a percentage and it is calculated using the formula Profit/Cost * 100. The markup percentage you chose to add to the breakeven cost depends upon the Profit Margin. While pricing the roofing job, one must aim for the margin above the industry average which is 6%. You need to markup your total cost with a percentage greater than the margin to achieve your desired margin." ]
[ null ]
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https://astarmathsandphysics.com/index.php?option=com_content&view=article&id=2047:cantor-s-theorem&catid=160&Itemid=1799
[ "## Cantor's Theorem\n\nWith the cardinality of a set defined as the number of elements of a set, it might seem obvious that thee is no largest cardinal number. To find a larger cardinal number, just find a set with more elemts. However, many sets have an infinite number of elements. What we really mean in saying that the is no largest cardinal number is that there is no limit to the order of infinity. No matter how infinitely large our set is, there is always an infinitely larger set.\n\nThis is called Cantor's Theorem. More concisely, it states: for any set", null, "", null, "(or", null, "where", null, "is the power set, the set of all subsets of", null, "If", null, "has", null, "elements, it has", null, "possible subsets.\n\nWe can prove the theorem by induction on successive power sets", null, "", null, "", null, "", null, "and so on", null, "Now set", null, "", null, "is infinite so", null, "and here is no largest cardinal number.", null, "" ]
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https://www.khanacademy.org/math/calculus-1/cs1-analyzing-functions/cs1-connecting-f-f-and-f/v/justification-using-first-derivative
[ "If you're seeing this message, it means we're having trouble loading external resources on our website.\n\nIf you're behind a web filter, please make sure that the domains *.kastatic.org and *.kasandbox.org are unblocked.\n\n# Justification using first derivative\n\nAP.CALC:\nFUN‑4 (EU)\n,\nFUN‑4.A (LO)\n,\nFUN‑4.A.10 (EK)\n,\nFUN‑4.A.11 (EK)\n\n## Video transcript\n\n- [Instructor] \"The differentiable function f \"and its derivative f prime are graphed.\" So, let's see. We see the graph of y is equal to f of x here in the blue. And then f prime we see in this brownish-orangish color right over here. \"What is an appropriate calculus-based justification \"for the fact that f is decreasing \"when x is greater than three?\" So, we can see that that actually is indeed the case. When x is greater than three, we see that our function is indeed decreasing. As x increases, the y value, the value of our function, decreases. So, a calculus-based justification, without even looking at the choices, well, I could look at the derivative. And we're going to be decreasing if the slope of the tangent line is negative, which means that the derivative is negative. And we can see that for x is greater than three, the derivative is less than zero. So, my justification, I haven't even looked at these choices yet. I would say for x is greater than three, f prime of x is less than a zero. That would be my justification, not even looking at these choices. Now let's look at the choices. \"f prime is decreasing when x is greater than three.\" Now, this isn't right. What we care about is whether f prime is positive or negative. If f prime is negative, if it's less than zero, than the function itself is decreasing. The slope of the tangent line will be negative. f prime could be positive while decreasing. For example, f prime could be doing something like this. And even though f prime would be decreasing in this situation, the actual value of the derivative would be positive, which means the function would be increasing in that scenario, so I would rule this one out. \"For values of x larger than three, as x values increase, \"the values of f of x decrease.\" Now, that is actually true. This is actually the definition that f is decreasing. As x values increase, the values of f of x decrease. But this is not a calculus-based justification, so I am going to rule this one out as well. \"f prime is negative when x is greater than three.\" Well, that's exactly what I wrote up here. If f prime is negative, then that means that our slope of the tangent line of our original function f is going to be downward sloping, or that our function is decreasing, so this one is looking good. And this one right over here says, \"f prime of zero is equal to negative three,\" so they're just pointing out this point. This isn't relative to the interval that we care about, or this isn't even relevant when x is greater than three, so we definitely wanna rule that one out. Let's do one more of these. So, here we're told, \"The differentiable function g \"and its derivative g prime are graphed.\" So, once again, g is in this bluish color, and then g prime, its derivative, is in this orange color. \"What is an appropriate calculus-based justification \"for the fact that g has a relative minimum point \"at x is equal to negative three?\" And we could see here, when x is equal to negative three, it looks like g is equal to negative six, and it looks like a relative minimum point there. So, what's the best justification? So, once again, without even looking at the choices, I would say a good justification is before we get to x equals negative three, before we get to x equals negative three, our derivative, and this is a calculus-based justification, before we go to x equals negative three, our derivative is negative. And after x equals negative three, our derivative is positive. That would be my justification. Because if our derivative is negative before that value, that means that we are downward sloping before that value. And if it's positive after that value, that means we're upward sloping after that, which is a good justification that we are at relative minimum point right over there. So, let's see, \"The point where x equals negative three \"is the lowest point on the graph of g \"in its surrounding interval.\" That is true, but that's not a calculus-based justification. You wouldn't even have to look at the derivative to make that statement, so let's rule that one out. \"g prime has a relative maximum at zero comma three.\" At zero comma three, it actually does not. Oh, g prime, yes, g prime actually does have a relative maximum at zero comma three, but that doesn't tell us anything about whether we're at a relative minimum point at x equals negative three, so I would rule that out. \"g prime of negative three is equal to zero.\" So, g prime of negative three is equal to zero, so that tells us that the slope of the tangent line of our function is going to be zero right over there, but that by itself is not enough to say that we are at relative minimum point. For example, I could be at a point that does something like this where the slope of the tangent line is zero, and then it keeps increasing again, or it does something like this and it keeps decreasing. So, even though you're at a point where the slope of your tangent line is zero, it doesn't mean you're at a relative minimum point, so I would rule that out. \"g prime crosses the x-axis from below it to above it \"at x equals negative three.\" g prime crosses the x-axis from below it to above it. Yep, and that's the argument that I made, that we're going from below the x-axis, so g prime goes from being negative to positive, which means the slope of the tangent lines of our points as we approach x equals negative three go from being downward sloping to upward sloping, which is an indication that we are at a relative minimum point." ]
[ null ]
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http://xcelvations.com/blog/ActivityManager.ipynb
[ "# ActivityManager.ipynb\n\nIn :\nfrom xv.math.activity import ActivityManager\n\nIn :\nke = ActivityManager()\nke\n\nOut:\n2641992486576@ActivityManager\n\nMisc activities for students, with external links\n\nExample:\nke = ActivityManager()\nke.getRandomProblem()\nke.getRandomProblem(problem_type = 0)\n...\n\nke.printProblem()\nke.printSolution()\n\nke.printProblemTypes()\n\nIn :\nke.printProblemTypes()\n\n0. _problem_mobius_strip\n1. _problem_four_color_theorem\n2. _problem_right_angle_similar_triangles\n3. _problem_triangle_with_angles_more_than_2_pi\n\nIn :\nke.getRandomProblem(problem_type = 1)\n\nOut:\nTake picture of a map and color all different countries of a region with minimum number of colors. How many colors you need?\nIn :\nke.printAnswer()\n\nOut:\nYou need four colors.\nIn :\nke.printSolution()\n\nOut:\nIt is called Four Colour Theorem. Try to draw a network map of all countries you are coloring.\n\nDraw a network graph of countries with edges for direct contact. Color the nodes with different colors. You will find that all you need is four different colors.\n\n#### Resources:\n\nIn [ ]:" ]
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http://sdhacc.org/index.php?m=index&c=exhibitors_pro&a=company&id=184
[ "## 商会工作 会员动态 资讯中心 供求信息 培训交流 function searchnew(n,m) { var sUrl; var a; var sel=document.getElementsByName(\"cate_idser\"); var p= sel.options[sel.options.selectedIndex].value;//你要的值 if(p=='1'){a = \"/index.php?m=index&c=commerce&a=index&k={keyword}\";} if(p=='2'){a = \"/index.php?m=index&c=dynamic&a=index&k={keyword}\";} if(p=='3'){a = \"/index.php?m=index&c=news&a=index&k={keyword}\";} if(p=='4'){a = \"/index.php?m=index&c=supply&a=index&k={keyword}\";} if(p=='5'){a = \"/index.php?m=index&c=promote&a=index&k={keyword}\";} s = encodeURIComponent(document.getElementById(n).value); sUrl = a.replace(/\\{keyword}/, s) window.location.href = sUrl; return; }", null, "", null, "I am honored on behalf of the company, to express my most sincere thanks to thos。。。。[更多]", null, "", null, "", null, "", null, "" ]
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http://www.jzus.zju.edu.cn/article.php?doi=10.1631/jzus.A1400199
[ "Full Text:", null, "<1759>\n\nSummary:", null, "<979>\n\nCLC number: U260.331\n\nOn-line Access: 2014-12-04\n\nRevision Accepted: 2014-11-03\n\nCrosschecked: 2014-11-07\n\nCited: 5\n\nClicked: 4506\n\nCitations:  Bibtex RefMan EndNote GB/T7714", null, "ORCID:\n\nXue-song JIN\n\nhttp://orcid.org/0000-0003-3033-758X\n\nShuo-qiao ZHONG\n\nhttp://orcid.org/0000-0003-1990-5865\n\n Journal of Zhejiang University SCIENCE A 2014 Vol.15 No.12 P.984-1001 http://doi.org/10.1631/jzus.A1400199", null, "Effect of the first two wheelset bending modes on wheel-rail contact behavior*\n\n Author(s):  Shuo-qiao Zhong, Jia-yang Xiong, Xin-biao Xiao, Ze-feng Wen, Xue-song Jin Affiliation(s):  . State Key Laboratory of Traction Power, Southwest Jiaotong University, Chengdu 610031, China Corresponding email(s):   zhongsq1234@163.com Key Words:  High-speed railway vehicle, Wheel-rail contact behavior, Rigid wheelset, Flexible wheelset, Modal analysis, Random track irregularity Share this article to: More <<< Previous Article|Next Article >>>\n\nShuo-qiao Zhong, Jia-yang Xiong, Xin-biao Xiao, Ze-feng Wen, Xue-song Jin. Effect of the first two wheelset bending modes on wheel-rail contact behavior[J]. Journal of Zhejiang University Science A, 2014, 15(12): 984-1001.\n\n@article{title=\"Effect of the first two wheelset bending modes on wheel-rail contact behavior\",\nauthor=\"Shuo-qiao Zhong, Jia-yang Xiong, Xin-biao Xiao, Ze-feng Wen, Xue-song Jin\",\njournal=\"Journal of Zhejiang University Science A\",\nvolume=\"15\",\nnumber=\"12\",\npages=\"984-1001\",\nyear=\"2014\",\npublisher=\"Zhejiang University Press & Springer\",\ndoi=\"10.1631/jzus.A1400199\"\n}\n\n%0 Journal Article\n%T Effect of the first two wheelset bending modes on wheel-rail contact behavior\n%A Shuo-qiao Zhong\n%A Jia-yang Xiong\n%A Xin-biao Xiao\n%A Ze-feng Wen\n%A Xue-song Jin\n%J Journal of Zhejiang University SCIENCE A\n%V 15\n%N 12\n%P 984-1001\n%@ 1673-565X\n%D 2014\n%I Zhejiang University Press & Springer\n%DOI 10.1631/jzus.A1400199\n\nTY - JOUR\nT1 - Effect of the first two wheelset bending modes on wheel-rail contact behavior\nA1 - Shuo-qiao Zhong\nA1 - Jia-yang Xiong\nA1 - Xin-biao Xiao\nA1 - Ze-feng Wen\nA1 - Xue-song Jin\nJ0 - Journal of Zhejiang University Science A\nVL - 15\nIS - 12\nSP - 984\nEP - 1001\n%@ 1673-565X\nY1 - 2014\nPB - Zhejiang University Press & Springer\nER -\nDOI - 10.1631/jzus.A1400199\n\nAbstract:\nThe objective of this paper is to develop a new wheel-rail contact model, which is suitable for considering the effect of wheelset bending deformation on wheel-rail contact behavior at high speeds. Dummies of the two half rigid wheelset are introduced to describe the spacial positions of the wheels of the deformed wheelset. In modeling the flexible wheelset, the first two wheelset bending modes are considered. Based on the modal synthesis method, these mode values of the wheelset axle are used to solve the motion equations of the flexible wheelset axle modeled as an Euler-Bernoulli beam. The wheel is assumed to be rigid and always perpendicular to the deformed axle at the wheel centre. In the vehicle model, two bogies and one car body are modeled as lumped masses. Spring-damper elements are adopted to model the primary and secondary suspension systems. The ballasted track is modeled as a triple layer discrete elastic supported model. Two high-speed vehicle-track models, one considering rigid wheelset models and the other considering flexible wheelset models, are used to analyze the differences of the numerical results of the two models in both frequency and time domains. In the simulation, a random high-speed railway track irregularity is used as wheel-rail excitations. Wheel-rail forces are calculated and analyzed in the time and frequency domains. The results clarify that this new contact model can characterize very well the influence of the first two bending modes of the wheelset on contact behavior.\n\n## 1.  Introduction\n\nHigh-speed railways are currently popular globally. However, there are some problems including passenger riding comfort, noise pollution, and even operational safety (Jin et al., ). Rail corrugation, rail welding irregularity, wheel burning, and wheel out-of-roundness (OOR) generate high-frequency components of the dynamic wheel-rail contact forces that contribute significantly to the total wheel-rail contact forces (Nielsen et al., ), and reduce the life of the components of track and vehicle, such as wheels, rails, and fasteners. Rail grinding and wheel re-profiling are the most common measures that have been proved to be effective in controlling rail irregularities and wheel OOR. However, these measures lead to notably high maintenance costs. A lot of measurements at the sites and coupling vehicle-track dynamics modeling have been carried out to investigate the mechanism and development of these phenomena. In the vehicle-track dynamics modeling, a rigid multi-body system is often adopted to simulate railway vehicles, based on several commercial codes available for the low-frequency domain, such as GENSYS, NUCARS, SIMPACK, and VAMPIRE. These computer programs are generally used to analyze railway vehicle dynamics responses at frequencies below 20 Hz, where the influence of rigid motions of the vehicle on wheel-rail contact forces is dominant (Nielsen et al., ). To analyze the vehicle dynamic responses at mid- and high-frequencies, the vehicle structural flexibility should be taken into account in the modeling. It is obvious that wheelset structural flexibility has an influence on wheel-rail contact behaviors at mid- and high-frequencies. Different flexible wheelset models have been set up due to various motivations in the past (Chaar, ).\n\nThe methods applied to modeling flexible wheelset can be summarized as three major categories (Chaar, ). The first is a lumped model developed in a simple and convenient way, in which a wheelset is divided into several parts interconnected with springs and dampers. This model can describe the bending and torsional motions of the wheelset with only a few degrees of freedom, which could not be applied to studying wear phenomena on wheel treads or rails (Popp et al., ). The second is a continuous model developed by Szolc (; ), in which the wheelset axle was modeled as a beam, and two wheels and brake discs were modeled as rigid rings attached to the axle through a massless, elastically isotropic membrane. The model can characterize the wheelset dynamic behavior in the frequency range of 30–300 Hz. In the model proposed by Popp et al. (), the wheelset axle was considered as a 1D continuum, having the properties of a bar, a torsional rod, and a Rayleigh beam. The wheel was considered as a 2D continuum, having the properties of a disc and a Kirchhoff plate. The third was developed based on finite element method (FEM), which simulates wheelset flexibility more realistically than the first two categories of model. The wheelset modes and corresponding natural frequencies were obtained through the modal analysis of the finite element (FE) model by using the commercial software, and they were input into the simulation by means of the commercial codes (SIMPACK, NEWEUL) (Meinders and Meinker, ) or some non-commercial multi-body dynamic system codes. The non-commercial code developed by Fayos et al. () and Baeza et al. (; ) introduced the Eulerian coordinate system to replace the Lagrangian coordinate system in the flexible wheelset modeling. In this way it is convenient to obtain the motion of fixed physical nodes, and consider the inertial effect due to wheelset rotation. Relying on current computing power, it is feasible to use FEM to consider the effect of flexible wheelset in modeling a railway vehicle coupling with a track.\n\nRegarding the wheel-rail contact treatment in considering flexible wheelset influence, wheel-rail rolling contact condition is simplified based on different prior assumptions, especially in the detection of wheel-rail contact points. This is the prerequisite for the calculation of wheel-rail creepages and contact forces. Baeza et al. () neglected the effect of the high-frequency deformation and the deviation of a rotating flexible wheelset rolling over a flexible track model on the wheel-rail contact point in the investigation into the effect of the rotating flexible wheelset on rail corrugation. Through the detailed calculation Kaiser and Popp () found that the contact point was in the location where the wheel and the rail had positive penetration maxima, and the penetration direction was orthogonal to the common tangent plane of the wheel and the rail before their deformations. A linear wheel-rail contact model was proposed and used to carry out the detection of wheel-rail contact point and the contact zone’s normal direction (Andersson and Abrahamsson, ). In the detection, the functions were created using a first-order Taylor expansion around a reference state described by a group of parameters which represent a configuration, in which the train was in static equilibrium and the wheel and the track were free from geometric imperfections. The advantage of this approach is that the contact position and orientation in each time step can be calculated by interpolation replacing iterations, which results in a low computational cost. But the approach is only suitable for the case that the effect of all the parameters is very small on the contact point position and the contact patch orientation around the references is in static equilibrium. The wheel-rail contact point position and the contact patch orientation greatly depend on parameters, such as the curvatures of wheel and rail. In (Torstensson et al., ; Torstensson and Nielsen, ), the contact point detection was done before the simulation and used in the subsequent time integration analysis in the form of look-up table. The commercial software GENSYS allows for such calculations using the pre-processor KPF (from Swedish contact point function). In the KPF, the location and orientation of the contact patch were assumed to be dependent only on the relative displacement in the lateral direction between the wheelset and the rails, and hence the influence of the wheelset yaw angle was not taken into account. In some other papers detailed discussions on the wheel-rail contact model were omitted. In this study, the wheel-rail contact model considering the effect of wheelset flexibility (Zhong et al., ; ) is further improved and the new contact model is suitable for the analysis on the effect of the local higher-frequency deformation of the wheels on the wheel-rail contact behavior.\n\n## 2.  Vehicle-track coupling dynamic system\n\nA flexible wheelset model (to be illustrated in Section 2.1) and a suitable wheel-rail contact model (to be discussed in Section 2.2) are integrated into the vehicle-track coupling dynamic system model. All parts of the vehicle system, except for its four wheelsets, are considered as rigid bodies. The primary and secondary suspension systems of the vehicle are modeled with spring-damper elements. A triple layer model of discrete elastic support is adopted to simulate the ballasted track. The rails are modeled as Timoshenko beams. The sleepers are modeled as rigid bodies and the ballast model consists of discrete equivalent masses. The equivalent spring-damper elements are used as the connections between the rails and the sleepers, the sleepers and the equivalent ballast bodies, and the ballast bodies and the roadbed. Fig. 1 shows the vehicle-track coupling dynamic system model. The equations of motion of each component of the vehicle excluding wheelsets and the track are illustrated in detail in (Xiao et al., ; ; ). The parameters and their values describing the dynamic models are given in Appendix A.\n\n### 2.1.  Flexible wheelset model\n\nThe wheelset structural flexibility is considered by modeling the wheelset axle as an Euler-Bernoulli beam in two planes, one perpendicular to the track centerline and the other parallel to the track level. The crossing effect of the bending deformations in the two planes is ignored. In the first two bending modes obtained using the modal analysis of the FE model of a wheelset, two wheels have little deformation (Fig. 2), and their frequencies are in the available frequency range (0–500 Hz) of an Euler-Bernoulli beam model. Therefore, two wheels can be treated as rigid bodies in this study.", null, "Fig.2\nThe first two bending modes obtained using FE model\n\nThere are two force systems acting on the wheelset, one is the wheel-rail contact forces and the other is the forces of the primary suspension system (Fig. 3).", null, "Fig.3\nForce analysis diagram of the flexible wheelset\n\nIn Fig. 3, O fL and O fR are the left and right points on the axle, respectively, where the primary suspension force systems are applied. O CL and O CR are the left and right contact points of wheel-rail, respectively. O indicates the origin of the coordinate system O-XYZ that is a coordinate system with a translational motion along the tangent track centerline at operational speed. If the speed is constant, this coordinate system is an inertial coordinate system, and therefore regarded as an absolute coordinate system (geodetic coordinate system).\n\nTo analyze the axle’s deformation, the force systems from wheel-rail interaction acting on the left and right wheel treads are translated to the nominal circle centers O L and O R, respectively, and extra moments are produced in the procedure of translating contact forces. Thus, the force systems acting on the axle in the two planes are obtained in Fig. 4.", null, "Fig.4\nForce analysis diagram in the plane O-YZ (a) and in the O-XY plane (b)\n\nThe notations of the variables and symbols are defined in Table 1. The subscript p denotes the primary suspension, the subscripts x, y, and z denote X-, Y-, and Z-direction, respectively, and A denotes the axle.\n\n#### Table 1\n\nThe notations of the variables\n Variable Explanation u pLz , u pRz Z-direction components of the displacements of the nodes where the left and right primary suspension forces are applied on the axle, respectively u pLy , u pRy Y-direction components of the displacements of the nodes where the left and right primary suspension forces are applied on the axle, respectively u pLx , u pRx X-direction components of the displacements of the nodes where the left and right primary suspension forces are applied on the axle, respectively L Length of the wheelset axle F pLx , F pLy , F pLz X-, Y-, and Z-direction components of the primary suspension forces on the left sides of a wheelset F pRx , F pRy , F pRz X-, Y-, and Z-direction components of the primary suspension forces on the right sides of a wheelset F ALx , F ALy , F ALz X-, Y-, and Z-direction components of the forces between the left wheel and the axle of a wheelset F ARx , F ARy , F ARz X-, Y-, and Z-direction components of the forces between the right wheel and the axle of a wheelset M ALx , M ALz X- and Z-direction components of the moments between the left wheel and the axle of a wheelset M ARx , M ARz X- and Z-direction components of the moments between the right wheel and the axle of a wheelset E Young’s modulus Ix Cross-sectional area moment of inertia about the X axis Iz Cross-sectional area moment of inertia about the Z axis t Time uz (y,t), ux (y,t) X- and Z-direction components of the displacements of the nodes on the axle at time t, respectively Qz (y,t), Qx (y,t) X- and Z-direction components of the forces on the axle at time t, respectively Mz (y,t), Mx (y,t) X- and Z-direction components of the moments on the axle at time t, respectively m w Mass of a wheel g Gravity acceleration a Lz , a Rz Z-direction components of the accelerations of the left and right wheels, respectively a Lx , a Rx X-direction components of the accelerations of the left and right wheels, respectively J w Mass moment of inertia about the diameter of the wheel α Lx , α Rx X-direction components of the angular acceleration of the left and right wheels, respectively α Lz , α Rz Z-direction components of the angular acceleration of the left and right wheels, respectively u′ z (y,t), u′ x (y,t) The first derivative of uz (y, t), ux (y, t) with respect to y, respectively y wL, y wR y coordinates of the joints of the left and right wheels and the axle, respectively F wrLx , F wrLy , F wrLz X-, Y-, and Z-direction components of the left wheel-rail contact forces, respectively F wrRx , F wrRy , F wrRz X-, Y-, and Z-direction components of the right wheel-rail contact forces, respectively O cL, O cR Left and right wheel-rail contact point, respectively O wL, O wR Centers of the nominal circles of the left and right wheels, respectively O wL-X wL Y wL Z wL, O wR-X wR Y wR Z wR Body coordinate systems attached to the left and right wheels, respectively qzk , The kth generalized coordinate and the kth generalized acceleration coordinate in the plane O-YZ qxk , The kth generalized coordinate and the kth generalized acceleration coordinate in the plane O-XY ωk The kth circular frequency N Considered number of the modes Uzk (y), U′ zk (y) The kth mode function of the axle in the O-YZ plane and its first derivative with respect to y Uxk (y), U′ xk (y) The kth mode function of the axle in the O-XY plane and its first derivative with respect to y\n\nThe differential equation for the flexural vibration of an Euler-Bernoulli beam (the axle) in the plane O-YZ is written as , where , .\n\nThe force analysis diagram of the two wheels including the D’Alembert forces is shown in Fig. 5, based on which differential equations of motion of the two wheels are written as , .\n\nNote that the lateral accelerations of the wheels are assumed to be the same as the wheelset axle so there is no relative motion between wheels and axle.\n\nSubstituting the expressions of F A(L,R)z and M A(L,R)x obtained through Eqs. (4) and (5) into Eqs. (2) and (3), respectively, we can obtain: , , , where .\n\nConsider a solution of Eq. (8) in the form: . Using the calculus of variation (Qiu et al., ), the modal function satisfies: , , , where δij is the Kronecker delta. For i=j, Eq. (11) can be written as .\n\nTo obtain the mode shape functions with the wheelset axle modeled as a uniform Euler-Bernoulli beam carrying two particles (wheels), the segment of the beam from the left end to the first particle is referred to as the first portion, in between the two particles as the second portion and from the second particle to the right end as the third portion. The beam mode shape will be the superposition of the mode shapes of the three portions. The derivation of the mode shape functions is presented in Appendix B. The first three modes have the frequencies of f 1=111 Hz, f 2=245 Hz, and f 3=547 Hz, respectively. These mode shape functions are normalized so as to satisfy Eq. (14), as shown in Fig. 6. The third mode is not in the frequency range of 0–500 Hz where the Euler-Bernoulli beam is available to analyze the system. Hence, the effect of the first two modes on dynamic responses is conducted in this study.", null, "Fig.6\nThe first three bending mode shapes of the wheelset\n\nAccording to the modal analysis, we let the solution of Eq. (8) have the form: .\n\nSubstituting Eq. (15) into Eq. (8), the differential equation can be written as .\n\nMultiplying both sides of Eq. (16) by and integrating over the domain 0<y<L, we can obtain: .\n\nUsing the orthogonality of the modal shape function as expressed in Eqs. (11) and (13), Eq. (17) can be written as , where .\n\nEq. (18) can be expressed as . Eq. (20) can be written in the matrix form: , where\n\nThe explicit integral method illustrated in (Zhai, ) is used to obtain the vector of each acceleration coordinate.\n\nFor the vibration in the plane YOX, the differential equation expressed with respect to can be written as .\n\nThe derivation of Eq. (23) is similar to that of Eq. (20) and omitted here. Eq. (23) can be expressed in matrix form: , where\n\n### 2.2.  Wheel-rail contact model\n\nAs mentioned in Section 2.1, the main concern in this work is the wheelset axle bending. The wheels are assumed to be rigid and their nominal rolling circles are always perpendicular to the deformed wheelset axle at their interference fit surfaces. Fig. 7 shows that the flexible wheelset moves from its initial reference state (O 1(t 1)) to its t 2 status (O 2(t 2)), which is described in the plane of O-YZ. O 1 is the center of the un-deformed wheelset at t 1, and O 2 is the center of the deformed wheelset at any time t. O 1 O 2 is the displacement vector of the wheelset center due to its rigid motion, and ϕ R1 is the roll angle due to the wheelset rigid motion. The auxiliary line, , is the central line of the un-deformed wheelset axle, is obtained by moving from O 1(t 1) to O 2(t 2), and is obtained through rotating by ϕ R1. is actually the central line of the rigid wheelset axle at t 2. Fig. 7 shows that the wheels are assumed to be rigid and always perpendicular to the deformed axle line at their connections at any time t 2.", null, "Fig.7\nA flexible wheelset moving from its initial reference state (O 1(t 1)) to its any status (O 2(t)) in the plane of O-YZ\n\nTo clearly describe the new wheel-rail contact model, the dummies of the two rigid half wheelsets, as shown in Fig. 8, are employed to describe wheel-rail rolling contact behavior affected by the wheelset bending. The two dummies are indicated by DWL and DWR, respectively, and the wheels of the DWL and the DWR are assumed to overlap the left and right wheels of the flexible wheelset, respectively, all the time, namely, the motion of the assumed rigid wheels of the flexible wheelset can be described by the DWL and the DWR (Fig. 8). ϕ R2 is the roll angle of the right wheel due to the bending deformation of the flexible wheelset. It is exactly the included angle between the line and the axle line of the right wheel or the wheel of the DWR.", null, "Fig.8\nThe relationship between the two rigid half-wheelset dummies and the flexible wheelset\n\nIt is not difficult to calculate the wheel-rail contact geometry considering the effect of the flexible deformation of the wheelset or the local high-frequency deformations of the wheels if the spatial positions of the DWL and the DWR are determined. Determining the spatial positions of the DWL and the DWR involves calculating their motion parameters, such as the lateral displacements of the centers of the wheels of the DWL and the DWR, indicated by y DWL and y DWR, respectively, the vertical displacements, z DWL and z DWR, the roll angles, ϕ DWL and ϕ DWR, and the yaw angles, ψ DWL and ψ DWR. These parameters are key to calculating the contact geometry of the flexible wheelset in rolling contact with a pair of rails by using this new wheel-rail contact model. This will now be demonstrated in detail.\n\nFig. 8 describes the motion of the DWL and the DWR influenced by the wheelset bending and its rigid motion in the O-YZ plane only. After the rigid wheelset moves with the center displacement of O 1 O 2 and the rolling angle of ϕ R1 in the O-YZ plane of the global reference, O-XYZ, its center position O 1(t 1) reaches the position O 2(t 2) and reaches (or becomes) . Note that the vector O 1 O 2 and the roll angle ϕ R1 around axis X are described in the O-YZ plane. The dash-dot line is through point O 2(t 2) and parallel to . From Fig. 6, it is obvious that the rolling angle of the DWR caused by the wheelset rigid motion is just ϕ R1, and that caused by the wheelset bending deformation is ϕ R2, so the total rolling angle of the DWR is ϕ DWR=ϕ R1+ϕ R2, as shown in Fig. 6.\n\nIn addition, the displacement of the DWR is the vector O 1 O 3R, which could be written as .\n\nIn Fig. 8, the vector O 2 A 1 is parallel to O 3R A 2 with the same length l 0. l 0 is actually the distance between the center of the wheel nominal circle and the center of the un-deformed wheelset. The vector O 2 O 3R is parallel to A 1 A 2, with the same length. Thus, O 1 O 3R can be written as .\n\nMoreover, the vector O 2 A 1 is described by {x 1 y 1 z 1}[ i j k ]T in O-XYZ, and can be obtained by rotating the vector {0 l 0 0}[ i j k ]T (coinciding with the line ) about the X-axis by ϕ DWR. O 2 A 1 is written as .\n\nThe curve (Fig. 6) is the deformed axle center line of the wheelset, which does not consider the influence of the rotation caused by the wheelset rigid motion. The point B R is the center of the right nominal circle. The axle center line () of the deformed wheelset, can be obtained by rotating about the X-axis by ϕ R1. According to the definition of the curve , the vector O 2 B R is defined as , where {Δx 2 Δy 2 Δz 2}[ i j k ]T is the displacement vector of the center of the right nominal circle due to the axle bending. Then the vector O 2 A 2 is defined as {x 3 y 3 z 3}[ i j k ]T, and can be written as , which is obtained according to the relationship between and , or obtained by rotating by ϕ R1. The wheelset center displacement vector O 1 O 2 is defined as {x 0 y 0 z 0}[ i j k ]T.\n\nSubstituting Eqs. (28) and (30) and the expression of O 1 O 2 into Eq. (27), the vector O 1 O 3R can be written as\n\nSimilarly, when considering the wheelset bending deformation in the plane O-XY, the vector O 1 O 3R should be given as where ψ R1 and ψ R2 are the yaw angles caused by the rigid motion and the bending deformation in the plane O-XY, respectively.\n\nψ DWR=ψ R1+ψ R2 is the total yaw angle of the DWR. Similarly, the position of the DWL can be obtained. When the positions of the two dummies are known at t 2, the wheel-rail contact geometry can be calculated. Then the positions of the wheel-rail contact points are easily found and the wheel-rail contact forces can be calculated. The normal wheel-rail contact forces are calculated by the Hertzian nonlinear contact spring model, and the tangent contact forces and spin moments are calculated by means of the model by Shen et al. (). Compared with the conventional wheel-rail contact model (Wang, ; Zhai, ), this new wheel-rail contact model can characterize the independent high-frequency deformations of the two wheels of the flexible wheelset more conveniently.\n\n## 3.  Results and discussion\n\nWhen a vehicle is running on an ideal track, it is only excited by sleepers. Note that the “flexible” wheelset model used in this section denotes the model considering the first two bending modes. The dynamic system with flexible wheelset models is used in the simulation on an ideal track at the speed of 300 km/h. Figs. 9a and 9b show the vertical forces in the frequency domain in steady and unsteady stages, respectively. In the unsteady stage, the peaks appear not only at a set of harmonic frequencies nf s (n=1, 2, 3, …) produced by passing sleeper but also at f b1, while the influence of the second bending mode is small since there is no peak at f b2. In the steady stage, the contribution of the component at f b1 is weakened and only the peaks at nf s (n=1, 2, 3, …) remain. These results are reasonable because when a system comes to a steady stage, its responses only contain the component at the excitation frequency.", null, "Fig.9\n\nBased on a large range of site measurements, the components of roughness on rails mostly appear in the range of 1–20 m. The natural frequencies of the first two bending modes are below 250 Hz, meaning the available frequency of this model is limited. Therefore, the components of the random irregularity on the rails are mainly in the frequency range of 0–150 Hz at the speed of 300 km/h. Fig. 10a presents the local section of 900–950 m in the time domain, and Fig. 10b shows the irregularity in the frequency domain. Note that the results below are from the steady stage.", null, "Fig.10\nRandom irregularity in the time domain (a) and frequency domain (b)\n\nFigs. 11 and 12 show the wheel-rail contact forces acting on the rigid and flexible wheelsets in the time and frequency domains, respectively. As shown in Fig. 11a, the average of the oscillation of the lateral contact force acting on the flexible model is a little smaller than that on the rigid wheelset model, and the shapes of the oscillation are different. As shown in Fig. 11b, the vertical contact forces acting on the two models oscillate around a similar average, while their shapes are different. These differences are caused by the wheelset flexibility.", null, "Fig.11\nLateral contact forces (a) and vertical contact forces (b) in the time domain\n\nIn the frequency domain, the distributions of the components contained in both the lateral and vertical contact forces are in the excitation frequency range of the random irregularity. A peak at frequency 2f s appears in Figs. 11a and 11b. The contribution of the component at frequency f s is overwhelmed by the effect of the irregularity. In addition, the uniform distribution in 0–150 Hz of the irregularity results in the non-uniform distribution of contact forces. As shown in Figs. 12a and 12b, the components in 80–150 Hz are higher than those in 0–80 Hz. This shows that under this present irregularity, this dynamic system is more sensitive to the excitation in 80–150 Hz than to those in 0–80 Hz.\n\nIn the frequency domain, the component at f b1 of the lateral contact force acting on the flexible model is a little larger than that on the rigid model, as marked using the arrow in Fig. 12a. This shows that the first bending mode is excited, and the availability of the model to characterize the wheelset bending is proved. However, there is no evident difference at f b1 for vertical contact forces acting on the two models. This shows that the wheelset bending deformation has a stronger effect on the lateral contact force than on the vertical contact force.", null, "Fig.12\nLateral contact forces (a) and vertical contact forces (b) in the frequency domain\n\nThe wheel-rail contact force is affected by the position of the lateral contact points. Figs. 13a and 13b show the oscillations of the contact points in lateral direction described in the body coordinate system attached to the rail cross-section in the time and frequency domains, respectively. The average of the magnitudes of oscillation of the contact points on the flexible model in the time domain is larger than that on the rigid model. This is caused by the wheelset bending. Moreover, it can weaken the relative movement between rail and wheel caused by the irregularity. Therefore, it is one cause of the smaller average of the lateral contact force acting on the flexible model (Fig. 11a). As shown in Fig. 13b, the difference of the components between the two models at f b1 is evident. This explains the difference in the time domain (Fig. 13a) and again shows the effectiveness of the proposed model.", null, "Fig.13\nOscillation of contact points in lateral direction in the time domain (a) and frequency domain (b)\n\n## 4.  Conclusions\n\nIn this study a new wheel-rail contact model is integrated into the high-speed vehicle-track coupling dynamics system model, which takes into account the effect of wheelset structural flexibility. Based on the new vehicle-track model the effect of the first two bending modes of the wheelset on wheel-rail contact behavior is analyzed under the random irregularity in a frequency range of 0–150 Hz. The numerical results of the rigid wheelset model and the flexible wheelset model are compared in detail. The following conclusions can be drawn from the results:\n\n1. The present vehicle-track model considering flexible wheelsets can very well characterize the effect of the flexible wheelset on wheel-rail dynamic behavior.\n\n2. Under the excitation, the shapes of the oscillations of the wheel-rail contact forces and contact points for the new and conventional vehicle-track models are different. The difference is caused by the excited first bending mode of the wheelset.\n\nFor future work, the first improvement to be considered is to model a wheelset using the FEM or the Timoshenko beam theory to broaden the model’s available frequency range. This could allow it to help investigate the mechanisms behind the generation and development of wheel-rail wear and noise.\n\n* Project supported by the National Natural Science Foundation of China (No. U1134202), the National Basic Research Program (973) of China (No. 2011CB711103), the Program for Changjiang Scholars and Innovative Research Team in University (Nos. IRT1178 and SWJTU12ZT01), the Fundamental Research Funds for the Central Universities, and the 2014 Doctoral Innovation Funds of Southwest Jiaotong University, China\n\n## APPENDIX A\n\nThe vehicle notations and track parameters are given in Table A1.\n\n## References", null, "Andersson, C., Abrahamsson, T., 2002. Simulation of interaction between a train in general motion and a track. Vehicle System Dynamics, 38(6):433-455.", null, "", null, "Baeza, L., Vila, P., Rodaa, A., 2008. Prediction of corrugation in rails using a non-stationary wheel-rail contact model. Wear, 265(9-10):1156-1162.", null, "", null, "Baeza, L., Vila, P., Xie, G., 2011. Prediction of rail corrugation using a rotating flexible wheelset coupled with a flexible track model and a non-Hertzian/non-steady contact model. Journal of Sound and Vibration, 330(18-19):4493-4507.", null, "", null, "Chaar, N., 2007.  Wheelset Structural Flexibility and Track Flexibility in Vehicle/track Dynamic Interaction. PhD Thesis, Royal Institute of Technology,Stockholm, Sweden :", null, "Fayos, J., Baeza, L., Denia, F.D., 2007. An Eulerian coordinate-based method for analysing the structural vibrations of a solid of revolution rotating about its main axis. Journal of Sound and Vibration, 306(3-5):618-635.", null, "", null, "Jin, X.S., Xiao, X.B., Ling, L., 2013. Study on safety boundary for high-speed train running in severe environments. International Journal of Rail Transportation, 1(1-2):87-108.", null, "", null, "Kaiser, I., Popp, K., 2006. Interaction of elastic wheelsets and elastic rails: modeling and simulation. Vehicle System Dynamics, 44(S1):932-939.", null, "", null, "Meinders, T., Meinker, P., 2003. Rotor dynamics and irregular wear of elastic wheelsets, system dynamics and long-term behavior of railway vehicles, track and subgrade. System Dynamics and Long-term Behaviour of Railway Vehicles, Track and Subgrade, 6:133-152.", null, "", null, "Nielsen, J.C.O., Lundn, R., Johansson, A., 2003. Train-track interaction and mechanisms of irregular wear on wheel and rail surfaces. Vehicle System Dynamics, 40(1-3):3-54.", null, "", null, "Nielsen, J.C.O., Ekberg, A., Lundn, R., 2005. Influence of short-pitch wheel/rail corrugation on rolling contact fatigue of railway wheels. Journal of Rail and Rapid Transit, 219(3):177-188.", null, "", null, "Popp, K., Kruse, H., Kaiser, I., 1999. Vehicle/track dynamics in the mid-frequency range. Vehicle System Dynamics, 31(5-6):423-463.", null, "", null, "Popp, K., Kaiser, I., Kruse, H., 2003. System dynamics of railway vehicles and track. Archive of Applied Mechanics, 72(11-12):949-961.", null, "", null, "Qiu, J.B., Xiang, S.H., Zhang, Z.P., 2009.  Computational Structural Dynamics. (in Chinese), Press of University of Science and Technology of China,Hefei, China :", null, "Shen, Z.Y., Hedrick, J.K., Elkins, J.A., 1983. A comparison of alternative creep force models for rail vehicle dynamic analysis. Vehicle System Dynamics, 12(1-3):79-83.", null, "", null, "Szolc, T., 1998. Medium frequency dynamic investigation of the railway wheelset-track system using a discrete-continuous model. Archive of Applied Mechanics, 68(1):30-45.", null, "", null, "Szolc, T., 1998. Simulation of bending-torsional-lateral vibrations of the railway wheelset-track system in the medium frequency range. Vehicle System Dynamics, 30(6):473-508.", null, "", null, "Torstensson, P.T., Nielsen, J.C.O., 2011. Simulation of dynamic vehicle-track interaction on small radius curves. Vehicle System Dynamics, 49(11):1711-1732.", null, "", null, "Torstensson, P.T., Pieringer, A., Nielsen, J.C.O., 2012. Simulation of rail roughness growth on small radius curves using a non-Hertzian and non-steady wheel-rail contact model. , 9th International Conference on Contact Mechanics and Wear of Rail/Wheel Systems, Chengdu, China, 223-230. :223-230.", null, "", null, "Wang, K.W., 1984. Wheel contact point trace line and wheel/rail contact geometry parameters computation. Journal of Southwest Jiaotong University, (in Chinese),1:89-99.", null, "Xiao, X.B., Jin, X.S., Wen, Z.F., 2007. Effect of disabled fastening systems and ballast on vehicle derailment. Journal of Vibration and Acoustics, 129(2):217-229.", null, "", null, "Xiao, X.B., Jin, X.S., Deng, Y.Q., 2008. Effect of curved track support failure on vehicle derailment. Vehicle System Dynamics, 46(11):1029-1059.", null, "", null, "Xiao, X.B., Jin, X.S., Wen, Z.F., 2010. Effect of tangent track buckle on vehicle derailment. Multibody System Dynamics, 25(1):1-41.", null, "", null, "Zhai, W.M., 2007.  Vehicle/Track Coupling Dynamics (3rd Edition). (in Chinese), Chinese Science Press,Beijing, China :", null, "Zhong, S.Q., Xiao, X.B., Wen, Z.F., 2013. The effect of first-order bending resonance of wheelset at high speed on wheel-rail contact behavior. Advances in Mechanical Engineering, 2013:296106", null, "", null, "Zhong, S.Q., Xiao, X.B., Wen, Z.F., 2014. A new wheel-rail contact model integrated into a coupled vehicle-track system model considering wheelset bending. , 2nd International Conference on Railway Technology Research, Development and Maintenance, Ajacocia, France, 1-10. :1-10.", null, "<1>\n\nRamesh<rcdohare@gmail.com>\n\n2016-12-28 17:32:30\n\nNo where forces values are given ,Like if a 31Tonne axle load running at 300km/hr then at what force track will experiencing in longitudinal direction,vertical direction, thrust which over turn track?", null, "" ]
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https://www.rocknets.com/converter/temperature/64.4-c-to-f
[ "# Convert 64.4 Celsius to Fahrenheit (64.4 c to f)\n\n What is 64.4 Celsius in Fahrenheit? Celsius: ℃ Fahrenheit: ℉\n\nYou may also interested in: Fahrenheit to Celsius Converter\n\nThe online Celsius to Fahrenheit (c to f) Converter is used to convert temperature from Degrees Celsius (℃) to Fahrenheit (℉).\n\n#### The Celsius to Fahrenheit Formula to convert 64.4 C to F\n\nHow to convert 64.4 Celsius to Fahrenheit? You can use the following formula to convert Celsius to Fahrenheit :\n\nX(℉)\n= Y(℃) ×\n9 / 5\n+ 32\n\nTo convert 64.4 Celsius to Fahrenheit: ?\n\nX(℉)\n= 64.4(℃) ×\n9 / 5\n+ 32\n\n#### Frequently asked questions to convert C to F\n\nHow to convert 40 celsius to fahrenheit ?\n\nHow to convert 84 celsius to fahrenheit ?\n\nHow to convert 41 celsius to fahrenheit ?\n\nHow to convert 4 celsius to fahrenheit ?\n\nHow to convert 147 celsius to fahrenheit ?\n\nHow to convert 178 celsius to fahrenheit ?\n\nTo convert from degrees Celsius to Fahrenheit instantly, please use our Celsius to Fahrenheit Converter for free.\n\n#### Best conversion unit for 64.4 ℃\n\nThe best conversion unit defined in our website is to convert a number as the unit that is the lowest without going lower than 1. For 64.4 ℃, the best unit to convert to is 64.4 ℃." ]
[ null ]
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https://metanumbers.com/51513
[ "## 51513\n\n51,513 (fifty-one thousand five hundred thirteen) is an odd five-digits composite number following 51512 and preceding 51514. In scientific notation, it is written as 5.1513 × 104. The sum of its digits is 15. It has a total of 4 prime factors and 16 positive divisors. There are 26,640 positive integers (up to 51513) that are relatively prime to 51513.\n\n## Basic properties\n\n• Is Prime? No\n• Number parity Odd\n• Number length 5\n• Sum of Digits 15\n• Digital Root 6\n\n## Name\n\nShort name 51 thousand 513 fifty-one thousand five hundred thirteen\n\n## Notation\n\nScientific notation 5.1513 × 104 51.513 × 103\n\n## Prime Factorization of 51513\n\nPrime Factorization 3 × 7 × 11 × 223\n\nComposite number\nDistinct Factors Total Factors Radical ω(n) 4 Total number of distinct prime factors Ω(n) 4 Total number of prime factors rad(n) 51513 Product of the distinct prime numbers λ(n) 1 Returns the parity of Ω(n), such that λ(n) = (-1)Ω(n) μ(n) 1 Returns: 1, if n has an even number of prime factors (and is square free) −1, if n has an odd number of prime factors (and is square free) 0, if n has a squared prime factor Λ(n) 0 Returns log(p) if n is a power pk of any prime p (for any k >= 1), else returns 0\n\nThe prime factorization of 51,513 is 3 × 7 × 11 × 223. Since it has a total of 4 prime factors, 51,513 is a composite number.\n\n## Divisors of 51513\n\n1, 3, 7, 11, 21, 33, 77, 223, 231, 669, 1561, 2453, 4683, 7359, 17171, 51513\n\n16 divisors\n\n Even divisors 0 16 8 8\nTotal Divisors Sum of Divisors Aliquot Sum τ(n) 16 Total number of the positive divisors of n σ(n) 86016 Sum of all the positive divisors of n s(n) 34503 Sum of the proper positive divisors of n A(n) 5376 Returns the sum of divisors (σ(n)) divided by the total number of divisors (τ(n)) G(n) 226.965 Returns the nth root of the product of n divisors H(n) 9.58203 Returns the total number of divisors (τ(n)) divided by the sum of the reciprocal of each divisors\n\nThe number 51,513 can be divided by 16 positive divisors (out of which 0 are even, and 16 are odd). The sum of these divisors (counting 51,513) is 86,016, the average is 5,376.\n\n## Other Arithmetic Functions (n = 51513)\n\n1 φ(n) n\nEuler Totient Carmichael Lambda Prime Pi φ(n) 26640 Total number of positive integers not greater than n that are coprime to n λ(n) 1110 Smallest positive number such that aλ(n) ≡ 1 (mod n) for all a coprime to n π(n) ≈ 5269 Total number of primes less than or equal to n r2(n) 0 The number of ways n can be represented as the sum of 2 squares\n\nThere are 26,640 positive integers (less than 51,513) that are coprime with 51,513. And there are approximately 5,269 prime numbers less than or equal to 51,513.\n\n## Divisibility of 51513\n\n m n mod m 2 3 4 5 6 7 8 9 1 0 1 3 3 0 1 6\n\nThe number 51,513 is divisible by 3 and 7.\n\n## Classification of 51513\n\n• Arithmetic\n• Deficient\n\n### Expressible via specific sums\n\n• Polite\n• Non-hypotenuse\n\n• Square Free\n\n### Other numbers\n\n• LucasCarmichael\n\n## Base conversion (51513)\n\nBase System Value\n2 Binary 1100100100111001\n3 Ternary 2121122220\n4 Quaternary 30210321\n5 Quinary 3122023\n6 Senary 1034253\n8 Octal 144471\n10 Decimal 51513\n12 Duodecimal 25989\n20 Vigesimal 68fd\n36 Base36 13qx\n\n## Basic calculations (n = 51513)\n\n### Multiplication\n\nn×i\n n×2 103026 154539 206052 257565\n\n### Division\n\nni\n n⁄2 25756.5 17171 12878.2 10302.6\n\n### Exponentiation\n\nni\n n2 2653589169 136694338862697 7041535477834110561 362730617069668537328793\n\n### Nth Root\n\ni√n\n 2√n 226.965 37.2082 15.0653 8.75756\n\n## 51513 as geometric shapes\n\n### Circle\n\n Diameter 103026 323666 8.3365e+09\n\n### Sphere\n\n Volume 5.72584e+14 3.3346e+10 323666\n\n### Square\n\nLength = n\n Perimeter 206052 2.65359e+09 72850.4\n\n### Cube\n\nLength = n\n Surface area 1.59215e+10 1.36694e+14 89223.1\n\n### Equilateral Triangle\n\nLength = n\n Perimeter 154539 1.14904e+09 44611.6\n\n### Triangular Pyramid\n\nLength = n\n Surface area 4.59615e+09 1.61096e+13 42060.2\n\n## Cryptographic Hash Functions\n\nmd5 9f36a921c26b879747bb6c172907d903 e0f7cff0aace8112eec2c9d5605fab043e49e138 8fb09d5d5ffc41ff1cd7a6feb86f021bd0bea84bc3b45c5e10bcb2d7e20e56d0 631e90e7892991c25489ee019b0e080cec3c50fdb573016d479fe59a026ce675822559991ec031e5e7cd30ec97bcf3069b69340b8b2c5fa698383b6d0476c7a2 d1d5ff341eb9336ec229506c08ddd2641d71a318" ]
[ null ]
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https://polymerfem.com/community/constitutive-models/question-about-stress-update-in-umat/
[ "Clear all\n\n# Question about stress update in UMAT\n\n4 Posts\n2 Users\n0 Likes\n503 Views", null, "Posts: 7\nTopic starter\n(@donngall84)\nActive Member\nJoined: 15 years ago\n\nHi everyone,\n\nAny comments would be helpful for me, I really appreciate you guys.\n\nThank you.\n\nOkyle\n\nHi friends\n\nIt is inconvenient to download a zip file, so i uploaded the picture of my description to Flicker.\n\nLook forwards to your response, than you all.\n\nTopic Tags\n3 Replies", null, "Posts: 3993\n(@jorgen)\nMember\nJoined: 4 years ago\n\nThe stress you need to calculate is the stress at time t+dt.\nYou are given the stress at time t.\nHence: stress(t+dt) = stress(t) + dstress\n\nThere is no need to double the initial stress.\n\n-Jorgen\n\nTopic Tags\n3 Replies", null, "Posts: 7\nTopic starter\n(@donngall84)\nActive Member\nJoined: 15 years ago\n\nThank you very much, Jorgen.\n\nLet me make my question clearer: I want to calculate dstress, but I dont understand the expression (W*Sigma(t)-Sigma(t)*W)*delta t = R*Sigma*RT (just as the above picture describing).\n\nHow should I obtain R*Sigma*RT?\n\nOr should I just throw this item (R*Sigma*RT), and calculate the dtress via dstress= the co-rotational stress increment?", null, "Posts: 3993\n(@jorgen)\nMember\nJoined: 4 years ago\n\nI looked at your original equations again and the first equation in the image does not make sense. As you said, it would give twice the stress which does not make sense. Are you sure you wrote the equation right?\n\nI also agree with your statement regarding: (W*Sigma(t)-Sigma(t)*W)*delta t = R*Sigma*RT. That does not make sense to me.\n\nYou can obtain R from the deformation gradient so you can calculate R*Sigma*RT if you like.\n\nYou need to make sure you stress update is consistent, which will depend on your material model formulation.\n\n-Jorgen\n\nShare:" ]
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http://jfxpt.com/2020/draft-gbw-node-frontend-part-3/
[ "# Fixpoint\n\n## 2020-01-17\n\n### Draft gbw-node frontend, part 3\n\nFiled under: Bitcoin, Software — Jacob Welsh @ 18:02\n\nContinued from:\n\n### Base58\n\nBitcoin addresses are conventionally written in a special-purpose encoding and include a hash truncated to 32 bits for error detection. As the reference implementation explains:\n\nWhy base-58 instead of standard base-64 encoding?\n- Don't want 0OIl characters that look the same in some fonts and could be used to create visually identical looking account numbers.\n- A string with non-alphanumeric characters is not as easily accepted as an account number.\n- E-mail usually won't line-break if there's no punctuation to break at.\n- Doubleclicking selects the whole number as one word if it's all alphanumeric.\n\nOf course, all these points would have been answered just as well by hexadecimal, and without the various burdens: case-sensitivity for the user (the surest way I've found to read these out is the fully explicit: \"one five big-A three little-X ...\"); more code for the implementer; and more work for the machine (as the lack of bit alignment demands a general base conversion algorithm).\n\nWe start with lookup tables to convert the digits 0-57 to the specified alphabet and back. I was once surprised to learn the scope of iteration variables in a Python \"for\" loop is not restricted to the loop body: a potential source of referential confusion, reflecting the language's casual approach to mutation. Thus, when at the global scope I like to ensure throwaway names, like \"index\" and \"character\" here, are safely contained in a function.\n\n```base58_alphabet = (string.digits + string.uppercase + string.lowercase).translate(None, '0OIl')\nbase58_inverse = [None]*256\ndef init_base58_inverse():\nfor index, character in enumerate(base58_alphabet):\nbase58_inverse[ord(character)] = index\ninit_base58_inverse()\n```\n\nTo do base conversion we'll need to treat byte sequences as integers with the same ordering conventions as the reference code. Otherwise put: to decode from base-256 to abstract integers. Python 2 doesn't have a builtin for this. The algorithm is not optimal, but the base-58 part will be worse anyway.\n\n```def bytes_to_int(b):\n\"Convert big-endian byte sequence to unsigned integer\"\ni = 0\nfor byte in b:\ni = (i << 8) + ord(byte)\nreturn i\n```\n\nTo complete the bytes-to-ASCII converter we extract digits from the integer, least significant first, by iterated division with remainder by 58. Since the conversion to integer loses track of field width, the convention is to pad with the same number of base-58 zeros as there were base-256 leading zeros in the input. In further fallout from using a non-bit-aligned encoding, these are not naturally constant time or constant control-flow operations.\n\nFor the same bit cost of the error detection code we could have had error correction. But that would have required, like, math, and stuff.\n\n```def b2a_base58check(data):\ndata += sha256d(data)[:4]\n\nfor b in data:\nif b != '\\x00':\nbreak\n\ndata_num = bytes_to_int(data)\n\ndigits = []\nwhile data_num:\ndata_num, digit = divmod(data_num, 58)\ndigits.append(digit)\n\nreturn ''.join(base58_alphabet[digit] for digit in reversed(digits))\n```\n\nConverting back to bytes uses the inverse operation at each step, but now there are cases of invalid input to reject: digits outside the specified alphabet and corruption detected by the checksum. (The precise function decomposition is a bit arbitrary and asymmetrical I'll admit.)\n\n```class Base58Error(ValueError):\npass\n\npass\n\npass\n\ndef a2b_base58(data):\ndigits = [base58_inverse[ord(b)] for b in data]\nif None in digits:\n\nfor digit in digits:\nif digit != 0:\nbreak\n\ndata_num = 0\nfor digit in digits:\ndata_num = 58*data_num + digit\n\ndata_bytes = []\nwhile data_num:\ndata_bytes.append(data_num & 0xFF)\ndata_num = data_num >> 8\n\nreturn ''.join(chr(b) for b in reversed(data_bytes))\n\ndef a2b_base58check(data):\ndata = a2b_base58(data)\ncheck = data[-4:]\n```\n\nFinally we apply this encoding to Bitcoin addresses, which have a fixed 160-bit width plus an extra \"version\" byte that becomes the familiar leading \"1\".\n\n```class BadAddressLength(ValueError):\npass\n\npass\n\nb = a2b_base58check(a)\nif len(b) != 21:\nif b != '\\x00':\nreturn b[1:]\n\nreturn b2a_base58check('\\x00' + b)\n```\n\nAll this format conversion groundwork out of the way, we'll start talking to the database and putting it all together. To be continued!" ]
[ null ]
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https://www.predictiveanalyticstoday.com/predictive-modeling/
[ "Predictive Analytics\nWhat is Predictive Modeling ?\n\n# What is Predictive Modeling ?\n\nWhat is Predictive Modeling ?\n4.7 (94.19%) 310 ratings\n\nPredictive modeling is the process of creating, testing and validating a model to best predict the probability of an outcome. A number of modeling methods from machine learning, artificial intelligence, and statistics are available in predictive analytics software solutions for this task.\n\nThe model is chosen on the basis of testing, validation and evaluation using the detection theory to guess the probability of an outcome in a given  set amount of input data. Models can use one or more classifiers in trying to determine the probability of a set of data belonging to another set. The different models available on the Modeling portfolio of predictive analytics software enables to derive new information about the data and to develop the predictive models.\n\nEach model has its own strengths and weakness and is best suited for particular types of problems. A model is reusable and is created by training an algorithm using historical data and saving the model for reuse purpose to share the common business rules which can be applied to similar data, in order to analyze results without the historical data, by using the trained algorithm.", null, "Predictive Analytics Value Chain\n\nMost of the predictive modeling software solutions has the capability to export the model information into a local file in industry standard Predictive Modeling Markup Language, (PMML) format for sharing the model with other PMML compliant applications to perform analysis on similar data.\n\n## Business process on Predictive Modeling\n\n1. Creating the model : Software solutions allows you to create a model to run one or more algorithms on the data set.\n\n2. Testing the model: Test the model on the data set. In some scenarios, the testing is done on past data to see how best the model predicts.\n\n3. Validating the model : Validate the model run results using visualization tools and business data understanding.\n\n4. Evaluating the model : Evaluating the best fit model from the models used and choosing the model right fitted for the data.\n\n## Predictive modeling process\n\nThe process involve running one or more algorithms on the data set where prediction is going to be carried out. This is an iterative processing and often involves training the model, using multiple models on the same data set and finally arriving on the best fit model based on the business data understanding.", null, "Predictive Modeling\n\n## Models Category\n\n1.Predictive models :The models in Predictive models analyze the past performance for future predictions.\n\n2.Descriptive models: The models in descriptive model category quantify the relationships in data in a way that is often used to classify data sets into groups.\n\n3.Decision models: The decision models describe the relationship between all the elements of a decision in order to predict the results of decisions involving many variables.\n\n## Algorithms\n\nAlgorithms perform data mining and statistical analysis in order to determine trends and patterns in data. The predictive analytics software solutions has built in algorithms such as regressions, time series, outliers, decision trees, k-means and neural network for doing this. Most of the software also provide integration to open source R library.\n\n1. Time Series Algorithms which perform time based predictions. Example Algorithms are Single Exponential Smoothing, Double Exponential Smoothing and Triple Exponential Smoothing.\n\n2. Regression Algorithms which predicts continuous variables based on other variables in the dataset. Example algorithms are Linear Regression, Exponential Regression, Geometric Regression, Logarithmic Regression and Multiple Linear Regression.\n\n3. Association Algorithms which Finds the frequent patterns in large transactional dataset to generate association rules. Example algorithms are Apriori\n\n4. Clustering Algorithms which clustor observations into groups of similar Groups. Example algorithms are K-Means , Kohonen, and TwoStep.\n\n5. Decision Trees Algorithms classify and predict one or more discrete variables based on other variables in the dataset. Example algorithms are C 4.5 and CNR Tree\n\n6. Outlier Detection Algorithms detect the outlying values in the dataset. Example algorithms are Inter Quartile Range and Nearest Neighbour Outlier\n\n7. Neural Network Algorithms does the forecasting, classification, and statistical pattern recognition. Example algorithms are NNet Neural Network and MONMLP Neural Network\n\n8.Ensemble models are a form of Monte Carlo analysis where multiple numerical predictions are conducted using slightly different initial conditions.\n\n9.Factor Analysis deals with variability among observed, correlated variables in terms of a potentially lower number of unobserved variables called factors. Example algorithms are Maximum likelihood algorithm.\n\n10.Naive Bayes are probabilistic classifier based on applying Bayes' theorem with strong (naive) independence assumptions.\n\n11.Support vector machines are supervised learning models with associated learning algorithms that analyze data and recognize patterns, used for classification and regression analysis.\n\n12.Uplift modeling, models the incremental impact of a treatment  on an individual's behavior.\n\n13.Survival analysis are analysis of time to events.\n\n## Features in Predictive Modeling\n\n1) Data Analysis and manipulation : Tools for data analysis, create new data sets, modify, club, categorize, merge and filter data sets.\n\n2) Visualization : Visualization features includes interactive graphics, reports.\n\n3) Statistics : Statistics tools to create and confirm the relationships between variables in the data. Statistics from different statistical software can be integrated to some of the solutions.\n\n4) Hypothesis testing : Creation of models, evaluation and choosing of the right model.\n\n## Predictive Analytics Software\n\nYou may also like to review the predictive analytics free software list :\n\nYou may also like to review the predictive analytics software API :\n\nYou may also like to review the top predictive analytics proprietary software list:\n\nFor more information of predictive analytics process, please review the overview of each components in the predictive analytics process: data collection (data mining), data analysis, statistical analysis, predictive modeling and predictive model deployment.\n\nWhat is Predictive modeling?\n\nPredictive modeling is the process of creating, testing and validating a model to best predict the probability of an outcome. A number of modeling methods from machine learning, artificial intelligence, and statistics are available in predictive analytics software solutions for this task.\n\n2 Reviews\n•", null, "November 6, 2016 at 5:58 am\n\nGood summary on how to perform a predictive analysis! I just would like to share some more information about specific models and how to implement them…\n\nI’ve written a book on how to apply predictive models using Excel. In case it is of your interest, I’m publishing these models with ready-to-use templates in Excel.\n\n•", null, "January 10, 2017 at 4:10 am\n\nGood article. I´m mostly interested in predictive modeling classification. Any suggested readings?\n\nLove It\n4%\nVery Good\n8%\nINTERESTED\n46%\nCOOL\n39%" ]
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https://www.webster-dictionary.org/definition/joule
[ "Word:\n\njoule\n\nPronunciation: jŌl\nn.1.(Physics.) A unit of work which is equal to 107 ergs (the unit of work in the C. G. S. system of units), and is equivalent to one watt-second, the energy expended in one second by an electric current of one ampere in a resistance of one ohm; also called the absolute joule. It is abbreviated J or j. The international joule is slightly larger, being 1.000167 times the absolute joule. The absolute joule is approximately equal to 0.737562 foot pounds, 0.239006 gram-calories (small calories), and 3.72506 x 10-7 horsepower-hours, and 0.000948451 B.t.u.\n Joule's equivalent See under Equivalent, n.\n Noun 1 joule - a unit of electrical energy equal to the work done when a current of one ampere passes through a resistance of one ohm for one secondSynonyms: J, watt second 2 Joule - English physicist who established the mechanical theory of heat and discovered the first law of thermodynamics (1818-1889)Synonyms: James Prescott Joule\nenergy unit, erg, heat unit, J, watt second, work unit\nDefinitions Index: # A B C D E F G H I J K L M N O P Q R S T U V W X Y Z" ]
[ null ]
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https://electronics.stackexchange.com/tags/feedback/new
[ "# Tag Info\n\n## New answers tagged feedback\n\n0\n\nThe best way to understand the differences between negative feedback and positive feedback is study the case when feed-forward block is dynamic system then extend the results to ideal linear block, let suppose that the transfer function of feedforward system is: The Feedforward block has a single pole at $s=-p_1$: $$A(s)=\\dfrac{a_0}{1+\\dfrac{s}{p_1}}$$...\n\n0\n\nIn an astable configuration, is there some way to measure output frequency, compare it with some desired value, and use this to change the resistance in the config? (Basically a feedback loop) Sure, thats relatively easy, but it requires that you have something to compare it to Ie. to check whether your output signal is actually let's say 100kHz, then you ...\n\n-1\n\nThe large swing slew Rate is always limited by drive current limit and load capacitance which near 0 ESR compare to load R. Thus dV/dt = Ic/C. Where Ic=V/R where for FETs, R = RdsOn or Ron and for BJT drivers , Ic is an active current limiter with the bulk Rce added to it. Where f(-3dB)=0.35/Tr , and Tr= 10~90% rise time, this is always less than the ...\n\n3\n\nI agree with you that the Professor's statement is unclear and confusing. When used as a voltage buffer, the DC voltage at inverting and non-inverting inputs and the output are determined by the DC voltage at the non-inverting input. As you mention, the feedback loop takes care of that. Designing the output to be biased at Vdd/2 by itself (without feedback)...\n\n1\n\nThe change in voltage with current is greater on the resistor side than on the transistor side when the current is in the normal operating range for this circuit. The derivative of voltage with respect to current is R on the resistor side and the dynamic resistance of the diode on the other side. At, say, 1uA the dynamic resistance will be around 26K ohms. ...\n\n0\n\nIn addition to Justin's answer here's a mathematical way of looking at it: Using Vout = A(Vp - Vn) The incorrect assumption that I was making was that Vout == Vp == Vn which is wrong as: Vp - Vn = 0, which is a contradiction as this would make Vout = 0 Looking as Justin's answer we can see that Vout (and therefore Vn) start at 0v and rises with time until ...\n\n1\n\nWhen you are considering a step response, you need to include the time delays at the different locations for the answer to be reasonable. One way to model this is to add an RC filter at the output of the op-amp. The other thing that you haven't accounted for is that the op-amp can't actually drive the output to greater than the positive supply voltage. ...\n\n0\n\nI'm trying to get an understanding of how negative feedback works. Think of it like a control system and an error amplifier. You set the \"demand\" on the non-inverting input and the negative feedback causes the op-amp output to rapidly change to a voltage that makes the input error minimal. In other words, the inverting input is made to be nearly the same ...\n\nTop 50 recent answers are included" ]
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http://www.kurpinskisclass.com/unit-d-mechanical-systems-i/
[ "# Mechanical Systems\n\n### Machines are tools that help humans do work\n\nMachines help people use energy more effectively.\n\n## Machine :\n\nA device that helps us to do work.\n\nAn example of technology developing is a combine harvester.\n\n# Simple Machines – Meet Human Needs\n\n### Early machines\n\n1)    Were very simple devices\n\n2)    Depended on people & animals for their source of energy.\n\n3)    Example: Plow\n\n### How did earlier civilizations get water to their homes?\n\nRoman Aqueducts\n\nUsed for transporting water for many kilometres to supply cities.\n\nHad 3 parts:  Pump – raise water into reservoirs.\n\nChannels – on a slope to carry the water.\n\nDistribution system – distributes water within a city.\n\nSakia (Persian wheel)\n\n• Series of buckets attached to a long rope, draped over a wheel.\n\n• Wheel is turned by animals which raises the buckets of water.\n\n• After water is raised it is stored in tanks.\n\n• Gravity moves water through pipes and into homes.\n\nArchimedes Screw\n\n• A screw picks up the water and carries it up to the top of the tube.\n\n• Originally powered by hand, then later by gas or electric motors.\n\n• Leonardo da Vinci later used 2 Archimedes screws to increase efficiency\n\nPresent Day Pumps\n\n• Pumps keep the water flowing and are powered by motors.\n\n# Simple Machines\n\n## Simple Machine:\n\nA tool or device made up of one basic machine.\n\n• There are 6 simple machines that help us do work.\n\n• Each machine has its own advantages and disadvantages.\n\n• A simple machine can increase or change the direction of the force that you apply. But, the cost is that the force the user applies must move farther than the load.\n\n## 1)  Lever:\n\nA rigid bar or plank that can rotate around a fixed point called a pivot or fulcrum.\n\n• Enables the user to move a larger load than without.\n\n• But the user must move a greater distance than the load.\n\n### 3 types of Levers:\n\n1. First class lever – fulcrum between the load and the point of effort.\n\n2. Second class lever – load is between the effort and the fulcrum.\n\n3. Third class lever – has the effort between the load and the fulcrum.\n\n## 2) Inclined Plane:\n\nA flat surface that is at an angle to another flat surface, such as the ground.\n\n• Enables the user to move a larger load than without.\n\n• But the user must move a greater distance than the load.\n\n• The ramp cannot be too steep in order to work.\n\n## 3) Wedge:\n\nSimilar to an inclined plane, but is forced into an object.\n\n• By pressing on the wide end, the narrow end splits the object.\n\n• Can only be used in one direction, to push objects apart.\n\n• Enables the user to apply a greater force on an object.\n\n• But the user must move a greater distance than the split.\n\n## 4) Screw:\n\nConsists of a cylinder with a groove cut in a spiral on the outside.\n\n• Can penetrate materials using a relatively small force.\n\n• Convert rotational motion to linear motion.\n\n• Most screws move objects very slowly.\n\n## 5)Pulley:\n\nMade up of a wire, rope, or cable moving on a grooved wheel.\n\n• May be made up of one or many wheels.\n\n• Can be fixed in place or movable.\n\n## 6) Wheel and Axle:\n\nMade up of two wheels of different diameters the turn together.\n\n• A longer motion on the wheel produces a shorter more powerful motion on axle.\n\n• Enable the user to apply a greater force on an object.\n\n• But the user must move the wheel a greater distance to apply the force.\n\n• Can also be used to increase speed (ex. Bicycle).\n\n# Complex Machines – Simple machines working together\n\n### Why complex machines?\n\n1. As larger communities developed, newer more complicated machines developed.\n\n2. New larger energy sources like coal, oil, and electricity combined with new technologies, caused an industrial revolution.\n\n3. This led to an increase in people’s standard of living.\n\n4. But has also led to people now being dependent on technology.\n\n## Complex Machines:\n\nA system in which simple machines all work together.\n\n## System:\n\nA group of parts that work together to perform a function.\n\nEx. Bicycle (which simple machines does a bicycle employ)\n\n## Subsystem:\n\nA smaller group of parts in a complex machine with one function.\n\n(Ex) Car - braking and steering\n\n# Subsystems that Transfer Forces\n\nA belt or chain to transfer energy from a energy source to an object.\n\n• (Ex) bicycle chain\n\n## Transmission:\n\nA special type of linkage for transferring energy from the engine  to the wheel in large vehicles such as cars or trucks.\n\n• more useful when larger loads must be moved.\n\n## Gears:\n\nA pair of wheels with teeth that interlink; when they rotate together, one gearwheel transfers turning motion and force to the other.\n\n• are important because control the transfer of energy in a system.\n\n• gear wheels work together in gear trains (2 or more gears).\n\n## DRIVING GEAR:\n\nGear that has original force applied to it.\n\n## DRIVEN GEAR:\n\nGear that receives the force after.\n\n### How do gears affect speed?\n\n(I) When driving gear is smaller than the driven gear   =  The turning speed in the system decreases.\n\n• For every turn the larger wheel makes the smaller gear will do many more.\n\n• Are called multiplying gears.\n\n(II) When the driving gear is larger than the driven gear  =   The turning speed in the system increases.\n\n• Are called reducing gears.\n\n• In some systems the gears are meshed together, but in some cases they are connected by a linkage.\n\n# Understanding of mechanical advantage and work helps determine the efficiency of machines\n\nUnderstanding simple & complex machines advanced world exploration,\n\n• (Ex) Sail boat\n\n### Machines Make Work Easier.\n\n-       A winding road is actually a series of inclined planes with switchbacks, which allow cars to drive up a steep hill.\n\nSWITCHBACKS OF LOMBARD STREET SAN FRANCISCO\n\n## Mechanical Advantage :\n\nAmount by which a machine can multiply a force. Also called the force ratio\n\n## Input Force:\n\nForce applied to the machine.\n\n## Output Force:\n\nForce the machine applies to the object.\n\n### Force is measured in Newtons (N).\n\nMechanical  Advantage  (MA) =   Force Output (N) / Force Input (N)\n\n### EX 1\n\nTo pull a weed out of a garden, you can apply a force of 50 N to the shovel. The shovel applies a force of 600 N to the weed. What is the mechanical advantage of the shovel?\n\n### EX 2\n\nTo pry open a soda can lid, you can apply a force of 50 N to a car key. The car key applies a force of 390 N to the lid. What is the mechanical advantage of the car key?\n\n### EX 3\n\nTo pry a wooden board off of a treehouse, you can apply a force of 50 N to a lever. The lever applies a force of 750 N to the board. What is the mechanical advantage of the lever?\n\nREVIEW QUESTIONS\n\n## Speed:\n\nMeasures the distance an object travels in a given amount of time.\n\nSpeed =   Distance (m)/ Time (s)\n\n## Speed Ratio:\n\nMeasure of how the speed of the object is affected by a machine.\n\nSR describes how much faster the user is moving than the load is working.\n\nSpeed Ratio  (SR)   = Input Distance (m)/ Output Distance (m)\n\n### Ex 1\n\nA gear mechanism of two gear is in motion. The driving gear moves a total of 3m, while the driven gear moves a total of 12m. What is the speed ratio of this mechanism?\n\n### EX 2\n\nA pulley system is pulled a distance of 10 m, this moves a box that is attached to the pulley 1.5m. What is the speed ratio of the pulley system?\n\n** A machine can increase or change the direction of the force that you apply. But, the cost is that the force the user applies must move farther than the load.\n\nREVIEW QUESTIONS\n\n### A Mechanical Advantage Less Than 1\n\nUseful for tasks that do not require a large output force.\n\n• (Ex) Bicycle – the output force is used for speed.\n\n# The Effect of Friction\n\n• Mechanical Advantage does NOT always equal Speed Ratio.\n\n• Friction can affect MA, but not SR.\n\n• Speed ratio represents the ideal mechanical advantage (No friction).\n\nFRICTION WELDING OF TWO METAL PIECES\n\n## Friction:\n\nForce that opposes motion.\n\n• caused by the roughness of surfaces.\n\n• as roughness of a surface increases so does the effect of friction.\n\n• friction creates HEAT, and must be released to protect the system.\n\n# Efficiency\n\n## Efficiency:\n\nMeasurement of how well a machine or device uses energy.\n\n• affected by friction.\n\n• most energy lost is unusable (ex. Heat).\n\nEfficiency  =   Mechanical Advantage /  Speed Ratio\n\nMost complex machines are very inefficient: waste energy.\n\nex) Car – 15% efficient.\n\n# The Science of Work\n\n## Work:\n\nDone when a force acts on an object to make the object move.\n\nMovement is needed before one can say that work has been done.\n\nAlso reffered to as 'Energy'\n\nMeasure in Joules (J) (N x m)\n\nAmount of work done depends on 2 things:\n\n1. amount of force exerted on the object\n\n2. distance the object moved in the direction of the applied force.\n\nWork (N x m) = Force (N) x Distance (m)\n\n- The joule is also used in calculating Energy.\n\n### EX 1\n\nYou apply 300 N of force in 15 m. How much work did you do?\n\n### EX 2\n\nA forklift lifts a box 2 m by applying 1000 N of force. How much work did the forklift do?\n\n### Ex 3\n\nYou have used 1000 J of energy to apply a force of 200 N to an object. How far did that object move?\n\nREVIEW QUESTIONS\n\n## Power:\n\nHow much work is achieved in a certain amount of time, measured in Watts\n\nPower (W) = Work (J) / Time (s)\n\n### EX 1\n\nYou apply 200 J to an object in 15 s. How much power did you use?\n\n### EX 2\n\nAn engine provides 5000 J of work to an axle over the period of 10 seconds. How much power does the engine have?\n\n### Ex 3\n\nA horse pulls a wagon by working 4500 J over a time of 6 s. How much power does the horse produce?\n\n# Energy and Work\n\nEnergy and work are closely related, can not have one without the other.\n\n(Ex) Car – needs energy (gasoline) in order to work (move)\n\n### Work and Machines\n\nUsing a machine does not decrease the amount of work, it decreases the force.\n\nWork Input   =   Work Output\n\nThis equation is affected by friction (just like mechanical advantage)\n\nHere is another way of calculating efficiency:\n\nEfficiency = Work Output/ Work Input\n\n### EX 1\n\nA construction worker puts 20 J of energy in to one strike of his hammer on the head of a nail. The energy transferred to driving the nail in to the wood is 8.0 J. What is the efficiency of the construction worker's hammering?\n\n### EX 2\n\nMr. K spent 25 J of energy to spike a volleyball over the net. A player received that volleyball and determined that the energy transferred to the ball was 20 J of energy. What is the efficiency of Mr. K's spike?\n\n### EX 3\n\nA particular chemical process has an energy efficiency of only 3.00%. To complete this large-scale chemical process, 140,000 J of energy is input. What is the energy output of this process?\n\nREVIEW QUESTIONS" ]
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https://www.learner.org/courses/mathilluminated/glossary/12.php
[ "", null, "Teacher resources and professional development across the curriculum\n\nTeacher professional development and classroom resources across the curriculum", null, "", null, "# Glossary\n\n## Deravative\n\nTo capture the notion of rates of change that can themselves change, we need the concept of a derivative.\n\n## Differential Calculus\n\nFirst described rigorously by Newton and Leibniz, differential calculus is the mathematics of changing quantities.\n\n## Differential Equation\n\nA differential equation is an expression that relates quantities and their rates of change. The solution to a differential equation is not simply a number; it is a function.\n\n## Non-Constant Slope\n\nA non-constant slope describes a rate of change that itself can change.\n\n## Oscillators\n\nAn oscillator is a function that varies between two values.\n\n## Slope-Intercept\n\nThe slope-intercept form of a linear equation is a common way to represent the mathematics of change. An example of this concern with relationships is the familiar slope-intercept form of the equation of a line: y = mx +b.", null, "## Spontaneous Synchronization\n\nSpontaneous synchronization is a special case of complicated dynamic phenomena. Understanding the mathematics of how, and under what circumstances, entities can come into synchronization with one another provides a starting point for exploring the vast world of nonlinear dynamics." ]
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http://www.mdsk.net/read/0-d2-d1-d6-aa-b6-a8-d2-e5-d3-f2-ce-aaR-b5-c4-ba-af-ca-fdf-a3-a8x-a3-a9-ce-aa-c6-e6-ba-af-ca-fd-a3-ac-c7-d2-c2-fa-d7-e3f-a3-a8x-2b4-a3-a9-3df-a3-a8x-a3-a9-a3-ac-b5-b1x-a1-ca-5b0-a3-ac1-5d-ca-b1-a3-acf-a3-a8x-a3-a9-3d2....html
[ "# 已知定义域为R的函数F(x)为奇函数,且满足F(x+4)=F(x),当x∈[0,1]时,F(x)=2...\n\n(1)令x∈[-1,0),则-x∈(0,1],∴f(-x)=2-x-1,又∵f(x)是奇函数,∴f(\n\n(x+1)=f(3−x)-------周期=4 x∈(0,2]时f(x)=&a\n\n(1)f(x)=-f(x-4),为奇函数 ∴f(x+2)=-f(x+2-4)=-f(x-2)=f(\n\n∵f(x-4)=-f(x) ∴f(x)=-f(x-4) ∴f(x+8)=-f(x+8-4)=\n\n∵f(x)是定义在R上的奇函数,故f(0)=0,即0是函数f(x)的零点,又由f(x)是定义在R上且" ]
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https://math.stackexchange.com/questions/132677/how-can-you-add-not-g-to-a-formal-system-without-introducing-omega-inconsisten
[ "# How can you add 'not G' to a formal system without introducing omega inconsistency?\n\nIn any formal system S that is susceptible to Godel's proof, we can make a formula G which is undecidable. That should mean that we can add either $G$ or $\\neg G$ as an axiom to S and still end up with a consistent system, but I'm not sure exactly how $S + \\neg G$ can be consistent.\n\nSo, $G$ says: \"There does not exist a number $n$, which is the Godel number for a proof of $G$.\" If G were provable, it would be false, and the system would be inconsistent (because $G$ implies $\\neg G$). If $\\neg G$ were provable, however, the system does not have to be blatantly inconsistent, but only omega-inconsistent. $\\neg G$ says \"There does exist a number $n$, which is the Godel number for a proof of $G$.\" But it doesn't specify what that number is. So S can still have theorems: \"1 does not prove $G$\", \"2 does not prove $G$\", \"3 does not prove $G$\" and so on, and it would only be omega-inconsistent (since there is no provable statement that is blatantly the negation of another). But we assume that $S$ is omega-consistent, so we are forced to conclude that $G$ is undecidable. Okay. (as a side-note, I thought that Godel's proof didn't need the assumption of omega-consistency, but it seems required here ... ?)\n\nNow, I understand what happens when you add $G$ to S. In this new $S+G$ system, $G$ says, \"There is no number which is the Godel number of a proof for $G$ in S\", which is, of course, true (and presumably consistent).\n\nBut in $S + \\neg G$, $\\neg G$ says \"There is a number which is the Godel number of a proof for $G$ in S\"; yet, since every provable statement of $G$ is also provable in $S + \\neg G$, this new system will also say \"1 does not prove $G$ in S\", \"2 does not prove $G$ in S\", ... and so on. So isn't $S + \\neg G$ omega-inconsistent? And doesn't that go against the idea that we should be able to add either $G$ or $\\neg G$ to S and still end up with a consistent system? Does that \"consistency promise\" not extend to omega-consistency? If not, isn't there a \"logically better\" way to extend S, even though both extensions are possible?\n\n• The notion of \"number\" in $S+\\neg G$ is not the same. In fact, you want to understand $G$ as saying \"there does not exist an '$S$-number' that is the number of a proof of $G$.\", however, there well can be an \"$S+\\neg G$\"-number that is a proof (and indeed there is), because you have new axioms, so your function \"is a proof in $S$ of\" is different from the function \"is a proof in $S+\\neg G$ of\". Also, note that there are versions of Goedel's proof that avoid the issue of $\\omega$-inconsistent. – Arturo Magidin Apr 16 '12 at 20:55\n• In addition to Arturo's previous comment, your first paragraph is slightly wrong. No one guarantees that $S+G$ and $S+\\lnot G$ are consistent. However if $S$ is consistent then so are $S+G$ and $S+\\lnot G$. We simply did not introduce contradictions to the system, but we might not be able to prove the consistency of $S$. – Asaf Karagila Apr 16 '12 at 21:02\n• @ArturoMagidin I understand that $\\neg G$ in $S + \\neg G$ talks about provability in $G$, but why would it talk about S numbers and not $S + \\neg G$ numbers? I understand that the function \"is provable in S\" is different from the function \"is provable in $S + \\neg G$\". But when I prove, in $S + \\neg G$, that \"there is a number that proves G in S\" and \"1 is not that number\", \"2 is not that number\", etc., am I not talking about the same type of numbers in each case? – Ord Apr 16 '12 at 21:03\n• @AsafKaragila But we assume the consistency of S, don't we? We assume it, and then go ahead and show that $S + \\neg G$ must be omega-inconsistent! How does that work? Surely, Godel's proof does not say that a consistent formal system cannot exist? – Ord Apr 16 '12 at 21:05\n• @Ord: There is no \"absolute\" consistency, you need to have some basic system which you believe is consistent. Even the rules of first-order logic require a certain degree of belief or the fact we can use induction. We have good reasons to believe these are consistent, but no proof of that. Suppose that we are all wrong, and all mathematics in its current form is inconsistent and we can only prove these things because our most basic intuition is inconsistent? This is why we say that if $S$ is consistent then $S+G$ and $S+\\lnot G$ are, but this is a big if sometimes. – Asaf Karagila Apr 16 '12 at 21:26\n\n## 2 Answers\n\nYour conclusion that $S+\\neg G$ is not $\\omega$-consistent is right. It is (assuming that $S$ is consistent) consistent, but fails to be $\\omega$-consistent. Being $\\omega$-consistent is a stronger condition than consistency, satisfied by fewer systems.\n\nWould it be \"logically better\" to extend $S$ in an $\\omega$-consistent way than in one that isn't? I don't think so. As a sometimes Platonist, I would certainly favor the extension $S+G$ over $S+\\neg G$, perhaps even claiming that the former is true whereas the latter isn't, but that preference is not based on logical properties (being true is not a logical property).\n\nPart of the confusion is that \"$\\omega$-consistency\" is something of a misnormer -- because the name contains \"consistency\" one is tempted to think that like ordinary consistency it is an intrinsic property of the theory. But really it isn't; saying that a theory is $\\omega$-consistent is a statement between the relation between what the theory proves and arithmetic at the meta-level. Being $\\omega$-consistent is a necessary criterion for the theorems of the theory to be truths about the intuitive naturals, but failure to express arithmetic truth is not a logical problem for the theory -- it is innocent of our ambitions about what we might like it to model or not.\n\nOne might consider modifications of the concept of $\\omega$-consistency such that it looks more intrinsic to the theory. For example we could define that a theory $T$ is $\\omega'$-consistent iff, whenever $T\\vdash \\exists x. \\phi(x)$ there is some closed term $t$ such that $T\\vdash \\phi(t)$. (The difference is that in ordinary $\\omega$-consistency we require $t$ to be a \"numeral\"; the generalized definition allows arbitrary closed terms). However, under this generalization it is still not clear why one would consider $\\omega'$-consistency to be a desirable property of theories in general, even if we don't intend the theory to model arithmetic.\n\n• Excuse my ignorance, but what exactly is a \"closed term\", and why would omega-prime-consistency be undesirable? – Ord Apr 16 '12 at 23:25\n• A closed term is one that contains no variables -- such as $S(S(S(0)))+S(0)$ in the language of arithmetic opposed to $S(S(S(x)))+y$. -- I'm not saying that $\\omega'$-consitency would be actively undesirable, just that I don't see why one would explicitly desire it. For example, ZFC is not $\\omega'$-consistent, but I don't think one should count that as a disadvantage. – Henning Makholm Apr 16 '12 at 23:31\n• Okay, thank you very much for your response! I think I have a much better handle on the situation now. – Ord Apr 16 '12 at 23:40\n• But your notion of $ω'$-consistency is not analogous, because it is not at all related to the original. To even say that ZFC is $ω$-consistent, we need a suitable translation of arithmetical terms and sentences into terms and sentences over ZFC, so of course the nature of natural numbers and their codes is inbuilt into the notion of $ω$-consistency. So it is justifiable to consider $ω$-consistency desirable but consider $ω'$-consistency a completely different notion, namely that the term model exists. No? – user21820 May 2 '16 at 13:24\n• @user21820: The relation is that a theory in the language of arithmetic that extends Q is $\\omega'$-consistent if and only if it is $\\omega$-consistent. The last paragraph was intended to explain that at least one way to escape the non-logicalness of $\\omega$-consistency by attempting to phrase it in a way that is not specific to the language of arithmetic, doesn't seem to work very well. – Henning Makholm May 2 '16 at 13:32\n\nOmega-consistency is certainly a syntactical property; in that sense, it is an intrinsic property of systems, not a property they have under a particular interpretation.\n\nHowever, if consistency is desirable on simple logical grounds, the desirability of omega-consistency is arithmetical, for only if we take our universe of discourse to be the natural numbers (or some other items with the same structure), we will consider desirable for a system denying a property P of each numeral (0, S0, SS0, ...) to not prove the existence of an object with P.\n\nIf we wish to admit objects other than the naturals in our universe, omega-consistency need not be desirable." ]
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https://downloads.hindawi.com/journals/mpe/2009/696253.xml
[ "MPEMathematical Problems in Engineering1563-51471024-123XHindawi Publishing Corporation69625310.1155/2009/696253696253Research ArticleImproving Accuracy of Coarse Grid Numerical Solution of Solid-Solid Reactions by Taylor Series Expansion of the Reaction TermHassanzadehHassanPooladi-DarvishMehranAbediJalalJiangJ.Department of Chemical and Petroleum EngineeringSchulich School of EngineeringUniversity of Calgary2500 University Drive NWCalgary, ABCanadaT2N 1N4ucalgary.ca200928042009200928112008120220092009Copyright © 2009This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.\n\nExothermic solid-solid reactions lead to sharp reaction fronts that cannot be captured by coarse spatial mesh size numerical simulations that are often required for large-scale simulations. We present a coarse-scale formulation with high accuracy by using a Taylor series expansion of the reaction term. Results show that such expansion could adequately maintain the accuracy of fine-scale behavior of a constant pattern reaction front while using a smaller number of numerical grid cells. Results for a one-dimensional solid-solid reacting system reveal reasonable computational time saving. The presented formulation improves our capabilities for conducting fast and accurate numerical simulations of industrial-scale solid-solid reactions.\n\n1. Introduction\n\nModeling of reactive flow has diverse applications in engineering and science. Applications include heavy oil recovery processes, combustion in porous media, ground water flow, and transport and reaction processes in biofilms. An important class of reactions is that of solid-solid reactions. Modeling of solid-solid reactions is of significant interest in various industrial operations, including oxidation of metallic and nonmetallic mixed powders, cement industry , ferrites manufacturing, solid-state polymerization [2, 3], ceramic manufacturing , catalyst preparation , and drug storage (for more details, see a comprehensive review by Tamhankar and Doraiswamy ). Numerous investigations on modeling reactive flow have been reported over the years that greatly improved the understanding of such systems, where the emphasis has primarily been on approximate analytical solutions for special cases, fine grid direct numerical simulation, and upscaling of reaction-transport from pore scale to continuum scale .\n\nAccurate numerical simulation of solid-solid reactions is a challenging task due to the multiscale nature of the physical phenomena. Physical processes involved in solid-solid reactive systems include diffusive (heat and mass) and reactive processes. Reactions in porous media intrinsically often take place at the small scale, causing development of subdiffusive-scale concentration and temperature gradients, while heat and mass diffusive processes have scales orders of magnitude larger than the reactions. Large-scale simulation of such coupled processes is computationally expensive due to limitations in computational resources. Therefore, a formulation that captures the subdiffusive scale improves our capabilities for conducting industrial-scale simulation of the involved processes with high accuracy. In this paper, we provide a coarse-scale formulation to capture the subgrid-scale phenomena appropriate for large-scale numerical simulations. The paper is organized as follows. First, the fine-scale mathematical model used in this study is presented. Next, the coarse-scale model is described. Then, application of the coarse-scale model is given for a constant pattern reaction front, followed by summary and conclusions.\n\n2. Fine-Scale Conservation Equations\n\nThe exothermic solid-solid reaction is assumed to take place in a one-dimensional semi-infinite domain. The system, which consists of a mixture of two solid materials, is initially at temperature T0. The concentration of one of the solids is in excess such that the reaction can be considered of first order with respect to the second solid. The initial concentration of the second solid is C0. At time t=0, the initial temperature T0 at x=0 is suddenly raised to ignition temperature high enough to initiate the reaction by local heating. The temperature dependence of the reaction rate is assumed to follow Arrhenius type behavior, and all physical properties are assumed to be constant. Mass diffusion is considered to be negligible, and the reaction front is planar and nonoscillatory. It is further assumed that the solid reacting mixture acts as an isotropic homogeneous system and that radiation effects are negligible . The dimensionless energy and mass balances can be presented by parabolic coupled partial differential equations given by θtD=2θxD2+CDexp(θβθ+1),CDtD=γCDexp(θβθ+1), where the following dimensionless groups are used [11, 13]: θ=E(TT*)RT*2,CD=CC0,tD=tt*,t*=ρcpRT*2Ek(ΔH)C0exp(ERT*),xD=xx*,x*=λt*ρcp¯,γ=ρcp¯RT*2E(ΔH)C0,β=RT*E, where T is temperature, C is concentration of reactant, ρ is density, cp is heat capacity, λ is the average thermal conductivity, k is the pre-exponential factor, E is activation energy, ΔH is the heat of reaction, R is the universal gas constant, t is time, T* is the scale temperature, and x is the spatial coordinate. We used a standard scaling available in the combustion literature to render the equations dimensionless [13, 1921]. The scaling variable x* corresponds to an approximate measure of the heating zone length, and x*/t* is a measure of the reaction front velocity .\n\nThe initial and boundary conditions are then given by θ=θ0,0xD,tD=0,CD=1,0xD,tD=0,θ=0,atxD=0,tD>0,θxD=0,x,tD>0,CDxD=0,x,tD>0. The behavior of such a reacting convection diffusion system is primarily determined by the inverse of dimensionless activation energy and inverse of dimensionless heat of reaction, namely, β and γ, respectively. Puszynski et al. presented a detailed analysis of the frontal behavior of such a system. Small β or γ values correspond to a reacting system with high activation energy or heat of reaction and vice versa. Large values of γ (small values of heat of reaction and/or small values of activation energy) lead to a degenerated combustion regime, whereas low values of γ (large values of heat of reaction and/or large values of activation energy) result in an oscillatory reaction front. Low β values (large activation energy) and intermediate γ values result in a constant pattern profile regime. Choosing large grid cells results in significant smearing of the reaction front, as we will see in the following sections. In the subsequent part of the paper, we present the model formulation that is able to maintain the accuracy of fine grid behavior while using coarse grid cell sizes.\n\n3. Coarse-Scale Conservation Equations\n\nNumerical simulation of reactive front propagation with a large number of grid cells is computationally expensive and therefore we are interested in using a coarse model that preserves the accuracy of fine grid behavior. The coarse-scale variable can be defined by ψ¯=1vvψdv, where v represents the coarse grid.\n\nWe intend to represent the differential equations (2.1) with their corresponding coarse grid equivalents (3.2). In these equations, ¯ represents the “equivalent” reaction rate that would allow close agreement between the (2.1) set and the (3.2) set, correspondingly. The coarse-scale numerical model can be expressed by θ¯tD=2θ¯xD2+¯,C¯DtD=γ¯, where =CDexp(θβθ+1),¯=1vvCDexp(θβθ+1)dv=CDexp(θβθ+1)¯ are the fine-scale reaction rate and coarse-scale average reaction rate, respectively. The reaction rate can be approximated by a Taylor series expansion around the coarse-scale temperature and concentration. The above expansion can be represented in terms of deviation from the coarse-scale variables as given by (C¯D,θ¯)+CD|C¯D,θ¯CD+θ|C¯D,θ¯θ+12!(2CD2|C¯D,θ¯(CD)2+22CDθ|C¯D,θ¯CDθ+2θ2|C¯D,θ¯(θ)2)+, where CD=CDC¯D and θ=θθ¯ are the concentration and temperature deviations from the fine scale solution, respectively. The terms involving derivatives account for the information that is normally lost in a coarse grid numerical solution; those will be evaluated and accounted for herein. By using (3.1), the average coarse-scale reaction rate can be expressed by ¯(C¯D,θ¯)+12!(2CD2|C¯D,θ¯(CD)2¯+22CDθ|C¯D,θ¯CDθ¯+2θ2|C¯D,θ¯(θ)2¯)+,2θ2|C¯D,θ¯=12β(1+βθ¯)(βθ¯+1)4C¯Dexp(θ¯βθ¯+1),2CD2|C¯D,θ¯=0,2CDθ|C¯D,θ¯=exp(θ¯/(βθ¯+1))(βθ¯+1)2, where by definition the terms with first derivatives are dropped in the averaging process . Equation (3.5) is a coarse-scale representation of the reaction rate that includes both coarse-scale concentration and temperature and their deviations from fine scale, namely, CD and θ, respectively. We do not have an explicit definition of the deviation terms CD and θ as functions of the coarse-scale concentration and temperature. Instead, we intend to express the quantities (θ)2¯ and CDθ¯ in a form proportional to θ¯/xD and (θ¯/xD)(C¯D/xD) such that the final coarse-scale model can be presented as a function of coarse-scale temperature and concentration only. Similar approach has been used by Meile and Tuncay for linear convection-diffusion-reaction problem. The common practice in a volume averaging method [1417, 22] is to solve the closure problem, which is obtained by subtraction of the fine-scale and the coarse-scale equations. Here, due to the complexity arising from the nonlinearity of the problem, subtraction does not lead to (an) equation(s) in terms of the perturbed quantities. However, consistent with the volume averaging method , an appropriate approximation for the deviation terms is linear proportionality of temperature and concentration deviations with their corresponding gradient. Using this approximation, one may write (θ)2¯=α(θ¯xD)2,CDθ¯=α(θ¯xD)(C¯DxD). By substituting (3.9) in (3.5), the coarse-scale equations (3.2) can be written as θ¯tD=2θ¯xD2+(C¯D,θ¯)+α2!(22CDθ|C¯D,θ¯(θ¯xD)(C¯DxD)+2θ2|C¯D,θ¯(θ¯xD)2),C¯DtD=γ(C¯D,θ¯)γ{α2!(22CDθ|C¯D,θ¯(θ¯xD)(C¯DxD)+2θ2|C¯D,θ¯(θ¯xD)2)}, where α is the proportionality constant or coarse-scale parameter and is a function of coarse grid size. The coarse-scale formulation is not closed so far, and the proportionality constant α as a function of coarse grid size needs to be determined. Numerical experiments reveal that the term containing cross derivatives in the internal bracket in the right-hand side in (3.10) is small as compared to the second term. Given that the cross derivatives are small as compared to the second term, it may be ignored. Therefore, the coarse-scale formulation can be rendered as θ¯tD=2θ¯xD2+(C¯D,θ¯)+α2!2θ2|C¯D,θ¯(θ¯xD)2,C¯DtD=γ(C¯D,θ¯)γ{+α2!2θ2|C¯D,θ¯(θ¯xD)2}. The coarse grid model represented by (3.11) is of the same form as (2.1) with the same dimensionless groups, γ and β; however, the reaction term is replaced by (C¯D,θ¯)+α(2/θ2)C¯D,θ¯(θ¯/xD)2/2.\n\nIn order to find the proportionality constant α as a function of coarse spatial mesh size, a series of numerical experiments needs to be conducted for different spatial mesh sizes for each specific reacting system (i.e., using fixed γ and β). The functionality (α versus spatial mesh size) for a specific reacting system can be determined by matching the coarse spatial mesh size solution with the fine scale or reference solution. In matching process, to estimate the deviations of the coarse-scale model predictions from the fine-scale reference solution, we define a numerical error using the following expression as a measure of accuracy: ε={[(ψψ¯)2dxD][ψ2dxD]}1/2, where ψ can be either temperature or concentration.\n\nThe proportionality constant is obtained by the minimization of the numerical error given by (3.12). By repeating the matching process for different number of spatial mesh sizes, the proportionality constant for each spatial mesh size can be obtained. Once the functionality of the proportionality constant with respect to coarse spatial mesh size is obtained, the coarse-scale formulation (3.11) is complete and can be used for subsequent large-scale simulation of a solid-solid reactive system. In the following, we use the above procedure for determining the parameter α as a function of coarse spatial mesh size for some solid-solid reacting systems.\n\n4. Application of the Coarse-Scale Formulation\n\nBased on the scaling groups used in nondimensionalizing the governing equations, the frontal behavior of a solid-solid reaction depends on two parameters, namely, β (inverse of dimensionless activation energy) and γ (inverse of dimensionless heat of reaction). The coarse-scale formulation described previously is applied for two solid-solid reactions. The governing differential equations are discretized using an explicit-in-time finite difference approximation. A block-centered scheme is used, where the diffusive flux is calculated based on grid block center values. Numerical simulations are conducted to determine the parameter α appropriate for large-scale numerical simulation of such reacting systems. The dimensionless constants for these reacting systems are given in Table 1. The data are taken from examples of solid-solid reactions given by Puszynski et al. . For each reacting system, temperature at one end is rapidly increased to an ignition temperature. Since the temperature is scaled with the adiabatic temperature of the reaction (Ta=T*), the minimum dimensionless temperature in the system is equal to the negative of the dimensionless heat of reaction (1/γ). Figure 1 shows α as a function of numerical spatial mesh size for different solid-solid reaction systems given in Table 1. In all cases, the conditions are selected such that a constant pattern profile exists. The condition for existence of a constant pattern reaction front can be predicted by the following expression : γc=12(θcθ0), where θc=θ0+212β. For γ<γc, a reacting system demonstrates constant pattern reaction front propagation. The parameter γc for reactions studied is given in Table 1.\n\nDimensionless parameters for solid-solid reacting systems used in this study.\n\nReaction βγθ0θiγc\n10.10.2500.2\n20.06450.147.14300.218\n\nCoarse-scale parameter α as a function of grid size for two reactions in Table 1.\n\nFigure 1 shows the coarse-scale parameter αobtained for the two reactions given in Table 1. Using this methodology, the coarse-scale parameter αas a function spatial mesh size can be obtained for a specific solid-solid reaction system. This parameter then can be used for large-scale numerical simulation of a reactive system. Figure 1 shows that for both reactions the coarse parameter α  starts increasing about a dimensionless grid size of 5 suggesting that x*=0.2Δx. Figure 2 shows the reaction rate as a function of dimensionless distance. The dimensionless size of the reaction zone ΔxDf=Δxf/x* is approximated by the region, where the reaction rate is larger than 0.01 times of the peak reaction rate. Results show that for both reactions the approximate dimensionless size of the reaction zone is about 13 suggesting that using fine-scale model one needs to use grid size of 5/13 of the size of the reaction zone to roughly capture the reaction front. The presented coarse-scale formulation allows us to use larger grid size while maintaining accuracy of the solution. Figures 3 and 4 show comparisons of concentration and temperature profiles with and without use of the presented coarse-scale formulation. Results show that the coarse-scale formulation could represent the location of the reaction front accurately with a small number of grid cells. Figures 3 and 4 also show that by using coarse-scale formulation one might choose a coarse spatial mesh size two times of the reaction zone while maintaining the numerical solution accuracy.\n\nReaction rate for the two reactions as a function of dimensionless distance.\n\nConcentration and temperature distributions at tD=400 for Reaction 1 given in Table 1 with and without coarse-scale formulation for three grid sizes of 25, 16.7, and 9.1. (—) reference solution, () without using coarse-scale parameter, and () with using coarse-scale parameter.\n\nConcentration and temperature distributions at tD=650 for Reaction 2 given in Table 1 with and without coarse-scale formulation for three grid sizes of 25, 16.7, and 9.1. (—) reference solution, () without using coarse-scale parameter, and () with using coarse-scale parameter.\n\nThe calculated numerical errors for the reactions given in Table 1 are presented in Figure 5 for concentration and temperature for different grid sizes. Results show that the presented coarse-scale formulation could significantly reduce the numerical error. In addition, the ratio of CPU time for coarse-scale formulation and fine grid reference solutions is presented in Figure 6. Results show that the CPU time ratio scales with the inverse of grid size, suggesting a ten-fold reduction in CPU time with a ten-fold increase in grid size. Currently, we are working toward finding scaling or proportionality constant for multidimensional problems. CPU time savings is expected to be much more significant for multidimensional problems.\n\nNumerical error in temperature (left) and concentration (right) distributions for reactions given in Table 1 with and without coarse-scale formulation for different grid sizes.\n\nRatio of coarse to fine grid (reference) CPU times versus dimensionless grid size for the two reactions given in Table 1.\n\n5. Concluding Remarks\n\nPropagation of solid-solid reaction fronts often results in a thin reaction zone that is difficult to resolve numerically unless a large number of numerical grid cells are used. Such numerical simulations are computationally expensive to perform. In this study, a coarse-scale formulation for numerical modeling of a one-dimensional solid-solid reacting system is presented. The presented formulation is based on a Taylor series expansion of the reaction term and presents the modification of the reaction term in the coarse model that would allow an accurate solution. A key parameter in this formulation is α or so-called coarse-scale parameter, which is a function of the coarse-scale spatial mesh size. Using the presented formulation, this parameter as a function of spatial mesh size can be obtained. This parameter then can be used for numerically solving a large scale and computationally intensive reacting system. It is shown that this formulation could reasonably obtain the accuracy of a fine grid numerical solution. It is shown that the coarse-scale formulation considerably reduces the numerical error. In addition, it is revealed that the ratio of CPU times of a coarse-scale model to that of a fine grid solution scales with the inverse of grid size. Such inverse proportionality implies a significant reduction in CPU time of a coarse-scale model compared to that of a fine grid-scale model for large-scale simulations. Results obtained in this study for a one-dimensional reacting system are promising in terms of reducing computational time. However, the presented methodology has a number of limitations that are the subject of our current research. First, the coarse-scale parameter needs to be characterized as a function of the governing dimensionless numbers. In addition, the applicability of this method needs to be tested for multidimensional problems, where we expect a major reduction in CPU time. Presently, we are working toward implementation of the presented methodology for multidimensional problems and determination of the coarse-scale parameter as a function of dimensionless numbers for solid-solid reactions. We anticipate that the computational time saving for multidimensional problems is more promising. The presented formulation improves our capabilities for conducting more accurate and faster numerical simulation of industrial-scale solid-solid reactions.\n\nNomenclaturecp:\n\nHeat capacity, Jkg1K1\n\nC:\n\nConcentration, kg/m3\n\nD:\n\nMolecular diffusion coefficient, m2/s\n\nE:\n\nActivation energy, Jkmol1\n\nΔH:\n\nHeat of reaction, J/kg\n\nk:\n\nPre-exponential rate constant, s1\n\nR:\n\nGas constant, Jkmol1K1\n\nt:\n\nTime, s\n\nT:\n\nTemperature, K\n\nx:\n\nCoordinate, m.\n\nGreek Lettersα:\n\nCoarse-scale parameter\n\nβ:\n\nInverse of dimensionless activation energy\n\nγ:\n\nInverse of dimensionless heat of reaction\n\nε:\n\nNumerical error\n\nv:\n\nCoarse-scale volume, m3\n\nψ:\n\nFine-scale variable can be temperature, concentration, or reaction rate\n\n:\n\nReaction rate, kgm3s1\n\nλ:\n\nEffective thermal conductivity, Jm1s1K1\n\nρ:\n\nDensity, kgm3\n\nθ:\n\nDimensionless temperature.\n\nSubscriptsa:\n\nc:\n\nCritical\n\nD:\n\nDimensionless\n\ni:\n\nIgnition\n\n0:\n\nInitial value\n\n*:\n\nScale value.\n\nSuperscripts':\n\nDeviation from coarse scale\n\n:\n\nAverage or coarse scale.\n\nAcknowledgments\n\nThe authors would like to acknowledge constructive comments from Dr. Brian Wood and Dr. Christof Meile. Helpful discussion with Dr. Mohsen Sadeghi is also acknowledged. The financial support of the Alberta Ingenuity Centre for In Situ Energy (AICISE) is acknowledged. The authors would like to thank the reviewers for useful comments.\n\nLeaF. M.The Chemistry of Cement and Concrete19703rdLondon, UKEdward ArnoldsChechiloN. M.KhvilivitskiiR. J.EnikolopyanN. S.On the phenomenon of polymerization reaction spreadingDoklady Akademii Nauk SSSR197220411801181IlyashenkoV. M.SolovyovS. E.PojmanJ. A.Theoretical aspects of self-propagating reaction fronts in condensed mediumAIChE Journal199541122631263610.1002/aic.690411212KingeryW. D.Introduction to Ceramics1967New York, NY, USAJohn Wiley & SonsBleijenbergA. C. A. M.LippensB. C.SchuitG. C. A.Catalytic oxidation of 1-butene over bismuth molybdate catalysts. I. The system Bi2O3-MoO3Journal of Catalysis19654558158510.1016/0021-9517(65)90163-6TamhankarS. S.DoraiswamyL. K.Analysis of solid-solid reactions: a reviewAIChE Journal197925456158210.1002/aic.690250402ZeldovichYa. B.Frank-KamenetzkiiD. A.A theory of thermal propagation of flameACTA Physico-Chimica URSS193892341350MargolisS. B.An asymptotic theory of condensed two-phase flame propagationSIAM Journal on Applied Mathematics198343235136910.1137/0143024MR700343ZBL0511.76098MargolisS. B.An asymptotic theory of heterogeneous condensed combustionCombustion Science and Technology1985433-419721510.1080/00102208508947004MargolisS. B.ArmstrongR. C.Two asymptotic models for solid propellant combustionCombustion Science and Technology1986471-213810.1080/00102208608923862PuszynskiJ.DegreveJ.HlavacekV.Modeling of exothermic solid-solid noncatalytic reactionsIndustrial and Engineering Chemistry Research19872671424143410.1021/ie00067a026RajaiahJ.DandekarH.PuszynskiJ.DegreveJ.HlavacekV.Study of gas-solid, heterogeneous, exothermic, noncatalytic reactions in a flow regimeIndustrial and Engineering Chemistry Research198827351351810.1021/ie00075a023DandekarH.PuszynskiJ. A.DegreveJ.HlavacekV.Reaction front propagation characteristics in non-catalytic exothermic gas-solid systemsChemical Engineering Communications19909219922410.1080/00986449008911431WoodB. D.WhitakerS.Diffusion and reaction in biofilmsChemical Engineering Science199853339742510.1016/S0009-2509(97)00319-9WoodB. D.WhitakerS.Erratum to “Diffusion and reaction in biofilms”Chemical Engineering Science20005512234910.1016/S0009-2509(99)00504-7WoodB. D.brian.wood@pnl.govWhitakerS.Multi-species diffusion and reaction in biofilms and cellular mediaChemical Engineering Science200055173397341810.1016/S0009-2509(99)00572-2WoodB. D.brian.wood@oregonstate.eduRadakovichK.GolfierF.Effective reaction at a fluid-solid interface: applications to biotransformation in porous mediaAdvances in Water Resources2007306-71630164710.1016/j.advwatres.2006.05.032MeileC.cmeile@uga.eduTuncayK.Scale dependence of reaction rates in porous mediaAdvances in Water Resources2006291627110.1016/j.advwatres.2005.05.007MerzhanovA. G.FilonenkoA. K.BorovinskayaI. P.New phenomena in combustion of condensed systemsDoklady Akademii Nauk SSSR1973208892894MerzhanovA. G.BorovinskayaI. P.A new class of combustion processesCombustion Science and Technology1975105-619520110.1080/00102207508946671MerzhanovA. G.KhaikinB. I.Theory of combustion waves in homogeneous mediaProgress in Energy and Combustion Science198814119810.1016/0360-1285(88)90006-8WoodB. D.brian.wood@orst.eduCherblancF.QuintardM.quintard@imft.frWhitakerS.swhitaker@ucdavis.eduVolume averaging for determining the effective dispersion tensor: closure using periodic unit cells and comparison with ensemble averagingWater Resources Research2003398121010.1029/2002WR001723" ]
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https://www.friedsamengineering.com/polymerase-chain-reaction
[ "# Polymerase Chain Reaction Machine\n\nPolymerase chain reaction is the process of DNA replication. It consists of three phases: denaturation, annealing and extension. Those phases are cycled through between 30 and 40 times to exponentially generate copies of a a DNA segment. For more information on the reaction you can read this Wikipedia article or watch the video to the right. The science department at my high school wanted an additional PCR machine and rather than spending thousands of dollars buying one, they tasked me with building one. I created a Github Repository with all of the code, schematics and other necessary files for anyone interested in recreating the machine.\n\n# Final Product:", null, "# Components and Schematic:", null, "# PCB:\n\nIn efforts to consolidate the circuitry and build a more robust machine I designed and ordered a printed circuit board. The printed circuit board will also ensure better connections soldered down rather than connected with a breadboard. An image of the circuit board schematic is to the right. If you are interested in recreating this project I highly recommend using a PCB. To order a copy of the one that I made you can download the gerber file (along with all other important files) from my Github Repository and then order the board from a PCB fabricator. I recommend JLCPCB.com.", null, "# Testing:", null, "This is a photograph of all of the components put together without an enclosure/case which I am currently designing and plan to make using a laser cutter.\n\n# Cycle Data:", null, "This graph shows the temperature in celsius of the aluminum block throughout one cycle. The three plateaus at 95C, 50C and 72C show the machine holding a steady temperature at each of the 3 PCR stages.\n\n# Code:\n\n/* Pin Layout:\n\n* JOYSTICK:\n\n* X to A0\n\n* SW to D2\n\n* LCD\n\n* SDA to A4\n\n* SCL to A5\n\n* Thermocouple\n\n* DO to D3\n\n* CS to D4\n\n* CLK to D5\n\n* Relay\n\n* Pos to D13\n\n*/\n\n//Include libraries required for components\n\n#define MAXDO 3\n\n#define MAXCS 4\n\n#define MAXCLK 5\n\n#include <Wire.h>\n\n#include <LiquidCrystal_I2C.h>\n\nLiquidCrystal_I2C lcd(0x27, 2,1,0,4,5,6,7);\n\n// Define variables\n\nlong duration;\n\nint cycles = 1;\n\nint currentCycle = 1;\n\nlong startTime;\n\nlong timeEllapsed;\n\nlong firstDenaturationDuration;\n\nlong fDDSeconds = 0;\n\nlong fDDMins = 02;\n\nlong lastExtensionDuration;\n\nlong fEDSeconds = 0;\n\nlong fEDMins = 05;\n\nlong endTime;\n\nlong remainder;\n\ndouble annealingTemp = 50.00;\n\n// Create non-return functions to turn on the heater and fan\n\nvoid heaterOn() {digitalWrite(13, HIGH);}\n\nvoid fanOn() {digitalWrite(13, LOW);}\n\n// Non return function to set up how many cycles to run\n\nvoid getCycles() {\n\nlcd.setCursor(5,0);\n\nlcd.print(\"CYCLES:\");\n\nlcd.setCursor(7,1);\n\nlcd.print(cycles);\n\n// Read Joystick and determine if user is going up or down\n\nif (analogRead(0) < 100 && cycles >= 2) {\n\ncycles -= 1;\n\ndelay(200);\n\n}\n\ncycles += 1;\n\ndelay(200);\n\n}\n\n// Keep prompting for input\n\ngetCycles();\n\n}\n\n}\n\n// Non return func to determine first denaturation duration (different duration from rest)\n\nvoid getFirstDenaturationDuration() {\n\n// Set up screen and times\n\nlcd.setCursor(0,0);\n\nlcd.print(\"1st Denaturation\");\n\nlcd.setCursor(0,1);\n\nlcd.print(\"Time: \");\n\nlcd.setCursor(6,1);\n\nlcd.print(fDDMins);\n\nlcd.setCursor(7,1);\n\nlcd.print(\":\");\n\n// Handle seconds over 59\n\nif (fDDSeconds > 59) {\n\nfDDMins += 1;\n\nfDDSeconds = 0;\n\ndelay(250);\n\n}\n\n// Handle seconds less than 0\n\nif (fDDSeconds == 0 && analogRead(0) < 100) {\n\nfDDMins -= 1;\n\nfDDSeconds = 59;\n\ndelay(250);\n\n}\n\nif (fDDSeconds >= 9) {\n\nlcd.setCursor(8,1);\n\nlcd.print(fDDSeconds);\n\n}\n\nif (fDDSeconds < 10 && fDDSeconds > 0) {\n\nlcd.setCursor(8,1);\n\nlcd.print(\"0\");\n\nlcd.setCursor(9,1);\n\nlcd.print(fDDSeconds);\n\n}\n\n// Print seconds when seconds = 0\n\nif (fDDSeconds == 0) {\n\nlcd.setCursor(8,1);\n\nlcd.print(\"00\");\n\n}\n\n// Define duration\n\nfirstDenaturationDuration = ((fDDMins * 60000) + (fDDSeconds * 1000));\n\nif (analogRead(0) < 100 && firstDenaturationDuration>30000) {\n\nfDDSeconds -= 1;\n\ndelay(200);\n\n}\n\n// Plus 1 second\n\nif (analogRead(0) > 900 && fDDMins < 8) {\n\nfDDSeconds += 1;\n\ndelay(200);\n\n}\n\n// Set duration\n\nfirstDenaturationDuration = (fDDMins * 60000) + (fDDSeconds * 1000);\n\n// Keep prompting for input\n\ngetFirstDenaturationDuration();\n\n}\n\n}\n\n// Get annealing temp\n\nvoid getAnnealTemp() {\n\n// Set up LCD\n\nlcd.setCursor(1,0);\n\nlcd.print(\"ANNEALING TEMP:\");\n\nlcd.setCursor(5,1);\n\nlcd.print(annealingTemp);\n\n// Read joystick and inc/dec in decrements of 0.25 degrees C\n\nif (analogRead(0) < 100 && annealingTemp >= 49) {\n\nannealingTemp -= 0.25;\n\ndelay(200);\n\n}\n\nannealingTemp += 0.25;\n\ndelay(200);\n\n}\n\n// Keep prompting for input\n\ngetAnnealTemp();\n\n}\n\n}\n\n// Get last extension duration function (diff from other extension durrations)\n\nvoid getLastExtensionDuration() {\n\n// Set up LCD\n\nlcd.setCursor(1,0);\n\nlcd.print(\"Last Extension\");\n\nlcd.setCursor(0,1);\n\nlcd.print(\"Time: \");\n\nlcd.setCursor(6,1);\n\nlcd.print(fEDMins);\n\nlcd.setCursor(7,1);\n\nlcd.print(\":\");\n\n// Same as above: Handle joystick input, change times based on input, keep prompting until joystick is clicked\n\nif (fEDSeconds > 59) {\n\nfEDMins += 1;\n\nfEDSeconds = 0;\n\ndelay(250);\n\n}\n\nif (fEDSeconds == 0 && analogRead(0) < 100) {\n\nfEDMins -= 1;\n\nfEDSeconds = 59;\n\ndelay(250);\n\n}\n\nif (fEDSeconds >= 9) {\n\nlcd.setCursor(8,1);\n\nlcd.print(fEDSeconds);\n\n}\n\nif (fEDSeconds < 10 && fEDSeconds > 0) {\n\nlcd.setCursor(8,1);\n\nlcd.print(\"0\");\n\nlcd.setCursor(9,1);\n\nlcd.print(fEDSeconds);\n\n}\n\nif (fEDSeconds == 0) {\n\nlcd.setCursor(8,1);\n\nlcd.print(\"00\");\n\n}\n\nlastExtensionDuration = ((fEDMins * 60000) + (fEDSeconds * 1000));\n\nif (analogRead(0) < 100 && lastExtensionDuration>60000) {\n\nfEDSeconds -= 1;\n\ndelay(200);\n\n}\n\nif (analogRead(0) > 900 && fEDMins < 8) {\n\nfEDSeconds += 1;\n\ndelay(200);\n\n}\n\nlastExtensionDuration = (fEDMins * 60000) + (fEDSeconds * 1000);\n\ngetLastExtensionDuration();\n\n}\n\n}\n\n// Configure LCD to prompt for begin command\n\nvoid enter() {\n\nlcd.setCursor(2,0);\n\nlcd.print(\"FRIEDSAM PCR\");\n\nlcd.setCursor(1,1);\n\nlcd.print(\"CLICK TO BEGIN\");\n\nenter();\n\n}\n\n}\n\n// Function to run above functions to set up machine\n\nvoid getInput() {\n\ngetCycles();\n\nlcd.clear();\n\ndelay(500);\n\ngetFirstDenaturationDuration();\n\nlcd.clear();\n\ndelay(500);\n\ngetAnnealTemp();\n\nlcd.clear();\n\ndelay(500);\n\ngetLastExtensionDuration();\n\nlcd.clear();\n\ndelay(500);\n\nenter();\n\nlcd.clear();\n\ndelay(500);\n\n}\n\n//Function to be called recursively until temp for denaturation is reached\n\nvoid prepDenaturation() {\n\nheaterOn();\n\ndelay(500);\n\nlcd.clear();\n\nlcd.setCursor(5,0);\n\nlcd.print(\"HEATING\");\n\nlcd.setCursor(2,1);\n\nlcd.print(\"Temp: \");\n\nif (isnan(temp) == false) {\n\nlcd.setCursor(8,1);\n\nlcd.print(temp);\n\n}\n\nif (temp<95 || isnan(temp)) {\n\nprepDenaturation(); //if it is less than 95 degrees keep heating\n\n}\n\n}\n\n// Function to be called recursivley until denature duration has passed\n\nvoid denature() {\n\n// Switch between fan and heater to keep tempt between 94.75 and 95.25\n\nif (temp <= 94.75) {\n\nheaterOn();\n\n}\n\nif (temp >= 95.25) {\n\nfanOn();\n\n}\n\ntimeEllapsed = millis();\n\nendTime = startTime + duration;\n\nremainder = endTime - timeEllapsed;\n\ndelay(500);\n\nlcd.clear();\n\nlcd.setCursor(0,0);\n\nlcd.print(\"PHASE: DENATURE\");\n\nlcd.setCursor(0,1);\n\nlcd.print(\"CYCLE:\");\n\nlcd.setCursor(7,1);\n\nlcd.print(currentCycle);\n\nlcd.setCursor(10,1);\n\nlcd.print(temp);\n\nlcd.setCursor(15,1);\n\nlcd.print(\"C\");\n\nif (timeEllapsed < endTime) {\n\ndenature();\n\n}\n\n}\n\n// Function to cool down until temp is met for annealing\n\nvoid prepAnnealing() {\n\nfanOn();\n\ndelay(500);\n\nlcd.clear();\n\nlcd.setCursor(5,0);\n\nlcd.print(\"COOLING\");\n\nlcd.setCursor(2,1);\n\nlcd.print(\"Temp: \");\n\nif (isnan(temp) == false) {\n\nlcd.setCursor(8,1);\n\nlcd.print(temp);\n\n}\n\nif (temp >= annealingTemp + 0.25 || isnan(temp)) {\n\nprepAnnealing();\n\n}\n\n}\n\n// Anneal until annealing duration has passed (recursion)\n\nvoid anneal() {\n\nif (temp <= annealingTemp - 0.25) {\n\nheaterOn();\n\n}\n\nif (temp >= annealingTemp + 0.25) {\n\nfanOn();\n\n}\n\ntimeEllapsed = millis();\n\nendTime = startTime + duration;\n\nremainder = endTime - timeEllapsed;\n\ndelay(500);\n\nlcd.clear();\n\nlcd.setCursor(0,0);\n\nlcd.print(\"PHASE: ANNEAL\");\n\nlcd.setCursor(0,1);\n\nlcd.print(\"CYCLE:\");\n\nlcd.setCursor(7,1);\n\nlcd.print(currentCycle);\n\nlcd.setCursor(10,1);\n\nlcd.print(temp);\n\nlcd.setCursor(15,1);\n\nlcd.print(\"C\");\n\nif (timeEllapsed < endTime) {\n\nanneal();\n\n}\n\n}\n\n// Heat back up to prep for extension\n\nvoid prepExtension() { //heat back up\n\nheaterOn();\n\ndelay(500);\n\nlcd.clear();\n\nlcd.setCursor(5,0);\n\nlcd.print(\"HEATING\");\n\nlcd.setCursor(2,1);\n\nlcd.print(\"Temp: \");\n\nif (isnan(temp) == false) {\n\nlcd.setCursor(8,1);\n\nlcd.print(temp);\n\n}\n\nif (temp < 72 || isnan(temp)) {\n\nprepExtension();\n\n}\n\n}\n\n// Maintain extension tempt until extension time duration has passed (recursion)\n\nvoid extend() {\n\nif (temp <= 71.75) {\n\nheaterOn();\n\n}\n\nif (temp >= 72.25) {\n\nfanOn();\n\n}\n\ntimeEllapsed = millis();\n\nendTime = startTime + duration;\n\nremainder = endTime - timeEllapsed;\n\ndelay(500);\n\nlcd.clear();\n\nlcd.setCursor(0,0);\n\nlcd.print(\"PHASE: EXTEND\");\n\nlcd.setCursor(0,1);\n\nlcd.print(\"CYCLE:\");\n\nlcd.setCursor(7,1);\n\nlcd.print(currentCycle);\n\nlcd.setCursor(10,1);\n\nlcd.print(temp);\n\nlcd.setCursor(15,1);\n\nlcd.print(\"C\");\n\nif (timeEllapsed < endTime) {\n\nextend();\n\n}\n\n}\n\n// Run everything multiple times based on number of cycles defined above\n\nvoid PCR() {\n\nfor (int i = 0; i <= cycles-1; i++) {\n\nprepDenaturation();\n\nlcd.clear();\n\nif (currentCycle == 1) {duration = firstDenaturationDuration;}\n\nelse {duration = 30000;}\n\nstartTime = millis();\n\ndenature();\n\nlcd.clear();\n\nprepAnnealing();\n\nlcd.clear();\n\nduration = 30000;\n\nstartTime = millis();\n\nanneal();\n\nlcd.clear();\n\nprepExtension();\n\nlcd.clear();\n\nif (cycles - currentCycle == 0) {duration = lastExtensionDuration;}\n\nelse {duration = 60000;}\n\nstartTime = millis();\n\nextend();\n\nlcd.clear();\n\ncurrentCycle += 1;\n\n}\n\nfanOn();\n\nlcd.clear();\n\nlcd.setCursor(2,0);\n\nlcd.print(\"FRIEDSAM PCR\");\n\nlcd.setCursor(0,1);\n\nlcd.print(\"PHASE: COMPLETE\");\n\n}\n\nvoid setup() {\n\n// Configure I/O\n\npinMode(13, OUTPUT);\n\nlcd.begin (16,2);\n\nlcd.setBacklightPin(3,POSITIVE);\n\nlcd.setBacklight(HIGH);\n\nSerial.begin(9600);\n\npinMode(2, INPUT);\n\ndigitalWrite(2, HIGH);\n\n// Get input and run machine\n\ngetInput();\n\nPCR();\n\n}\n\nvoid loop() {\n\n}" ]
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https://pure.au.dk/portal/en/publications/a-linear-time-algorithm-for-the-k-maximal-sums-problem(43737830-9d8e-11dc-bee9-02004c4f4f50).html
[ "", null, "## A Linear Time Algorithm for the k Maximal Sums Problem\n\nResearch output: Contribution to book/anthology/report/proceedingArticle in proceedingsResearchpeer-review\n\n• Department of Computer Science\nFinding the sub-vector with the largest sum in a sequence of n numbers is known as the maximum sum problem. Finding the k sub-vectors with the largest sums is a natural extension of this, and is known as the k maximal sums problem. In this paper we design an optimal O(n + k) time algorithm for the k maximal sums problem. We use this algorithm to obtain algorithms solving the two-dimensional k maximal sums problem in O(m 2·n + k) time, where the input is an m ×n matrix with m ≤ n. We generalize this algorithm to solve the d-dimensional problem in O(n 2d − 1 + k) time. The space usage of all the algorithms can be reduced to O(n d − 1 + k). This leads to the first algorithm for the k maximal sums problem in one dimension using O(n + k) time and O(k) space.\nOriginal language English Mathematical Foundations of Computer Science 2007 : 32nd International Symposium, MFCS 2007 Ceský Krumlov, Czech Republic, August 26-31, 2007 Proceedings Ludek Kucera, Antonin Kucera 12 Springer 2007 442-453 978-3-540-74455-9 https://doi.org/10.1007/978-3-540-74456-6_40 Published - 2007 32nd International Symposium on Mathematical Foundations of Computer Science - Cesky Krumlov, Czech RepublicDuration: 26 Aug 2007 → 31 Aug 2007Conference number: 32\n\n### Conference\n\nConference 32nd International Symposium on Mathematical Foundations of Computer Science 32 Czech Republic Cesky Krumlov 26/08/2007 → 31/08/2007\nSeries Lecture Notes in Computer Science 4708 0302-9743\n\n### Research areas\n\n• maximum sum problem\n\nCitationformats" ]
[ null, "https://cdn.au.dk/2016/assets/img/au_segl.svg", null ]
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http://npvw.xhrh.pw/anova-lmer.html
[ "In a repeated-measures design, each participant provides data at multiple time points. Random and mixed e ects ANOVA STAT 526 Professor Olga Vitek January 27, 2011 Reading: KNNL Ch. stats = anova(lme) returns the dataset array stats that includes the results of the F-tests for each fixed-effects term in the linear mixed-effects model lme. Here is a solution for an Anova table using the command capture. The following is an abbreviated example of a nested anova using the lmer function in the lme4 package. A very basic tutorial for performing linear mixed effects analyses (Tutorial 2) Bodo Winter1 University of California, Merced, Cognitive and Information Sciences Last updated: 01/19/2013; 08/13/2013 This tutorial serves as a quick boot camp to jump-start your own analyses with linear mixed effects models. Generalized Linear Mixed Models (illustrated with R on Bresnan et al. Another crucial advantage of mixed logit models over ANOVA for CDA is their greater power. One of the frequent questions by users of the mixed model function lmer of the lme4 package has been: How can I get p values for the F and t tests for objects returned by lmer? The lmerTest package extends the 'lmerMod' class of the lme4 package, by overloading the anova and summary functions by providing p values for tests for fixed effects. Repeated measures analysis with R Summary for experienced R users The lmer function from the lme4 package has a syntax like lm. ##### # # # STAT 599 Spring 2013 # # # # Example R code # # # # Chapter 8 # # # ##### ### Installing the add-on packages needed for this course: # If you haven't. We illustrate the use of the modular functions in lme4 to fit such a model. The former is the REML log likelihood, the latter the ML likelihood. Also, this uses ML/REML techniques, as above. Even ignoring the cheating and p-value chasing aspect of it, I think that using ANOVA is statistically problematic for the above reason alone. plot(partcount. statistics) submitted 22 days ago by ice_shadow I have a dataset where some biomarkers from Mice are measured at 4 different time points (call it 1/2/3/4) in response to 2 different drugs A and B. 7 Repeated measures ANOVA using the lme4 package. If you are not familiar with three-way interactions in ANOVA, please see our general FAQ on understanding three-way interactions in ANOVA. In contrast, afex focuses on tests of effects. PyData Singapore is a group for users and developers of data analysis tools to share ideas and learn from each other. It is important when discussing the behavior of lmer and other functions in the lme4 package to state the version of the package that you are using. The interpretation of the statistical output of a mixed model requires an. Experimental Designs - Between Subject ANOVA Models. ANOVA table with F-tests and p-values using Satterthwaite's or Kenward-Roger's method for denominator degrees-of-freedom and F-statistic. Working with orthogonal contrasts in R. The lme() and lmer() functions assume that the sampling variances are not exactly known, but again just up to a proportionality constant, namely the residual variance. homogeneity) and equal correlations between any pair of time points [e. Indeed, for a balanced design, the estimates and hypothesis for Factor A will be identical to that produced via nested ANOVA. Many research questions require comparisons of several groups of subjects representing different populations. subj_intercepts_mod <-lmer(Reaction ~ A + (1 | Subject)) A model that allows intercepts to vary across subjects does just that: it does a great job of estimating overall Reaction for each subject, but it is. Homepage for the Language and Cognitive Dynamics Laboratory, headed by Dan Mirman in the Department of Psychology at Drexel University. This article describes how to compute manova in R. We really cannot work out why its > not working!!. ANOVA table and lmer. 1 Fitting Linear Mixed Models with a Varying Intercept We will now work through the same Ultimatum Game example from the regression section and the introduction using the lme4 package. Anova(lm(time ~ topic * sys, data=search, contrasts=list(topic=contr. ##### # # # STAT 599 Spring 2013 # # # # Example R code # # # # Chapter 8 # # # ##### ### Installing the add-on packages needed for this course: # If you haven't. The summary() method uses the REML estimates (the latter is clearly indicated in the output). An interaction term (presence of hiatus:preceding glottalization) was included because it improved the model’s fit (which was assessed by the anova function in R, following Baayen (2008)). The entire random-e ects expression should be enclosed in parentheses. For a simple completely balanced nested ANOVA, it is possible to pool together (calculate their mean) each of the sub-replicates within each nest (=site) and then perform single factor ANOVA on those aggregates. Note: the lmer function in the lme4 package also can be used for the same results. If we look at the different inputs for the LMER function we: have \"popular\", which indicates the dependent variable we want to predict. Compute an ANOVA-like table with tests of random-effect terms in the model. Model selection methods include step, drop1 and anova-like tables for random effects (ranova). nobody knows what is going on ? the \"Why do I recieve NaN's in the ANOVA table when I try to analyze my data using. Calculates type-II or type-III analysis-of-variance tables for model objects produced by lm, glm, multinom (in the nnet package), polr (in the MASS package), coxph (in the survival package), lmer in the lme4 package, lme in the nlme package, and for any model with a linear predictor and asymptotically normal coefficients that responds to. Because the multi-way ANOVA model is over-parameterised, it is necessary to choose a contrasts setting that sums to zero, otherwise the ANOVA analysis will give incorrect results with respect to the expected hypothesis. ANOVA/LMER vs paired t tests I have a dataset where some biomarkers from Mice are measured at 4 different time points (call it 1/2/3/4) in response to 2 different drugs A and B What is the appropriate analysis tool for this dataset?. These expressions are used to calculate the ANOVA table entries for the (fixed effects) two-way ANOVA. search(\"linear models\") A window will pop up that lists commands available and the packages that include them. But unlike an ANOVA a LMM does not have to be averaged over repetitions. This is Part 2 of a two part lesson. aov() uses ordinary least squares as the methodology for calculating the ANOVA table. lmer doesn't currently express uncertainty in the variance parameters In R2. I wrote several functions that handled it. example stats = anova( lme , Name,Value ) also returns the dataset array stats with additional options specified by one or more Name,Value pair arguments. 's datives data) Christopher Manning 23 November 2007 In this handout, I present the logistic model with fixed and random effects, a form of Generalized Linear. > Subject: Re: [R] anova statistics in lmer > > The issue is not unresolved within lmer, but with the > statistical model itself. Because this requires fitting as many models as there are terms in the formula, the function may take a while to complete its calculations. The following output results from fitting models using lmer and lm to data arising from a split-plot experiment (#320 from \"Small Data Sets\" by Hand et al. Three ways to get parameter-specific p-values from lmer How to get parameter-specific p -values is one of the most commonly asked questions about multilevel regression. In this design only one factor, C, is crossed with subjects (is a within-subjects factor), while the other two factors, A and B, are between-subjects factors. Lmer (formula, data, family='gaussian') [source] ¶ Model class to hold data outputted from fitting lmer in R and converting to Python object. 3) why the anova summary don't say if differences in classes are significance (or not significance)? 4) I'd like to perform a post-hoc test with the package \"multicomp\" but the lmer function give me a lmer object (and this kind of object is not read by the \"multicomp\" package). lme4 Luke Chang Last Revised July 16, 2010 1 Using lme4 1. Supplement Material Description (For publication) RGxE: An R Program for Genotype x Environment Interaction Analysis Description The supplemental material provides RGxE program, instructions for user enetered field needed in RGxE program, independent module of ANOVA model case 2 to 5 (Table 1), interpretation of univariate. Statistics 203: Introduction to Regression and Analysis of Variance Fixed vs. A good online presentation on ANOVA in R can be found in ANOVA section of the Personality Project. The issue is that in a major recent paper the authors did an ANOVA after they fail to get statistical significance with lmer. If > 1 verbose output is generated during the individual penalized iteratively reweighted least squares (PIRLS) steps. In this post, I want to take a quick look at how you would actually run a mixed-effects model, using the lmer() function furnished by the lme4 package, written by Doug Bates (Bates, 2010 - appears to a preprint of his presumed new book, see also Pinheiro & Bates, 2000). Also the difference between repeated measures ANOVA and ANOVA. R lmer ONE WAY ANOVA by horacio3miranda3varg. The following is an abbreviated example of a nested anova using the lmer function in the lme4 package. This requires the \"lme4\" package. If > 0 verbose output is generated during the optimization of the parameter estimates. Raccoon is Quantide’s third web book after “ Rabbit – Introduction to R ” and “ Ramarro – R for Developers “. It is also intented to prepare the reader to a more complicated model. This makes a comparison between the size of the differences between groups, as measured by a contrast and the accuracy with which that contrast can be measured by a given study or experiment. Statistics > ANOVA models > Repeated Measures. sum, sys=contr. Analysis of variance is merely regression when the predictive variables are qualitative -- more precisely, it refers to the tests one performs in that context. We really cannot work out why its > not working!!. As a result, this approach allows researchers to describe, specify, and interpret a wide range of effects in an LMER more easily. And, for future reference, when the experts ask you for a data example to work on, they do not mean a copy of your printout, although that may help. The e ects of Grand Mean Centering In the case of grand mean centering, we subtract the value of the independent variable for each \\i\" student from their grand. Here we'll introduce anova() and TukeyHSD() which help us understand our linear model in ways that complement the output from summary() ‹ 12. The stan_lmer approach just calls stan_glm but specifies a normal prior with mean zero for the deviations from $$\\alpha$$ across groups. However, I. Specifying a single object gives a sequential analysis of variance table for that fit. 485) for Variety is the same for aov, lme and lmer, but lmer's mean square for variety is 1. Need to load the library lme4. Notice that this model contains an additional term, (1|id), which specifies a random effect for each subject. 485 times the subplot residual mean square. Models should be fitted with lmer from the lmerTest-package. The lme4 package is unique in that it allows for correlated random variance structures and also allows. It is intended to be very basic. example stats = anova( lme , Name,Value ) also returns the dataset array stats with additional options specified by one or more Name,Value pair arguments. Four different methods are available for estimating the variance components: minimum norm quadratic unbiased estimator (MINQUE), analysis of variance (ANOVA), maximum likelihood (ML), and restricted maximum likelihood (REML). Testing significance. lmer() One of the challenges with our previous analysis is that aov() ran the analysis and considered our block effect as a fixed effect. Repeated measures ANOVA is the equivalent of the one-way ANOVA, but for related, not independent groups, and is the extension of the dependent t-test. Basic Features; Notation for the Mixed Model. ANOVA table and lmer. Because of the balance in the data, the F-test requires no adjustment and the outcome is identical with that presented in the printed textbook. The ANOVA model is then fit using lmer(). 7 Repeated measures ANOVA using the lme4 package. To do this, you should use the lmer function in the lme4 package. For the second part go to Mixed-Models-for-Repeated-Measures2. 4 - Repeated Measures Using Mixed Effects II up 18. Unlike most statistical packages, the default assumes unequal variance and applies the Welsh df modification. Compare Likelihoods of Fitted Objects Description. However, afex involves many functions that support nice printing of the \"mixed\" objects returned from mixed. To begin with, we will use the example I had in class. Statistics Question ANOVA/LMER vs paired t tests (self. Compute for each pair of means, where M i is one mean, M j is the other mean, and n is the number of scores in each group. Simulations show that lmer's quasi-likelihood. • [gn]lmer now produces objects of class merMod rather than class mer as before •the new version uses a combination of S3 and reference classes (see ReferenceClasses, merPredD-class, and lmResp-class) as well as S4 classes; partly for this reason it is more interoperable with nlme. To illustrate, the figure below shows the output after loading the lmerTest package. VCs (in lme the corresponding standard deviations, i. 485) for Variety is the same for aov, lme and lmer, but lmer's mean square for variety is 1. That is, the reductions in the residual sum of squares as each term of the formula is added in turn are given in as the rows of a table, plus the residual sum of squares. If you wanted to see if Year is important for predicting Crime in Maryland, we can build a null model with only County as a random-effect and a year model that includes Year. To enter these data into SPSS we use the same procedure as the repeated measures ANOVA that we came across last week, except that we also need a variable (column) that codes whether the helper was an elf or a reindeer. (Degrees of freedom for the t -test is N-k-1 where k equals the number of predictor variables. So, let’s dive into the intersection of these three. sum','contr. • The model formula consists of two expressions separated by the ∼ symbol. √VC) are obtained by applying the function summary. The F-ratio (1. Mar 11 th, 2013. One of the frequent questions by users of the mixed model function lmer of the lme4 package has been: How can I get p values for the F and t tests for objects returned by lmer? The lmerTest package extends the 'lmerMod' class of the lme4 package, by overloading the anova and summary functions by providing p values for tests for fixed effects. In this post, I want to take a quick look at how you would actually run a mixed-effects model, using the lmer() function furnished by the lme4 package, written by Doug Bates (Bates, 2010 - appears to a preprint of his presumed new book, see also Pinheiro & Bates, 2000). The interpretation of the statistical output of a mixed model requires an. a \"~\", that we use to indicate that we now give the other variables of interest. As this post shows, it can detect multivariate patterns in the DVs that ANOVA is simply unable to detect at all. Extrusion and Wear ex8_3_15 has data on the relationship between extrusion pressure (x, in KPa) and wear (y, in mg). anova (reduced. lmer() One of the challenges with our previous analysis is that aov() ran the analysis and considered our block effect as a fixed effect. Simulations show that lmer's quasi-likelihood. I am trying to perform a mixed-model analysis using the lmer() function. ANOVA/LMER vs paired t tests I have a dataset where some biomarkers from Mice are measured at 4 different time points (call it 1/2/3/4) in response to 2 different drugs A and B What is the appropriate analysis tool for this dataset?. * glance puts model summary statistics into a data frame. The lme() and lmer() functions assume that the sampling variances are not exactly known, but again just up to a proportionality constant, namely the residual variance. start with the full model and then do stepwise removal. As a result, this approach allows researchers to describe, specify, and interpret a wide range of effects in an LMER more easily. Posts about lmer() written by robayedavies. First, you will run an anova() on it to see if group explains a significant amount of variability. com What actually the “P” value tells us in ANOVA table. The logic and computational details of the two-way ANOVA for independent samples are described in Chapter 16 of Concepts and Applications. Notice above: Two-point panels such as Panel 4 and Panel 11 have lines not going exactly through the two points. For linear mixed models with little correlation among predictors, a Wald test using the approach of Kenward and Rogers (1997) will be quite similar to LRT test results. Four different methods are available for estimating the variance components: minimum norm quadratic unbiased estimator (MINQUE), analysis of variance (ANOVA), maximum likelihood (ML), and restricted maximum likelihood (REML). Si nous ne comparons que deux moyennes, l'ANOVA nous donnera les mêmes résultats qu'un test t pour des échantillons indépendants (pour comparer deux groupes différents d'observations), ou qu'un test t pour des échantillons appariés (pour comparer. Note anova() for balanced designs. Contrast Coding in R: An Exploration of a Dataset Rachel Baker Phonatics, Sept. In other software packages like SAS, Type III tests of fixed effects are presented with the regression output. I know that the variance of counts can often be stabilized by square roots, so I'll try. lmer : For models with random effects. The former is the REML log likelihood, the latter the ML likelihood. a random e ect is a linear model term conditional on the level of the grouping factor. rand is an alias for ranova. Beautiful Piano Music 24/7: Study Music, Relaxing Music, Sleep Music, Meditation Music Soothing Relaxation 2,324 watching Live now. The library lmerTest has functions lsmeans for testing the treatment effects,. aov() uses ordinary least squares as the methodology for calculating the ANOVA table. This function is equivalent to ‘lme(fixed=formula,random=~1|random)’, except that the block variance component is not constrained to be non-negative, but is faster and more accurate for small to moderate size data sets. ® Levels of repeated measures variables go in different columns of the SPSS data editor. If > 0 verbose output is generated during the optimization of the parameter estimates. xlsx dataset with a mixed effects model. mod) Book recommendations. The lmer package can be used for modeling, and the general syntax is as follows: ` modelname <- lmer (dv ~ 1 + IV +(randomeffects), data = data. # independent 2-group t-test. Whereas the factorial ANOVAs can have one or more independent variables, the one-way ANOVA always has only one dependent variable. To do this, you should use the lmer function in the lme4 package. This makes a comparison between the size of the differences between groups, as measured by a contrast and the accuracy with which that contrast can be measured by a given study or experiment. The last argument is optional. When only one fitted model object is present, a data frame with the numerator degrees of freedom, denominator degrees of freedom, F-values, and P-values for Wald tests for the terms in the model (when Terms and L are NULL), a combination of model terms (when Terms in not NULL), or linear combinations of the model coefficients (when L is not NULL). It is a generalization of two sample t-test. adjust=TRUE) - bootstrap - nonparametric method using ranks (Kruskal-Wallis) kruskal. singular vs. This page is intended to simply show a number of different programs, varying in the number and type of variables. • [gn]lmer now produces objects of class merMod rather than class mer as before •the new version uses a combination of S3 and reference classes (see ReferenceClasses, merPredD-class, and lmResp-class) as well as S4 classes; partly for this reason it is more interoperable with nlme. Roughly: restrict the data to n −p modified observations,. The lme4 package is unique in that it allows for correlated random variance structures and also allows. Experimental Designs - Between Subject ANOVA Models. The F-ratio (1. 9-0 VarCorr(mcmcsamp(lmerModel, 10), \"varcov\") works (OK, with >10 iterations). For lmer this can be a numeric vector or a list with one component named \"theta\". As for the choice between RM anova and mixed regression, I have a strong bias in favor of mixed regression because it is tolerant of missing data (though apparently you don't have this problem, as both models ran with the same N), and because it dispenses with stringent assumptions such as compound symmetry (sphericity), and therefore does not. The last argument is optional. To compare the fits of two models, you can use the anova() function with the regression objects as two separate arguments. Assumptions. The SSCC does not recommend the use of Wald tests for generalized models. Home › forums › Mixed Models › Sum coding for ANOVA style results with unbalanced lmer data Tagged: lmer anova sum coding treatment coding This topic contains 1 reply, has 2 voices, and was last updated by henrik 1 year, 9 months ago. ANOVA (CRD) · General format of ANOVA in R · Testing the assumption of homogeneity of variances using Levene's Test · One-way ANOVA of nested design · Obtaining and interpreting Components of Variance Linear Models in R The primary R function for the analysis of variance of a fixed-effects model is the linear model (lm()) function. You are interested in seeing if tutorial performance is related to final grade. Because the multi-way ANOVA model is over-parameterised, it is necessary to choose a contrasts setting that sums to zero, otherwise the ANOVA analysis will give incorrect results with respect to the expected hypothesis. Do we still > need > to worry about the interaction as a whole, and if yes, how would we > evaluate > it? If you want to follow ANOVA logic, do model comparison. So, let's dive into the intersection of these three. Supplement Material Description (For publication) RGxE: An R Program for Genotype x Environment Interaction Analysis Description The supplemental material provides RGxE program, instructions for user enetered field needed in RGxE program, independent module of ANOVA model case 2 to 5 (Table 1), interpretation of univariate. 3 - Regression Assumptions in ANOVA ›. 1 Fitting Linear Mixed Models with a Varying Intercept We will now work through the same Ultimatum Game example from the regression section and the introduction using the lme4 package. The 95% prediction interval of the eruption duration for the waiting time of 80 minutes is between 3. For a simple completely balanced nested ANOVA, it is possible to pool together (calculate their mean) each of the sub-replicates within each nest (=site) and then perform single factor ANOVA on those aggregates. plot command is going to make four plots, one for each explicit random effect and two for residuals. interceptonlymodel<-lmer(popular~1 + (1|class), data=popular2data) #to run the model. The default in lmer is to fit models using the REML (REstricted Maximum Likelihood) criterion. 6 - Using anova() to Compare Models ›. adjust=TRUE) - bootstrap - nonparametric method using ranks (Kruskal-Wallis) kruskal. On Oct 8, 2012, at 1:57 AM PDT, Holger Mitterer wrote: > Dear Fotis, > > All the points aside that Florian alreadly addressed, part of your message > reflects a typical problem in interpreting the output of an lmer > in comparison with the output of an ANOVA. 2-0 Date 2012-01-09 Author Alexandra Kuznetsova, Per Bruun Brockhoff, Rune Haubo Bojesen Christensen Maintainer Alexandra Kuznetsova Depends Matrix, stats. Many designs involve the assignment of participants into one of several groups (often denoted as treatments) where one is interested in differences between those treatments. 9788 for the mixed model vs 227. Random effects in models for paired and repeated measures As an example, if we are measuring the left hand and right of several individuals, the measurements are paired within each individual. library (lmerTest) anova (lmer. If you are not familiar with three-way interactions in ANOVA, please see our general FAQ on understanding three-way interactions in ANOVA. Rather, we explain only the proper way to report an F-statistic. MODEL SELECTION: To compare different lmer models it's best to avoid REML when the fixed effects are different between models. The following output results from fitting models using lmer and lm to data arising from a split-plot experiment (#320 from \"Small Data Sets\" by Hand et al. singular vs. A Kenward-Roger method is also available via the pbkrtest package. Posts about lmer() written by robayedavies. Lmer in the above table gives you (some of) the > contrasts, but doesn't evaluate the interaction as a whole. In this case, the random fertility level of each field. The last argument is optional. We can also test the main effect terms although we are not able to exactly reproduce the results in the text because we must frame the test as model comparisons in contrast to the ANOVA table in text. Horses are mainly housed in individual boxes. Nested ANOVA - Replication vs. The LRT is generally preferred over Wald tests of fixed effects in mixed models. Statistics 203: Introduction to Regression and Analysis of Variance Fixed vs. To illustrate this, we can again factor in that constant into the sampling variances and refit the model with rma() :. Kyle Roberts A Brief History of Multilevel Models • Nested ANOVA designs • Problems with the ANCOVA design – “Do schools differ” vs. R lmer ONE WAY ANOVA by horacio3miranda3varg. See the previous example in this chapter for explanation and model-checking. We can also compare the AIC values and note that the model with the lowest AIC value is the one with no fixed effects at all, which fits with our understanding that sex and social. Journal of Clinical Medicine Article The E ect of Tapered Abutments on Marginal Bone Level: A Retrospective Cohort Study Simone Marconcini 1,*, Enrica Giammarinaro 2, Ugo Covani 1, Eitan Mijiritsky 3, Xavier Vela 4. 0954) 0. plot(partcount. 1564 minutes. Each random-effect term is reduced or removed and likelihood ratio tests of model reductions are presented in a form similar to that of drop1. The chapter begins by reviewing paired t-tests and repeated measures ANOVA. Statistics Question ANOVA/LMER vs paired t tests (self. For example, we may conduct an experiment where we give two treatments (A and B) to two groups of mice, and we are interested in the weight and height of. lmer - lmer(mathgain ~ 1. P-value in ANOVA table – iSixSigma Isixsigma. In this tutorial, I’ll cover how to analyze repeated-measures designs using 1) multilevel modeling using the lme package and 2) using Wilcox’s Robust Statistics package (see Wilcox, 2012). lmer : For models with random effects. To begin with, we will use the example I had in class. Repeated Measures and Mixed Models - m-clark. The lmer_out model you build in the previous exercise has been loaded for you. Select two of the levels and run the one-way ANOVA. There are three schools, with two students nested in each school. As for the choice between RM anova and mixed regression, I have a strong bias in favor of mixed regression because it is tolerant of missing data (though apparently you don't have this problem, as both models ran with the same N), and because it dispenses with stringent assumptions such as compound symmetry (sphericity), and therefore does not. The following information is a best approximation of how to test assumptions of mixed and multilevel models as of November 2016. Using the \"Repeated-measures / within-subjects ANOVA in R\", \"repeated measure anova using regression models (LM, LMER)\", and \"How to convert Afex or car ANOVA models to lmer? Observed variables \" questions and Chapter 4 of the lme4 book , I created the following code that uses the CO2 sample data. Analysis of variance using distance matrices — for partitioning distance matrices among sources of variation and fitting linear models (e. And random (a. Lmer in the above table gives you (some of) the > contrasts, but doesn't evaluate the interaction as a whole. This function is equivalent to 'lme(fixed=formula,random=~1|random)', except that the block variance component is not constrained to be non-negative, but is faster and more accurate for small to moderate size data sets. The following is an abbreviated example of a nested anova using the lmer function in the lme4 package. The following output results from fitting models using lmer and lm to data arising from a split-plot experiment (#320 from \"Small Data Sets\" by Hand et al. One of the frequent questions by users of the mixed model function lmer of the lme4 package has been: How can I get pvalues for the F and ttests for objects returned by lmer? The lmerTest package extends the 'lmerMod' class of the lme4 package, by overloading the anova and summary functions by providing pvalues for tests for xed e ects. In this case, the random fertility level of each field. Compute an ANOVA-like table with tests of random-effect terms in the model. • In lmer the model is specified by the formula argument. 's datives data) Christopher Manning 23 November 2007 In this handout, I present the logistic model with fixed and random effects, a form of Generalized Linear. lme4 Luke Chang Last Revised July 16, 2010 1 Using lme4 1. One of the advantages of lmerTest and afex is that all one has to do is load the package in R, and the output of lmer is automatically updated to include the p values. While I could get lmer() to work, I can't seem to get the anova t. In the simplest form you test the mean of one set of numbers against the mean of another set of numbers (one-way ANOVA). anova anova method for lmer model fits produces type I, II, and III anova tables for fixed-effect terms with Satterthwaite and Kenward-Roger methods for denominator degrees of freedom for F-tests. You are interested in seeing if tutorial performance is related to final grade. poly\")) lmod - aov(bright ~ operator, pulp) summary(lmod) coef(lmod) options(op) (0. MODEL SELECTION: To compare different lmer models it's best to avoid REML when the fixed effects are different between models. Package 'lme4' November 10, 2010 Version. Speaker and word were included as random intercepts. The data is given at the bottom of this message. We will use the following simulated dataset for illustration:. Assumptions. Recall that the likelihood function is the function links the model parameters to the data and is found by taking the probability density function and interpreting it as a function of the parameters instead of the a function of the data. Using Mixed-Effects Models for Confirmatory Hypothesis Testing (FAQ) This FAQ is intended for people using linear mixed effects models (LMEMs) as a replacement for the statistical techniques that are more traditionally used for confirmatory hypothesis testing, such as ANOVA or t-tests. Contrast Coding in R: An Exploration of a Dataset Rachel Baker Phonatics, Sept. Nested Designs in R Example 1. In a repeated-measures design, each participant provides data at multiple time points. Two-Way ANOVA Example: Data An evaluation of a new coating applied to 3 different materials was conducted at 2 different laboratories. ANOVA; One-way ANOVA; Two-way ANOVA; Analysis of covariance; One-way repeated-measures ANOVA; Two-way repeated-measures ANOVA; Two-way split-plot ANOVA; Three-way split-plot ANOVA; Mixed effects models; Sum of squares type I, II, and III; General Topics; Assess normality; Assess variance homogeneity. How to predict and graph non-linear varying slopes in lmer or glmer? r,ggplot2,lme4,mixed-models,lmer. You are interested in seeing if tutorial performance is related to final grade. Statistics Question ANOVA/LMER vs paired t tests (self. 's datives data) Christopher Manning 23 November 2007 In this handout, I present the logistic model with fixed and random effects, a form of Generalized Linear. tutorial 1 pdf tutorial 2 pdf dataset for tutorial 2 Please cite as: Winter, B. To do this, you should use the lmer function in the lme4 package. The last argument is optional. integer scalar. Here's the thing many don't realize is that the anytime you use (1|x) in lmer it is basically like there is an as. aov() uses ordinary least squares as the methodology for calculating the ANOVA table. Running a repeated measures analysis of variance in R can be a bit more difficult than running a standard between-subjects anova. creates both treatment (a. If you wanted to see if Year is important for predicting Crime in Maryland, we can build a null model with only County as a random-effect and a year model that includes Year. Extrusion and Wear ex8_3_15 has data on the relationship between extrusion pressure (x, in KPa) and wear (y, in mg). The term Analysis of Variance (ANOVA) refers to a number of different concepts, but here use it to describe experimental designs that are based on one or more discrete-valued variables called factors, where the unique values of each factor are called levels. 's datives data) Christopher Manning 23 November 2007 In this handout, I present the logistic model with fixed and random effects, a form of Generalized Linear. Interactions and Contrasts. The key issue is that the degrees of freedom are not trivial to compute for multilevel regression. Type library(lme4) to ensure it is active. This is Part 2 of a two part lesson. Non-nested (crossed) Random Effects in R June 13, 2015 Technical mixed-effects , nonlinear , R , statistics BioStatMatt The R script below illustrates the nested versus non-nested (crossed) random effects functionality in the R packages lme4 and nlme. However, we can use contrast and ANOVA-type commands to extract these effects. singular vs. Statistics Question ANOVA/LMER vs paired t tests (self. The factorial ANOVA is closely related to both the one-way ANOVA (which we already discussed) and the MANOVA (Multivariate Analysis of Variance). Each laboratory tested 3 samples from each of the treated materials. I wrote several functions that handled it. We really cannot work out why its > not working!!. Mixed Models Analysis of a psycholinguistic experiment Ruggero Montalto Seminar in Statistics and Methodology 17/05/2011. The library lmerTest has functions lsmeans for testing the treatment effects,. integer scalar. Nested ANOVA - Replication vs. In the situation where there multiple response variables you can test them simultaneously using a multivariate analysis of variance (MANOVA). Mar 11 th, 2013. lmer) And now we see a problem. anova anova method for lmer model fits produces type I, II, and III anova tables for fixed-effect terms with Satterthwaite and Kenward-Roger methods for denominator degrees of freedom for F-tests. Once you´ve done an Analysis of Variance (ANOVA), you may reach a point where you want to know: What levels of the factor of interest were significantly different from one another?. This article describes how to compute manova in R. A good online presentation on ANOVA in R can be found in ANOVA section of the Personality Project. Nested Designs in R Example 1. ANOVA assumes (1) errors are normally distributed, (2) variances are homogeneous, and (3) observations are independent of each other. You are interested in seeing if tutorial performance is related to final grade. Each random-effect term is reduced or removed and likelihood ratio tests of model reductions are presented in a form similar to that of drop1. Formula lmer() A random-e ects term in lmer() is speci ed by a linear model term and a grouping factor separated by ’j’; i. How to Calculate the Least Significant Difference (LSD): Overview. In the previous post, we ran through an example of a mixed-effects analysis completed using the lmer() function from the lme4 package (Bates, 2005; Bates, Maelchler & Bolker, 2013). com What actually the “P” value tells us in ANOVA table. lme4) via Satterthwaite's degrees of freedom method. The last argument is optional. 1 Fitting Linear Mixed Models with a Varying Intercept We will now work through the same Ultimatum Game example from the regression section and the introduction using the lme4 package. The goal is to test if the group means are different (at some significance level). 36-463/663: Hierarchical Linear Models Lmer model selection and residuals Brian Junker 132E Baker Hall [email protected] library (lmerTest) anova (lmer." ]
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http://rohitapte.com/2017/04/24/
[ "## Convolutions\n\nIn the previous post we discussed using Convolutional Neural Networks for Image Recognition. In order to better understand what the algorithms are doing we need to explore convolutions in more detail.\n\n#### Definition\n\nA convolution of f and g, denoted f*g, is the integral of the product of 2 functions after one is reversed and shifted. Mathematically", null, "One way of thinking about convolutions is an integral that expresses the amount of overlap of g as it is shifted over f. It “blends” one function with another. The below image courtesy of Wikipedia demonstrates this.", null, "Some more intuitive explanations of convolutions (and more applicable to machine learning):\n\nThink about a time series. Say we look at the fed funds rate over time.", null, "One way to smooth data is to convolve it against a smaller list. For example, to calculate the weekly moving average we convolve it against [1,1,1,1,1]. For a monthly moving average we would convolve it with a list of 25 ones (assuming 25 business days in a month).\n\nAs another example, consider rolling 2 six sided dice. The probability distribution looks as follows.", null, "This can be represented as a convolution… For example to get a 4 we have", null, "So what does the “Convolution” in Convolutional Neural Networks (aka Deep Learning) do to images? Convolutions (called Kernels in image processing) work as feature detectors. Lets look at a few convolutions on 2 images below.\n\n Convolution Matrix Image 1 Image 2 Original Image", null, "", null, "Average", null, "", null, "", null, "Sharpen", null, "", null, "", null, "Edge Detection 1", null, "", null, "", null, "Edge Detection 2", null, "", null, "", null, "Edge Detection 3", null, "", null, "", null, "Edge Detection 4", null, "", null, "", null, "Box Blur", null, "", null, "", null, "Gaussian Blur", null, "", null, "", null, "Gradient Detection 1", null, "", null, "", null, "Gradient Detection 2", null, "", null, "", null, "The amazing part about Deep Learning is we don’t have to teach the algorithm the convolutions to use. It learns them as part of the hyperparameter tuning!" ]
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http://oak.go.kr/central/journallist/journaldetail.do?article_seq=13110
[ "•", null, "• #### ABSTRACT\n\nThis paper presents a zero-IF CMOS RF receiver, which supports three channel bandwidths of 5/10/40MHz for LTE-Advanced systems. The receiver operates at IMT-band of 2,500 to 2,690MHz. The simulated noise figure of the overall receiver is 1.6 dB at 7MHz (7.5 dB at 7.5 kHz). The receiver is composed of two parts: an RF front-end and a baseband circuit. In the RF front-end, a RF input signal is amplified by a low noise amplifier and Gm with configurable gain steps (41/35/29/23 dB) with optimized noise and linearity performances for a wide dynamic range. The proposed baseband circuit provides a -1 dB cutoff frequency of up to 40MHz using a proposed wideband OP-amp, which has a phase margin of 77° and an unit-gain bandwidth of 2.04 GHz. The proposed zero-IF CMOS RF receiver has been implemented in 0.13-μm CMOS technology and consumes 116 (for high gain mode)/106 (for low gain mode) mA from a 1.2 V supply voltage. The measurement of a fabricated chip for a 10-MHz 3G LTE input signal with 16-QAM shows more than 8.3 dB of minimum signal-to-noise ratio, while receiving the input channel power from -88 to -12 dBm.\n\n• #### KEYWORD\n\nCMOS , LTE , LTE Advanced , RF Receiver , Passive Mixer , Wideband OP-Amp.\n\n• ### Ⅰ. INTRODUCTION\n\nCurrently, smartphone use continues to increase and is now an essential part of people’s daily lives. Mobile applications that utilize long-term evolution (LTE) of 3rd generation partnership project (3GPP) are now popular because of highly responsive mobile voice and data services. However, the development of new mobile communication systems such as LTE-Advanced is required to satisfy demands for high-speed multimedia data communications such as real-time video streaming. The LTE-Advanced system offers a peak data-rate of 1 Gbps downlink, which is 10 times higher than 100 Mbps of the 3G LTE systems . Accordingly, many RF receivers for LTE-Advanced systems have been reported in [2-4]. A high data-rate can be achieved by increasing the modulation level and expanding the signal bandwidth as effective techniques .", null, "This paper presents a zero-IF CMOS RF receiver for LTE-Advanced system, which can support up to a 40MHz channel bandwidth for high data-rate applications. The proposed RF receiver operates at an IMT-band of 2,500 to 2,690MHz and provides a gain from 25 dB (low gain mode) to 99 dB (high gain mode). The simulated noise figure of the receiver is 1.6 dB in channel bandwidth from 5 to 40 MHz and 7.5 dB at 7.5MHz. Since the sub-carrier channel bandwidth is 15 kHz and a null-tone has been allocated in the LTE-Advanced system, the baseband signal power is located from 7.5 kHz to 10/20/40MHz.\n\nFig. 1 shows a block diagram of the proposed zero-IF RF receiver, which consists of two parts: the RF front-end and the baseband circuit. The RF front-end is composed of a narrow-band low noise amplifier (LNA), a Gm (transconductor), a current-driven passive mixer, and transimpedance amplifiers (TIAs). The baseband circuit is composed of several variable gain amplifiers (VGAs), low-pass filters (LPFs), and DC-offset cancellation (DCOC) circuits. Here, a local oscillator (LO) signal for the passive mixer is externally provided from a signal generator.\n\n### Ⅱ. RF FRONT-END DESIGN\n\nAs shown in Fig. 2, the proposed LNA is a differential common-source amplifier with an inductive source degeneration to achieve a low noise characteristic and a high voltage gain versus power consumption. The LNA has an RLC resonant load centered at 2.6 GHz and provides a voltage gain of 29/35/41 dB by controlling the load resistors R1 and R2.\n\nIn Fig. 2, the current-driven passive mixer architecture , which is composed of the Gm, the quadrature passive mixer core, and the quadrature TIAs, is adopted to overcome a trade-off between signal-to-noise ratio (SNR) and linearity. The Gm has adopted a differential common-source topology and uses inductive loads (L3 and L4) to eliminate input parasitic capacitance of the passive mixer . This inductive load provides high impedance to the following TIA through the passive mixer’s on-resistor Ron so that 1/f noise from the TIAs can be mitigated.", null, "In the passive mixer, a trade-off between linearity and noise figure occurs directly, depending on the LO bias levels. In this work, the on-overlap LO biasing level has been chosen for the proposed passive mixer considering noise figure, conversion gain, and linearity.\n\nThe proposed TIA is a common-gate amplifier with low input impedance for the current-to-voltage conversion. It has the 1st-order RC load for filtering unwanted spurious noise from the mixing operation and LO leakage. In the TIA, long-channel NMOS devices (L = 5 μm) for M11-M18 have been used to suppress 1/f noise.\n\nIn order to ensure a wide dynamic range of the overall RF receiver, the gain of the RF front-end should be in the range of 41 to 23 dB with a step of 6 dB for the incoming input signal. The gain control from 41 to 29 dB has been achieved in the LNA load by adjusting the value of the resistors (R1 and R2). However, even though the LNA has a gain of 23 dB, the following Gm is saturated by the LNA output voltage swing. Thus, a minimum gain mode switch (M5 and M6) is added between the LNA and the Gm . As shown in Fig. 2, in order to achieve minimum voltage gain of 23 dB, the cascode transistors (M3 and M4) in the LNA and input transistors (M7 and M8) in the Gm turn off and the switches (M5 and M6) simultaneously turn on. Thus, the LNA’s input stage (M1 and M2) and the Gm’s cascode stage (M9 and M10) are operated as another new cascode amplifier. Using this method, the RF front-end can achieve the minimum gain of 23 dB without severe distortion for the high input signal of -18 dBm.\n\n### Ⅲ. BASE-BAND CIRCUIT DESIGN\n\nFig. 3 shows the proposed analog baseband circuit (only I-path), comprising a VGA1, a channel-selection LPF, a VGA chain (VGA2), and a DCOC circuit. A lower noise figure of the receiver is achieved by locating the LPF between VGA1 and VGA2. The gain of the VGA1 suppresses noise from the LPF. The proposed analog baseband circuit provides a voltage gain from -23 to 79 dB in a 0.25 dB gain step.", null, "", null, "In general, since active RC LPF shows higher linearity than Gm-C LPF, a 5th-order active RC Chebyshev LPF is adopted in this work [9-11]. The LPF provides a -1 dB cutoff frequency of 5MHz, 10MHz, and 40MHz with a frequency compensation circuit. The -1 dB cutoff bandwidth of the channel-selection LPF is given by 1/(RS۰C1-5) and can be changed by varying the capacitance of C1-5. An insertion loss of the LPF is given by K/2 where K is a proportionality constant, which is implemented in input resistance of the LPF. In this work, the K of 2 was chosen to make an insertion loss of 0 dB.\n\nFig. 4 shows the simulated frequency response of the proposed channel-selection LPF, where the cutoff frequencies of 5, 10, and 40MHz are not much changed for corner states of SS (-80℃), TT (27℃), and FF (40℃) mode. In Fig. 4, the peaking at 40MHz channel bandwidth comes from the deficient unit-gain bandwidth (UGBW) of 2.04 GHz in the proposed OP-amp. However, from the overall receiver measurements, the receiver does not show any oscillation problem or performances degradation.\n\nThe proposed VGAs (VGA1 and VGA2), which are composed of a fully differential OP-amp with a negative feedback resistor for high linearity, are designed to achieve -1 dB cutoff frequency of 50MHz for the maximum channel bandwidth of 40MHz .\n\nIn Fig. 3, the VGA1 provides a voltage gain from -12 to 12 dB with a 6 dB step. The VGA2 provides voltage gain from -11 to 67 dB with a 0.25 dB fine gain step to compensate I-Q gain mismatch. To provide the total gain of 67 dB, the VGA2 consists of 7 stages; the 1st, 3rd, and 5th amplifiers have a voltage gain from -12 to 12 dB with a 6 dB step respectively, the 2nd and 7th amplifiers provide a fixed voltage gain of 12 dB, the 4th amplifier provides a voltage gain from 1 to 6 dB with a 1 dB step, and the 6th amplifier provides a voltage gain from 0 to 1 dB with a 0.25 dB step.\n\nA DCOC in a zero-IF receiver is inevitable, since an unexpected DC-offset may saturate the baseband output. The DC-offset problem is solved by building a DCOC loop based on voltage-current negative-feedback, as shown in Fig. 3. The high-pass cutoff frequency of the DCOC circuits is set to less than 1 kHz to ensure active sub-carriers around DC. However, due to this cutoff frequency of 1 kHz, the required capacitances Cf are 2 μF, which cannot be integrated on a chip. Thus, they are externally implemented at the cost of extra pads. The constant cutoff frequency in the DCOC circuit has been achieved by digital control of the value of input resistor RD1 in the DCOC circuit as the variation of voltage gain in the feed-forward path. The post-layout simulation shows that the analog baseband output can be tolerated for up to 700 mV input DC-offset.\n\nFig. 5 shows the frequency response of the baseband circuit with a cutoff frequency of 10MHz. The baseband circuit provides a voltage gain from -23 to 79 dB, and the high pass cutoff frequency of less than 1 kHz. The simulated results of the proposed baseband circuit are summarized in Table 1.\n\nTo achieve the channel bandwidth of up to 40MHz, the LPF and VGAs need a wideband OP-amp. Fig. 6 shows the proposed wideband two-stage OP-amp, which uses a crossconnected PMOS load (M3 to M6) at the first stage . The cross-connected PMOS load provides a very wideband characteristic of the OP-amp by putting the second pole far away from the dominant pole. However, the cross-connected PMOS load generates nonlinear components such as evenorder harmonics. To eliminate this problematic effect, a diode-connected PMOS load (M9 and M10) is added at the second stage. The even-order harmonics from the first stage can be eliminated after combining with another even-order harmonic from the diode-connected PMOS load (M9 and M10) of the second stage. Additionally, for immunity of common-mode signals, a diode-connected NMOS load (M11 and M12) with a high value of the resistor, which has high common-mode rejection ratio, is used at the second stage. To secure an enough phase-margin of the OP-amp, an RC compensation circuit (RZ, CC) is adopted between the first and the second stage .", null, "", null, "", null, "", null, "Fig. 7 shows simulated results of the proposed wideband OP-amp. The proposed OP-amp provides a phase margin 77° and a UGBW of 2.04 GHz, which is about 50 times the maximum channel bandwidth (40MHz). An OP-amp consumes 3.47 mA from a 1.2 V supply.\n\n### Ⅳ. MEASUREMENT RESULTS\n\nThe proposed zero-IF CMOS RF receiver for LTE-Advanced systems has been implemented in 0.13-μm CMOS technology, as shown in Fig. 8. The receiver consumes 116 (high gain mode)/106 (low gain mode) mA from a 1.2 V supply.\n\nFigs. 9-11 show the measured results of the fabricated chip. A 10-MHz 3G LTE signal only is applied to the input of the chip for measurements, even though the receiver supports multi-channels of 5, 10, and 40MHz.\n\nFigs. 9 and 10 show the measured an input 1- dB gain compression point (P1dB) of the proposed RF receiver with the high and low gain modes, respectively. Due to the sufficient linearity for all the signal paths, the proposed RF receiver achieves P1dB of -92 dBm (high gain mode) and -18 dBm (low gain mode) for a fixed output power of 6 dBm for 50 Ω loading. At the high and the low gain mode, a simulated overall gain of the RF receiver is 103/29 dB but the measurements show the 99/25 dB because of unexpected parasitic capacitances in the RF paths.\n\nFig. 11 shows the measured SNR for the 10-MHz 3G LTE input signal with 16-QAM. The proposed RF receiver provides more than 8.3 dB of minimum SNR , while receiving the input channel power from -88 to -12 dBm.", null, "", null, "Table 2 summarizes the measured results and compares them with the state-of-the-art measurements [12,13]. The proposed RF receiver achieves the widest channel bandwidth, the highest gain, and the lowest noise figure.\n\n### Ⅴ. CONCLUSION\n\nThis paper has presented a zero-IF CMOS RF receiver for LTE-Advanced systems, which is implemented in 0.13-μm CMOS technology. The simulated and the measurement results demonstrate that the proposed RF receiver can favorably support the LTE-Advance systems.", null, "", null, "", null, "• [Fig. 1.] Simplified block diagram of the proposed RF receiver.", null, "• [Fig. 2.] Schematic of the proposed RF front-end receiver. LNA=low noise amplifier, Gm=transconductor, TIA=transimpedance amplifier.", null, "• [Fig. 3.] Block diagram of the proposed base-band circuit (I-path). VGA = variable gain amplifier, LPF = low-pass filter, DCOC = DC-offset cancellation circuit.", null, "• [Fig. 4.] Frequency response of the proposed low-pass filter.", null, "• [Fig. 5.] Frequency response of the proposed baseband circuits.", null, "• [Table 1.] Performance summary of the baseband circuit", null, "• [Fig. 6.] Schematic of the proposed operational amplifier.", null, "• [Fig. 7.] Phase and gain curve of the operational amplifier. UGBW = unit-gain bandwidth.", null, "• [Fig. 8.] Chip micrograph. LNA = low noise amplifier, Gm = transconductor, TIA = transimpedance amplifier, LPF = lowpass filter, DCOC = DC-offset cancellation circuit, VGA = variable gain amplifier.", null, "• [Fig. 9.] Measured P1dB at the high gain mode.", null, "• [Fig. 10.] Measured P1dB at the low gain mode.", null, "• [Fig. 11.] Measured SNR of the proposed RF receiver using a 10-MHz LTE signal. SNR = signal-to-noise ratio, LTE = long-term evolution.", null, "• [Table 2.] Performance comparison", null, "" ]
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https://svi.nl/BytesAndBits
[ "# Bits and bytes (Image sizes)\n\nbit (b)\nOne bit is the smallest unit of information. In a binary numerical system it is what you can represent with a one or a zero. (more).\n\nbyte (B)\nNowadays one byte is always 8 bits. Therefore, in a 16 bit image every PiXel intensity is represented by 2 bytes. (more).\n\nThe size of an image in bits (b) can be computed multiplying:\n\n• the total number of PiXels or VoXels in the image by\n• the number of bits per pixel by\n• the total number of channels\n\nThis number divided by 8 expresses the file size in bytes (B).\n\nIf you divide the size in bytes by 2^10> = 1024, you obtain the size in kilo-bytes (kB). If you divide it again by 1024 you obtain mega-bytes (MB).\n\n### Example\n\nA Two Channel, 16 bit, 3D image that is 512 × 512 × 100 large will need\n\n2 × 16 × 512 × 512 × 100 = 838860800 bits\n\nof storage size only for the intensity values, plus some extra space if metadata exists describing the image. This is at least\n\n838860800 bits / 8 = 104857600 bytes\n\nor\n\n104857600 / 1024 = 102400 kB\n\nor\n\n102400 / 1024 = 100 MB" ]
[ null ]
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https://openhome.cc/Gossip/Scala/ShadowOverride.html
[ "``val x = 10{ val x = 20 println(x) // 顯示 20}println(x) // 顯示 10``\n\nScala支援區塊可視範圍,在上例中,{}區塊外宣告了一個x變數,而區塊內也宣告了一個x變數,在區塊中x的變數定義遮蔽了區塊外的x定義。\n\nclass A {\nprotected int x = 10;\n}\n\nclass B extends A {\npublic int x = 20;   // 這邊 x 遮蔽了 A 類別中的 x\n}\n\npublic class Main {\npublic static void main(String[] args) {\nB b = new B();\nA a = b;\nSystem.out.println(b.x);    // 顯示 20\nSystem.out.println(a.x);    // 顯示 10\n}\n}\n\nclass Parent {\nprotected val x = 10\n}\n\nclass Child extends Parent {\nval x = 20\n}\n\nerror: error overriding value x in class Parent of type Int; value x needs `override' modifier\nval x = 20\n^\n\n``class Parent { protected val x = 10}class Child extends Parent { override val x = 20}val c = new Childprintln(c.x) // 顯示為 20``\n\n``class Parent { private val x = 10}class Child extends Parent { val x = 20 // 因為 Parent 的 x 在這邊不可視,所以不用 override}val c = new Childprintln(c.x)``\n\nclass Parent {\nval x = 10\n}\n\nclass Child extends Parent {\noverride protected val x = 20  // error, value x has weaker access privileges\n}\n\n``class Parent { val x = 10}class Child extends Parent { private[this] val x = 20 def getX = x}val c = new Childprintln(c.x) // 顯示 10println(c.getX) // 顯示 20``\n\nclass Parent {\nvar x = 10\n}\n\nclass Child extends Parent {\noverride val x = 10    // error, value x cannot override a mutable variable\n}" ]
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https://www.carvadia.com/how-do-you-identify-influential-observations/
[ "• September 27, 2022\n\n### How Do You Identify Influential Observations?\n\n•", null, "How do you identify influential observations? If the predictions are the same with or without the observation in question, then the observation has no influence on the regression model. If the predictions differ greatly when the observation is not included in the analysis, then the observation is influential.\n\n## What is the difference between an outlier and an influential observation?\n\nAn outlier is a data point that diverges from an overall pattern in a sample. An influential point is any point that has a large effect on the slope of a regression line fitting the data. They are generally extreme values.\n\n## Are there any outliers or influential observations?\n\nAll outliers are influential data points. The correct answer is (E). Data sets with influential points can be linear or nonlinear. For example, when the data set is very large, a single outlier may not have a big effect on the regression equation.\n\n## How do you identify influential data points?\n\nAn influential data point has two key properties: It has properties that are not representative of the other data points. It doesn't follow the general trend, and it's dependent variable value is unexpected given values you would get from predictor variables.\n\n## Why outliers are sometimes called influential observations?\n\nSometimes outliers can be called influential observations since they can significantly tilt a regression line towards them. When an outlier is included in a regression of Y versus a single X, the slope of the line is greatly tilted towards the outlier. This change in slope normally leads to a shift in the y-intercept.\n\n## Related faq for How Do You Identify Influential Observations?\n\n### Which of the following measures are used for identifying influential observations in the data?\n\nIn this section, we learn the following two measures for identifying influential data points: Difference in fits (DFFITS) Cook's distance.\n\n### What makes a point influential?\n\nAn influential point is an outlier that greatly affects the slope of the regression line. The slope is larger when the outlier is present, so this outlier would be considered an influential point.\n\n### What are influential points in acupuncture?\n\nThe Influential Points are eight important points where qi of the respective body tissues is infused into the body surface, namely zang, fu, qi, blood, tendons, vessels, bones and marrow. \"Hui\" means influential in particular.\n\n### How do you find influential points in R?\n\nThere are two common measures for identifying influential data points: difference in fits (DFFITS), and Cook's distance.\n\n### What is an influential case in statistics?\n\nAn influential case is any case that significantly alters the value of a regression coefficient whenever it is deleted from an analysis. If the deletion of particular cases in an analysis alters the parameters of the regression equation significantly, then these cases represent influential cases.\n\n### When one has influential points in their data How should regression and correlation be done?\n\nWhen one has influential points in their​ data, how should regression and correlation be​ done? When one has influential points in their​ data, they should do the regression and correlation with and without these points and comment on the differences.\n\n### What are influence statistics?\n\nInfluence statistics measure the effects of individual data points or groups of data points on a statistical analysis. The effect of individual data points on an analysis can be profound, and so the detection of unusual or aberrant data points is an important part of nearly every analysis.\n\n### What is influential data?\n\nInfluential data points are observations that exert an unusually large effect on the results of regression analysis. Influential data might be classified as outliers, as leverage points, or as both. An outlier is an anomalous response value, whereas a leverage point has atypical values of one or more of the predictors.\n\n### What is an influential observation in a linear regression setting?\n\nIn statistics, an influential observation is an observation for a statistical calculation whose deletion from the dataset would noticeably change the result of the calculation. In particular, in regression analysis an influential observation is one whose deletion has a large effect on the parameter estimates.\n\n### What is an influential point quizlet?\n\nAn influential point is a point that changes the regression by a large amount. The coefficient of determination, or r2, is a measure of how well the regression line summarizes the data.\n\n### How do outliers affect correlation?\n\nInfluence Outliers\n\nIn most practical circumstances an outlier decreases the value of a correlation coefficient and weakens the regression relationship, but it's also possible that in some circumstances an outlier may increase a correlation value and improve regression.\n\n### How do you identify outliers?\n\nDetermining Outliers\n\nMultiplying the interquartile range (IQR) by 1.5 will give us a way to determine whether a certain value is an outlier. If we subtract 1.5 x IQR from the first quartile, any data values that are less than this number are considered outliers.\n\n### How Dffits are used to detect influential observations?\n\nDFFITS Plot\n\nDFFIT - difference in fits, is used to identify influential data points. It quantifies the number of standard deviations that the fitted value changes when the ith data point is omitted. Steps to compute DFFITs: delete observations one at a time.\n\n### How do you read an influence plot?\n\nAn influence plot shows the outlyingness, leverage, and influence of each case. The plot shows the residual on the vertical axis, leverage on the horizontal axis, and the point size is the square root of Cook's D statistic, a measure of the influence of the point.\n\n### What does a high CovRatio mean?\n\nDelete-1 change in covariance ( CovRatio ) identifies the observations that are influential in the regression fit. Values of CovRatio larger than 1 + 3*p/n or smaller than 1 – 3*p/n indicate influential points, where p is the number of regression coefficients, and n is the number of observations.\n\n### Do residual plots identify influential points?\n\nYou can't see influence in the usual residual plot.\n\n### Does an influential point affect correlation?\n\nOutliers and high-leverage points can be influential to different measurements in least-squares regression like the slope, y-intercept, and correlation coefficient (r).\n\n### How do you read Dffits?\n\nThe DFFITS statistic is a scaled measure of the change in the predicted value for the ith observation and is calculated by deleting the ith observation. A large value indicates that the observation is very influential in its neighborhood of the X space. , where n and p are as defined previously.\n\n### What does joy do to Qi?\n\nJoy relaxes and slows the movement of Qi. Symptoms from a Heart or Joy imbalance can result in: Palpitations. Restlessness.\n\n### What are Luo connecting points?\n\nThe Luo (connecting) points are locations at which the qi of the twelve regular meridians converges. All of the fifteen collaterals are the passages through which qi and blood are transported into the zangfu organs and tissues of the body.\n\n### What are front mu points?\n\nFront-Mu points are located at the chest and abdomen where the Qi of Zang-Fu organs is infused. These points are named according to corresponding zang-fu organs. When a Zang-Fu organ is diseased , there is an abnormal sensation (tenderness or a sensitive spot) in the corresponding Back-Shu points.\n\n### What is influence plot in R?\n\nInfluence Index Plots for Multivariate Linear Models. Description. Provides index plots of some diagnostic measures for a multivariate linear model: Cook's distance, a generalized (squared) studentized residual, hat-values (leverages), and Mahalanobis squared dis- tances of the residuals. Usage.\n\n### Are high leverage points always influential?\n\nNot all leverage points are influential, unless they have large residuals. Observations with large values of hii and large residuals are likely to be influential.\n\n### What does Studentized residuals measure?\n\nIn statistics, a studentized residual is the quotient resulting from the division of a residual by an estimate of its standard deviation. It is a form of a Student's t-statistic, with the estimate of error varying between points. This is an important technique in the detection of outliers.\n\n### What is Homoscedasticity in statistics?\n\nHomoskedastic (also spelled \"homoscedastic\") refers to a condition in which the variance of the residual, or error term, in a regression model is constant. That is, the error term does not vary much as the value of the predictor variable changes.\n\n### What are observations in regression?\n\nRegression analysis is the method of using observations (data records) to quantify the relationship between a target variable (a field in the record set), also referred to as a dependent variable, and a set of independent variables, also referred to as a covariate." ]
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https://users.rust-lang.org/t/error-t-might-need-a-bound-for-std-partialeq-in-singly-linked-list/41867
[ "# Error `T` might need a bound for `std::cmp::PartialEq` in singly linked list\n\nWhile doing the Rust track in Exercism, I came accross the singly linked list exercise. Once my compilation passed the tests, I continued to work on the code to add some more functionality and train myself.\nThe error I get while compiling is error[E0369]: binary operation `==` cannot be applied to type `T`\n\nThe code is something like this:\n\n``````#[derive(Default)]\nstruct Node<T>{\ndata: T,\nnext: Option<Box<Node<T>>>,\n}\n\nimpl<T: PartialEq> PartialEq for Node<T> {\nfn eq(&self, other: &Self) -> bool {\nself.data == other.data\n}\n}\n\n#[derive(Default)]\nlength: usize,\n}\n``````\n\nSome implementation and then the problem\n\n``````pub fn find(&self, value: T) -> bool {\n\nwhile let Some(node) = head {\nmatch node.next {\nNone => return false,\nSome(a) => {if a.data == value { return true }},\n}\n}\nfalse\n}\n``````\n\nThe error happens when comparing a.data with value.\nI thought that the PartialEq implementation for Node should take care of that.\nIf possible, I would like some assistance in that matter.\n\nThanks\n\nCould you share the full code which reproduces an error? I wasn't able to get it in your current variant - playground.\n\n``````use std::iter::FromIterator;\n\n#[derive(Default)]\nstruct Node<T>{\ndata: T,\nnext: Option<Box<Node<T>>>,\n}\n\nimpl<T: PartialEq> PartialEq for Node<T> {\nfn eq(&self, other: &Self) -> bool {\nself.data == other.data\n}\n}\n\n#[derive(Default)]\nlength: usize,\n}\n\npub fn new() -> Self {\nlength: 0\n}\n}\n\npub fn len(&self) -> usize {\nself.length\n}\n\npub fn push(&mut self, _element: T) {\nlet node = Box::new(Node {\ndata: _element,\n});\nself.length += 1;\n}\n\npub fn pop(&mut self) -> Option<T> {\nNone => None,\nSome(node) => {\nself.length -= 1;\nSome(node.data)\n}\n}\n}\n\npub fn peek(&self) -> Option<&T> {\nNone => None,\nSome(node) => Some(&node.data),\n}\n}\n\npub fn find(&self, value: T) -> bool {\nself.head.iter().find(| node | node.data == value).is_some()\n}\n\npub fn rev(mut self) -> SimpleLinkedList<T> {\nlet mut previous = None;\n\nwhile let Some(mut node) = current_node {\nlet next = node.next;\nnode.next = previous;\nprevious = Some(node);\ncurrent_node = next;\n}\nself\n}\n\npub fn is_empty(&self) -> bool {\nself.len() == 0\n}\n}\n\nfn from_iter<I: IntoIterator<Item = T>>(_iter: I) -> Self {\nfor i in _iter {\nc.push(i);\n}\nc\n}\n}\n\n// In general, it would be preferable to implement IntoIterator for SimpleLinkedList<T>\n// instead of implementing an explicit conversion to a vector. This is because, together,\n// FromIterator and IntoIterator enable conversion between arbitrary collections.\n// Given that implementation, converting to a vector is trivial:\n//\n// let vec: Vec<_> = simple_linked_list.into_iter().collect();\n//\n// The reason this exercise's API includes an explicit conversion to Vec<T> instead\n// of IntoIterator is that implementing that interface is fairly complicated, and\n// demands more of the student than we expect at this point in the track.\n\nfn into(mut self) -> Vec<T> {\nlet mut vec = vec![];\n\nwhile let Some(element) = self.pop() {\nvec.push(element);\n}\nvec.reverse();\nvec\n}\n}``````\n\nSorry, wrong version. This is the version that uses the iterator\n\nJust use the find method from the code I sent before. The rest is identical\n\n``````error[E0599]: no method named `borrow` found for enum `std::option::Option<std::boxed::Box<Node<T>>>` in the current scope\n--> src/lib.rs:30:34\n|\n|\n= help: items from traits can only be used if the trait is in scope\nhelp: the following trait is implemented but not in scope; perhaps add a `use` for it:\n|\n1 | use std::borrow::Borrow;\n|\n``````\n\nAre you sure that the structure is correct?\n\n``````use std::borrow::Borrow;\n``````\n\nat the top of your module, and changing\n\n``````match node.next {\n``````\n\nwith\n\n``````match &node.next {\n``````\n\nSince you can't move out of node since it's under a reference.\n\nThanks, but those are only there due to the change in the find function from the two versions I sent. That's my fault.\nBut still, the error I mentioned in the post about comparing T values is still there.\nPlayground\n\nOh, add a bound to `T` on the `find` method:\n\n``````pub fn find(&self, value: T) -> bool\nwhere T: PartialEq<T> { /* */ }\n``````\n\nOr, make another impl block:\n\n``````impl<T: PartialEq<T>> SimpleLinkedList<T> {\npub fn find(&self, value: T) -> bool {\n/* */\n}\n}\n``````\n2 Likes\n\nHere you didn't specify that you're only implementing these methods if `T: PartialEq`, so you can't rely on that in the body of `find()`.\n\nThank you very much.\n\nThis topic was automatically closed 90 days after the last reply. New replies are no longer allowed." ]
[ null ]
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https://dsp.stackexchange.com/questions/22945/root-locus-for-a-system
[ "# Root Locus for a system\n\nI know this subject tends more to control theory but I am certain its part of the global knowledge basis for engineers, thus I believe I can find the answer here. I'm trying to draw Root Locus for $K<0$, but can't understand how the system behaves.\n\nI have this open loop system:\n\n$$\\frac{20(1+s)^2}{(1+\\frac{s}{10})(1+\\frac{s}{2})}$$\n\nI know it has no asymptotes, but yet by one of the drawing rules for $k<0$, it tends to $\\pm \\infty$ in the real axis. How is it possible?\n\n• Is $s10$ a typo, or is that \"s times 10\"? Apr 23 '15 at 15:56\n• it is an s/10 sir. Apr 23 '15 at 15:58\n• @minimalrisk do you know how to get the closed loop transfer function and how to get its poles? Apr 23 '15 at 17:07\n• yes, its $$1+K(s)*G(s)$$ and the poles are -2, -10, and the two zeroes are in -1 Apr 23 '15 at 17:17\n\nI will denote the given system as,\n\n$$G(s) = \\frac{20(1+s)^2}{(1+\\frac{s}{2})(1+\\frac{s}{10})}$$\n\nThe input or reference signal to the closed loop will be denoted by $R(s)$ and the output by $Y(s)$. The controller will initially be denoted by $H(s)$, while in this case it is equal to $K$. The block diagram of the closed loop system can then be drawn as,", null, "With its transfer function from input to output equal to,\n\n$$\\frac{Y(s)}{R(s)} = \\frac{G(s)}{1 + H(s) G(s)}.$$\n\nFor root locus analysis you want to find the poles of this transfer function as function of $H(s)$. The poles can be found by solving when the denominator is equal to zero. However the denominator (and numerator) are polynomials of $s$, so can't be fractions themselves. In order to ensure this I will slit $G(s)$ up in to two parts, its numerator, $G_n(s)$, and denominator, $G_d(s)$. The same can be done for $H(s)$. The resulting transfer function can then be written as,\n\n$$\\frac{Y(s)}{R(s)} = \\frac{\\frac{G_n(s)}{G_d(s)}}{1 + \\frac{H_n(s)}{H_d(s)} \\frac{G_n(s)}{G_d(s)}} = \\frac{H_d(s) G_n(s)}{H_d(s) G_d(s) + H_n(s) G_n(s)}.$$\n\nAs stated before, in this case $H(s)$ is equal to $K$, thus $H_d(s)$ is equal to one. By substituting in $K$ for $H_n(s)$ and the two polynomials, from this first equation, for $G_n(s)$ and $G_d(s)$, then the following expression can be obtained,\n\n$$\\frac{Y(s)}{R(s)} = \\frac{20(1+s)^2}{(1+\\frac{s}{2})(1+\\frac{s}{10}) + 20K(1+s)^2}.$$\n\nThe resulting denominator is a second order polynomial, so solving for the poles yields two solutions, which can be simplified to,\n\n$$p=-\\frac{400 K \\pm 4 \\sqrt{1 - 225 K} + 6}{400 K + 1}.$$\n\nFor $K=-\\frac{1}{400}$ the limits of both $p$ are $\\pm\\infty$ depending if you approach that value from the left or the right. Thus near $K=-\\frac{1}{400}$ there will be values for the poles of the closed loop transfer function which will have a positive real values.\n\n• Nice answer; welcome to the site. Apr 24 '15 at 0:34\n• Thanks, but I think it missed my question. Lets have a look at the denominator We got 2 poles,2 zeros, thus we conclude that each pole has its zero buddy that it tends to as K goes to negative infinity. We have no asymptotes, so no pole is going to infinity. Here comes the But, for the negative K, root locus diagram, by rule number 5, the portion of the real axis of the right of the -1 zeroes and the portion of the real axis of the left of the -10 poles belongs to the $$RL$$, plus we have no breach/escape points beyond these points, so a loop is out of consideration. Apr 24 '15 at 6:05\n• @minimalrisk Could you maybe elaborate what you mean by rule number 5, because not all literature uses the same (order of) rules for drawing root locus. And these rules are mainly useful to estimate it for higher order systems. For a second order system you can calculate it analytically. Apr 24 '15 at 9:41\n• Rule number 5 states that the portion of the real axis is part of the RL if and only if the number of open loop poles and zeroes to its right is an even number. Apr 24 '15 at 10:38\n• @minimalrisk I added an expression for the poles of the closed loop system, from which it will become obvious why it tends $\\pm\\infty$. For simple second order systems like this it can be worth it to finding the analytical solution for the poles. Apr 24 '15 at 11:55" ]
[ null, "https://i.stack.imgur.com/wYXPH.png", null ]
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https://explain.depesz.com/s/qQGl
[ "# Result: qQGl\n\nSettings\n# exclusive inclusive rows x rows loops node\n1. 0.000 0.000 ↓ 0.0\n\n(cost=8,087.04..8,087.04 rows=2 width=592) (actual rows= loops=)\n\n• Sort Key: o_e.partner_reporting_date\n2. 0.000 0.000 ↓ 0.0\n\n(cost=8,070.75..8,087.03 rows=2 width=592) (actual rows= loops=)\n\n3. 0.000 0.000 ↓ 0.0\n\n(cost=8,070.60..8,070.64 rows=2 width=476) (actual rows= loops=)\n\n4.\n\nCTE reasons_cte\n\n5. 0.000 0.000 ↓ 0.0\n\n(cost=2,505.29..2,505.31 rows=1 width=35) (actual rows= loops=)\n\n6. 0.000 0.000 ↓ 0.0\n\n(cost=2,505.29..2,505.30 rows=1 width=35) (actual rows= loops=)\n\n• Sort Key: obligation_reasons.id, obligation_reasons.kind, obligation_reasons.external_id\n7. 0.000 0.000 ↓ 0.0\n\n(cost=9.17..2,505.28 rows=1 width=35) (actual rows= loops=)\n\n8. 0.000 0.000 ↓ 0.0\n\n(cost=8.88..2,504.89 rows=1 width=4) (actual rows= loops=)\n\n9. 0.000 0.000 ↓ 0.0\n\n(cost=8.60..2,504.56 rows=1 width=4) (actual rows= loops=)\n\n10. 0.000 0.000 ↓ 0.0\n\n(cost=8.31..2,498.67 rows=19 width=8) (actual rows= loops=)\n\n• Hash Cond: (obligations_2.from_party_id = from_parties_2.id)\n11. 0.000 0.000 ↓ 0.0\n\nSeq Scan on obligations obligations_2 (cost=0.00..2,216.49 rows=104,249 width=12) (actual rows= loops=)\n\n12. 0.000 0.000 ↓ 0.0\n\n(cost=8.30..8.30 rows=1 width=4) (actual rows= loops=)\n\n13. 0.000 0.000 ↓ 0.0\n\nIndex Scan using parties_idx_uniq on parties from_parties_2 (cost=0.28..8.30 rows=1 width=4) (actual rows= loops=)\n\n• Index Cond: ((external_id = '5bec27212440da00050000df'::bpchar) AND ((kind)::text = 'partner'::text))\n14. 0.000 0.000 ↓ 0.0\n\nIndex Scan using parties_pkey on parties to_parties_2 (cost=0.28..0.31 rows=1 width=4) (actual rows= loops=)\n\n• Index Cond: (id = obligations_2.to_party_id)\n• Filter: (((kind)::text = 'driver'::text) AND (external_id = '5bebe344b344be0010aa42db'::bpchar))\n15. 0.000 0.000 ↓ 0.0\n\nIndex Scan using obligation_events_pkey on obligation_events o_e_2 (cost=0.29..0.33 rows=1 width=8) (actual rows= loops=)\n\n• Index Cond: (id = obligations_2.event_id)\n• Filter: ((partner_reporting_date >= '2017-01-01 00:00:00'::timestamp without time zone) AND (partner_reporting_date < '2020-01-01 00:00:00'::timestamp without time zone) AND ((event_kind)::text = 'create'::text))\n16. 0.000 0.000 ↓ 0.0\n\nIndex Scan using obligation_reasons_pkey on obligation_reasons (cost=0.28..0.40 rows=1 width=35) (actual rows= loops=)\n\n• Index Cond: (id = o_e_2.reason_id)\n17. 0.000 0.000 ↓ 0.0\n\n(cost=5,565.29..5,565.30 rows=2 width=476) (actual rows= loops=)\n\n• Sort Key: from_parties.external_id, to_parties.external_id, o_e.event_kind, reasons_cte.cte_reason_external_id, reasons_cte.cte_reason_kind, obligations.kind_id, o_e.partner_reporting_date, obligations.amount\n18. 0.000 0.000 ↓ 0.0\n\n(cost=285.18..5,565.28 rows=2 width=476) (actual rows= loops=)\n\n19. 0.000 0.000 ↓ 0.0\n\n(cost=285.18..2,782.63 rows=1 width=299) (actual rows= loops=)\n\n• Hash Cond: (o_e.reason_id = reasons_cte.cte_id)\n20. 0.000 0.000 ↓ 0.0\n\n(cost=285.15..2,782.53 rows=15 width=81) (actual rows= loops=)\n\n21. 0.000 0.000 ↓ 0.0\n\n(cost=284.86..2,777.71 rows=15 width=66) (actual rows= loops=)\n\n• Hash Cond: (obligations.to_party_id = to_parties.id)\n22. 0.000 0.000 ↓ 0.0\n\n(cost=142.20..2,632.55 rows=950 width=44) (actual rows= loops=)\n\n• Hash Cond: (obligations.from_party_id = from_parties.id)\n23. 0.000 0.000 ↓ 0.0\n\nSeq Scan on obligations (cost=0.00..2,216.49 rows=104,249 width=22) (actual rows= loops=)\n\n24. 0.000 0.000 ↓ 0.0\n\n(cost=141.57..141.57 rows=50 width=30) (actual rows= loops=)\n\n25. 0.000 0.000 ↓ 0.0\n\nSeq Scan on parties from_parties (cost=0.00..141.57 rows=50 width=30) (actual rows= loops=)\n\n• Filter: ((kind)::text = 'partner'::text)\n26. 0.000 0.000 ↓ 0.0\n\n(cost=141.57..141.57 rows=87 width=30) (actual rows= loops=)\n\n27. 0.000 0.000 ↓ 0.0\n\nSeq Scan on parties to_parties (cost=0.00..141.57 rows=87 width=30) (actual rows= loops=)\n\n• Filter: ((kind)::text = 'driver'::text)\n28. 0.000 0.000 ↓ 0.0\n\nIndex Scan using obligation_events_pkey on obligation_events o_e (cost=0.29..0.32 rows=1 width=23) (actual rows= loops=)\n\n• Index Cond: (id = obligations.event_id)\n29. 0.000 0.000 ↓ 0.0\n\n(cost=0.02..0.02 rows=1 width=226) (actual rows= loops=)\n\n30. 0.000 0.000 ↓ 0.0\n\nCTE Scan on reasons_cte (cost=0.00..0.02 rows=1 width=226) (actual rows= loops=)\n\n31. 0.000 0.000 ↓ 0.0\n\n(cost=285.18..2,782.63 rows=1 width=299) (actual rows= loops=)\n\n• Hash Cond: (o_e_1.reason_id = reasons_cte_1.cte_id)\n32. 0.000 0.000 ↓ 0.0\n\n(cost=285.15..2,782.53 rows=15 width=81) (actual rows= loops=)\n\n33. 0.000 0.000 ↓ 0.0\n\n(cost=284.86..2,777.71 rows=15 width=66) (actual rows= loops=)\n\n• Hash Cond: (obligations_1.from_party_id = from_parties_1.id)\n34. 0.000 0.000 ↓ 0.0\n\n(cost=142.20..2,632.55 rows=950 width=44) (actual rows= loops=)\n\n• Hash Cond: (obligations_1.to_party_id = to_parties_1.id)\n35. 0.000 0.000 ↓ 0.0\n\nSeq Scan on obligations obligations_1 (cost=0.00..2,216.49 rows=104,249 width=22) (actual rows= loops=)\n\n36. 0.000 0.000 ↓ 0.0\n\n(cost=141.57..141.57 rows=50 width=30) (actual rows= loops=)\n\n37. 0.000 0.000 ↓ 0.0\n\nSeq Scan on parties to_parties_1 (cost=0.00..141.57 rows=50 width=30) (actual rows= loops=)\n\n• Filter: ((kind)::text = 'partner'::text)\n38. 0.000 0.000 ↓ 0.0\n\n(cost=141.57..141.57 rows=87 width=30) (actual rows= loops=)\n\n39. 0.000 0.000 ↓ 0.0\n\nSeq Scan on parties from_parties_1 (cost=0.00..141.57 rows=87 width=30) (actual rows= loops=)\n\n• Filter: ((kind)::text = 'driver'::text)\n40. 0.000 0.000 ↓ 0.0\n\nIndex Scan using obligation_events_pkey on obligation_events o_e_1 (cost=0.29..0.32 rows=1 width=23) (actual rows= loops=)\n\n• Index Cond: (id = obligations_1.event_id)\n41. 0.000 0.000 ↓ 0.0\n\n(cost=0.02..0.02 rows=1 width=226) (actual rows= loops=)\n\n42. 0.000 0.000 ↓ 0.0\n\nCTE Scan on reasons_cte reasons_cte_1 (cost=0.00..0.02 rows=1 width=226) (actual rows= loops=)\n\n43. 0.000 0.000 ↓ 0.0\n\nIndex Scan using obligation_kinds_pkey on obligation_kinds o_k (cost=0.15..8.17 rows=1 width=120) (actual rows= loops=)\n\n• Index Cond: (id = obligations.kind_id)" ]
[ null ]
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https://bravelearn.com/tag/probability/
[ "# Tag: probability\n\n## Problems for Cumulative Distribution Function\n\nEarlier we discussed the introduction of a continuous random variable and cumulative distribution...\n\n## Continuous Random Variables and Cumulative Distribution Function\n\nThe problem with Discrete random variables was they can’t be used for continuous data. In...\n\n## Practice Problems (Introduction to Probability Theory)\n\nA few practice problems related to Probability theory are given here. These problems are adapted...\n\n## Random Variables\n\nA random variable is a real valued function of the elements of sample space S which maps each...\n\n## Assigning Probability and its Building Blocks", null, "" ]
[ null, "https://bravelearn.com/wp-content/themes/Extra/images/pagination-loading.gif", null ]
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https://mediatum.ub.tum.de/node?id=1632607&change_language=en
[ "User: Guest", null, "Login\nmediaTUM Gesamtbestand", null, "Einrichtungen", null, "Schools und Fakultäten", null, "Fakultät für Mathematik", null, "Zentrum Mathematik", null, "Arbeitsgruppe Mathematische Statistik", null, "Abschlussarbeiten", null, "Masterarbeiten", null, "2021", null, "Document type:\nMasterarbeit\nAuthor(s):\nMatthieu Bulté\nTitle:\nHigher-order statistics for high-dimensional problems with applications to graphical models\nAbstract:\nA Gaussian graphical model is a statistical model, where the data follows a multivariate Normal distribution in which conditional independence relations of the random vector are encoded in a graph. Testing the hypothesis that a Gaussian graphical model is associated to either a graph or a specific subgraph corresponds to a composite hypothesis test in the Normal model. However, the standard likelihood ratio test for this problem has both poor power and size, and is only suitable if the sample siz...    »\n\nSubject:\nMAT Mathematik\nDDC:\n510 Mathematik\nMathias Drton\nDate of acceptation:\n27.05.2021\nYear:\n2021\nQuarter:\n2. Quartal\nYear / month:\n2021-05\nMonth:\nMay\nPages:\n71\nLanguage:\nen\nUniversity:\nTechnische Universität München\nFaculty:\nFakultät für Mathematik\nTUM Institution:\nLehrstuhl für Mathematische Statistik\nOccurrences:" ]
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https://www.codingninjas.com/codestudio/problems/swap-two-numbers_1112577
[ "Problem title\nDifficulty\nAvg time to solve\n\nSet Matrix Zeros\nEasy\n30 mins\nBeautiful String\nEasy\n18 mins\nYogesh And Primes\nModerate\n20 mins\nSwap Two Numbers\nEasy\n10 mins\nFirst Missing Positive\nModerate\n18 mins\nLongest Univalue Path\nModerate\n10 mins\nFind Unique\nEasy\n--\nValid Sudoku\nModerate\n40 mins\nReverse Nodes in k-Group\nHard\n56 mins\nSum Of Max And Min\nEasy\n10 mins", null, "235\n\n# Swap Two Numbers\n\nDifficulty: EASY\nAvg. time to solve\n10 min\n\nProblem Statement\n\n#### Take two numbers as input and swap them and print the swapped values.\n\n##### Input Format:\n``````The first line of input contains a single integer 't', representing the total number of test cases.\n\nThe second line of input contains two integers 'a' and 'b', representing the second number.\n``````\n##### Output Format:\n``````The first line of output prints the swapped value of 'a' and 'b'.\n``````\n##### Note:\n``````You do not need to print anything, it has already been taken care of. Just implement the given function.\n``````\n##### Constraints:\n``````1 <= 'T' <= 10^2\n-10^5 <= 'a', 'b' <= 10 ^ 5\n\nTime Limit: 1 sec\n``````\n##### Sample Input 1:\n``````2\n1 2\n3 4\n``````\n##### Sample Output 1:\n``````2 1\n4 3\n``````\n##### Explanation For Sample Input 1:\n``````The output of the above test case is 2 1 for the first test case.\nThe output of the 2nd test case is 4 3.\n``````\n##### Sample Input 2:\n``````2\n5 6\n7 8\n``````\n##### Sample Output 2:\n``````6 5\n8 7\n``````\n##### Explanation For Sample Input 2:\n``````The output of the above test case is 6 5 for the first test case.\nThe output of the 2nd test case is 8 7.\n``````", null, "", null, "", null, "Console" ]
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https://groupprops.subwiki.org/wiki/Amalgamated_free_product_of_Z_and_Z_over_2Z
[ "# Amalgamated free product of Z and Z over 2Z\n\nView a complete list of particular groups (this is a very huge list!)[SHOW MORE]\n\n## Definition\n\n### Definition as an amalgamated free product\n\nThe group is defined as the amalgamated free product", null, "$\\mathbb{Z} *_{2\\mathbb{Z}} \\mathbb{Z}$, i.e., we take two copies of the group of integers, take their free product, and then take the quotient group by the identification of the subgroup", null, "$2\\mathbb{Z}$.\n\n### Definition by presentation\n\nThe group can be defined by the presentation:", null, "$\\langle x,y \\mid x^2 = y^2 \\rangle$\n\n## Group properties\n\nProperty Meaning Satisfied? Explanation\nabelian group any two elements commute No", null, "$x,y$ do not commute\nnilpotent group upper central series reaches the whole group in finitely many steps No The quotient group by the center", null, "$\\langle x^2 \\rangle$ is isomorphic to the infinite dihedral group, which is centerless.\nsolvable group has a normal series where all the quotients are abelian Yes The quotient by the center is infinite dihedral group, which is a metacyclic group." ]
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https://www.autoswiat-polska.pl/2021-apr-16/9203.html
[ "[email protected]\n\nNews Center\n\nHere, we will provide you with fresh corporate dynamics, industry information, and market focus, allowing you to grasp the dynamics of the mining machinery industry at any time, grasp the forefront of the market, and grasp the opportunities for entrepreneurship!\n\n1. Home\n2. Qtty Of Sand In 1 Cubic Metre Of Concrete", null, "Qtty Of Sand In 1 Cubic Metre Of Concrete\n\n•", null, "Quantities of Materials Per Cubic Meter of Concrete Mix\n\nQuantity of materials such as cement, sand, coarse aggregates and water required per cubic meter of concrete and mortar for different mix proportions varies with the mix design of the concrete and mortar respectively. Following table gives the estimated quantity of materials required per cubic meter of mortar and concrete for various nominal mixes.\n\n•", null, "Quantities of Materials Per Cubic Meter of Concrete Mix\n\n24 rows Oct 16, 2014 Quantity of materials such as cement, sand, coarse aggregates and water required per cubic ...\n\n•", null, "Sand and Aggregate Quantity In 1 Cubic metre Concrete\n\nDec 29, 2020 Tagged Sand and Aggregate Quantity In 1 Cubic metre Concrete . 1. Civil Topics. December 29, 2020. What is Retrofitting of Structures Its Types amp Benefits. ... Self Healing Concrete and Asphalt, Civil Drawing. 20 X 40 House Plan and Structure CAD Drawing CAD Blocks For Architect, Draftsman, designers\n\n•", null, "How many bags of cement do I need to make 1 cubic metre\n\nDec 30, 2011 1 Cement 2 Sand 3 Aggregate gravel is too strong. 16bags costly 1 Cement 2.5 Sand 4 Aggregate is OK for fence posts. 13bags of cement per cubic metre. The more cement the more costly of course so dont over do it. Note These are 20kg bags of General Purpose cement.\n\n•", null, "Rate Analysis of RCC Reinforcement Cement Concrete\n\nAssume of reinforcement 2 of the total volume of concrete. so, 1 cu.m. concrete for reinforcement 1.0 x 2 0.02 ton of steel this 2 only assumse as per exprience Her, 10 Cu.m concrete requirement 0.02 ton x 10 co.m. 0.20 ton 200 kg for 10 cu.m. Also, read What is Bitumen And Bitumens Types. Labour for Rate Analysis of Concrete\n\n•", null, "Quantities of Cement Sand and Aggregate in Cubic Meter\n\nJan 17, 2021 Hello, friends in this article you will learn to calculate the Quantity of Cement, Sand, and Aggregate In Kilograms, Cubic Meter and Cubic Feet. Also, you find the Table where you will get the Quantity of Cement, sand, and aggregate of different Grade of Concrete\n\n•", null, "How much cement sand amp aggregate required for M20 concrete\n\nAns. -0.42 m3 quantity of sand is required for 1 cubic metre of M20 concrete. How much sand required for M20 concrete in Kgs step 8 -calculate sand required for 1 cubic metre of M20 concrete in kgs kilogram is equal to 1.55.5 1.54m3 1620 Kgm3 680Kgs. Ans. -680 Kgs quantity of sand is required for 1 cubic metre of M20 concrete\n\n•", null, "How much cement sand amp aggregate required for m25 concrete\n\nAns. -624 Kgs quantity of sand is required for 1 cubic metre of M25 concrete. How much sand required for M25 concrete in cft step 9 -calculate sand required for 1 cubic metre of M25 concrete in cft cubic feet is equal to 14 1.54m335.3147 1620 Kgm3 18 cft. Ans.- 18 cft quantity of sand is required for 1 cubic metre of M25 concrete.\n\n•", null, "How to Calculate Cement Sand amp Aggregate Quantity in Concrete\n\nFor M25 1 part of cement, 1 part of sand and 2 part of aggregate. Density of materials. Cement 1440 kgm 3. Dry Sand 1540 to 1600 kgm 3. Aggregate 1560 to 1600 kgm 3. Wet to Dry Conversion. Dry Volume Wet Volume 54 of wet volume Dry Volume Wet Volume x 1.54. How to calculate quantity for 10 cubic meter concrete.\n\n•", null, "Metric calculator for concrete cement sand gravel etc\n\nBoth of these concrete calculators make an allowance for the fact that material losses volume after being mixed to make concrete. Calculator are provided for a general mix and a paving mix, the different ratio of materials are General mix - 15 cementall-in ballast or 12 3 cementsharp sandgravel. Paving mix - 13 cementall-in ...\n\n•", null, "How to Calculate Quantities of Cement Sand and Aggregate\n\nSo 1.54 Cum of dry materials cement, sand and aggregate is required to produce 1 Cum of concrete. Volume of Cement required 1124 X 1.54 17 X 1.54 0.22 Cum. Volume of Sand required 27 X 1.54 0.44 Cum or 15.53 cft. Volume of Aggregate required 47 X 1.54 0.88 Cum or 31.05 cft. Note 1 cubic meter 35.29 cubic feet\n\n•", null, "How To Calculate Cement Bags In 1 Cubic Meter\n\nDec 21, 2016 Procedure To Calculate Cement Bags In 1 Cubic Meter To achieve 1 cum output, we need 10.67 1.49 say 1.50 cum dry mix. Now add the wastage of 2, i.e 1.50 0.02 1.52 cum. Weight of 1 bag cement 50 kg. 6.25 bags. Note You can use the same formula for calculating cement for other nominal mixes.\n\n•", null, "Calculate Quantities of Materials for Concrete Cement\n\nWe have considered an entrained air of 2. Thus the actual volume of concrete for 1 cubic meter of compacted concrete construction will be 1 -0.02 0.98 m 3. Thus, the quantity of cement required for 1 cubic meter of concrete 0.980.1345 7.29 bags of cement. The quantities of materials for 1 m3 of concrete production can be calculated as ...\n\n•", null, "How to Calculate Cement Sand and Aggregate required for\n\nMar 18, 2017 Density of concrete 2400 kgcum. So, 1 bag of cement produces 4002400 0.167 cum. No. of bags required for 01 cum of concrete 10.167 5.98 bags 6 bags. From above, if the concrete mix is 124 , to get a cubic meter of concrete we require. 1.Cement 6 bags 300 kgs. 2.Fine Aggregate 1150.167 689 kg.\n\n•", null, "Calculate Quantities of Materials for Concrete Cement\n\nApr 01, 2015 Thus, the quantity of cement required for 1 cubic meter of concrete 0.980.1345 7.29 bags of cement. The quantities of materials for 1 m3 of concrete production can be calculated as follows The weight of cement required 7.29 x 50 364.5 kg. Weight of fine aggregate sand 1.5 x 364.5\n\n•", null, "How to calculate quantity of cement sand amp aggregate in\n\nThere are two main ways to design the concrete mix. Design mix method - In this method, materials are proportioned based on the procedure and rules given in IS 456 2000 and IS 10262 code . In this method, cement, sand and aggregates are always batched in terms of weight, and concrete can be designed for different environmental conditions and different needs.\n\n•", null, "Sand Calculator how much sand do you need in tons\n\nHow much does a cubic meter of sand weigh A cubic meter of typical sand weighs 1,600 kilograms 1.6 tonnes. A square meter sandbox with a depth of 35 cm weighs about 560 kg or 0.56 tonnes. The numbers are obtained using this sand calculator. How much is a ton of sand A ton of sand is typically about 0.750 cubic yards 34 cu yd, or 20 cubic feet.\n\n•", null, "what is the cement quantity of nominal mix 124 for 1\n\nMay 14, 2009 7 cubic meters of loose mix will give 5 cubic meters of solid concrete. 136, 1 cubic meter of cement 3 c.m. of sand 6 c.m. of aggregate will give 10 cubic meters of loose material. when mixed in a mixture will give 10 x 57 7.143 cubic meters of solid containing 1440 Kg of cement. So 1 cubic meter will have 1440 7.143 201.59 Kg ...\n\n•", null, "How to Calculate Cement Sand and Coarse Aggregate\n\nConcrete Ingredients Calculation. For Cement, Sand and Coarse Aggregate. This is a Volumetric Calculation. Assuming we need 2 m 3 of concrete for M20 Concrete Mix, Mix Ratio, M20 1 1.5 3 Total Part of the Concrete 11.53 5.5 Parts. Therefore, Cement Quantity Cement Part Concrete Parts Concrete Volume\n\n•", null, "How to Calculate Brick Cement and Sand in Brickwork\n\nCement 0.043 28.8 1.238 bags Numbers of cement bags in 1 Cum 28.8 Sand 0.043 6 0.258 cum. But as the cement will go to fill up the voids in the sand, 0.045 cum of cement and 0.27 cum of sand may be taken. I hope now you understood how to calculate quantity of materials in brickwork.\n\n•", null, "How much cement sand amp aggregate required for M15\n\nJul 26, 2020 Ans. - 713 Kgs quantity of sand is required for 1 cubic metre of M15 concrete. How much sand required for M15 concrete in cft step 9 - calculate sand required for 1 cubic metre of M15 concrete in cft cubic feet is equal to 27 1.54m335.3147 1620 Kgm3 20 cft. Ans. - 20 cft quantity of sand is required for 1 cubic metre of M15 ...\n\n•", null, "How much cement sand amp aggregate required for M20\n\nJul 26, 2020 We have given dry volume of concrete is equal to 1.54 cubic metre and part of sand in concrete mix is equal to 1.55.5, density of sand is equal to 1620 Kgm3 and one cubic metre is equal to 35.3147 cu ft. How much sand required for M20 concrete in cubic metre.\n\n•", null, "How To Calculate the Quantity of Materials Sand and\n\nJul 20, 2016 Therefore, if we were to render a cubic meter of Mortar 1m3 with a mix ratio 16 Meaning One Bag Of Cement for 6 Parts Of sand, The quantity of sand needed here would be 1.371m 3 Volume of sand needed\n\n•", null, "Calculate Cement Sand amp Aggregate M20 M15 M10 M5\n\nCalculate the concrete quantity required in cubic meter and then multiply the quantity with the cement sand and aggregate for 1 cubic meter of concrete. In your case Volume of concrete 1.7 x 1.7 x 0.5 1.4 cu.m It looks like you are using m20 grade mix with extra sand. If you follow that mix proportion then to calculate use this following ...\n\n•", null, "How much Cement Sand Quantity in Brickwork Civil\n\nOct 13, 2018 You can add mortar if width of wall is more than 1 brick. Required Number of Bricks 2.140.00245 873 Bricks. So Actual Number of Bricks for 1 Cubic metre in field 8732.14 408 Bricks. Actual number varies from meson to meson because some one use less mortar and some one use more mortar. so it is mainly 390 to 430.\n\n•", null, "Cement Mortar Estimation of Cement Sand amp Water in\n\nJul 09, 2019 Estimation of Water, Cement amp Sand quantity for Cement Mortar. Let us assume a standard quantity of 1m 3 Cement mortar and a mix proportion of CM 16 1 part Cement amp 6 parts Sand. The quantity can calculated in two ways, one is by weight and the other by volume. Let us consider the volume method for the calculation of cement amp sand quantity.\n\n•", null, "Calculate Cement Sand amp Aggregate M20 M15 M10 M5\n\nSep 08, 2015 Calculate the concrete quantity required in cubic meter and then multiply the quantity with the cement sand and aggregate for 1 cubic meter of concrete. In your case Volume of concrete 1.7 x 1.7 x 0.5 1.4 cu.m It looks like you are using m20 grade mix with extra sand. If you follow that mix proportion then to calculate use this following method.\n\n•", null, "Tutorial How Many WheelBarrows Of Cement Sand And\n\nJul 12, 2017 ASSUMEConcrete Density is 2400kgm3 and a head pan is 25kg max carrying weight. A ratio of 124 gives 7 parts. Cement is 1 part therefore 17 of 2400 342kg 6.8 x 50kg bags. Sand is 2 parts, therefore 27 of 2400 684kg. 27 head pans Stone is 4 parts, therefore 47 of 2400 1368kg.55 head pans THIS IS ALL TO MAKE 1 meter cube of ...\n\n•", null, "Cement Concrete Calculator PCC Calculator RCC\n\nStrength of PCC is defined as compressive strength after 28 days, expressed as M15, M20, where M stands for Mix and 15 stands for 15 Nmm 2 nmm 2 must be read as Newtons per millimeter Cubic compressive strength at 28 days. The proportions of materials cement, sand, coarse aggregate for nominal mixdesign mix concrete that are normally used are 136 or 148.\n\n•", null, "How to Calculate Cement Sand and Aggregate required for 1\n\nDensity of concrete 2400 kgcum. So, 1 bag of cement produces 4002400 0.167 cum. No. of bags required for 01 cum of concrete 10.167 5.98 bags 6 bags. From above, if the concrete mix is 124 , to get a cubic meter of concrete we require. 1.Cement 6 bags 300 kgs. 2.Fine Aggregate 1150.167 689 kg\n\n•", null, "SAND CALCULATOR How Much Sand do I Need\n\nOur sand calculator can be used to work out how much sand your next landscaping project will require. Work out the total volume, weight and cost of the sand." ]
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https://hsm.stackexchange.com/questions/11624/what-is-the-origin-of-the-term-non-derogatory-matrix
[ "# What is the origin of the term (non-)derogatory matrix?\n\nA non-derogatory matrix $$A$$ is one, whose minimal polynomial $$m(z)$$ equals its characteristic polynomial $$p(z)$$, where we apply the convention $$p(z) = det(zI-A)$$, while a matrix is derogatory, if they do not coincide. I have certainly never felt particularly offended when dealing with the identity matrix $$I$$, so seriously I wonder, where that strange name has its origin.\n\nSome background:\n\nI would like to know about it, because I teach some advanced pupils at a german gymnasium school, who will be considering a field of study in the STEM-area, some linear algebra using examples from polynomial geometry. In that context, certain polynomials generate matrices with a double eigenvalue, which are either non-derogatory or diagonalizable, and where the non-derogatory ones are indeed preferable to the diagonalizable ones due to the particular application.\n\nIn order to make the rather involved notion more palatable to the audience, it is always good to have a story to tell about it, even if it turns out to be rather dull in the end.\n\nMy native language is german and I know of only one place in the german literature, where non-derogatory matrices get a special name. That is in E.Brieskorn \"Lineare Algebra und analytische Geometrie II\", where they are called \"regular\", which the author immediately distinguishes from another use of that word as invertible.\n\nOn the contrary, the english denomination sems to be well-established when refering to Google and I found it already mentioned in the first chapter of J.H. Wilkinson \"The Algebraic Eigenvalue Problem\" from 1965 without further comment, so it seems to have been established by then.\n\n• The term seems self-explanatory (=deficient matrix, non-diagonalizable matrix). And the question on historical usage is better to ask in History of Science and Maths SE. – Alexandre Eremenko Apr 5 at 19:37" ]
[ null ]
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https://www.jiskha.com/questions/977578/The-blades-of-a-fan-running-at-low-speed-turn-at-230rpm-When-the-fan-is-switched
[ "# Physics (angular motion)\n\nThe blades of a fan running at low speed turn at 230rpm . When the fan is switched to high speed, the rotation rate increases uniformly to 370rpm in 5.80s .\n\nPart A\nWhat is the magnitude of the angular acceleration of the blades?\n\nPart B\nHow many revolutions do the blades go through while the fan is accelerating?\n\n1. 👍 0\n2. 👎 0\n3. 👁 237\n1. angular acceleration=(wf-wi)/time\n\nfor here, you have to choose your units. I think I would change time to minutes, so angular acceleration would be in rev/min^2\n\nacceleration= (370-230)/(5.8/60)\n= 140*60/5.8 work that our rpm^2\n\nrev=wi*time+1/2 acceleration*time^2\n= 230*5.8/60 + 1/2 above acc*(5.8/60)^2\nor you could have done it with avg velocity\nrev=avgvelocity*time=(wf+wi)/2 * 5.8/60\n\n1. 👍 0\n2. 👎 0\n\n## Similar Questions\n\n1. ### Physics\n\nThe blades of a fan running at low speed turn at 200 rpm. When the fan is switched to high speed, the rotation rate increases uniformly to 340 rpm in 5.92 s. (a) What is the magnitude of the angular acceleration of the blades? (b)\n\nasked by Kelsey on December 11, 2010\n2. ### physics\n\nThe blades of a fan running at low speed turn at 200 rpm. When the fan is switched to high speed, the rotation rate increases uniformly to 340 rpm in 5.92 s. How many revolutions do the blades go through while the fan is\n\nasked by Kelsey on December 11, 2010\n3. ### Physics\n\nThe blades of a fan turn at 1250rpm at low speed. When the fan is switched to high speed, the rotation rate increases uniformly to 1750rpm in a period of 3.0sec. What is the average angular acceleration of the blades, in\n\nasked by Tii on January 3, 2011\n4. ### physics\n\nThe motor of a fan turns a small wheel of radius rm = 1.60 cm.This wheel turns a belt, which is attached to a wheel of radius rf = 2.90 cmthat is mounted to the axle of the fan blades. Measured from the center of this axle, the\n\nasked by mymi on October 21, 2011\n5. ### physics\n\nA ceiling fan has four blades, each with a mass of 0.40 kg and a length of 65 cm. Model each blade as a rod connected to the fan axle at one end. When the fan is turned on, it takes 4.45 s for the fan to reach its final angular\n\nasked by Ashley on August 2, 2011\n6. ### college\n\nA ceiling fan has 15 -inch blades (so the radius of the circular fan is 15 inches). Suppose the fan turns at a rate of 60 revolutions per minute. (a) Find the angular speed of the fan in radians per minute. (b) Find the linear\n\nasked by Ange on September 11, 2016\n7. ### science\n\n2. An electric fan having a radius of 0.5 m is running on HIGH. After the LOW button is pressed, the angular speed of the fan decreases to 83.8 rad/s in 17.5 s. the deceleration is 42.0 rad/s2. Determine a) The initial angular\n\nasked by Jeff on April 11, 2012\n8. ### precalc\n\nA celing fan with 16 inch blades rotates at 45 revolutions per minute. Find angular speed of fan in radians per minute. Find linear speed of the tips of blades in inches per minute.\n\nasked by Andy G on April 29, 2014\n9. ### Physics\n\nThe blades of a ceiling fan have a radius of 0.399 m and are rotating about a fixed axis with an angular velocity of +1.65 rad/s. When the switch on the fan is turned to a higher speed, the blades acquire an angular acceleration\n\nasked by Josh on December 4, 2010\n10. ### Physics\n\nThe blades of a ceiling fan have a radius of 0.393 m and are rotating about a fixed axis with an angular velocity of +1.36 rad/s. When the switch on the fan is turned to a higher speed, the blades acquire an angular acceleration\n\nasked by Anon on October 18, 2014\n\nMore Similar Questions" ]
[ null ]
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https://www.aggiesbakery.com/product/two-tier-cake-14/
[ "# Two Tier Cake 14\n\nFrom: \\$160.00\n\nThis is a 6″ and 8″ cake that serves 25. For additional sizes please call the bakery.\n\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 0 \\$\n• + 0 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• + 16 \\$\n• + 16 \\$\n• + 16 \\$\n• + 16 \\$\n• + 16 \\$\n• + 16 \\$\n• + 16 \\$\n• + 16 \\$\n• + 0 \\$\n• + 0 \\$\n• + 10 \\$\n• + 10 \\$\n• + 10 \\$\n• \\$\n• \\$\n• \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 5 \\$\n• + 5 \\$\n• + 5 \\$\n• + 5 \\$\n• + 5 \\$\n• + 5 \\$\n• + 5 \\$\n• + 5 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• + 0 \\$\n• \\$\n\nPlease limit your comments to clarifying which accent colors should be utilized on which part of the cake’s decorations, i.e. “Use the red I selected for the flowers and the green I selected for the balloons”. We do not allow any changes to the design of the cake you selected other than customizing colors. If you would like a modified version of this cake, please call the bakery to discuss your design. Also, please note we require at least a 1-week notice for any cakes requiring unique designs other than what we offer on our website.\n\n• \\$\nSKU: TTS-7-1-1 Category: Tags: , ," ]
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https://jprm.sms.edu.pk/analysis-of-steady-non-isothermal-two-dimensional-flow-of-second-grade-fluid-in-a-constricted-artery/
[ "Journal of Prime Research in Mathematics\n\nA.A. Mirza\nDepartment of Mathematics, S.S.(N.H) Govt. Degree College GujarKhan, Rawalpindi, 44000 Pakistan.\nA.M. Siddiqui\nDepartment of Mathematics, Pennsylvania State University, York Campus, 1031 Edgecomb Avenue, York, PA 17403, USA.\nT. Haroon\n$$^{1}$$Corresponding Author: azharali_mirza1@yahoo.com\nSteady analytical solution of non-isothermal, second grade fluid through an artery having constriction of cosine shape in two dimension is presented. The governing equations are transformed into stream function formulation which are solved analytically with the help of regular perturbation technique. The solutions thus obtained are presented graphically in terms of streamlines, wall shear stress, separation points, pressure gradient and temperature distribution. It is observed that an increase in height of constriction $$(\\in)$$ gives rise in wall shear stress, pressure gradient and temperature, whereas critical Reynolds  number $$(R_e)$$ decreases. Further an increase in second grade parameter $$(α)$$ increases the temperature, pressure gradient, velocity and wall shear stress while critical Re decreases. Its worthy to mention that the present results are compared with the already published results which ensures good agreement." ]
[ null ]
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https://www.jpost.com/international/three-injured-in-heidelberg-car-ramming-482568
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[ null ]
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https://www.quantumstudy.com/practice-zone/numerical-laws-of-motion/
[ "# Numerical Problems , Laws of Motion\n\n#### LEVEL – I\n\nQ:1. Two blocks A and B of masses M1 and M2 respectively kept in contact with each other on a smooth horizontal surface. A constant horizontal force (F) is applied on ‘ A ‘ as shown in figure. Find the acceleration of each block and the contact force between the blocks", null, "[Ans: a= F/( M1 + M2) , N=M2F/( M1 + M2) ]\n\nQ:2. A bob of mass m = 50 gm is suspended from the ceiling of a trolley by a light inextensible string. If the trolley accelerates horizontally, the string makes an angle θ = 30° with the vertical. Find the acceleration of the trolley.", null, "[Ans: 5.7 m/s2]\n\nQ:3. Two small bodies connected by a light inextensible string passing over a smooth pulley are in equilibrium on a fixed smooth wedge as shown in the figure. Find the ratio of the masses. Given that θ = 60° and α = 30°", null, "[Ans: m1/m2 = 1/√3]\n\nQ:4. Both the springs shown in Figure are unstretched. If the block is displaced by a distance x and released, what will be the initial acceleration?", null, "[Ans: 2kx/m]\n\nQ:5. A block of mass m = 1 kg is at rest on a rough horizontal surface having coefficient of static friction 0.2 and kinetic force 0.15. Find the frictional forces if a horizontal force (a) F = 1 N, (b) F = 1.96 N and (c) F = 2.5 N are applied on a block which is at rest on the surface.", null, "[Ans: (a) 1N (b) 1.96 N (c) 1.5 N ]\n\nQ:6. Two masses m1 = 5 kg, m2 = 2 kg placed on a smooth horizontal surface are connected by a light inextensible string. A horizontal force F = 1 N is applied on m1. Find the acceleration of either block. Describe the motion of m1 and m2 if the string breaks but F continues to act.\n\nAns : [a = 1/7 m/s2 , a’ = 1/5 m/s2]\n\nQ:7. The coefficient of static friction between a block of mass m and an incline is μs = 0.3.\n(a) What can be the maximum angle θ of the incline with the horizontal so that the block does not slip on the plane?\n(b) If the incline makes an angle θ/2 with the horizontal, find the frictional force on the block.\n\nAns: [θ = tan-1(0.3) , f = 0.145 mg ]\n\nQ:8. A 20 kg box is dragged across a rough level floor having a coefficient of kinetic friction of 0.3 by a rope which is pulled upward at angle of 30° to the horizontal with a force of magnitude 80 N.\n\n(a) What is the normal force?\n\n(b) What is the frictional force?\n\n(c) What is the acceleration of the box?\n\n(d) If the force is reduced until the acceleration becomes zero, what is the tension in the rope?\n\nAns: [(a)160 N (b)48 N (c) 1.06 m/s2 (d) 55.42 N ]\n\nQ:9. A small body A starts sliding down from the top of a wedge (fig.) whose base is equal to l = 2.10 m. The coefficient of friction between the body and the wedge surface is k = 0.140. For what value of the anlge α will the time of sliding be the least? What will it be equal to?", null, "Ans : $\\displaystyle \\frac{2l}{((g/2)\\sqrt{1 + k^2 – k)^{-1}}}$\n\nQ:10. A chain of length l is placed on a smooth spherical surface of radius R with one of its ends fixed at the top of the sphere. What will be the acceleration a of each element of the chain when its upper end is released? It is assumed that the length of the chain l < (πR/2).\n\nAns: Tangential acceleration $\\displaystyle a_t = \\frac{R g}{l}(1- cos\\frac{l}{R})$\n\nNext Page → Laws Of Motion (Level-II)" ]
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http://forums.wolfram.com/mathgroup/archive/2002/Sep/msg00236.html
[ "", null, "", null, "", null, "", null, "", null, "", null, "", null, "Re: Arbitrary Crash with Compile\n\n• To: mathgroup at smc.vnet.net\n• Subject: [mg36541] Re: Arbitrary Crash with Compile\n• From: Jens-Peer Kuska <kuska at informatik.uni-leipzig.de>\n• Date: Wed, 11 Sep 2002 13:27:19 -0400 (EDT)\n• Organization: Universitaet Leipzig\n• References: <alev2a\\$5dm\\$1@smc.vnet.net>\n• Sender: owner-wri-mathgroup at wolfram.com\n\n```Hi,\n\nmy Mathematica 4.2 does not crash and you may upgrade\n\nRegards\nJens\n\nWizard Lab wrote:\n>\n> Dear Group,\n>\n> I have a program to take the local polynomial non parametric regression\n> of two variables. It uses Compile, unfortunately, and regularly, but\n> inconsistently, causes Mathematica to crash (in Win2K, with I forget\n> what error, and in Win98/Mathematica4.0 with an invalid memory access from\n> MathDLL.dll). I am running Mathematica 4.1, and have this problem consistently\n> on 4 different machines.\n>\n> Here is the code, if it doesn't crash the first time, it will the second\n> or third:\n>\n> (*\n> w = Compile[{{xj, _Real, 0}, {XX, _Real, 1}, {YY, _Real, 1}, {h, _Real,\n> 0},\n> {nn, _Integer, 0}, {ord, _Integer, 0}},\n> First[Inverse[Sum[Outer[Times, Table[If[Positive[q], (XX[[i]] - xj)^q,\n> 1], {q, 0, ord}],\n> Table[If[Positive[q], (XX[[i]] - xj)^q, 1.], {q, 0,\n> ord}]*E^(-0.5*((XX[[i]] - xj)/h)^2)], {i, nn}]] .\n> Sum[(Table[If[Positive[q], (XX[[i]] - xj)^q, 1.], {q, 0, ord}]*YY[[i]])*\n> E^(-0.5*((XX[[i]] - xj)/h)^2), {i, nn}]]];\n> *)\n>\n> (*\n> \\!\\(tt = MemoryInUse[];\n> ListPlot[Table[{\\((i + 1)\\)\\^2, \\(Timing[\n> nn = \\((i + 1)\\)\\^2; \\[Epsilon] = Table[Random[]*3, {i,\n> nn}];\n> testX = Table[i* .3 - Random[]*2, {i, nn}];\n> testY = Table[Sin[i/3] - 2, {i, nn}] + \\[Epsilon];\n> Map[w[#, testX, testY, .1 + Random[], nn, 0] &,\n> testX];]\\)[\\(\\)]/Second}, {i, 15}], PlotJoined ->\n> True,\n> PlotLabel -> \"\\<Calculation Times as a function of n\\>\"];\n> MemoryInUse[] - tt\\)\n> *)\n>\n> I have followed Ted Ersek's tips and tricks\n> and have tried changing all variable names (works sometimes), removing\n> any hidden spaces, restructuring the formulas, changing all 0's to 0. 's\n> and all 1's to 1. 's, etcetera etcetera, but I still can't comprehend\n> what the problem might be. Doing \"w[[-2]]\" shows a list of op-code\n> numbers, and one function name, Inverse[#1]&, so it seems to me that\n> there are no problems with the use of Compile here. Would anyone have\n> any thoughts???\n>\n> Regards,\n>\n> Bernard Gress\n> burnthebiscuit at netscape.net\n\n```\n\n• Prev by Date: Re: 2 gifs side by side -- with hyperlinks\n• Next by Date: Re: executing a notebook from the command line\n• Previous by thread: Arbitrary Crash with Compile\n• Next by thread: Re: Arbitrary Crash with Compile" ]
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https://file.scirp.org/Html/3-1490354_60999.htm
[ " H<sub>∞</sub> Optimal Control Problems for Jump\n\nJournal of Mathematical Finance\nVol.05 No.04(2015), Article ID:60999,11 pages\n10.4236/jmf.2015.54029\n\nH¥ Optimal Control Problems for Jump Linear Equations\n\nIvan G. Ivanov1,2, Ivelin G. Ivanov2\n\n1Faculty of Economics and Business Administration, Sofia University “St. Kliment Ohridski”, Sofia, Bulgaria\n\n2Pedagogical College Dobrich, Shoumen University, Shoumen, Bulgaria", null, "", null, "", null, "Received 8 September 2015; accepted 8 November 2015; published 11 November 2015", null, "ABSTRACT\n\nWe consider a set of continuous algebraic Riccati equations with indefinite quadratic parts that arise in H¥ control problems. It is well known that the approach for solving such type of equations is proposed in the literature. Two matrix sequences are constructed. Three effective methods are described for computing the matrices of the second sequence, where each matrix is the stabilizing solution of the set of Riccati equations with definite quadratic parts. The acceleration modifications of the described methods are presented and applied. Computer realizations of the presented methods are numerically compared. In addition, a second iterative method is proposed. It constructs one matrix sequence which converges to the stabilizing solution to the given set of Riccati equations with indefinite quadratic parts. The convergence properties of the second method are commented. The iterative methods are numerically compared and investigated.\n\nKeywords:\n\nH¥ Optimal Control Problem, Generalized Riccati Equation, Indefinite Sign, Stabilizing Solution", null, "1. Introduction\n\nRecently the algebraic Riccati equations with indefinite quadratic part have been investigated intensively. The paper of Lanzon et al. is the first where is investigated an algebraic Riccati equation with an indefinite quadratic part in the deterministic case. Further on, the Lanzon’s approach has been extended and applied to the algebraic Riccati equations of different types - and for the stochastic case . Many situations in management, economics and finance - are characterized by multiple decision makers/players who can enforce the decisions that have enduring consequences. The similar game models lead us to the solution of the Riccati equations with an indefinite quadratic part. The findings in show how to model economic and financial applications using a discrete-time H¥-approach to simulate optimal solutions under a flexible choice of system parameters. Here, a continuous H¥-approach to jump linear equations is studied and investigated.\n\nMore precisely, how to find the stabilizing solution of the coupled algebraic Riccati equations of the optimal control problem for jump linear systems with indefinite quadratic part:", null, "(1)\n\nis considered. In the above equations the matrix coefficients", null, "are", null, "real matrices,", null, "are", null, "real matrices,", null, "is a", null, "real matrix and the unknown", null, "is a symmetric", null, "matrix", null, ". The considered set of Riccati Equation (1) is connected to the stochastic controlled system with the continuous Markov process (see ), which is called a", null, "control problem. The parameter", null, "presents a level of attenuation of the corresponding", null, "control problem. In order to solve a given", null, "control problem, we have to find the control", null, "which is given by\n\nwhere is a right continuous Markov process and is the stabilizing solution to (1) (see ).\n\nThe stabilizing solution of the considered game theoretic Riccati equation is obtained as a limit of a sequence of approximations constructed based on stabilizing solutions of a sequence of algebraic Riccati equations of stochastic control with definite sign of the quadratic part. The main idea is to construct two matrix sequences such that the sum of corresponding matrices converges to the stabilizing solution of the set of Riccati Equation (1). Such approach is considered in . The properties of this approach are considered in terms of the concept of mean square stabilizability and the assumption that the convex set is not empty (see Dragan and coauthors in ).\n\nHere we introduce the sufficient conditions for the existence of stabilizing solutions of the set of Riccati Equation (1). We will prove under these conditions some convergence properties of constructed matrix sequences in terms of perturbed Lyapunov matrix equations. In addition, we introduce a second iterative method where we construct one matrix sequence. We show that the second iterative method constructs a convergent matrix sequence. Moreover, if the sufficient conditions of the first approach are satisfied then the second iterative method converges.\n\n2. Preliminary Facts\n\nThe notation stands for the linear space of symmetric matrices of size n over the field of real numbers. For any, we write or if is positive definite or is positive semidefinite.\n\nWe use notation. The notations and the inequality mean that for and, respectively. The linear space is a Hilbert space with the Frobenius inner product. A linear operator on is called asymptotically stable if the\n\neigenvalues to lie in the open left half plane and almost asymptotically stable if the eigenvalues to lie in the closed left half plane.\n\nWe denote and define the matrix function as follows:\n\n(2)\n\nWe will rewrite the function in the form:\n\n(3)\n\nwhere and\n\nNote that transition coefficients if and for all i. Thus if, we have.\n\nWe introduce the following perturbed Lyapunov operator\n\nand will present the solvability of (1) through properties if the perturbed Lyapunov operator.\n\nProposition 1: The following are equivalent:\n\n1) The matrix is the stabilizing solution to (1);\n\n2) The perturbed Lyapunov operator is asymptotically stable where:\n\nThe above proposition presents a deterministic characterization of a stabilizing solution to set of Riccati Equation (1).\n\nA matrix is called stabilizing for if eigenvalues of lie in the open left half plane. In order words the stabilizing to (1) stabilizes the operators.\n\nKnowing the stabilizing solution to (1) we consider and and therefore the matrix builds a perturbed Lyapunov operator which is asymptotically stable.\n\nDragan et al. have introduced the following iteration scheme for finding the stabilizing solution to set of algebraic Riccati Equation (1). They construct two matrix sequences and as follows:\n\n(4)\n\nEach matrix is computed as the stabilizing solution of the algebraic Riccati equation with definite quadratic part:\n\n(5)\n\nwhere\n\nHowever, it is not explained in how Equation (5) has to be solved.\n\nIn our investigation we present a few iterative methods for finding the stabilizing solution to (5). Convergence\n\nproperties of the matrix sequence will be derived. A second iterative method is derived. The\n\nsecond aim of the paper is to provide a short numerically survey on iterative methods for computing the stabilizing solution to the given set of Riccati equations. Results from the numerical comparison are given on a family of numerical examples.\n\nLemma 1. For the map the following identities are valid:\n\ni) (6)\n\nfor any symmetric matrices.\n\nii) (7)\n\nwith\n\nProof. The statements of Lemma 1 are verified by direct manipulations. □\n\nLemma 2. Assume there exist positive definite symmetric matrices with and is the stabilizing solution to\n\nThen\n\ni) if is asymptotically stable for with then;\n\nii) if then the Lyapunov operator is asymptotically stable for.\n\nProof. Assume the index i is fixed. We have . Applying some matrix manipulations we obtain the equation:\n\nThus. The statement 1) is proved.\n\nIn order to prove the statement 2) we derive:\n\n(8)\n\nSince the matrices and are positive definite then the Lyapunov operator is asymptotically stable for because Riccati Equation (8) has the stabilizing positive semidefinte solution.\n\n.\n\nThe lemma is proved.\n\n3. Iterative Methods\n\nIn this section we are proving the some convergence properties of the matrix sequences and defined by iterative loop (4)-(5). We present the main theorem where the convergence properties for matrix sequences are derived.\n\nTheorem 1. Assume there exist symmetric matrices and such that and and, and the Lyapunov operator is asymptotically stable. Then for the matrix sequences defined as the stabilizing solution of (5) satisfy\n\ni) The Lyapunov operator is asymptotically stable;\n\nii);\n\niii) The Lyapunov operator is asymptotically stable where ;\n\niv) for.\n\nProof. The algorithm begins with. Then. The matrix is a solution of the Riccati equation:\n\n(9)\n\nUnder the assumption the Lyapunov operator is asymptotically stable . Thus, is the unique stabilizing solution of the above Riccati equation and .\n\nUsing Lemma 1 1) and the fact that is a solution to (9) we have . In addition, the operator\n\nis asymptotically stable and\n\nThe Lyapunov operator is asymptotically stable. In addition, is a solution to and applying Lemma 1 we obtain:\n\nSince is the stabilizing solution to the latest equation, then the Lyapunov operator is asymptotically stable with\n\nThus, following Lemma 2, 1) we conclude that.\n\nThus, the properties 1), 2), 3) and 4) are true for. We compute.\n\nCombining iteration (5) with equality we construct the following matrix sequences:\n\nwe prove by induction the following for:\n\n(ak): The Lyapunov operator is asymptotically stable,;\n\n(bk):;\n\n(gk): The Lyapunov operator is asymptotically stable where ;\n\n(dk):.\n\nWe have seen the statements (a0), (b0), (g0) and (d0)) are true. We assume the statements (ak), (bk), (gk) and (dk) are true for. We prove the same statements for.\n\nWe know. We compute, and. We have to find as a unique stabilizing solution to (5) with. The matrix is positive semidefinite because is true. It remains to show that is asymptotically stable.\n\nFollowing Lemma 2, 2) the operator is asymptotically stable because . Thus the operator is asymptotically stable. In addition, . Thus the operator is asymptotically stable,. There exists a unique positive semidefinite solution to (5) with. The last fact in combination of the presentation of from Lemma 1, 1) we conclude that and moreover is positive semidefnite. The assertions (ar) and (br) are proved.\n\nWe have to prove the operator is asymptotically stable and . In addition, the operator is asymptotically stable because (ar). Moreover, Thus the (gr) is true for.\n\nFurther on, we have and and thus\n\nis asymptotically stable by Lemma 2, 2) Using again Lemma 2, 1) we conclude. Hence. All statements are proved for.\n\nThe theorem is proved. □\n\nThe problem is to find the stabilizing solution to the general equation\n\n(10)\n\nThe Riccati Iterative Method. We choose and is the stabilizing solution to\n\n(11)\n\nwith Note that the matrix is a positive semidefinite matrix for.\n\nIt is well know that if the matrix pair is stabilizable and the matrix is positive semidefinite, then there exists a semidefinite solution to the “perturbed” Riccati Equation (10).\n\nBased on Riccati iteration (11) we consider the improved modification given by:\n\n(12)\n\nwith\n\nThe Lyapunov Iterative Method. We choose and is the stabilizing solution to\n\n(13)\n\nwith and\n\nWe consider the Lyapunov iteration (13) as a special case of the Lyapunov iteration introduced and investigated by Ivanov . Following the numerical experience in we improve iteration (13) and introduce the improved Lyapunov iteration\n\n(14)\n\nwhere\n\nConvergence properties of the matrix sequence defined by (14) are given with Theorem 2.1 .\n\nFurther on, we consider an alternative iteration process where one matrix sequence is constructed. This sequence converges to the stabilizing solution of the given set of Riccati equations. We are proving that this in-\n\ntroduced iteration is equivalent to the iteration loop (4)-(5). We substitute from (3) in recurrence Equation (5) and after matrix manipulations we obtain for:\n\n(15)\n\nThus, we can construct the matrix sequence with and each subsequent matrix is computed as a unique stabilizing solution to (15). In fact we just proved that the matrix sequence defined by (15) is equivalent to the matrix sequence defined by (4)-(5). In order to apply the iteration (15) we change the term from (15) with.\n\nThe unknown matrix is a solution to the set of continuous-time algebraic Riccati equation with the independent matrix\n\n4. Numerical Simulations\n\nWe have considered two iterative methods for computing the matrix sequence: the Riccati iteration\n\n(15) and the Lyapunov iteration (14). In the begining we remark the LMI approach for finding the stabilizing solution to (5). Following similar investigations we conclude that the optimization problem (for given k)\n\n(16)\n\nhas a solution which is the stabilizing solution to (5).\n\nWe carry out experiments for solving a set of Riccati Equation (1). We construct two matrix sequences and for each example. The first matrix sequence is computed using iterative method (4)-(5). In order to form the second matrix sequence we apply Riccati iteration (15), Lyapunov iteration (14) and LMI approach (16). In addition, we construct a matrix sequence for each example using recurrence Equation (15) for this purpose.\n\nThe matrices are computed in terms of the solutions of N Riccati equations for (15) and N\n\nalgebraic Lyapunov equations for (14) at each step. For this purpose the MATLAB procedure care is applied where the flops are per one iteration. Lyapunov iteration (14) solves N algebraic Riccati equations at each step. The MATLAB procedure lyap is used and the flops are per one iteration. In order to find the symmetric solution to (16) we adapt MATLAB’s software functions of LMI Lab.\n\nOur experiments are executed in MATLAB on a 2.20 GHz Intel(R) Core(TM) i7-4702MQ CPU computer. We use two variables tolR and tol for small positive numbers to control the accuracy of computations. We de-\n\nnote and. The iterations (15) and (14) stop when the inequality is satisfied for some. That is a practical stopping criterion for (15) and (14). The variable It means the maximal number of iterations for which the inequality holds. The last inequality is used as a practical stopping criterion for main iterative process (4)-(5). The tolerance tol controls accuracy of the procedure mincx which is used for numerical solution to (16).\n\nWe consider a family of examples in case for two given values of and. The coefficient real matrices are given as follows: were constructed using the MATLAB notations:\n\nand\n\nand\n\nIn our definitions the functions randn (p, k) and sprand (q, m, 0.3) return a p-by-k matrix of pseudorandom scalar values and a q-by-m sparse matrix respectively (for more information see the MATLAB description). The following transition probability matrix\n\nis applied for all examples.\n\nFor our purpose we have executed hundred examples of each value of m for all tests. Table 1 reports the average number of iterations for the main iterative process “ItM” and the average number of iterations for the second iterative process “ItS” needed for achieving the relative accuracy for all examples of each size. The column “CPU” presents the CPU time for executing the corresponding iterations. Results from experiments are given in Table 1 with for all tests. Results from experiments with the iteration (15) are given in Table 2 with for all tests.\n\n5. Conclusions\n\nWe have studied two iterative processes for finding the stabilizing solution to a set of continuous-time genera-\n\nTable 1. Results from 50 runs for each value of n.\n\nTable 2. Results from 50 runs for each value of n.\n\nlized Riccati Equation (1). We have made numerical experiments for computing this solution and we have compared the numerical results. In fact, it is a numerical survey on iterative methods for computing the stabilizing solution. We have compared the results from the experiments in regard of the number of iterations and CPU time for executing. Our numerical experiments confirm the effectiveness of proposed new method (15).\n\nThe application of all iterative methods shows that they achieve the same accuracy for different number of iterations. The executed examples have demonstrated that the two iterations “(4)-(5) with RI: (15)” and “(4)-(5) with LI: (14)” require very close average numbers of iterations (see the columns “ItS” for all tests). However, the CPU time is different for these iterations. In addition, by comparing iterations based on the solution, the linear matrix Lyapunov equations shows that iteration “(4)-(5) with LI: (14)” is slightly faster than the second iteration (15). This conclusion is indicated by numerical simulations. Based on the experiments, the main conclusion is that the Lyapunov iteration is faster than the Riccati iteration because these methods carry out the same number of iterations.\n\nAcknowledgements\n\nThe present research paper was supported in a part by the EEA Scholarship Programme BG09 Project Grant D03-91 under the European Economic Area Financial Mechanism. This support is greatly appreciated.\n\nCite this paper\n\nIvanG. Ivanov,Ivelin G.Ivanov, (2015) H&#8734 Optimal Control Problems for Jump. Journal of Mathematical Finance,05,337-347. doi: 10.4236/jmf.2015.54029\n\nReferences\n\n1. 1. Lanzon, A., Feng, Y., Anderson, B. and Rotkowitz, M. (2008) Computing the Positive Stabilizing Solution to Algebraic Riccati Equations with an Indefinite Quadratic Term via a Recursive Method. IEEE Transactions on Automatic Control, 53, 2280-2291.\nhttp://dx.doi.org/10.1109/TAC.2008.2006108\n\n2. 2. Dragan, V., Freiling, G., Morozan, T. and Stoica, A.-M. (2008) Iterative Algorithms for Stabilizing Solutions of Game Theoretic Riccati Equations of Stochastic Control. Proceedings of the 18th International Symposium on Mathematical Theory of Networks & Systems, Blacksburg, Virginia, 28 July-1 August 2008, 1-11.\nhttp://scholar.lib.vt.edu/MTNS/Papers/078.pdf\n\n3. 3. Vrabie, D. and Lewis, F. (2011) Adaptive Dynamic Programming for Online Solution of a Zero-Sum Differential Game. Journal of Control Theory and Applications, 9, 353-360.\nhttp://dx.doi.org/10.1007/s11768-011-0166-4\n\n4. 4. Praveen, P. and Bhasin, S. (2013) Online Partially Model-Free Solution of Two-Player Zero Sum Differential Games. 10th IFAC International Symposium on Dynamics and Control of Process Systems, India, 18-20 December 2013, 696-701.\n\n5. 5. Feng, Y.T. and Anderson, B.D.O. (2010) An Iterative Algorithm to Solve State-Perturbed Stochastic Algebraic Riccati Equations in LQ Zero-Sum Games. Systems & Control Letters, 59, 50-56.\nhttp://dx.doi.org/10.1016/j.sysconle.2009.11.006\n\n6. 6. Dragan, V. and Ivanov, I. (2011) Computation of the Stabilizing Solution of Game Theoretic Riccati Equation Arising in Stochastic H Control Problems. Numerical Algorithms, 57, 357-375.\nhttp://dx.doi.org/10.1007/s11075-010-9432-7\n\n7. 7. Hata, H. and Sekine, J. (2013) Risk-Sensitive Asset Management under a Wishart Autoregressive Factor Model. Journal of Mathematical Finance, 3, 222-229.\nhttp://dx.doi.org/10.4236/jmf.2013.31A021\n\n8. 8. Hudgins, D. and Na, J. (2013) H-Optimal Control for Robust Financial Asset and Input Purchasing Decisions. Journal of Mathematical Finance, 3, 335-346.\nhttp://dx.doi.org/10.4236/jmf.2013.33034\n\n9. 9. Pang, W.-K., Ni, Y.-H., Li, X. and Yiu, K.-F. (2014) Continuous-Time Mean-Variance Portfolio Selection with Partial Information. Journal of Mathematical Finance, 4, 353-365.\nhttp://dx.doi.org/10.4236/jmf.2014.45033\n\n10. 10. Dragan, V., Morozan, T. and Stoica, A.M. (2013) Mathematical Methods in Robust Control of Linear Stochastic Systems. Springer, New York.\n\n11. 11. Ivanov, I. (2008) On Some Iterations for Optimal Control of Jump Linear Equations. Nonlinear Analysis Series A: Theory, Methods & Applications, 69, 4012-4024.\n\n12. 12. Rami, M. and Zhou, X. (2000) Linear Matrix Inequalities, Riccati Equations, and Indefinite Stochastic Linear Quadratic Controls. IEEE Transactions on Automatic Control, 45, 1131-1143.\nhttp://dx.doi.org/10.1109/9.863597\n\n13. 13. Ivanov, I. (2012) Accelerated LMI Solvers for the Maximal Solution to a Set of Discrete-Time Algebraic Riccati Equations. Applied Mathematics E-Notes, 12, 228-238." ]
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https://socratic.org/questions/how-do-you-solve-5-6-3m-20#356703
[ "# How do you solve 5*6^(3m)=20?\n\nDec 26, 2016\n\n$m = 0.2579$\n\n#### Explanation:\n\n$5 \\cdot {6}^{3 m} = 20$\n$\\implies {6}^{3 m} = \\frac{20}{5} = 4$\ntake log of both sides:\n$\\log {6}^{3 m} = \\log 4$\n$\\implies 3 m \\log 6 = \\log 4$\n$\\implies 3 m = \\log \\frac{4}{\\log} 6 = 0.7737$\n$\\implies m = \\frac{0.7737}{3} = 0.2579$" ]
[ null ]
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https://webapps.stackexchange.com/questions/136360/conditional-formatting-based-on-another-sheet-tying-a-value-to-a-colour-google
[ "# Conditional Formatting based on another sheet, tying a value to a colour, Google Sheets\n\nDoes anyone know how I'd be able to make a specific value always appear with the same formatting & colour in my sheet, based on another tab in the sheet?\n\nThey're labels for my hobby, I've set it up so that the ref tab goes into each label in order but when I reference a number it won't bring the formatting from the tab named \"DMC no.\" with it, I was hoping someone would be able to help me with this in some way, whether it means conditional formatting on the label sheet or being able to reference a cell and the format being bought with it. Conditional formatting on the label sheet would be preferable, but whatever you can do to help me would be good!\n\nI changed and edited the google sheet to further explain what I want to achieve, with a better explanation at the top of the labels sheet. Thank you\n\n• I don't understand how the DMC tab is relevant, if you give me an example of desired output and your non working solution I can make it work. Nov 17, 2019 at 23:30\n• Welcome. Your goal is unclear and there are many unexplained issues. 1) \"Labels\" and \"Ref\" have 130 values but \"DMC no\" has 456 values over 10 columns and 46 rows. 2) The relationship between values on \"Ref\", \"Labels\" and \"DMC no\" is not explained. 3) \"Labels\" links to Ref! Column B & C (which are empty) are not explained. Please read How do I ask a good question? and then edit your question to clarify the outcome you are trying to achieve. Also please provide an example of a successful outcome. Nov 20, 2019 at 4:43\n• May I try to clarify; please correct me. Use Label 11 as an example. There are three cells: A6, B6 and A7. A6 = `=Ref!A11` with value \"11\". B6 = `=Ref!B11` that returns an image. You want to enter a number in Cell A7. That number will also be a value on \"DMC no\"; each value on \"DMC no\" has a unique fill colour. When you enter the number in Cell A7, you want the fill colour to change to match the equivalent fill colour on \"DMC no\". e.g., you enter \"333\" in cell A7. On \"DMC no\", value \"333\" has a fill colour of hex #6E2E9B; you wish the fill colour of Cell A7 will change to hex#6E2E9B. Nov 21, 2019 at 11:37\n• Hi, yes that is correct. Sorry that I'm not the best at explaining this Nov 24, 2019 at 18:07\n\nYou are trying to update the value AND the background colour of a cell when a certain \"DMC\" number is entered. DMC information is held on a sheet (\"DMC no.\") and consists of cells with given numerical values and specific background colours.\n\nRevising the DMC data format\n\nThere is no function that enables Google Sheets to get the background colour of a given cell, so I propose that the DMC information needs to be recorded in a different format - a 2 Column list. The first column is the DMC value and the second column is the hex colour value associated with that DMC value.\n\nThis function modifies the existing DMC information. I created a new sheet \"DMC_data\" to hold the revised information.\n\n``````function wa13636001() {\n\n// built a DMC value/colour matrix\n\nvar sheetname = \"DMC no.\";\nvar sheet = ss.getSheetByName(sheetname);\n\n// get DMC sheet info\nvar dmcLR = sheet.getLastRow();\nvar dmcLC = sheet.getLastColumn();\n\n// get the Range and Values\nvar dmcRange = sheet.getRange(1, 1, dmcLR, dmcLC);\nvar dmcValues = dmcRange.getValues();\n\n// create termporary array\nvar dmctemparray=[];\n\n// loop rows and columns to build value list\nfor (var i = 0; i<dmcLR;i++){\nfor (k=0;k<dmcLC;k++){\ndmctemparray.push([dmcValues[i][k]])\n}\n}\n\n// get length\nvar rows = dmctemparray.length\n\n// setup target sheet\nvar targetname = \"DMC_data\";\nvar target = ss.getSheetByName(targetname);\n\n// get target range - Column 1 - values\nvar targetRange = target.getRange(1, 1, rows);\n// update values\ntargetRange.setValues(dmctemparray);\n\n// get the background colours\nvar bgColors = dmcRange.getBackgrounds();\n\n// create a temporaryarray for the colours\nvar dmccoloursarray = [];\nfor (var i in bgColors) {\nfor (var j in bgColors[i]) {\ndmccoloursarray.push([bgColors[i][j]]);\n}\n}\n\n// get target range - Column 2 - cdolours\nvar targetRange = target.getRange(1, 2, rows);\n// update colour values\ntargetRange.setValues(dmccoloursarray);\n\n}\n``````\n\nCustom Function - not an option\n\nI wrote a custom function to update the background colour in the target cell (A7) and got an error:\n\n\"You do not have permission to call setBackground\".\n\nI then read Google Apps script - change the background color of a cell with a hex value from another cell and, as they point out, \"Formulas cannot modify cell format\". So it's not feasible to create a function that will do this in real time.\n\nTwo options seemed available:\n\n• a script that can be called from a button which would update any/all DMC values.\n• an `onEdit(e)` script. This is a far more sensible option in the circumstances\n\nonEdit() - a logical option\n\n`onEdit(e)` needs to take advantage of the Event objects.\n\nThe evaluation of edited data is in three parts:\n\n1. `sheetname === labelsname`: ensure that the edit took place on sheet = \"Labels\".\n2. `modrow === 0 && modcol===0`\n\n• DMC Values appear in predictable rows and columns.\n• Rows: the first row is #4, and then every third row thereafter. So the remainder value is predictable.\n• `var modrow = (+row-dmcstartrow)%3;`: this value should be zero; if not then the DMC value has not been edited.\n• Columns: the first column is 1, and then every third column thereafter. Again the remainder value is predictable.\n• `var modcol = (+col-dmcstartcol)%3;`: this value should be zero; if not, then the DMC value has not been edited.\n3. the script then loops through the DMC data looking for a match on the edited value. If a match is found, then the hex background colour is obtained from the adjacent column, and the edited cell is updated\n\n• `range.setBackground(data[nn]);`\n\n`````` function onEdit(e) {\n// wa13636003\n\nvar labelsname = \"Labels\";\nvar labels = ss.getSheetByName(labelsname);\n//Logger.log(JSON.stringify(e)); //DEBUG\n\n// get event objects\nvar range = e.range;\nvar row = range.getRow();\nvar col = range.getColumn();\nvar value = e.value\nvar sheetname = range.getSheet().getSheetName();\n\n// dmc sheet start row/col\nvar dmcstartrow = 4;\nvar dmcstartcol = 1;\n// calculate mod on row and colum\nvar modrow = (+row-dmcstartrow)%3;\nvar modcol = (+col-dmcstartcol)%3;\n//Logger.log(\"DEBUG: modrow:\"+modrow+\", modcol:\"+modcol)\n\n// test if mod for row and col are zero and that the sheet is Labels.\nif (modrow === 0 && modcol===0 && sheetname === labelsname){\n// Logger.log(\"DEBUG: this cell is a match\")\n\n// get DMC data\nvar dmc = ss.getSheetByName(\"DMC_data\");\nvar last=dmc.getLastRow();\nvar data=dmc.getRange(1,1,last,2).getValues();// create an array of data from columns A and B\n\n//loop through dmc data to find the match on the value, and return the colour\nfor(nn=0;nn<data.length;++nn){\nif (data[nn]==value){\n// Logger.log(\"DEBUG: \"+data[nn]+\" is a match for \"+value);\n\n// set the background colour\nrange.setBackground(data[nn]);\n\n// break out rather than cvontinue going through the loop.\nbreak;\n} // if a match in column B is found, break the loop\nelse{\n// Logger.log(\"DEBUG: \"+data[nn]+\" is NOT a match for \"+value)\n}\n}\n}\nelse{\n// Logger.log(\"DEBUG: this cell is NOT a match\")\n}\n\n}\n``````" ]
[ null ]
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https://www.numberempire.com/357079349
[ "Home | Menu | Get Involved | Contact webmaster", null, "", null, "", null, "", null, "", null, "# Number 357079349\n\nthree hundred fifty seven million seventy nine thousand three hundred forty nine\n\n### Properties of the number 357079349\n\n Factorization 11 * 11 * 11 * 11 * 29 * 29 * 29 Divisors 1, 11, 29, 121, 319, 841, 1331, 3509, 9251, 14641, 24389, 38599, 101761, 268279, 424589, 1119371, 2951069, 12313081, 32461759, 357079349 Count of divisors 20 Sum of divisors 406812300 Previous integer 357079348 Next integer 357079350 Is prime? NO Previous prime 357079343 Next prime 357079357 Is a Fibonacci number? NO Is a Bell number? NO Is a Catalan number? NO Is a factorial? NO Is a regular number? NO Is a perfect number? NO Polygonal number (s < 11)? NO Binary 10101010010001001100100110101 Octal 2522114465 Duodecimal 9b703185 Hexadecimal 15489935 Square 127505661482263801 Square root 18896.543308235 Natural logarithm 19.693468581153 Decimal logarithm 8.5527647343298 Sine 0.19116924529377 Cosine -0.98155708935029 Tangent -0.19476120886694\nNumber 357079349 is pronounced three hundred fifty seven million seventy nine thousand three hundred forty nine. Number 357079349 is a composite number. Factors of 357079349 are 11 * 11 * 11 * 11 * 29 * 29 * 29. Number 357079349 has 20 divisors: 1, 11, 29, 121, 319, 841, 1331, 3509, 9251, 14641, 24389, 38599, 101761, 268279, 424589, 1119371, 2951069, 12313081, 32461759, 357079349. Sum of the divisors is 406812300. Number 357079349 is not a Fibonacci number. It is not a Bell number. Number 357079349 is not a Catalan number. Number 357079349 is not a regular number (Hamming number). It is a not factorial of any number. Number 357079349 is a deficient number and therefore is not a perfect number. Binary numeral for number 357079349 is 10101010010001001100100110101. Octal numeral is 2522114465. Duodecimal value is 9b703185. Hexadecimal representation is 15489935. Square of the number 357079349 is 127505661482263801. Square root of the number 357079349 is 18896.543308235. Natural logarithm of 357079349 is 19.693468581153 Decimal logarithm of the number 357079349 is 8.5527647343298 Sine of 357079349 is 0.19116924529377. Cosine of the number 357079349 is -0.98155708935029. Tangent of the number 357079349 is -0.19476120886694\n\n### Number properties\n\nExamples: 3628800, 9876543211, 12586269025" ]
[ null, "https://www.numberempire.com/images/graystar.png", null, "https://www.numberempire.com/images/graystar.png", null, "https://www.numberempire.com/images/graystar.png", null, "https://www.numberempire.com/images/graystar.png", null, "https://www.numberempire.com/images/graystar.png", null ]
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https://programs.programmingoneonone.com/2022/01/hackerrank-lambdas-problem-solution-in-ruby.html
[ "# HackerRank Lambdas problem solution in ruby\n\nIn this HackerRank Lambdas, the problem solution in ruby programming Lambdas is anonymous functions. Lambdas in Ruby are objects of the class Proc. They are useful in most of the situations where you would use a proc. The simplest lambda takes no argument and returns nothing as shown below:\n\nExample:\n\n#Ruby version <= 1.8\n\nlambda { .... }\n\nlambda do\n\n....\n\nend\n\n#Ruby version >= 1.9, \"stabby lambda\" syntax is added\n\n-> { .... }\n\n-> do\n\n....\n\nend\n\nRuby version >= 1.9 can use both lambda and stabby lambda, ->.\n\nLambdas can be used as arguments to higher-order functions. They can also be used to construct the result of a higher-order function that needs to return a function.\n\nYou are given a partially complete code. Your task is to fill in the blanks (______).\n\nThere are 5 variables defined below:\n\n1. square is a lambda that squares an integer.\n2. plus_one is a lambda that increments an integer by 1.\n3. into_2 is a lambda that multiplies an integer by 2.\n4. adder is a lambda that takes two integers and adds them.\n5. values_only is a lambda that takes a hash and returns an array of hash values.\n\n## Problem solution.\n\n```# Write a lambda which takes an integer and square it\nsquare = ->(a) { a * a }\n\n# Write a lambda which takes an integer and increment it by 1\nplus_one = ->(a) { a += 1}\n\n# Write a lambda which takes an integer and multiply it by 2\ninto_2 = ->(a) { a * 2 }\n\n# Write a lambda which takes two integers and adds them\nadder = ->(a,b) { a + b }\n\n# Write a lambda which takes a hash and returns an array of hash values\nvalues_only = ->(a) { a.values }\n\ninput_number_1 = gets.to_i\ninput_number_2 = gets.to_i\ninput_hash = eval(gets)\n\na = square.(input_number_1); b = plus_one.(input_number_2);c = into_2.(input_number_1);\nd = adder.(input_number_1, input_number_2);e = values_only.(input_hash)\n\np a; p b; p c; p d; p e\n```" ]
[ null ]
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https://www.engineersedge.com/excel_calculators/electrical_panelboard_load_calculator_excel_13473.htm
[ "Related Resources: excel calculators\n\n### Electrical Panelboard Load Calculator Excel\n\nExcel Engineering Calculators | Engineering Calculators\n\nDetermine following:\n\nCalculate Voltage / Voltage Difference of Each Phase\nCalculate Unbalanced Load in Neutral Wire.\nCalculate Expected Temperature rise in Each Phase.\nCalculate Load in Each Phase and Outgoing Feeders.\nCalculate Size of Cables for Each Outgoing Feeder.", null, "", null, "" ]
[ null, "https://www.engineersedge.com/engineering/contribute-article.jpg", null, "https://www.engineersedge.com/graphics/spider_trap.gif", null ]
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https://ion.icaew.com/technews/b/weblog/posts/excel-tip-of-the-week-210---switching-bases
[ "Excel Tip of the Week #210 - Switching bases\n\nHello and welcome back to the Excel Tip of the Week!  This week, we have a General User post in which we are going to look at how to convert numbers from one representation system to another.\n\nNon-decimal bases\n\nExcel contains several options for representing non-decimal based numbers.  Excel 2010 and earlier versions can represent and use - to an extent - numbers expressed in binary, octal, and hexadecimal.  Excel 2013 and later can use any base from 2 up to 36.\n\nIt's worth noting that numbers in non-decimal format are treated like text in Excel, and the usual mathematical functions such as SUM can't operate with them.  Compare these two additions of a column of number expressed in decimal vs in hexadecimal:", null, "It's clear that Excel doesn't understand that the text in the right-hand column represents numbers.  If you actually need to calculate data that is stored as e.g. binary numbers, you need to first convert into decimal.  This is of course quite ironic, as to actually do the computation Excel then has to convert back into binary!\n\nFunctions for converting between decimal and other bases\n\nExcel 2010 and earlier include the following suite of functions:\n\n=DEC2BIN(number, places)\n=DEC2OCT(number, places)\n=DEC2HEX(number, places)\n\nNumber is the decimal number, cell, or calculation to be converted.\nPlaces is an optional input that will ensure that the outputted string has a given minimum length - e.g. 37 could be represented as 00100101.\n\n=BIN2DEC(number)\n=OCT2DEC(number)\n=HEX2DEC(number)\n\nHere, the \"number\" is a cell with a text string that represents the number in the chosen base.\n\nYou will also note that you can't e.g. convert binary numbers into hexadecimal without an intermediate step of converting into decimal.\n\nExcel 2013 and later versions have these more flexible functions:\n\n=BASE(number, radix, min length)\n\nBASE uses a decimal number input: DECIMAL uses an appropriate text input for number.\nRadix is the chosen base - an integer between 2 and 36.\nMin length is an optional input that works like the \"places\" inputs for the functions discussed above.\n\nYou still have to work in decimal if you want to perform calculations on non-decimal numbers, and you still have to use decimal as a half-way house if you want to convert from one non-base-10 format to another.\n\nOne more thing\n\nIt's even rarer for it to be useful than the above functions, but Excel does also include functions for converting to and, since Excel 2013, from Roman numerals:\n\n=ROMAN(number)\n=ARABIC(text)\n\nBoth of these work with numbers up to and including 3,999.\n\nThis blog is brought to you by the Excel Community where you can find additional blogs, extended articles and webinar recordings on a variety of Excel related topics. In addition to live training events, Excel Community members have access to a full suite of online training modules from Filtered. There is also an online forum where you can ask questions and share ideas with other community members." ]
[ null, "https://ion.icaew.com/resized-image/__size/320x240/__key/communityserver-blogs-components-weblogfiles/00-00-00-00-05/pastedimage1507634528435v1.png", null ]
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https://randnyevg34.com/a-frequency-distribution-lists-the-______-of-occurrences-of-each-category-ofae-data-while-a-relative-frequency-distribution-lists-the-__________-of-occurrences-of-each-category-of-data/
[ "# A frequency distribution lists the ______ of occurrences of each category of​ data, while a relative frequency distribution lists the __________ of occurrences of each category of data.\n\nHere is the answer for the question – A frequency distribution lists the ______ of occurrences of each category of​ data, while a relative frequency distribution lists the __________ of occurrences of each category of data.. You’ll find the correct answer below" ]
[ null ]
{"ft_lang_label":"__label__en","ft_lang_prob":0.8890024,"math_prob":0.93979436,"size":1208,"snap":"2022-40-2023-06","text_gpt3_token_len":280,"char_repetition_ratio":0.15116279,"word_repetition_ratio":0.365,"special_character_ratio":0.26903972,"punctuation_ratio":0.08675799,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98824245,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-02-05T23:16:06Z\",\"WARC-Record-ID\":\"<urn:uuid:da71a145-0c91-42a0-a0d6-9592fc089001>\",\"Content-Length\":\"72612\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:976e1d40-cce7-4ebd-90b9-8bc131fb8204>\",\"WARC-Concurrent-To\":\"<urn:uuid:d8a12cb2-d345-44b0-893b-ba96b081d4aa>\",\"WARC-IP-Address\":\"104.21.75.114\",\"WARC-Target-URI\":\"https://randnyevg34.com/a-frequency-distribution-lists-the-______-of-occurrences-of-each-category-ofae-data-while-a-relative-frequency-distribution-lists-the-__________-of-occurrences-of-each-category-of-data/\",\"WARC-Payload-Digest\":\"sha1:CUACBMIGHAE5Z7PN22TYPBQNHQCMJS4D\",\"WARC-Block-Digest\":\"sha1:SICGQ7GIRADZJLPWZMA56O4RYXDRLGNK\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-06/CC-MAIN-2023-06_segments_1674764500294.64_warc_CC-MAIN-20230205224620-20230206014620-00342.warc.gz\"}"}
https://help.libreoffice.org/latest/ug/text/sbasic/shared/03080301.html
[ "# Randomize Statement\n\nInitializes the random-number generator used by the Rnd function.\n\n## Syntax:\n\n``````\nRandomize [Number]\n``````\n\n## پارامېتىر\n\nNumber: Any integer value. Used as seed to initialize the random-number generator. Equal seeds result in equal random-number sequences by the Rnd function. If the parameter is omitted, the Randomize statement will be ignored.", null, "Unless a predictable sequence of numbers is desired, there is no need to use the Randomize statement, as the random-number generator will be initialized automatically at first use – it will be seeded using a system-provided random-number generator that produces uniformly-distributed, non-deterministic random numbers. If no such generator is available on the system, the system time will be used as seed.\n\nThe Randomize statement affects BASIC's Rnd function only. Other random-number generators (for example the Calc's RAND() function, etc.) are not affected by it.\n\n## مىسال:\n\n``````\nSub ExampleRandomize\nDim iCount As Integer, iVar As Integer, sText As String\nDim iSpectral(10) As Integer\nRandomize 2^14-1\nFor iCount = 1 To 1000\niVar = Int(10 * Rnd) ' Range from 0 to 9\niSpectral(iVar) = iSpectral(iVar) +1\nNext iCount\nsText = \" | \"\nFor iCount = 0 To 9\nsText = sText & iSpectral(iCount) & \" | \"\nNext iCount\nMsgBox sText,0,\"Spectral Distribution\"\nEnd Sub\n``````" ]
[ null, "https://help.libreoffice.org/latest/ug/text/sbasic/shared/media/icon-themes/res/helpimg/note.svg", null ]
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https://mathematica.stackexchange.com/questions/2011/subplots-with-connector-lines/2024#2024
[ "# Subplots with connector lines\n\nI am looking for advice from people who have more experience in this area on what is the best (simplest, least effort) way to create a graphic like the following:", null, "This is a rough mockup made in a drawing program. There is a central graph, surrounded by smaller ones, each of which is showing some information about a point in the main graph. Those points are connected to the subgraphs with lines.\n\nRequirements:\n\n• Each plot must be able to have their own axes/frame\n\n• Proper alignments of the connector lines (red dashed lines on the mockup)---I have the coordinates of one end in the coordinate system of the central plot, while the other end must point at the smaller plots.\n\n• Consistent font sizes and line widths (i.e. everything must be 8 pt when printed)\n\n• Vector graphics (I'd like to avoid rasterizing to bitmaps)\n\nPossible approaches:\n\n• GraphicsGrid with Epilog (GraphicsGrid seems to be based on Inset.)\n\n• Lots of Insets in a graphic (the main issue is aligning the coordinate system of the central plot with that of the whole graphic)\n\n• Learn to use LevelScheme (I didn't use it for anything serious yet, but when I tried it last time it seemed to have issued with alignment).\n\nWhenever I start doing something like this, and the details must be accurate, lots of small issues tend to come up. I'd like to know which approach is likely to prove the least troublesome.\n\nThe main difficulty was the correct positioning of connector lines. The usual way of including subplots is by using Inset (which is also used by GraphicsGrid). One endpoint of the lines is in the main graphics coordinate system, while the other is in the central subplot coordinate system. Converting between the two is very difficult and depends on the scaling of graphics.\n\nHeike's solution uses FullGraphics to expand the axes/frames of subplots. Then all subplots can be directly included in the main graphic and scaled to size. There will be a single coordinate system to deal with.\n\nChris Degnen's solution uses image processing to align the main graphic coordinate system with the inset coordinate system. It places a red dot at the desired endpoints, rasterizes the graphic, measures the position of the dot, and then uses this information to compose a vector graphic with the connector lines going between these positions. The result is a vector graphic that looks correct only at a certain scale, but can be exported to PDF.\n\nThe other solutions recommend adding the connector lines manually.\n\n• Why not use one Graphicsobject? Then you would not have to fuss around with other coordinate systems. I for one find Inset cumbersome - always seem to spend too much time tweaking there. Feb 19 '12 at 17:38\n• @Yves Because I need separate Frames on each one. I don't know how to do this when using a single Graphics. I agree that Inset is cumbersome, that's exactly why I asked the question. Feb 19 '12 at 17:39\n• If you want framed text you could try Framed [see here]( mathematica.stackexchange.com/questions/1882/…) or something like that. More work if you want a tidy layout... Feb 19 '12 at 17:49\n• @Yves I don't mean that kind of frame, I mean a frame that has tick marks, as in Graphics[{},Frame->True]. Feb 19 '12 at 17:50\n• @Yves I am thinking of making the small plots Insets in the Graphics object of the central plot. It would spare me the nightmare of having to align the Inset coordinate system with the main one. Feb 19 '12 at 18:02\n\nThis solution uses FullGraphics to transform axes and ticks in a plot to lines which allows you to resize and translate the plot while keeping the ticks of the original plot. In raster, main is the main plot, list is the list of sub plots, pts is the list of points in the main plot corresponding to the begin points of the red lines, and {dx, dy} are the gaps between the sub plots and the main plot. The sub plots are placed in clockwise direction starting with the one in the upper right corner. The end plot is such that the plot range of the main plot is {{0, 0}, {1, 1}}.\n\nraster[main_, list_, pts_, {dx_, dy_}] :=\nModule[{fgmain, fglist, prm, prl, scmain, sclist, scpts, lines},\nfgmain = FullGraphics[main];\nfglist = FullGraphics /@ list;\nprm = OptionValue[AbsoluteOptions[main, PlotRange][],\nPlotRange];\nprl = OptionValue[Options[#, PlotRange][], PlotRange] & /@ list;\nscmain =\nTranslate[\nScale[fgmain[], 1/(prm[[All, 2]] - prm[[All, 1]]),\nprm[[All, 1]]], -prm[[All, 1]]];\nscpts = Transpose[{Rescale[pts[[All, 1]], prm[]],\nRescale[pts[[All, 2]], prm[]]}];\nTranslate[\nScale[#, (.5 - {dx, dy}/\n2)/(#2[[All, 2]] - #2[[All, 1]]), #2[[All, 1]]],\n-#2[[All, 1]] + #3] &,\n{fglist[[All, 1]], prl, {{-.5 - dx/2, 1 + dy},\n{0, 1 + dy}, {.5 + dx/2, 1 + dy}, {1 + dx, 1 + dy},\n{1 + dx, .5 + dy/2}, {1 + dx, 0}, {1 + dx, -.5 - dy/2},\n{.5 + dx/2, -.5 - dy/2}, {0, -.5 - dy/2}, {-.5 - dx/2, -.5 -\ndy/2},\n{-.5 - dx/2, 0}, {-.5 - dx/2, .5 + dy/2}}}];\nlines = Transpose[{scpts,\n{{-dx, 1 + dy}, {.25 - dx/4, 1 + dy}, {.75 + dx/4,\n1 + dy}, {1 + dx, 1 + dy},\n{1 + dx, .75 + dy/4}, {1 + dx, .25 - dx/4}, {1 + dx, -dy},\n{.75 + dx/4, -dy}, {.25 - dx/4, -dy}, {-dx, -dy},\n{-dx, .25 - dy/4}, {-dx, .75 + dy/4}}}];\nGraphics[{scmain, sclist, {Red, Dashed, Line[lines]}}]]\n\n\nExample:\n\nlist = MapIndexed[ParametricPlot[#, {x, 0, 2 Pi},\nFrame -> True, Axes -> False,\nPlotStyle -> (ColorData @@ #2)] &,\nTable[{(n - 1) 2 Pi + x, n Sin[x]}, {n, 12}]];\nmain = Show[list, PlotRange -> All];\npts = N[Table[{(n - 1) 2 Pi + x, n Sin[x]}, {n, 12}] /. x -> Pi];\n\nraster[main, list, pts, {.15, .15}]", null, "• I was really hoping you would come up with something. This is excellent. The only potential problem is that the frame tick lengths get scaled down too much, and I can't seem to fix this even when using an explicit tick specification. (But fortunately this is not a problem for my present application as I probably won't need ticks on the small plots, just a rough indication of the range) Feb 19 '12 at 22:52\n• Grrrrrrrrrrreat\n– Rojo\nFeb 22 '12 at 6:37\n\nLooking at your list of requirements, I think learning to use LevelScheme is the best option. It can easily handle all the requirements except the second one (which can of course be done with a hackjob). Here's a simple example reproducing a blank template for your layout:\n\n<<LevelScheme\nFigure[{\nMultipanel[{{0, 1}, {0, 1}}, {4, 4},\nXPanelSizes -> {1, 1, 1, 1}, XGapSizes -> 0.1,\nYPanelSizes -> {1, 1, 1, 1}, YGapSizes -> 0.1,\nFontSize -> 8\n],\n\nTable[If[! MemberQ[{2, 3}, i] || ! MemberQ[{2, 3}, j],\nFigurePanel[{i, j}, PanelLetter -> None,\nFrameTicks -> None],\n## &[]\n], {i, 1, 4}, {j, 1, 4}\n],\n\nFigurePanel[{2, 2}, PanelLetter -> None, FrameTicks -> None,\nPanelAdjustments -> {{0, 1.1}, {1.1, 0}}\n]\n}, ImageSize -> 300 {1, 1}, PlotRange -> {{-0.01, 1.01}, {-0.01, 1.01}}]", null, "### A few things to note:\n\n1. LevelScheme will provide you with (and require you to use) more fine tuning controls than you expect. From your question, it seems like you want these controls, but do note that it takes time to get a feel for it — so if you need it to produce the example figure in a couple of hours, good luck! I don't mean to say that it is difficult or non-intuitive, but it certainly is different from your usual Mathematica way of building up graphics, which you'll need to get used to.\n2. Each panel has its own handle, axis and plot range, making it easy to use each for different kinds of plots. You can also set fonts for each subpanel and style the labels and frame ticks separately for each of the four sides. You needn't worry about where to position each panel, as LS lays it out for you in a neat matrix. Here, I've created the outer ring of panels and then used a single panel ({2,2}) and expanded it to fill the rest of the gap. Note the adjustment lengths (1.1), which should take into account the XGapSizes and YGapSizesused to maintain the correct spacing.\n3. The documentation for LS is fairly decent, and was sufficient for me to get started and exploring. Do give it a good read.\n4. I've had issues in the past with getting some 3D graphics and some rasterized 2D plots to display properly (especially to get it to respect the plot range). However, I think that can be a separate question (on main or chat) if it arises.\n5. I've used a Table to quickly plot the panels, but in your usage, you'll probably do them individually with custom settings for each (unless if they all have the same options).\n6. The connector lines might be a bit tricky since LS uses a local coordinate system for each subpanel. I'll try to come up with a way to do it programmatically (someone else who knows how to can perhaps help me out here), but for now, I suggest using the drawing tools to do that. But do remember that the annotations get wiped out when you regenerate the figure. See this question for details, although I highly doubt that the answer there will work here (haven't tried it).\n• The big problem is indeed point 6: Making sure that the lines end at the correct position in the central plot. Feb 19 '12 at 18:48\n\nHere is a solution you may be able to use. It works by rasterising the graphic. For an image with more than one line you could use more colours.\n\nThis method works by building up a composite graphic with coloured dots (in Red) at the points on the graphs to be connected. The graphic is rasterised and the location of the dots obtained, then the (vector) graphic is recreated with the connecting line included. (Temporarily setting the colours to Black was not actually necessary in this example.)\n\nblock1 :=\nGraphics[{colour1, Rectangle[{0, 0}, {180, 150}]},\nPlotRange -> {{0, 180}, {0, 150}}]\n\nblock2 :=\nGraphics[{colour2, Rectangle[{0, 0}, {180, 150}],\nInset[Plot[Sin[x], {x, 0, 2 Pi}, PlotStyle -> Black,\nEpilog -> {Red, PointSize[0.001], Point[{Pi/2, 1}]},\nImageSize -> 160]]}, PlotRange -> {{0, 180}, {0, 150}}]\n\nmainblock :=\nGraphics[{colour3, Rectangle[{0, 0}, {390, 310}],\nInset[Plot[Sin[x], {x, 0, 2 Pi}, PlotStyle -> Black,\nEpilog -> {Red, PointSize[0.001], Point[{Pi/2, 1}]},\nImageSize -> 370]]}, PlotRange -> {{0, 390}, {0, 310}}]\n\nblocks[done_] := Graphics[{colour4, Rectangle[{0, 0}, {600, 330}],\nInset[block1, {100, 150 + 85 + 10}, {Center, Center}, {180, 150}],\nInset[block2, {100, 85}, {Center, Center}, {180, 150}],\nInset[mainblock, {200 + 390/2, 165}, {Center, Center}, {390, 310}]},\nPlotRange -> {{0, 600}, {0, 330}},\nIf[done, Epilog -> {Red, Thickness[0.001], Line[b]}, ## &[]],\nImageSize -> 600]\n\ncolour1 = colour2 = colour3 = colour4 = Black;\nc = blocks[False];\na = Rasterize[c];\nb = Reverse /@ Position[a[[1, 1]], {255, 0, 0}];\ncolour1 = Cyan;\ncolour2 = Orange;\ncolour3 = Green;\ncolour4 = Yellow;\nblocks[True]", null, "• Very interesting. I almost gave up on an automated solution. Can you please explain in your post how it works, so others can understand it too (without spending too much time)? And please also point out that it does produce a vector graphic in the end (it's not just resizable, but it's exportable at the correct size). Feb 19 '12 at 21:13\n• I wonder why this got downvoted. It is the most practical ( = usable) answer I got so far, even if it's a hack. Feb 19 '12 at 22:20\n• Maybe because of the rasterisation step, although as you mentioned it's the final image that you wanted in vector format. Feb 19 '12 at 22:23\n• Or maybe just a mis-tap on a touchscreen. Don't take it too seriously. Feb 19 '12 at 22:25\n• I have downvoted by mistake in the past by \"mis-tapping\", but it was not I this time! in fact I think that this is a clever (although hacky) approach, so upvoted it.\n– acl\nFeb 19 '12 at 22:52\n\nEdit: I made some minor adjustments to this. I know that this isn't a good solution (see above for those), but I didn't want to leave my attempt in an unfinished state:\n\ngraph1 = Plot[Sin[x], {x, 0, Pi}];\ngraph2 = Plot[Cos[x], {x, 0, Pi}];\ngraphBig = Plot[Tan[x], {x, 0, Pi}];\ngraph4 = Plot[ArcSin[x], {x, 0, Pi}];\n\ngroup =\nGraphicsGrid[\n{{graph1, graph2, graph2, graph1},\n{graph1, graphBig, SpanFromLeft, graph1},\n{graph4, SpanFromAbove, SpanFromBoth, graph1},\n{graph1, graph2, graph2, graph1}}]\n\narrow[tile_] := Block[{} ,\nfromX = 50 + Mod[tile, 4, 1] * 300;\nfromY = -140 + Quotient[tile, 4, 1] * -250;\ntoX = 800; toY = -550;\nArrow[{{fromX, fromY}, {toX, toY}}, {20, 260}]]\n\nShow[{group, Graphics[{\nOpacity[0.3], Blue, Thick,\nTable[arrow[tile],\n{tile, {1, 2, 3, 4, 5, 8, 9, 12, 13, 14, 15, 16}}]}]}]", null, "• The big problem is indeed making sure that coordinates are correct. I can't align with the coordinate system of an Inset` because how Mathematica mixes plot / scaled relative to different things / offset coordinates. Feb 19 '12 at 18:45" ]
[ null, "https://i.stack.imgur.com/xyJXQ.png", null, "https://i.stack.imgur.com/9IJDD.png", null, "https://i.stack.imgur.com/j3Yjt.jpg", null, "https://i.stack.imgur.com/7DrdJ.png", null, "https://i.stack.imgur.com/mJI4q.png", null ]
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https://altairuniversity.com/free-ebook-system-modeling-activate/
[ "### FREE eBook: Learn Basics of System Modeling and Control Systems with Altair Activate\n\nThis book is a basic introduction on “System Modeling and Control”. We assume that the readers are beginners to this subject and hence we have tried to provide the basic theoretical knowledge along with practical exercises. In this book, firstly, we discuss linear time-invariant systems and their analysis, the mathematical representation of the system, followed by solving differential equations representing the system using Laplace transforms and state space representation, we further discuss stability of systems, system modeling techniques and finally, different control systems and theories are discussed. Throughout the book a mass-spring-damper system is used to illustrate the concepts for easy understanding.", null, "" ]
[ null, "https://altairuniversity.com/wp-content/uploads/2019/10/Activate_new.png", null ]
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https://www.omtexclasses.com/2013/08/geometry-question-paper-1-2013.html
[ "SSC BOARD PAPERS IMPORTANT TOPICS COVERED FOR BOARD EXAM 2024\n\n### Geometry Question Paper 1 (2013)\n\nI. Solve any five sub - questions:\n\n1. In  triangle  PQR, line l || side QR. Line l intersects side PQ in the point M and Side PR in the point N. If PM:MQ = 4:7, find PN:PR.\n2. Find the distance between the centres of two circles with diameters 8 cm and 6 cm, if they touch each other internally.\n3. If cosec ϴ   =   5,   then what is the value of cot2 ϴ?\n4. In triangle ABC, D is a point on the side BC such that BD = 5 cm, and DC = 8 cm. What is A(△ABD): A(△ADC).\n5. What is the slope of a line having its inclination 300?\n6. What is the total surface area of a cube with side 6 cm?" ]
[ null ]
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https://rioasmara.com/category/reverse-engineering/page/2/
[ "# x86 Assembly, Function local variable\n\nHi Dear,\n\nHahah .. I am now posting the basic for the function local variable in assembly. Local varible is a variable where only be used just within the function and its operation. Lets see an example C code below\n\nThen we can load the exe to IDA. We can jump straight to the check function that as follow\n\nWe can see the above picture. After the function prologue there is additional assembly code that is sub esp, 10h this code actually creating the stack space as much as 16 bytes or 10h to contain all the variables int = 4 bytes, sinve we have 2 local variable then we need at least 2 x 4 bytes = 8. But since we compile it in debug mode then compiler spare some space to it\n\nWe can see from the above ilustration EBP is the reference point for accessing the variable in the stack.\n\nThe convension is for local variable must be assigned to lower memory address or from the picture above is local variable is at the top of EBP where to access it will be EBP-XX where XX is the number of bytes required.\n\nSo for example we want to access height variable then we need to do EBP+(-8) or accessing width using EBP+(-4)\n\nbut usually if you load to IDA then it will help creating like macro to change the instructio more readble\n\nso to access the variable EBP will be added by the macro then it will use EBP+width or EBP+height\n\nwe can see on the above assembly code that the we are assigning value to heigh and width using below code\n\nI will post the explanation for variable that is passed to the function in the next post\n\n# RE : x86 Function Call\n\nHi Everyone,\n\nToday I am going to explain about function call in assembly. We should understand it because function call is part of the essential things to understand because it has alot of next sub material such as memory stack, return value and also the application flow.\n\nTo make it easier, let start our assembly tutorial by coding an application in C as follow\n\nin the above code that the application will call a function called check where the function does nothing but return 5 to the main function. Let see how it is in the assembly after it is compiled into binary\n\nwe can see that in the above picture that the main fucntion will call _check. A function will always be initilized by at least 2 instructions\n\n.text:00401350 push ebp\n.text:00401351 mov ebp, esp\n\nthe above 2 instructions are called function prologue where it will save the value of old ebp from the previous frame and following instruction is to make the ebp to become equal to esp. why this operation is crucial because ebp will become the base pointer for the stack and as the reference to access local variable and passed variable where esp will always change because it will mark as the top of stack\n\nthe first push ebp is intended to save the main function ebp pointer or caller ebp address.\n\nthe second instruction is mov ebp, esp means it is to initiate the stack frame base address where ebp usually never change after it is initiated and esp will wander as the compiler want it to go\n\nSo the next is when the function finish its execution, the function shall return to the caller. it is called as function epilog\n\n.text:00401358 pop ebp\n.text:00401359 retn\n\nfuncton epilog is the sequence to return to the previous execution in the caller function that stored in retn. the sequece is pop ebp and next to return to address in retn\n\nwe will later talk about the stack in detail in the next post because it is very interesting and crucial to undertand it correctly" ]
[ null ]
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https://www.geeksforgeeks.org/how-to-use-vision-api-from-google-cloud-set-2/
[ "# How to use Vision API from Google Cloud | Set-2\n\nIn the previous article we have seen how to use Facial Detection, Logo Detection, Label Detection and Landmark Detection features of Vision using Vision API, now let’s see few more features like Optical Character Recognition, handwritten text detection, Image Properties Detection etc.\n\n### Text Detection (Optical Character Recognition):\n\nIt detects and extracts text from within an image.\n\n `import` `os ` `import` `io ` `from` `google.cloud ``import` `vision ` `from` `matplotlib ``import` `pyplot as plt ` `from` `matplotlib ``import` `patches as pch ` ` `  `os.environ[``'GOOGLE_APPLICATION_CREDENTIALS'``] ``=`  `     ``os.path.join(os.curdir, ``'credentials.json'``) ` ` `  `client ``=` `vision.ImageAnnotatorClient() ` ` `  `f ``=` `'image_filename.jpg'` `with io.``open``(f, ``'rb'``) as image: ` `    ``content ``=` `image.read() ` `     `  `image ``=` `vision.types.Image(content ``=` `content) ` `response ``=` `client.text_detection(image ``=` `image) ` `texts ``=` `response.text_annotations ` ` `  `a ``=` `plt.imread(f) ` `fig, ax ``=` `plt.subplots(``1``) ` `ax.imshow(a) ` ` `  `for` `text ``in` `texts: ` `    ``print``(text.description) ` `     `  `    ``vertices ``=` `([(vertex.x, vertex.y)  ` `                 ``for` `vertex ``in` `text.bounding_poly.vertices])  ` `   `  `    ``print``(``'Vertices covering text: {}\\n\\n'``.``format``(vertices)) ` `    ``rect ``=` `pch.Rectangle(vertices[``0``], (vertices[``1``][``0``] ``-` `vertices[``0``][``0``]),  ` `                        ``(vertices[``2``][``1``] ``-` `vertices[``0``][``1``]), linewidth ``=` `1``,  ` `                                       ``edgecolor ``=``'r'``, facecolor ``=``'none'``)  ` `    ``ax.add_patch(rect) ` `     `  `plt.show() `\n\nThe above code extracts text from a given image and also prints the coordinates of the vertices of the rectangle containing the text.\nFor example, when the following image is given as input:", null, "Output:\n\n```MY MORNING\nROUTINE\nHow Successful People Start\nEvery Day Inspired\nBENJAMIN SPALL and MICHAEL XANDER\n\nVertices covering text: [(38, 71), (348, 71), (348, 602), (38, 602)]\n\nMY\nVertices covering text: [(46, 71), (108, 82), (100, 128), (38, 117)]\n\nMORNING\nVertices covering text: [(129, 79), (348, 118), (338, 170), (120, 131)]\n\nROUTINE\nVertices covering text: [(96, 135), (292, 170), (283, 219), (87, 184)]\n\nHow\nVertices covering text: [(68, 200), (101, 205), (98, 221), (65, 216)]\n\nSuccessful\nVertices covering text: [(104, 207), (196, 222), (193, 238), (101, 224)]\n\nPeople\nVertices covering text: [(202, 222), (257, 231), (254, 251), (199, 242)]\n\nStart\nVertices covering text: [(265, 232), (311, 239), (309, 255), (262, 248)]\n\nEvery\nVertices covering text: [(112, 238), (155, 246), (152, 265), (109, 258)]\n\nDay\nVertices covering text: [(160, 246), (189, 251), (185, 271), (157, 266)]\n\nInspired\nVertices covering text: [(194, 251), (262, 263), (258, 283), (191, 271)]\n\nBENJAMIN\nVertices covering text: [(57, 534), (118, 546), (115, 561), (54, 549)]\n\nSPALL\nVertices covering text: [(122, 550), (160, 558), (157, 572), (119, 564)]\n\nand\nVertices covering text: [(165, 560), (185, 564), (182, 577), (162, 573)]\n\nMICHAEL\nVertices covering text: [(190, 564), (250, 576), (247, 590), (187, 578)]\n\nXANDER\nVertices covering text: [(254, 575), (311, 587), (308, 602), (251, 591)]```", null, "### Document/handwritten text detection:\n\nThis feature also performs Optical Character Recognition on dense documents, including handwritings.\n\n `import` `os ` `import` `io ` `from` `google.cloud ``import` `vision ` `from` `matplotlib ``import` `pyplot as plt ` ` `  `os.environ[``'GOOGLE_APPLICATION_CREDENTIALS'``] ``=`  `     ``os.path.join(os.curdir, ``'credentials.json'``) ` ` `  `client ``=` `vision.ImageAnnotatorClient() ` ` `  `f ``=` `'image_filename.jpg'` `with io.``open``(f, ``'rb'``) as image: ` `    ``content ``=` `image.read() ` `     `  `image ``=` `vision.types.Image(content ``=` `content) ` `response ``=` `client.document_text_detection(image ``=` `image) ` ` `  `a ``=` `plt.imread(f) ` `plt.imshow(a) ` ` `  `txt ``=` `[] ` `for` `page ``in` `response.full_text_annotation.pages: ` `        ``for` `block ``in` `page.blocks: ` `            ``print``(``'\\nConfidence: {}%\\n'``.``format``(block.confidence ``*` `100``)) ` `            ``for` `paragraph ``in` `block.paragraphs: ` ` `  `                ``for` `word ``in` `paragraph.words: ` `                    ``word_text ``=` `''.join([symbol.text ``for` `symbol ``in` `word.symbols]) ` `                    ``txt.append(word_text) ` `                     `  `print``(txt) `\n\nThe above code identifies and extracts handwritten texts from an image and outputs it.\nFor example, when we give the following image as input:", null, "Output:\n\n```Block confidence: 97.00000286102295%\n\n['Geeks', 'for', 'Geeks', 'A', 'computer', 'science', 'portal', 'for', 'Geeks', '.']```\n\n### Image Properties Detection:\n\nThis feature detects the general attributes of an image, like dominant color.\n\n `import` `os ` `import` `io ` `from` `google.cloud ``import` `vision ` `from` `matplotlib ``import` `pyplot as plt ` ` `  `os.environ[``'GOOGLE_APPLICATION_CREDENTIALS'``] ``=` `      ``os.path.join(os.curdir, ``'credentials.json'``) ` ` `  `client ``=` `vision.ImageAnnotatorClient() ` ` `  `f ``=` `'image_filename.jpeg'` `with io.``open``(f, ``'rb'``) as image: ` `    ``content ``=` `image.read() ` `     `  `image ``=` `vision.types.Image(content ``=` `content) ` ` `  `response ``=` `client.image_properties(image ``=` `image) ` `properties ``=` `response.image_properties_annotation ` ` `  `a ``=` `plt.imread(f) ` `plt.imshow(a) ` ` `  `for` `color ``in` `properties.dominant_colors.colors: ` `        ``print``(``'fraction: {}'``.``format``(color.pixel_fraction)) ` `        ``print``(``'\\tr: {}'``.``format``(color.color.red)) ` `        ``print``(``'\\tg: {}'``.``format``(color.color.green)) ` `        ``print``(``'\\tb: {}'``.``format``(color.color.blue)) `\n\nThe code takes an image as in input and returns its color properties i.e. amount of red, green and blue colors. For example, when the following image is given as input:", null, "Output:\n\n```fraction: 0.036332178860902786\nr: 5.0\ng: 185.0\nb: 6.0\nfraction: 0.03337658569216728\nr: 131.0\ng: 207.0\nb: 13.0\nfraction: 0.029988465830683708\nr: 253.0\ng: 169.0\nb: 5.0\nfraction: 0.0262399073690176\nr: 254.0\ng: 123.0\nb: 5.0\nfraction: 0.03553921729326248\nr: 253.0\ng: 248.0\nb: 12.0\nfraction: 0.02104959636926651\nr: 249.0\ng: 36.0\nb: 6.0\nfraction: 0.024581892415881157\nr: 3.0\ng: 35.0\nb: 188.0\nfraction: 0.03424163907766342\nr: 6.0\ng: 122.0\nb: 200.0\nfraction: 0.027032872661948204\nr: 140.0\ng: 32.0\nb: 185.0\nfraction: 0.029411764815449715\nr: 10.0\ng: 177.0\nb: 217.0```\n\n### Safe Search Properties Detection:\n\nDetects explicit content such as adult content or violent content within an image. This feature uses five categories (“adult”, “spoof”, “medical”, “violence”, and “racy”) and returns the likelihood that each is present in a given image.\n\n `import` `os ` `import` `io ` `from` `google.cloud ``import` `vision ` `from` `matplotlib ``import` `pyplot as plt ` ` `  `os.environ[``'GOOGLE_APPLICATION_CREDENTIALS'``] ``=`  `    ``os.path.join(os.curdir, ``'credentials.json'``) ` ` `  `client ``=` `vision.ImageAnnotatorClient() ` ` `  `f ``=` `'image_filename.jpg'` `with io.``open``(f, ``'rb'``) as image: ` `    ``content ``=` `image.read() ` `     `  `image ``=` `vision.types.Image(content ``=` `content) ` ` `  `a ``=` `plt.imread(f) ` `plt.imshow(a) ` ` `  `response ``=` `client.safe_search_detection(image ``=` `image) ` `safe ``=` `response.safe_search_annotation ` ` `  `likelihood_name ``=` `(``'UNKNOWN'``, ``'VERY_UNLIKELY'``, ``'UNLIKELY'``, ` `                   ``'POSSIBLE'``, ``'LIKELY'``, ``'VERY_LIKELY'``) ` ` `  `print``(``'Adult: {}'``.``format``(likelihood_name[safe.adult])) ` `print``(``'Medical: {}'``.``format``(likelihood_name[safe.medical])) ` `print``(``'Spoofed: {}'``.``format``(likelihood_name[safe.spoof])) ` `print``(``'Violence: {}'``.``format``(likelihood_name[safe.violence])) ` `print``(``'Racy: {}'``.``format``(likelihood_name[safe.racy])) `\n\nGiven an image, the code will determine the probability of it being an image with graphics or adult content.\n\n### Object Detection:\n\nDetects and extracts multiple objects from an image. It localizes multiple objects and returns their coordinates.\n\n `import` `os ` `import` `io ` `from` `google.cloud ``import` `vision ` `from` `matplotlib ``import` `pyplot as plt ` ` `  `os.environ[``'GOOGLE_APPLICATION_CREDENTIALS'``] ``=`  `      ``os.path.join(os.curdir, ``'credentials.json'``) ` ` `  `client ``=` `vision.ImageAnnotatorClient() ` ` `  `f ``=` `'image_filename.jpg'` `with io.``open``(f, ``'rb'``) as image: ` `    ``content ``=` `image.read() ` `     `  `image ``=` `vision.types.Image(content ``=` `content) ` ` `  `a ``=` `plt.imread(f) ` `plt.imshow(a) ` ` `  `response ``=` `client.object_localization(image ``=` `image) ` `objects ``=` `response.localized_object_annotations ` ` `  `print``(``'Number of objects found: '``, ``len``(objects)) ` `for` `object_ ``in` `objects: ` `    ``print``(``'Object: '``, object_.name) ` `    ``print``(``'Confidence: '``, object_.score) `\n\nFor example, when we input the following image:", null, "Output:\n\n```Number of objects found: 1\nObject: Scissors\nConfidence: 0.540185272693634```", null, "" ]
[ null, "https://media.geeksforgeeks.org/wp-content/uploads/20190523083200/book1-207x300.png", null, "https://media.geeksforgeeks.org/wp-content/uploads/20190523083557/book11.png", null, "https://media.geeksforgeeks.org/wp-content/uploads/20190523092432/gfg13-e1558583725996-300x225.jpg", null, "https://media.geeksforgeeks.org/wp-content/uploads/20190523104019/chw-300x225.jpeg", null, "https://media.geeksforgeeks.org/wp-content/uploads/20190523112603/st-300x207.jpg", null, "https://media.geeksforgeeks.org/auth/profile/2dxi9shgwsqtns59wh7l", null ]
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https://ask.truemaths.com/question/form-the-pair-of-linear-equations-in-the-following-problems-and-find-their-solutions-if-they-exist-by-the-elimination-methodii-five-years-ago-nuri-was-thrice-as-old-as-sonu-ten-years-later-nu/
[ "Guru\n\n# Form the pair of linear equations in the following problems, and find their solutions (if they exist) by the elimination method:(ii) Five years ago, Nuri was thrice as old as Sonu. Ten years later, Nuri will be twice as old as Sonu. How old are Nuri and Sonu? Q.2(2)\n\n• 0\n\nThe best question of class 10th math . I want the best solution for this question. The question is very important for class 10th math Form the pair of linear equations in the following problems, and find their solutions (if they exist) by the elimination method:(ii) Five years ago, Nuri was thrice as old as Sonu. Ten years later, Nuri will be twice as old as Sonu. How old are Nuri and Sonu?\n\nShare\n\n1. Let us assume, present age of Nuri is x\n\nAnd present age of Sonu is y.\n\nAccording to the given condition, we can write as;\n\nx – 5 = 3(y – 5)\n\nx – 3y = -10…………………………………..(1)\n\nNow,\n\nx + 10 = 2(y +10)\n\nx – 2y = 10…………………………………….(2)\n\nSubtract eq. 1 from 2, to get,\n\ny = 20 ………………………………………….(3)\n\nSubstituting the value of y in eq.1, we get,\n\nx – 3.20 = -10\n\nx – 60 = -10\n\nx = 50\n\nTherefore,\n\nAge of Nuri is 50 years\n\nAge of Sonu is 20 years.\n\n• 0" ]
[ null ]
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http://www.newtonproject.ox.ac.uk/view/texts/diplomatic/NATP00100
[ "<48v>\n\nNote yt if there happen to bee in any equation either a \\fraction or/ surde quantity or a Mechanichall one, (i:e: wch cannot bee Geometrically computed, but is expressed by ye {illeg} \\area/ or length or gravity or content of some curve line or sollid, &c) To find in what proportion they \\unknowne quantitys/ increase or decrease doe thus. |1| Take two letters ye one (as ξ) to signify yt quantity, ye other (as χ π) its motion of increase or decrease: And making an equation betwixt yt|ye| letter (ξ) & ye quantity signifyed by it, find thereby (by prop 7 if ye Equation \\quantity/ bee Geometricall, or by some other meanes if it bee mechanicall) ye valor of ye other letter (π). |2| Then substituting ye letter (ξ) signifying yt quantity, into its place in ye maine Equation esteeme yt letter (ξ) as an unknowne quantity & performe ye worke of seaventh proposition; & into ye resulting Equation instead of those letters ξ & π substitute theire valors. And soe you have ye Equation required.\n\nExample 1. To find p & q ye motions of x & y whose relation is, $yy=x\\sqrt{aa-xx}$. first suppose $\\xi =\\sqrt{aa-xx}$, Or $\\xi \\xi +xx-aa=0$. & thereby find π ye motion of ξ, viz: (by prop 7) $2\\pi \\xi +2px=0$. Or $\\frac{-px}{\\xi }=\\pi =\\frac{-px}{\\sqrt{aa-xx}}$. Secondly in ye Equation $yy=x\\sqrt{aa-xx}$, writing ξ in stead of $\\sqrt{aa-xx}$, the result is $yy=x\\xi$, whereby find ye relation of ye motions p, q, & π: viz (by prop 7) $2qy=p\\xi +x\\pi$ . In wch Equation instead of ξ & π writing theire valors, ye result is, $2qy=p\\sqrt{aa-xx}\\frac{-pxx}{\\sqrt{aa-xx}}$. wch was required \\to/.\n\n[wch equation multiplyed by $\\sqrt{aa-xx}$, is $2qy\\sqrt{aa-xx}=paa-2pxx$. & in stead of $\\sqrt{aa-xx}$, writing its valor $\\frac{yy}{x}$, it is $\\frac{2{qy}^{3}}{x}=paa-2pxx$. Or $2{qy}^{3}=paax-2pxxx$. Which {sic} Which conclusion will also bee found by taking ye surde quantity out ye given Equation for both parts being squared it is ${y}^{4}=aaxx-{x}^{4}$. & therefore (by prop 7) $4{py}^{3}=2qaax-4{x}^{3}$, as before.]\n\nNote also yt it may bee more convenient $$setting all ye termes on one side of ye Equation)/ to put {illeg} every fractionall, irrationall & mechanicall terme, as also ye summe of ye rationall termes, equall severally to some letter: & then to find ye motions corresponding to each letter of those letters ye sume of wch motions is ye Equation required. Example ye 2d. If ${x}^{3}-ayy+\\frac{{by}^{3}}{a+y}-xx\\sqrt{ay+xx}=0$ is ye relation twixt x & y, whose motions p & q are required. I make ${x}^{3}-ayy=\\tau$; $\\frac{{by}^{3}}{a+y}=\\phi$; & $-xx\\sqrt{ay+xx}=\\xi$. & ye motions of τ, φ, & ξ being called β, γ, & δ; ye first Equation {illeg} ${x}^{3}-ayy=\\tau$, gives (by prop 7) $3pxx-2qay=\\beta$. ye second ${by}^{3}=a\\phi +y\\phi$, gives $3qbyy=a\\gamma +y\\gamma +q\\gamma$; Or $\\frac{3qbyy-q\\phi }{a+y}=\\gamma =\\frac{3qabyy+2qb{y}^{3}}{aa+2ay+yy}$. & ye Third $ay{x}^{4}+{x}^{6}=\\xi \\xi$, gives, ${qax}^{4}+4{payx}^{3}+6{px}^{5}=2\\delta \\xi$; Or $\\frac{-qaxx-4payx-6{px}^{3}}{2\\sqrt{ay+xx}}=\\delta$. Lastly $\\beta +\\gamma +\\delta =3pxx-2qay\\frac{+3qabyy+2{qby}^{3}}{aa+2ay+yy}\\phantom{\\rule{10px}{0ex}}\\frac{-qaxx-4payx-6{px}^{3}}{2\\sqrt{ay+xx}}=0$, is ye Equation sought. Example 3d. If $x=ab\\perp bc=\\sqrt{ax-xx}$. be=y. & ye superficies abc=z", null, "suppose yt ax+xz−y3 $zz+axz-{y}^{4}=0$, is ye relation twixt x, y & z, whose motions are p, q, & r: & yt p & q are desired. The Equation $zz+axz-{y}^{4}=0$ gives (by prop 7), $2rz+rax+paz-4{qy}^{3}=0$. Now drawing dh∥ab⊥ad=1−bh. I consider ye superficies abhd=ab×bh=x×1=x, & abd=z doe increase in ye proportion of bh to bc: yt is, 1∶$\\sqrt{ax-xx}$ ∷p∶r. Or $r=p\\sqrt{ax-xx}$. Which valor of r being substituted into ye Equation $2rz+rax+paz-4{qy}^{3}=0$, gives $\\overline{2pz+pax}×\\sqrt{ax-xx}+paz-4{qy}^{3}=0$. wch was required. How to proceede in other cases (as when there are cube rootes, surde denominators, rootes within rootes (as $\\sqrt{ax+\\sqrt{aa-xx}}$ &c: in the equation) may bee easily bee deduced from what {ha}th bee{n} already said. <49r> October 1666. To resolve Problems by Motion these following Propositions are sufficient 1 If the body a in the Perimeter of ye cirkle or sphære adc", null, "moveth towards its center b, its velocity to each point (b, c, d /d, c, e,$$ of yt circumference is as ye chords (ad, ac, ae) drawne from that body to those points are.\n\n2 If ye s adc, aec, are alike \\viz ad = ec &c/ (though in divers plaines) & 3 bodys", null, "move from the point a uniformely & in equall times ye first to d, the 2d to e, ye 3d to c; Then is the thirds motion compounded of ye \\motion of the/ firsts & second.s motion.\n\n3. All the points of a Body keeping Parallel to it selfe are in equall motion \\velocity/.\n\n4. If a body move onely circularly | angularly about some axis, ye motion \\velocity/ of its points are as their distance from that axis.\n\n5. The motions of all bodys are either parallel or angular, \\Call these two simple motions, parallel & angular/ or mixed of ym both, after ye same manner yt the motion towards c (Prop 2) is compounded of that|os|e towards d & e. And in mixed motion any line may bee taken for ye axis (or if a line or superficies move in plano, any point in yt plane may bee taken for the center) of ye angular motion\n\n6 If ye lines ae, ah being moved doe continually intersect; I describe", null, "ye trapezium abcd, & its diagonall ac: & say yt, ye proportion & position of these five lines ab, ad, ac, cb, cd, being determined by requisite data; shall designe ye proportion & position of these five motions; viz: of ye point a fixed in ye line ae & moveing towards b, of ye point a fixed in ye line ah & moveing towards d; of ye point a intersection point a moveing in ye plaine abcd towards c, (for those five lines are ever in ye same plaine, though ae & ah may chanch onely to touch that plaine in their intersection point a); of ye intersection point a moveing in ye line ae parallely to cb & according to ye order of ye letters c, b; & of ye intersection point a move{ing} in ye line ah parallely to cd & according to ye order of the {lett}ers c, d.\n\nNote yt one of ye lines as ah (fig 3d & 4th) resting, ye points d & a are coincident, & ye point c shall bee in ye line ah if it bee streight (fig 3), otherwise in its tangent (fig 4th)\n\n7. Haveing an equation expressing ye relation twixt two or", null, "more lines x, y, z &c: described in ye same time by two or more moveing bodys A, B, C, &c. the relation of their velocitys may bee thus found p, q, r, &c may bee thus found, viz: Set all ye termes on one side of ye Equation that they become equall to nothing. And first multiply each terme by so many times $\\frac{p}{x}$ as x hath dimensions in yt terme. Secondly multiply each terme by so many times $\\frac{q}{y}$ as y hath dimensions in it. Thirdly (if there be 3 unknowne quantitys) multiply each terme by so many times $\\frac{r}{z}$ as z hath dimensions in yt terme. (& if there bee still more unknowne quantitys doe like to every unknowne quantity). The summe of all these products shall bee equall to nothing. wch Equation gives ye relation of ye velocitys p, q, r, &c Or thus. Translate all ye termes to one side of ye equation, & multiply them being ordered according to x by this progression, {illeg} $\\frac{3p}{x}.\\frac{2p}{x}.\\frac{p}{x}.0.\\frac{-p}{x}.\\frac{-2p}{x}.\\frac{-3p}{x}.\\frac{-4p}{x}.$ &c. or being ordered by ye dimensions of y multiply them by this,: $\\frac{3q}{y}.\\frac{2q}{y}.\\frac{q}{y}.0.\\frac{-q}{y}.\\frac{-2q}{y}.$ &c. The sume of these products shall bee equall to nothing, which equation gives ye relation of their velocitys p, q, &c.\n\n<49v>\n\nOr more Gera Generally ye Equation may bee multiplyed by ye terme of these progressions $\\frac{ap+4bp}{x}.\\frac{ap+3bp}{x}.\\frac{ap+2bp}{x}.\\frac{ap+bp}{x}.\\frac{ap}{x}.\\frac{ap-bp}{x}.\\frac{ap-2bp}{x}$ &c. And $\\frac{aq+2bq}{y}.\\frac{aq+bq}{y}.\\frac{aq}{y}.\\frac{aq-bq}{y}$ &c. (a & b signifying any two numbers whither rationall or irration\\all/\n\n8. If two Bodys A & B, by their velocitys p & q describe ye lines x & y. & an Equation bee given expressing ye relation twixt one of ye lines x, & y ratio $\\frac{q}{p}$ of their motions q & p; To find ye other line y.\n\nCould this bee ever done all problems whatever might bee resolved. But by ye following rules it may bee very often done. |(Note yt ±m & ±n are \\logarithmes or/ numbers signifying ye dimensions of x.)|\n\nffirst get yt valor of $\\frac{q}{p}$. Which if it bee rationall & its Denominator consist of but one terme: Multiply yt valor by x & divide each terme of it by ye logarithme of x in yt terme \\ye quote shall bee ye valor of y/. As if ${ax}^{\\frac{m}{n}}=\\frac{q}{r}$ . Then is $\\frac{na}{m+n}{x}^{\\frac{m+n}{n}}=y$. Or if ${ax}^{\\frac{m}{n}}=\\frac{q}{p}$. Then is $\\frac{na}{n+m}{x}^{\\frac{n+m}{n}}=y$. (Soe if $\\frac{a}{x}={ax}^{\\frac{\\overline{1}}{1}}=\\frac{q}{p}$. Then is $\\frac{a}{0}{x}^{0}=y$. soe yt y is infinite. But note yt in this case x & y increase in ye same proportio\\n/ yt {illeg} numb{illeg}|er|s & thi|thei|r logarithmes doe, y being like a logarithme added to an infinite number $\\frac{a}{0}$. But if x bee diminished \\by c/, as if $\\frac{a}{c+x}$=$\\frac{q}{p}$, y is also diminished by ye infinite number $\\frac{a}{0}{c}^{0}$ & becomes finite like a logarithme of ye number x. & so x being given, y may bee mechanichally found by a Table of logarithmes, as shall bee hereafter showne.)\n\nSecondly. But if ye denominator of ye valor of $\\frac{q}{p}$ consist of more termes yn one, it may bee reduced to such a forme yt ye denominator of each te \\of it/ shall have but one terme, unlesse yt te bee $\\frac{a}{c+x}$: Soe yt y may bee yn found by ye precedent rule. Which reduction is thus performed, viz: 1st, If neither ye numerrator nor \\neither ye numerator nor/ denominator bee \\the denominator bee not a+bx, nor all the \\its/ termes of/ \\its termes not/ multiplyed in all their termes by x \\or xx, or x3, &c/; Increase or diminish x untill ye last terme of ye Denominator vanish. 2dly, And when all ye termes in ye Denominator are multiplyed by x, xx, or x3 &c: Divide ye numerator by ye Denominr (as in Decimall numbers) untill ye Quotient consist of such ts none of wch whose Denominators are so multiplyed by x, x2 & begin ye Division in those termes in wch x is of its fewest dimensions \\unlesse ye Denominator be a+bx /. If yn ye termes in ye Denominator \\valor/ of $\\frac{q}{p}$ bee such as was before required ye valor of y may bee found by ye first te of this Prop: onely it must bee so much diminished or increased as it was before increased or diminished by increasing or diminishing x. But if t{illeg}y \\the/ denominator \\of any terme/ consist of two \\more/ termes yn one, in some of wch x is of more yn {illeg} \\one/ dimension \\unlesse yt terme bee $\\frac{a}{c+x}$ ./ First find those ts of y's valor wch correspond to ye other ts of $\\frac{q}{p}$ its valor. & yn seeke yt of y's valor belon {illeg} by ye preceding reductions \\&c/: seeke ye te of y's valor answering to this te of $\\frac{q}{p}$ its valor.\n\nExample 1st. If $\\frac{xx}{ax+b}=\\frac{q}{p}$. Then by Division tis $\\frac{x}{a}-\\frac{b}{aa}\\frac{+bb}{{a}^{3}x+aab}=\\frac{xx}{ax+b}=\\frac{q}{p}$. (as may appeare by multiplication.) Therefore (by 1st te of this Prop:) tis $\\frac{xx}{2a}\\frac{-bx}{aa}+⃞\\frac{bb}{{a}^{3}x+aab}=y$. ($⃞\\frac{bb}{{a}^{3}x+aab}$ signifys yt te of ye valor of y wch is correspondent to ye terme $\\frac{bb}{{a}^{3}x+aab}$ of ye valor of $\\frac{q}{p}$, wch will may bee found by a Table of logarithmes as may hereafter appeare.)\n\nExample 2d. If $\\frac{{b}^{3}}{-aa+xx}=\\frac{q}{p}$. I suppose x=a+c, & consequently $\\frac{{b}^{3}}{2az+zz}=\\frac{q}{p}$. <50r> =$\\frac{q}{p}$ & by Division, $\\frac{{b}^{3}}{2az}\\frac{-{b}^{3}}{4aa+2az}=\\frac{q}{p}$.\n\nExample 2d. If $\\frac{{x}^{3}}{aa-xx}=\\frac{q}{p}$. I suppose x=z−a. Or $\\frac{{z}^{3}-3azz+3aaz-{a}^{3}}{2az-zz}=\\frac{q}{p}$. And by Division $\\frac{-aa}{2z}-z+a\\frac{+aa}{4a-2z}=\\frac{q}{p}$, (as may appeare by multiplication.) {It} consequently by ye 1st te of ye Prop.) $az-\\frac{zz}{2}-\\square \\frac{aa}{2z}+\\square \\frac{aa}{4a-2z}-aa+\\frac{aa}{2}+\\square \\frac{aa}{2a}-\\square \\frac{aa}{4a-2a}$ $=y=az-\\frac{aa}{2}-\\frac{zz}{2}-\\square \\frac{aa}{2x+2a}+\\square \\frac{aa}{2a-2x}=\\frac{-xx}{2}+\\square \\frac{+aa}{2a-2x}+\\square \\frac{-aa}{2a+2x}=y$. And substituteing x+a into ye place of z, tis $x\\frac{-aa}{2x+2a}\\frac{+aa}{2a-2x}=\\frac{q}{p}=\\frac{{x}^{3}}{aa-xx}$ . And Therefore (by te 1st of Prop 8) $\\frac{xx}{2}+\\square \\frac{-aa}{2x+2a}+\\square \\frac{aa}{2a-2x}=y$.\n\nBut sometimes The last terme of ye Denominator cannot bee taken away, (as if ye Denominr bee aa+xx. or a4+x4 or a4+bbxx+x4 &c) And then it will bee necessary to have in readinesse some examples wth such Denominators to wch all other cases of like denomination may bee by Division reduced. As if $\\frac{cx}{a+bxx}=\\frac{q}{p}$ . Make bxx=z, Then is $\\square \\frac{c}{2ab+2bz}=y$.\n\n$\\frac{cxx}{a+b{x}^{3}}=\\frac{q}{p}$. Make bx3=z, Then is $\\square \\frac{c}{3ba+3bz}=y$.\n\n$\\frac{c{x}^{3}}{a+b{x}^{4}}=\\frac{q}{p}$. Make bx4=z, Then is $\\square \\frac{c}{4ba+4bz}=y$. &c. In Generall if $\\frac{c{x}^{n-1}}{a+b{x}^{n}}=\\frac{q}{p}$. Make bxn=z, & yn is $\\square \\frac{c}{nba+nbz}=y$. Also if $\\frac{c}{a+bxx}=\\frac{q}{p}$. Make $\\sqrt{\\frac{c}{a}}-\\sqrt{\\frac{c}{a+bxx}}=z$ & yn is $\\frac{cx}{a+bxx}+\\square 2\\sqrt{\\frac{2z\\sqrt{ac}}{b}-\\frac{azz}{b}}=y$. That is, if $\\sqrt{\\frac{c}{bx}-\\frac{a}{b}}=\\frac{q}{p}$; I make x=zz, & $\\square 2\\sqrt{\\frac{c}{b}-\\frac{a}{b}zz}=y$. Or if $\\frac{c}{a+bxx}=\\frac{q}{p}$. Make $\\sqrt{\\frac{c}{a+bxx}}=z=CB$, $2\\sqrt{\\frac{c}{b}-\\frac{a}{b}zz}=y=BD$ & =CDV=y", null, "Thirdly If ye valor of $\\frac{q}{p}$ is irrationall being a square{illeg} roote, The simplest cases may bee reduced to these following examples.\n\n1. If $\\frac{c{x}^{n}}{x}\\sqrt{a+b{x}^{n}}=\\frac{q}{p}$. Then $\\frac{2ac+2bc{x}^{n}}{3nb}\\sqrt{a+b{x}^{n}}=y$.\n\n2. If $\\frac{c{x}^{2n}}{x}\\sqrt{a+b{x}^{n}}=\\frac{q}{p}$. Then $\\frac{6bbc{x}^{2n}+2abc{x}^{n}-4aac}{15nbb}\\sqrt{a+b{x}^{n}}=y$\n\n3. If $\\frac{c{x}^{3n}}{x}\\sqrt{a+b{x}^{n}}=\\frac{q}{p}$. Then $\\frac{30{b}^{3}c{x}^{3n}+6abbc{x}^{2n}-8aabc{x}^{n}+16{a}^{3}c}{105n{b}^{3}}\\sqrt{a+b{x}^{n}}=y$.\n\n4. If $\\frac{c{x}^{4n}}{x}\\sqrt{a+b{x}^{n}}=\\frac{q}{p}$. Then $\\frac{210{b}^{4}c{x}^{4n}+30a{b}^{3}c{x}^{3n}-36aabbc{x}^{2n}+48{a}^{3}bc{x}^{n}-96{a}^{4}c}{945n{b}^{4}}\\sqrt{a+b{x}^{n}}=y$.\n\n5. If $\\frac{c{x}^{5n}}{x}\\sqrt{a+b{x}^{n}}=\\frac{q}{p}$. Then $\\frac{1890{b}^{5}c{x}^{5n}+210a{b}^{4}c{x}^{4n}-240aa{b}^{3}c{x}^{3n}+288{a}^{3}bbc{x}^{2n}-384{a}^{4}bc{x}^{n}+768{a}^{5}c}{10395n{b}^{5}}\\sqrt{a+b{x}^{n}}=y$.\n\n1. If $\\frac{c{x}^{n}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$. Then $\\frac{2c}{nb}\\sqrt{a+b{x}^{n}}=y$.\n\n2. If $\\frac{c{x}^{2n}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$. Then $\\frac{2bc{x}^{n}-4ac}{3nbb}\\sqrt{a+b{x}^{n}}=y$.\n\n3. If $\\frac{c{x}^{3n}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$. Then $\\frac{6bbc{x}^{2n}-8abc{x}^{n}+16aac}{15n{b}^{3}}\\sqrt{a+b{x}^{n}}=y$.\n\n4. If $\\frac{c{x}^{4n}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$. Then is $\\frac{30{b}^{3}c{x}^{3n}-36abbc{x}^{2n}+48aabc{x}^{n}-96{a}^{3}c}{105n{b}^{4}}\\sqrt{a+b{x}^{n}}=y$.\n\n5. If $\\frac{c{x}^{5n}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$. Then $\\frac{210{b}^{4}c{x}^{4n}-240a{b}^{3}c{x}^{3n}+288aabbc{x}^{2n}-384{a}^{3}bc{x}^{n}+768{a}^{4}c}{945n{b}^{5}}\\sqrt{a+b{x}^{n}}=y$.\n\n<50v>\n\n1. If $\\overline{\\frac{b}{x}-\\frac{a}{{2x}^{n+1}}}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Then $\\frac{a+b{x}^{n}}{n{x}^{n}}\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n1. If $\\frac{3a{x}^{n}+6b{x}^{2n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Then is $\\frac{2a{x}^{n}+2b{x}^{2n}}{n}\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n2. If $\\frac{-15aa{x}^{n}+48bb{x}^{3n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Then is $\\frac{-10a+12b{x}^{n}}{n}×\\overline{a{x}^{n}+b{x}^{2n}}×\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n3. If $\\frac{105{a}^{3}{x}^{n}+480{b}^{3}{x}^{4n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Then $\\frac{70aa-84ab{x}^{n}+96bb{x}^{2n}}{n}×\\overline{a{x}^{n}+b{x}^{2n}}×\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n4 $\\frac{-945{a}^{4}{x}^{n}+5760{b}^{4}{x}^{5n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. −630a3+\n\n1. If $\\frac{a{x}^{n}+2b{x}^{2n}}{x\\sqrt{a{x}^{n}+b{x}^{2n}}}=\\frac{q}{p}$. Then is $\\frac{2}{n}\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n2. $\\frac{3a{x}^{2n}+4b{x}^{3n}}{x\\sqrt{a{x}^{n}+b{x}^{2n}}}=\\frac{q}{p}$. Then is $\\frac{2{x}^{n}}{n}\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n3. If $\\frac{15aa{x}^{2n}-24bb{x}^{4n}}{x\\sqrt{a{x}^{n}+b{x}^{2n}}}=\\frac{q}{p}$. Then is $\\frac{10a{x}^{n}-8b{x}^{2n}}{n}\\sqrt{a{x}^{n}+b{x}^{2n}}=y$.\n\n4. If $\\frac{105{a}^{3}{x}^{2n}-192{b}^{3}{x}^{5n}}{x\\sqrt{a{x}^{n}+b{x}^{2n}}}=\\frac{q}{p}$. Then $\\frac{70aa{x}^{n}-56ab{x}^{2n}+48bb{x}^{3n}}{n}\\sqrt{a{x}^{n}+b{x}^{2n}}=y$\n\n1|2| If, $\\frac{c}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Make xn=zz. And yn is $\\square \\frac{2c}{n}\\sqrt{a+bzz}=y$.\n\n2|3|. If, $\\frac{c{x}^{n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Make xn=z. Then is $\\square \\frac{c}{n}\\sqrt{az+bzz}=y$.\n\n3|4|. If, $\\frac{c{x}^{2n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Make xn=z. Then, $\\frac{2ac{x}^{n}+2bc{x}^{2n}}{6nb}\\sqrt{a{x}^{n}+b{x}^{2n}}-\\square \\frac{ac}{2nb}\\sqrt{az+bzz}=y$.\n\n4|5|. If $\\frac{c{x}^{3n}}{x}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Make xn=z. yn is $\\frac{12bc{x}^{n}-10ac}{48nbb}×\\overline{a{x}^{n}+b{x}^{2n}}×\\sqrt{a{x}^{n}+b{x}^{2n}}+\\square \\frac{5aac}{16nbb}\\sqrt{az+bzz}=y$.\n\n1 If $\\frac{c}{x{x}^{n}}\\sqrt{a{x}^{n}+b{x}^{2n}}=\\frac{q}{p}$. Make xn=zz. yn is $\\frac{-2ac-2bc{x}^{n}}{na{x}^{n}}\\sqrt{a{x}^{n}+b{x}^{2n}}+\\square \\frac{4bc}{na}\\sqrt{a+bzz}=y$.\n\n1 If $\\frac{c{x}^{n}}{x\\sqrt{a{x}^{n}±b{x}^{2n}}}=\\frac{q}{p}$. Make $\\sqrt{a±b{x}^{n}}=z$. yn is $\\frac{2c}{na}\\sqrt{a{x}^{n}±b{x}^{2n}}\\mp \\square \\frac{4c}{na}\\sqrt{\\frac{zz-a}{±b}}=y$\n\n2 If $\\frac{c{x}^{2n}}{x\\sqrt{a{x}^{n}+b{x}^{2n}}}=\\frac{q}{p}$. Make $\\sqrt{a+b{x}^{n}}=z$. yn is $\\square \\frac{2c}{nb}\\sqrt{\\frac{zz-a}{b}}=y$.\n\n3 If $\\frac{c{x}^{3n}}{x\\sqrt{a{x}^{n}+b{x}^{2n}}}=\\frac{q}{p}$. Make $\\sqrt{a+b{x}^{n}}=z$. yn is $\\frac{c{x}^{n}}{2nb}\\sqrt{a{x}^{n}+b{x}^{2n}}-\\square \\frac{3ac}{2nbb}\\sqrt{\\frac{zz-a}{b}}=y$.\n\nIf $\\frac{c{x}^{n}}{x}\\sqrt{a+b{x}^{n}+d{x}^{2n}}=\\frac{q}{p}$. Make xn=z. Then is $\\square \\frac{c}{n}\\sqrt{a+bz+d{z}^{2}}=y$.\n\nIf $\\frac{c{x}^{n}\\sqrt{d+e{x}^{n}}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$. Make xn=z $\\sqrt{a+b{x}^{n}}=z$. Then is $\\square \\frac{2c\\sqrt{db-ae+ezz}}{nb\\sqrt{b}}=y$\n\nIf $\\frac{-c{x}^{2n}\\sqrt{a+b{x}^{n}}}{x\\sqrt{a-3b{x}^{n}}}=\\frac{q}{p}$. Then is $\\frac{ac+bc{x}^{n}}{6nbb}\\sqrt{aa-2ab{x}^{n}-3bb{x}^{2n}}=y$.\n\nIf $\\frac{c{x}^{3n}\\sqrt{3a+b{x}^{n}}}{x\\sqrt{-a+b{x}^{n}}}=\\frac{q}{p}$. Make $\\overline{\\frac{2a}{b}+{x}^{n}}\\sqrt{a+b{x}^{n}}=z$. Then is $\\square \\frac{2c\\sqrt{bbzz-4{a}^{3}}}{3nbb}=y$.\n\n<52r>\n\n1. $\\frac{a}{b+cz:}$$\\frac{a}{b+cz}$::Note 2. yt$\\sqrt{az+bzz:}$is to$\\sqrt{az+bzz:}$::3.$\\sqrt{a+bzz:}$$\\sqrt{a+bzz}$:: as ye ordinately applyed line bc", null, "in some of ye Conick sections: is to its corresponding superficies abc, ye axis ab being in like manner related to z. But all those areas (& consequently $\\frac{a}{b+cz}$, $\\sqrt{az+bzz}$, $\\sqrt{a+bzz}$) may bee Mechanichally found either by a Table of logarithmes or signes & Tangents. And I have beene therefore hitherto content to suppose ym knowne, as ye basis of most of ye precedent propositions.\n\nNote also yt if ye val|C| Valor of $\\frac{q}{p}$ consists of severall ts each t must bee considered severally, as if: $\\frac{a{x}^{3}-bbxx}{{c}^{4}}=\\frac{q}{p}$ . Then is $\\frac{a{x}^{3}}{{c}^{4}}=\\frac{a{x}^{4}}{4{c}^{4}}$ . & $\\frac{bbxx}{{c}^{4}}=\\frac{bb{x}^{3}}{3{c}^{4}}$ . Therefore $\\frac{a{x}^{3}-bbxx}{{c}^{4}}=\\frac{a{x}^{4}}{4{c}^{4}}-\\frac{bb{x}^{3}}{3{c}^{4}}=y$.\n\nNote also yt of ye valor denominator of ye valor of $\\frac{q}{p}$ consist of both rationall & surde quantitys or of two {illeg} or more surde quantitys First take those surde quantitys out of ye denominator, & yn seeke (y) by ye pe|r|ecedent {illeg} theoremes\n\nBut this eighth Proposition may bee ever thus resolved mechanichally. viz: Seeke ye Valor of $\\frac{q}{p}$ as if you were resolving ye equation in Decimall numbers either by Division or Extraction of rootes or Vieta's Analyticall resolution of powers; This operation may bee continued at pleasure, ye farther ther better. & from each terme ariseing from this operation may bee deduced a te of ye valor of y, (by te ye 1st of this prop).\n\nExample 1. If $\\frac{a}{b+cx}=\\frac{q}{p}$ . Then by division is $\\frac{q}{p}=\\frac{a}{b}-\\frac{acx}{bb}\\frac{+accxx}{{b}^{3}}-\\frac{a{c}^{3}{x}^{3}}{{b}^{4}}+\\frac{a{c}^{4}{x}^{4}}{{b}^{5}}-\\frac{a{c}^{5}{x}^{5}}{{b}^{6}}+\\frac{a{c}^{6}{x}^{6}}{{b}^{7}}$ &c. And consequently $y=\\frac{ax}{b}-\\frac{acxx}{2bb}+\\frac{acc{x}^{3}}{3{b}^{3}}-\\frac{a{x}^{3}{x}^{4}}{4{b}^{4}}+\\frac{a{c}^{4}{x}^{5}}{5{b}^{5}}$ &c.\n\nExample 2. If $\\sqrt{aa-xx}=\\frac{q}{p}$ . Extract ye roote & 'tis $\\frac{q}{p}=a-\\frac{xx}{2a}-\\frac{{x}^{4}}{8{a}^{3}}-\\frac{{x}^{6}}{16{a}^{5}}-\\frac{5{x}^{8}}{128{a}^{7}}-\\frac{7{x}^{10}}{256{a}^{9}}-\\frac{21{x}^{12}}{1024{a}^{11}}$ &c (as may appeare by squareing both ts). Therefore (by 1st te of Prop 8) $y=ax-\\frac{{x}^{3}}{6a}-\\frac{{x}^{5}}{40{a}^{3}}-\\frac{{x}^{7}}{112{a}^{5}}-\\frac{5{x}^{9}}{1152{a}^{7}}-\\frac{7{x}^{11}}{2816{a}^{9}}$ &c.\n\nExample 3. If $\\frac{{q}^{3}}{{p}^{3}}\\ast -ax\\frac{q}{p}-{x}^{3}=0$\n\n<52v>\n\nBut ye Demonstracons of hath beene said must not bee wholly omitted.\n\nProp 7 Demonstrated.", null, "Lemma. If two bodys A, B, move uniformely ye oneother from ab to c, d, e, f,g, h, k, l, &c: in ye same time. Then are ye lines ac,bg, & cd,gh, & de,hk, & ef,kl, &c: as their velocitys p.q. And though they move not uniformely yet{illeg} are ye infinitely little lines wch each moment they describe, as their velocitys wch they have while they describe ym. As if ye body A wth ye velocity p describe ye infinitely little line \\(cd=)/p×o in one moment, in yt moment ye body B wth ye velocity q, will describe ye line \\(gh=)/q×o. For p:q::po:qo. Soe yt if ye described lines bee (ac=)x, & (bg=)y, in one moment, they will bee (ad=)x+po, & (bh=)y+qo in ye next.\n\nDemonstr: Now if ye equation expressing ye relation twixt ye lines x & y bee x3−abx+a3−dyy=0. I may substitu{illeg}|t|e x+po & y+qo into ye place of x & y; because (by ye lemma) they as well as x & y, doe signify ye lines described by ye bodys A & B. By doeing so there results x3+3poxx+3ppoox+p3o3−dyy−2dqoy−dqqoo=0−abx−abpo+a3. But x3−abx+a3−dyy=0 (by supp). Therefore there remaines onely 3p{illeg}|o|xx+3ppoox+p3o3−abpo−2dqoy−dqqoo=0. Or dividing it by o tis 3px2+3ppox+p3oo−abp−2dqy−dqqo=0. Also those termes are infinitely little in wch o is yn those in wch tis not. Therefore b|o|mitting them there rests 3pxx−abp−2dqy=0. The like may bee done in all other equations.\n\nHence I observe. First yt those termes ever vanish in wch o is not \\are not multiplyed by o/, they being ye propounded equation. Secondly those termes also vanish in wch o is of more yn one dimension, because they are infinitely lesse yn those in wch o is but of one dimension. Thirdly ye rem still remaining termes, being divided by o will have yt forme wch, by ye 1st rule in Prop 7th, they should have (as may tly appeare by Mr Oughtreds ye second termes of Mr Oughtreds latter Analiticall table).\n\nAfter ye sàme manner may this \\7th/ Prop: bee demonstrn: there being 3 or more unknowne quantitys (x, \\y, z, &c/\n\nProp 8th is ye Converse of this 7th Prop. & may bee therefore Ab Analytically demonstrar|t|ed by it.\n\nProp 1st Demonstrated. If some body A move in ye \\right/ line", null, "gafc from g towards c. From any point d draw df⊥ac. & call, df=a. fg=x, dg=y. Then is aa+xx−yy=0. Now by Prop 7th, may ye proportion of (p) ye velocity of yt body towards f; to (q) e|i|ts velocity towards d bee found viz 2xp−2yq=0. Or x∶y∷q∶p. That is gf∶gd∷ its velocity to d: its velocity towards f or c. & {illeg} when ye body A is at a, yt is when ye points g & a are coincident then is ac∶ad∷ad∶af∷ velocity to c∶ velocity to d.\n\nProp 2d, Demonstrated.     From ye points d & e draw df⊥ac⊥ge.", null, "And let ye firsts bodys velocity (it moveing to d) bee called ad, ye seconds to e bee ae, & ye 3ds toward c bee ac. Then shall ye firsts velocity towards c bee af (by Prop 1): |&| The seconds towards c is ag, (prop 1). but af af=gc ({illeg}|for| adcsimilis/=\\aec, & adf {illeg}=gec. by sup). Therefore ac=ag+gc =ag+af. That is ye velocity of ye third body towards c is compo equall to ye \\summ of the/ velocitys of ye first & second body towards c.\n\n<53v>\n\nThe former Theorems Applyed to Resolving of Problems.\n\nProb. 1. To draw Tangents to crooked lines.\n\nSeeke (by prop 7th; or 3d, 4th & 2d, &c) ye motions of those streight lines to wch ye crooked line is cheifely referred, & wth what velocity they increase or decrease: & they shall give (by prop 6t, or 1st or 2d) ye motion of ye point describing ye crooked line; wch motion is in its tangent.\n\n|Tangents to Geometricall lines.|\n\nExample 1. If ye crooked line fac is described by ye", null, "intersection of two lines cb & dc ye one \\ye one/ moveing parallely, ye one viz: cb∥ad, & insisting upon ab, ye other \\&/ dc∥ab; & insisting soe yt if ab=x, & bc=y=ad, Their relation is x4−3y+10ax3+ayxx−2y3x+a4−y4=0. To draw ye tangent r|h|cr; I call p ye velocity of cb yt is ye velocity of ye increase of ab & q ye velocity of dc, yt is of ye increasing of {illeg} ad or cb. And so I have (by Prop 7) this Equation 4px3−9p{illeg}y{illeg}+3opa+{illeg}xx+2payx−2py3−3qx3+qaxx−6qyyx−4qy3=0. Now because ye crooked line fac\\{illeg}/ is described by ye intersection point of ye lines dc & cb, I consider yt ye point c fixed in ye line cb moves towards e parallely to ab (for so doth ye line cb (by supp:) & consequently all its points): also ye point c fixed in ye line dc moves towards g parallely to ad (by sup): therefore I draw ce∥ab & cg∥ad, makeing {yn} |&| in such proportions as ye motions they designe \\& so draw er∥cb, & gr∥dc, & ye diagonall cr,/ (by Prop 6), yt is, if ye velocity of ye line cb, (yt is ye celerity of ye increasing of ab, or dc; or ye velocity of ye point c from d) bee called p, & ye velocity of ye line cd bee called q; I make ce∶gc∷p∶q(∷ce∶er∷hb∶cb.) \\& ye point c shall move in the diagonall line cr (by prop 6) wch is therefore the required tangent/ Now ye relation of p & q may bee found by ye foregoing Equation (p signifying ye increase of x, & q of y) to bee 4px3−9pyxx+30paxx+2payx−2py3−3qx3+qaxx−6qyyx−4qy3=0. |by Prop 7| And therefore $hb=\\frac{py}{q}=\\frac{3y{x}^{3}-ayxx+6{y}^{3}x+4{y}^{4}}{4{x}^{3}-9yxx+30axx+2ayx-2{y}^{3}}$. wch determines ye tangent hc\n\nHence may bee observed this Generall Theorem for Drawing Tangnts to crooked lines thus referred to streight ones; yt is, to such lines in wch y=bc is ordinately{sic} applyed to x=ab at any given angle abc. viz: Multiply the termes of ye Equation ordered according to ye dimensions of y, by any Arimeticall {sic} progressiō wch product shall bee ye Numerator: Againe change ye signes of ye Equation & ordering it according to x, multiply ye termes by any Arithmeticall progression & ye product divided by x shall bee ye Denominator of ye valor of (hb, yt is, of) x produced from y to ye tangent hc.\n\nAs if $rx-\\frac{rxx}{q}=yy$ . 2.1.0.Then firstyy$+\\frac{r}{q}xx$=0−rx0.-1.-2., produceth 2yy, \\or, 2rx−2$\\frac{r}{q}$xx./ Secondly 2.1.0.Secondly$\\frac{-r}{q}xx$+rx−yy produceth $rx-\\frac{2r}{q}xx$ . Therefore $\\frac{2yy}{r-\\frac{2r}{q}x}=bh$ . Or else $\\frac{2rx-\\frac{2r}{q}xx}{r-\\frac{2r}{q}x}=bh=\\frac{2qrx-2rxx}{qr-2rx}$ .\n\nExample 2. If ye crooked line chm bee describe by", null, "ye intersection of two lines ac, bc circulating about their centers a & b, soe yt if ac=x, & bc=y; their relation is x3−abx+cyy=0. To draw ye tangent ec I consider yt ye point c moves to fixed in ye line bc moves towards f in ye line cf⊥bc (for ye tangnt to a circle is perpendicular to its radius). also ye point c fixed in ye line {illeg}|a|c moves towards {illeg}|d| in ye line cd⊥ac & from those lines c{illeg}|d| & c{illeg}|f| &|I| draw two others de∥cg & e{illeg}|f|∥bc wch must bee in such proportion one to another as ye motions represented by ym (prop 6), yt is (prop 6) as ye <54r> as ye {sic} motions{sic} of ye intersection point c moveing in ye lines ca & cb", null, "to or from ye centers a & b; yt is, as ye velocity of ye increase or decrease of ca=cx & cb={yn} (ye celerity of ye increase or decrease of x being called p, & of y being q), de∶ef∷p∶q. Then shall ye diagonall ce bee ye required tangent. Or wch is ye same, (for ecn|g|=ecd, & ecf=ecg\\n/,) I produce ac & bc to g & n, so yt cg∶cn∷p∶q. & yn draw n{e} ne⊥bn, & ge⊥n|a|g; & ye tane|g|ent diagonall |ce| to their intersection point e. Now ye relation of p & q may bee found by ye given Equation to bee, 3pxx−pab+2qcy=0 (by prop 7) Or 2cy∶ab−3xx∷p∶q∷cg∶cn, wchdetermins ye tangent ce.\n\nBut note yt if p, or q be negative cg or cn must bee drawn from c towards a or b, but from a or b if affirmative.\n\nHence tis easy to pronounce a s|T|heorems for Tangents in such like cases & ye like may bee done in all other cases however Geometricall lines bee referred to streight ones.\n\nTangents to Mechanichall lines\n\nExample ye 3d. If ye Quadratrix kbf is described by ye", null, "intersection \\(b)/ of ye two lines {illeg}|hb| & ap, ye one hp∥ma moving uniformly from k to a, whilest ye other ap circulates from k to m about ye center a. I d|D|raw ye circle gbl wth ye Rad. ab; & make ab⊥bd=bf bf= bl=bd⊥ab∥de; & to ye intersection point e of ye lines am & ed draw yt tan eb e{illeg} wch shall touch ye Quadratrix in b. For suppose ye motion of ye point p fixed in ye line ap, {illeg} \\towards m/ to bee pm, yn ye motion of ye point b fixed in ye line ab, \\towards d/ is bl\\=bd,/ (prop 4), & ye motion of ye line bh towards ca, & therefore of ye point b fixed in it towards c (prop 3) is ha=bc (by supp): Also ce∥bh & ed∥ap (sup). Therefore (by Prop 6) is ye diagonall {illeg} eb ye motion of ye intersection point b of those two lines ap & hb, moves in ye diagonall eb{illeg}, & consequently eb toucheth ye Quadratrix in b.\n\nExample 4th\n\n<54v>\n\nProb 2d. To find ye quantity of crookednesse of lines.\n\nLemma. The crookednesse of \\equall parts of/ circles are as their diameters reciprocally. For the crookednesse of a whole circle (acdea, bfghmb) amounts to 4 right angles. Therefore there is not more crookednesse in one whole circle acdea yn in another", null, "bfghmb. Suppose ye perimeter acde=bfgh. Then tis, \\ar∶br∷/ bfgh=acde∶bfghmb∷ crookednesse of bfgh∶crookednesse of bfghmb=crookednesse of acdea.\n\nLemma 2. That point of a Crooked Line's Perpendicular wch is in least motion is ye center required of ye circle of equall /whose\\ crookednesse wth ye given is required.\n\nResolution. This may bee done by drawing perpendiculars to 2 curved lines described by ye motion of any two points fixed in ye Tangent, wch two perpendiculars shall intersect in ye center of a Circle whose crookednesse was{illeg} required. One of those curve lines & it perpendiculars may bee ye given crooked line & ye perpendicular to it at its given point.\n\nBut if y bee ordinately applyed to x at right angles ye best way is\n\nResolution. \\Find/ That point of \\fixed in/ ye crooked line's perpendicular wch is |yn| in least motion, \\for it/ is ye center of a circle wch passing through{illeg} ye given point is of equall crookednesse wth ye line at yt given point. To find wch point I observe yt Now, since ye crooked line's tangent & perpendicular &c: (at yt moment) circulate about yt center; I observe, 1st yt every point fixed in ye Tangnt or Perpendicular, or whose position to ym is {illeg} determined, doth describe a curve line to wch ye right line drawne from yt center is perpendicular, & is also ye radius of a circle of equall crookedness wth it: 2dly yt ye motion of every such point is as its distance from yt center; & so are ye motions of ye intersection point, in wch any radius drawn from yt center intersects two parallel |lines.|\n\nExample 1. If cb=y is ordinately applyed to ab=x", null, "at a right angle abc, nc being tangent & mc perpendicular to ye curve line ac: I draw seeke ye motion of two points c & d fixed in ye perpendicular cd; or (wch is better & to ye same purpose) I draw cg∥ab, & seeke ye motions of ye two \\intersection/ points c & d in wch ye perpendicular cd intersects those \\fixed/ lines cfg, & abdk: & yn draw cg & dk in such proportion as those motions are, & ye line{sic} gkm drawn by their ends shall intersect ye perpendicular cd in ye required center m: mc being ye radius of a circle of equall crookednesse wth ye curve line ac at ye point c. Now, Making cegfe= & like ncdbc, suppose ye motion of ye line cb & consequently of ye points c & b fixed in it & moveing towards f f & k, to bee p=nb=cf: Then is ce=cn ye motion of ye point c in wch ye lines ne & bc intersect, yt is \\bc intersects ye tangent ne/ (by Prop 6), yt is of ye point c in|fix|e{illeg}|d| in ye perpendicular cd, & moveing in ye tangent ne: & therefore cg=nd={sic}p+bd(=p+v if bd=v), is ye motion of ye intersection point c towards g in wch point ye perp: cd intersects cg \\(by Prop 6)/. If also ye motion of ye intersection point d from ye point b {illeg} (yt is ye velocity of ye increase of v) bee called r, yn is dk=nb+r=p+r soe yt, cg−dk∶cd∷cg∶cm; yt is, $v-r:cd=\\sqrt{yy+vv}\\colon\\colon p+v:cm=\\frac{\\overline{p+v}×\\sqrt{yy+vv}}{v-r}$. Also $v-:y\\colon\\colon p+v:ck=\\frac{py+vy}{v-r}$. Lastly {illeg} ye motion of ye point c from b, (yt is ye velocity wth wch y=cb increaseth) will bee q=cb=y.\n\nAs if ye nature of ye crooked line bee {illeg} x3−axy+ayy=0. Then is $nb=\\frac{axy-2ayy}{3xx-ay}=p$ (by examp: 1. Prob: 1.), & $\\frac{3xxy-ayy}{ax-2ay}=v=bd$ (for nb∶bc∷bc∶bd) Soe that 3xxy−ayy+\\/axv+2b|a|yv=0. & therefore (by Prop 7) 6pxy−pavqay\\2/qay+3qxx+2qb|a|v−rax+\\2/rb|a|y/=0\\ <55r> & substituting ye $\\frac{axy-2ayy}{3xx-ay}$, & $\\frac{3xxy-ayy}{ax-2ay}$, & y, into ye places of p, v, & q in ye this equation The product will bee $\\frac{6axxyy-12ax{y}^{3}}{3xx-ay}-3ayy+3yxx\\frac{+6xxyy-2a{y}^{3}}{x-2y}-rax+2ray=0$. Or 6aax3yy $\\frac{9y{x}^{5}-6ayy{x}^{3}-12a{y}^{3}xx+24a{y}^{4}x+3aa{y}^{3}x-4{a}^{2}{y}^{4}}{3a{x}^{4}-12ay{x}^{3}-{a}^{2}yxx+12ayyxx+4{a}^{2}yyx-4{a}^{2}{y}^{3}}=r$. And therefore $\\frac{-18yy{x}^{4}+24a{y}^{3}xx-24a{y}^{4}x-2aa{y}^{3}x+2aa{y}^{4}}{3a{x}^{4}-12ay{x}^{3}-aayxx+12ayyxx+4aayyx-4aa{y}^{3}}=v-r=\\frac{2aa{y}^{4}-2aa{y}^{3}x-24a{y}^{4}x+24a{y}^{3}xx-18yy{x}^{4}}{3{x}^{3}-6yxx-ayx+2ayyinax-2ay}$. Also $p+v=\\frac{axy-2ayy}{3xx-ay}+\\frac{3xxy-ayy}{ax-2ay}=\\frac{9{x}^{4}y-6axxyy+5aa{y}^{3}-4aaxyy+aaxxy}{3xx-ay×ax-2ay}$. Soe yt $ck=\\frac{py+vy}{v-r}=\\frac{9{x}^{4}y-6axxyy+5aa{y}^{3}-4aaxyy+aaxxyin3{x}^{3}-6xxy-axy+2ayy}{2aa{y}^{3}-2aaxyy-24ax{y}^{3}+24axxyy-18{x}^{4}yin3xx-ay}$. That is $ck=\\frac{9{x}^{5}-6a{x}^{3}y+aa{x}^{3}-6aaxxy+13aaxyy+12axxyy-10aa{y}^{3}-18{x}^{4}y}{2aayy-2aaxy-24axyy+24axxy-18{x}^{4}}$. |Which Equation gives ye point k & consequently ye point m. for km∥abk.|\n\nBut in such cases where y is ordinately applyed to x at right angles, From ye consideration of ye Equation $\\frac{py+vy}{v-r}=ck$ ; Or rather $\\frac{py+vy}{r-v}=ck$ : may ye following Theoreme bee pronoundced. To wch purpose let X signify {illeg}|t|he given Equation, yt is, all ye algebraicall termes (expressing ye nature of ye given line) considered as equall to nothing & not some of ym to others. Let X· signify those termes multiplyed by ordered according to ye dimensions of x & yn multiplyed by any arithmeticall progressiō Let X· signify ye {illeg}|tho|se termes ordered according to ye dimensions of y & yn multiplyed by any Arithmeticall progression. Let :X signify those termes ordered by x & |yn| multiplyed by any two arithmetia|c|all progressions one of ym being greater yn ye other by a terme. Let X: signify those termes ordered by y & yn multiplied by any two Arith: Progr: one of ym being greater yn ye other \\differing/ by a terme. Let ·X· signify those termes ordered according to x, & yn multiplyed by ye greater of ye progressions wch multiplyed :X; & yn ordered by y & multiplyed by ye greater progression wch multiplyed X:. Then \\(observing yt all these progressions have the same difference & proceede ye same way in respect of ye dimension or {sic} x & y)/ will ye 3 Theorems bee\n\n1st. $\\frac{·X·XX·yy+X·X·X·xx}{-·X·XX:y+2·XX··X·y-X·X·:Xy}=ck=\\frac{·X·Xyy+X·X·xx}{-\\frac{·X·XX:y}{X·}+2·X·X·y-X·:Xy}$ .\n\n2d. $\\frac{·X·X·Xyy+·XX·X·xx}{-·X·XX:x+2·XX··X·x-X·X·:Xx}=km=bl=\\frac{·X·Xyy+X·X·xx}{-·XX:x+2X··X·x-\\frac{X·X·:Xx}{·X}}$.\n\n3d. $\\frac{·X·Xyy+X·X·xxin\\sqrt{·X·Xyy+X·X·xx}}{-·X·XX:yx+2·XX··X·yx-X·X·:Xyx}=cm=$ {illeg}radio circuli æqualis curvitatis cum curva ac in puncto c.\n\nAs if ye line bee x3−axy+ayy=0. Then is ·X=3x3−axy. X·=−axy+2ayy. :X=6x3=3×2.1×0.0 x−1. :X=6x3=x3axy+ayy. 0x−1.1×0.2×1.X:=2ayy=x3axy+ayy & 3×0.1×1.0×2.·X·=−axy=x3axy+ayy. Which valors of ·X, X· &c being substitu{illeg}|te|d into their places in ye first rule, ye result is; $\\frac{9{x}^{6}yy-6a{x}^{4}{y}^{3}+5aaxx{y}^{4}+aa{x}^{4}yy-4aa{x}^{3}{y}^{3}}{\\frac{-18a{x}^{6}{y}^{3}+12aa{x}^{4}{y}^{4}-2{a}^{3}xx{y}^{5}}{2ayy-axy}+2aaxx{y}^{3}-12a{x}^{3}{y}^{3}}=ck$ . Which being conveniently reduced is\n$\\frac{9{x}^{5}-6a{x}^{3}y+aa{x}^{3}-6aaxxy+13aaxyy+12axxyy-10aa{y}^{3}-18{x}^{4}y}{18{x}^{4}-24axxy+24axyy+2aaxy-aayy}=ck$ . As was found before. <55v> $ck=\\frac{1}{2}a+3y-\\frac{3ay}{2x}\\frac{+ay-3xx}{2a-6x}$ .\n\nOr suppose ye line is a Conick section whose nature $rx+\\frac{rxx}{q}=yy$ . Then is ·X=rx+$\\frac{2r}{q}{x}^{2}$ 210 =rx$\\frac{r}{q}$ $\\frac{r}{q}$ xx+rxyy . 0312 X·=−2yy=$\\frac{r}{q}$ xx+rxyyy . 2×1.1×0.0x−1. :X=$\\frac{2r}{q}$xx=$\\frac{r}{q}$ xx+rxyy . 0x−1.0x−1.1×0.2×1. X:=−2yy=$\\frac{r}{q}$ xx+rxyy . 2×01×00×2 ·X·=0=$\\frac{r}{q}$ xx+rxyy . Which valors of ·X, ·X, :X, &c being substituted into their places in ye first Theoreme, give $\\frac{rrxxyy+4\\frac{rr}{q}{x}^{3}yy+\\frac{4rr}{qq}{x}^{4}yy+4xx{y}^{4}}{-rrxxy-\\frac{4rr}{q}{x}^{3}y-\\frac{4rr}{qq}{x}^{4}y+\\frac{4r}{q}xx{y}^{3}}=ck=\\frac{qqrry+4qrrxy+4rrxxy+4qq{y}^{3}}{4qryy-qqrr-4qrrx-4rrxx}$ . Or (since 4qryy−4qrrx−4rrxx=0) tis, $-ck=y+\\frac{4xy}{q}+\\frac{4xxy}{qq}+\\frac{4{y}^{3}}{rr}=y+\\frac{4{y}^{3}}{qr}+\\frac{4{y}^{3}}{rr}=y+\\frac{4r{y}^{3}+4q{y}^{3}}{qrr}$ . So by ye second Theoreme tis $\\frac{rrxxyy+\\frac{4r}{q}xx{y}^{4}+4xx{y}^{4}}{2r{x}^{3}yy+\\frac{4r}{q}{x}^{3}yy\\frac{-\\frac{8r}{q}{y}^{4}{x}^{3}}{rx+\\frac{2r}{q}xx}}=km=bl=\\frac{r}{2}+\\frac{2yy}{q}+\\frac{2yy}{r}+\\frac{rx}{q}+\\frac{4xyy}{qr}+\\frac{4xyy}{qq}$ . Or $bl=\\frac{r}{2}$ +$\\frac{3rx}{q}$ +2x+$\\frac{3rx}{q}+\\frac{6xx}{q}+\\frac{6rxx}{qq}+\\frac{4{x}^{3}}{qq}+\\frac{4r{x}^{3}}{{q}^{3}}$ . And so by ye 3d Theoreme, tis $cm=\\frac{rrxxyy+\\frac{4rr}{q}{x}^{3}yy+\\frac{4rr}{qq}{x}^{4}yy+4xx{y}^{4}}{2rr{x}^{3}{y}^{3}+8\\frac{rr}{q}{x}^{4}{y}^{3}+\\frac{8rr}{qq}{x}^{5}{y}^{3}-8\\frac{r}{q}{x}^{3}{y}^{5}}×\\sqrt{rrxxyy+\\frac{4rr}{q}{x}^{3}yy+\\frac{4rr}{qq}{x}^{4}yy+4xx{y}^{4}}$ . Or $cm=\\frac{qqrr+4qrrx+4rrxx+4qqyyin\\sqrt{qqrr+4qrrx+rrxx+4qqyy}}{2{q}^{3}rr}$ . Or $cm=\\frac{qrr+4qyy+4ryy}{2qqrr}\\sqrt{qqrr+4qqyy+4qryy}$ .\n\nThis Theoreme may bee thus Demonstrated\n\nNote yt ye curvity of any curve whose ordinates are applyed at \\inclined from right to/ oblique angles is to ye curvity of the same curve whose ordinates are at right angles, as the curvity of an Ellipsis whose ordinates are in the sa a circle whose ordinates are in like manner inclined so as to make it becom an Ellipsis.\n\nProb: To find ye points of curves where they have a given degree of curvity.\n\n<56r>\n\nProb 3d. To find ye points distinguishing twixt ye concave & convex\nportions of crooked lines.\n\nResolution. The lines are not crooked at those points: & therefore ye radius cm determining ye crookednesse at yt point must bee infinitely greate. To wch purpose I put ye denominator of its valor (in rule ye 3d) to bee equall to nothing, & {sic} so have this Theoreme ·X·XX:−2·XX··X·+X·X·:X=0. Or better haps $\\frac{·XX:}{X·}-2·X·+\\frac{X·:X}{·X}=0$ .\n\nExample, was this point to \\be/ found in ye Concha whose nature is +bb x4+2bx3+ccxx−2bccx−bbcc=0. +yy . Then is ·X=2x4+2bx3+2bccx+2bbcc. X·=2xxyy=X: :X=2x4−4bccx−bbbcc. ·X·=0. Which valors subrogated into ye Theoreme, they produce 2x4+2bx3+2bccx+2bbcc+$\\frac{\\overline{2{x}^{4}-4bccx-6bbcc}×2xxyy}{2{x}^{4}+2b{x}^{3}+2bccx+2bbcc}=0$ . And subrogating −bb −x4−2bx3−ccxx +2bccx+bbcc ye valor of xxyy into its stead & \\twice/ reducing ye Equation by ye divisor x+b. Tis x3+bcc+$\\frac{\\overline{{x}^{4}-2bccx-3bbcc}×\\overline{cc-xx}}{{x}^{3}+bcc}=0$ . Or x4+4bx3+3bbxx−2bccx−2bbcc=0. Which being againe reduced by x+b=0. Tis x3+3bxx−2bcc=0. See Geometr: Chart: pag: 259.\n\n<56v>\n\nProbl: 4. To \\find/ ye points at wch lines are most or least crooked.\n\nResol: At those points ye afforesaid radius cm neither increaseth nor decreaseth. So yt ye center m in yt moment doth absolutely rest, & therefore neither ye line bk nor al doth increase or diminish, yt is, ck & bl doe soe much increase or diminish as x|y| & x (lb & ab) doe diminish or increase. Or in a word the point m resteth. Find therefore the motion of al or cm or lm & suppose it t nothing.\n\nThus in the Concha to find the point of least crookednes beyond ye point of reflection, having substituted ye valors of ·X, X· &c (exprest in the precedent problem) into this The computation is too tedious\n\nThus to find the point of least crookednesse in ye curve x3=\\cc/yy By the rule in prob 2 I make ·X=3x3. X·=−ccy. :X=6x3. X:=0 & ·X·equals;0 & thence obteine $ck=\\frac{3}{2}y+\\frac{cc}{6x}$, or $=\\frac{3{x}^{3}}{2cc}+\\frac{cc}{6x}$ wch is least when $\\frac{9{x}^{3}}{2cc}-\\frac{cc}{6x}=0$ or $x=\\sqrt{4}:\\frac{c4}{27}$. And then therefore happens the greatest crookednesse\n\nIn like mane|n|er if ye curve be xxy=a3 The rule gives ·X=2a3 X·=a3 {=} :X={illeg}\\−6a3/ X:;=0=·X· And thence $\\frac{2y}{3}+\\frac{xx}{6y}=ck$ which is least when $y=a\\sqrt{\\frac{1}{2}}$ .\n\nSoe if ye curve bee x3=byy. Th|e|i|n| is ·X=3x3. X·=−\\2/byy. :X=6x3 X:=−2yyc. ·X·=0. And therefore ck=3y+$\\frac{4xx}{3y}$ , which {illeg} \\hath no/ least when x=$\\frac{4b}{27}$ nor the curve any least crookednesse.\n\n<57r>\n\nProb 5t. To find ye nature of ye crooked line whose area is expressed by any given equation.\n\nThat is, ye nature of ye area being given to find ye nature of ye crooked line whose area it is.\n\nResol. If ye relation of ab=x, & abc=y bee given &", null, "ye relation of ab=x, & bc=q bee required (bc being ordinately applyed at right angles to ab). Make de∥ab⊥ad∥be=1. & yn is abed=x. Now supposing ye line cbe by parallel motion from ad to describe ye two superficies ae=x, & abc=y; The velocity wth wch they increase will bee, as be to bc: yt is, ye motion by wch x increaseth being be=p=1, ye motion by wch y increaseth will bee bc=q. which therefore may bee found by prop: 7th. viz: $\\frac{-·Xy}{X·x}=q=bc$ .\n\nExample 1. If 4rx3=9yy /$\\frac{2x}{3}\\sqrt{rx}=y$ \\. Or −4rx3+9yy=0. Then is $\\frac{12rxx}{18y}=q=\\sqrt{rx}$ . Or rx=qq & therefore abc is ye Parabola whose area \\abc/ is $\\frac{2x}{3}\\sqrt{rx}=\\frac{2qx}{3}$ .\n\nExample 2d. If x3−ay+xy=0. Then is $\\frac{3xx+y}{-x+a}=q$ . Or $\\frac{3axx-2{x}^{3}}{aa-2ax+xx}=q=bc$\n\nExample 3d. If $\\frac{na}{n+m}{x}^{\\frac{n+m}{n}}-y=0$ . Then is $a{x}^{\\frac{m}{n}}=q$ . Or if axm=bxn; yn is $\\frac{ma{x}^{m-1}}{nb{x}^{n-1}}=q$ .\n\nNote yt by this probleme may bee gathered a Catalogue of all those lines wch can bee squared. And therefore it will not bee necessary to shew how this Probleme may bee resolved in other cases in wch q is not ordinately applye{d} to x at right angles.\n\nProb 6. The nature of any Crooked line being given, to find other lines whose areas may bee compared to ye area of yt given line{illeg}.\n\nResol: Suppose ye given line to be ac & its area abc=s,", null, "ye sought line df & its area def=t; & yt bc=z is ordinately applyed to ab=x, & ef=v to de=y, soe yt ∠abc=∠def; & yt ye velocitys of y wth wch ab & de increase (yt is, ye velocity of ye points b & e, ofr of ye lines bc & ef moving from a & d) bee called p & q. Then may ye ordinately applyed lines bc & ef multiplyed by their velocitys p & q, (yt is pz & qv) signify ye velocitys wth wch ye areas abc\\=s/ & def\\=t/ increase. Now ye relation of ye areas s & t (taken at pleasure) gives ye relation of ye motions pz & qv describing those areas, by Proposition ye 7th.; Also ye relation of ye lines x & y ab=x & de=y (taken at pleasure) gives ye relation of p & q, by Prop 7th: wch two equations, together with ye given {illeg} Equation expressing ye nature of ye line ac, give ye relation of de=y & ef=v yt is ye \\desired/ nature of ye line df.\n\nExample 1. As if ax+bxx={illeg}zz is ye nature of ye line ac: & at pleasure I assume s=t {&}|t|o be ye relation of {illeg} ye areas abc & def; & {illeg}x=yy to bee ye relation of ye lines ab & de. Then is pz=qv (prop 7), & p=2qy (by prop 7). Therefore 2yz=v (by ye 2 last Equations), & $\\frac{vv}{4yy}$ =zz=ax+bxx=ayy+by4. or vv=4ay4+4by6. & $v=2yy\\sqrt{a+byy}$ : Wch is ye nature of ye line def whose area def is equall to ye area abc, supposing $\\sqrt{ab}=de=\\sqrt{x}=y$ .\n\n<57v>\n\nExample 2. If ax+bxx=zz as before; & I assume, as+bx=t, & x=yy. Then is apz+bp=qv (by prop 7), & p=2qy. 2azy+2by=v=2by+2ay$\\sqrt{ax+bxx}$ . Or v=2by+2ayy$\\sqrt{a+byy}$ ; The required nature of ye line def.\n\nExample 3d. If ax+bxx=xx as {if} $\\frac{4c}{a}\\sqrt{xx-a}=z$ : & at pleasure I assume $\\frac{2c}{a}\\sqrt{ay+yy}-s=t$ , & {illeg} xx−a=y. Then is 4ccay+ccyy=aass+2aast+aatt, And (by prop 7) 4ccaq+8ccyq=2aaspz+2aatpz+2aasqv+2aatqv=$\\overline{2aapz+2aaqv}×\\frac{2c}{a}\\sqrt{ay+yy}$ . & (by prop 7) 2px=q. Therefore $8cax+16cyx=\\overline{4az+8avx}×\\sqrt{ay+yy}$ . But $\\frac{4c}{a}\\sqrt{xx-a}=z=\\frac{4c}{a}\\sqrt{y}$ . Therefore & $x=\\sqrt{a+y}$ , Therefore $\\overline{8ca+16cy}\\sqrt{a+y}=\\overline{16c\\sqrt{y}+8av\\sqrt{a+y}}×\\sqrt{ay+yy}$ . That is 8 ca+2cy=2cy+$av\\sqrt{ay+yy}$ . Or $v=\\frac{c}{\\sqrt{ay+yy}}$ .\n\nExample 4th. If ax+bxx=zz as before & I assume ss=t, & x=yy. Then is 2spz=qv, & p=2qy (by prop 7) Therefore $4syz=v=4sy\\sqrt{ax+bxx}=4syy\\sqrt{a+byy}$ . Where note yt in this case ye area line $v=4syy\\sqrt{a+byy}$ is a Mechanicall one because s ye area of ye line ax+bxx=zz canott bee Geometrically found. The like is to bee observed in other such like cases.\n\nProbl: 7. The Nature of any Crooked line being given to find its area when it may bee. Or more generally, two crooked lines being given to fin{g}|d| the relation of their areas, when it may bee.\n\nResol: Reassuming ye figure of the 5t probleme in wch ye given line is ac, & supposing its area y & {x}|th|e other area x to bee described \\by ye line ce moving from a/ as was there taught: {illeg} Suppose the motion describing x bee p=be=1, Then ye motion describing y is cb=q=$\\frac{q}{1}=\\frac{q}{p}$ . Now having ye relation twixt ab{illeg}=abed=x, & bc=q=$\\frac{q}{1}=\\frac{q}{p}$ . (By supp:); I may (some times viz when it may bee) find\n\nResolution. In ye figure of ye fift probleme Let abc=y represent ye area of ye given line acf; cb=q ye motion describing yt area; abed=x another area wch is equall to ye basis ab=x of yt given line acf, (viz: supposing ab∥de⊥be∥ad=1); & be=p=1 ye motion describing yt other area. Now haveing (by supp) ye relation twixt ab=x=abed, & bc=q=$\\frac{q}{1}=\\frac{q}{p}$ given, I seeke ye area abc=y by ye Eight propo/sition\\\n\nExample 1. If ye nature of ye line bee, $\\frac{ax}{\\sqrt{aa-xx}}=bc=\\frac{q}{p}$ . I looke in ye tables of ye Eight proposition for ye Equation corresponding to this Equati{ō} wch I find to bee $\\frac{c{x}^{n}}{x\\sqrt{a+b{x}^{n}}}=\\frac{q}{p}$ , (For if instead of c, a, b, n I write a, aa, −1, 2, it will be $\\frac{ax}{\\sqrt{aa-xx}}=\\frac{q}{p}$ .) And against it is ye equation $\\frac{2c}{nb}\\sqrt{a+b{x}^{n}}=y$. And substituting a, aa, −1, 2 into ye places of c, a, b, n it will bee, $-a\\sqrt{aa-{x}^{n}}=y=abc$ ye required area.\n\nExample 2. If $\\sqrt{\\frac{{x}^{3}}{a}}-\\frac{eeb}{x\\sqrt{ax-xx}}=bc=\\frac{q}{p}$ . T|B|ecause there are two termes in ye valor of bc I consider them severally & first I find ye area correspondent to ye terme $\\sqrt{\\frac{{x}^{3}}{a}}$ , or $\\frac{1}{{a}^{\\frac{1}{2}}}{x}^{\\frac{3}{2}}$ ; To bee $\\frac{2}{5{a}^{\\frac{1}{2}}}{x}^{\\frac{5}{2}}$ , or $\\frac{2}{5}\\sqrt{\\frac{{x}^{5}}{a}}$ , \\by prop: 8. part 1./ Secondly to find ye area corresponding to ye other terme $\\frac{eeb}{x\\sqrt{ax-xx}}$ I looke ye Equation (in prop 8. part 3) corresponding to it wch is $\\frac{c{x}^{n}}{x\\sqrt{a+c{x}^{n}}}=\\frac{q}{p}$, (for if instead of c, a, b, n, I write eeb, −1, a, −1, it will bee $\\frac{eeb{x}^{\\overline{1}}}{x\\sqrt{-1+a{x}^{\\overline{1}}}}$ , Or $\\frac{eeb}{x\\sqrt{-xx+ax}}$ ): Against which is ye Equation $\\frac{2c}{nb}\\sqrt{a+b{x}^{n}}=y$ . In {sic} <58r> In which writing eeb, −1, a, −1, instead of c, a, b, n, the result will bee $\\frac{2eeb}{-a}\\sqrt{-1+a{x}^{\\overline{1}}}$ ; Or, $\\frac{-2eeb}{ax}\\sqrt{-xx+ax}=y$ wch is the", null, "the {sic} area corresponding to yt {illeg}|ot|her terme. Lastly \\Now/ to see how these areas stand related one to another I draw ye annexed scheme, in which is ab=x, bE=q=$\\frac{q}{p}$, adg ye fkeg the given curved line, & adg ye curve line described by one of its parts $\\sqrt{\\frac{{x}^{3}}{a}}=bd$ ab=x. $bd=\\sqrt{\\frac{{x}^{3}}{a}}$ . $de=\\frac{eeb}{x\\sqrt{ax-xx}}$ . & $be=\\sqrt{\\frac{{x}^{3}}{a}}-\\frac{eeb}{x\\sqrt{ax-xx}}=\\frac{q}{p}=\\frac{q}{p}=q$ . Soe that $abd=\\frac{2}{5}\\sqrt{\\frac{{x}^{5}}{a}}$ is ye superficies corresponding to ye first terme b{illeg}|d|, wch because it is affirmative must bee extended (or lye) from ye side ye from ye line bd towards a. Also ye other superficies correspondent to ye 2d terme de, being negative must lye on ye other side bd from a, wch is therefore gde $gde=\\frac{-2eeb}{ax}\\sqrt{ax-xx}$ . Lastly if x=ab=r Then is $abd=\\frac{2}{5}\\sqrt{\\frac{{r}^{5}}{a}}$ . & $gde=\\frac{-2bee}{ar}\\sqrt{ar-rr}$ . And if aB=x=s, yn is $\\frac{2}{5}\\sqrt{\\frac{{s}^{5}}{a}}=aBD$ , And $gDE=\\frac{-2bee}{as}\\sqrt{as-ss}$ . Soe yt, $\\frac{2}{5}\\sqrt{\\frac{{s}^{5}}{a}}-\\frac{2}{5}\\sqrt{\\frac{{r}^{5}}{a}}=bBDd$ . & $\\frac{-2bee}{as}\\sqrt{as-ss}+\\frac{2bee}{ar}\\sqrt{ar-rr}=DdeE$ & substracting DdeE from bBDd there remaines bBEe{illeg} $bBEe=\\frac{2\\sqrt{{s}^{5}}-2\\sqrt{{r}^{5}}}{5\\sqrt{a}}+\\frac{2bee}{as}\\sqrt{as-ss}-\\frac{2bee}{ar}\\sqrt{ar-rr}=bBEe$ . wch is ye required Area of ye given line &cfkeEg. Where note yt takging \\for/ ye quantitys r=ab & s=aB taking any numbers you may thereby finde ye area bBdD correspond to their difference bB.\n\nNote yt sometimes one parte of ye Area may bee Affirmative & ye other negative. as if a2B=r, & ab=s. Then is b2B2Ee=kbe−k2B2B|E|={sic}$\\frac{2\\sqrt{{s}^{5}}-2\\sqrt{{r}^{5}}}{5\\sqrt{a}}+\\frac{2bee}{as}\\sqrt{as-ss}-\\frac{2bee}{ar}\\sqrt{ar-rr}$ =b2B2Ee=kbe−k2B2E.\n\n<59r>\n\nProb 8|9|. To find such crooked lines whose lengths may bee found &also to find theire lengths.\n\nLemma 1. If to any crooked immovable line acg", null, "the streight line dcmσ moves to & fro perpendicularly every point of ye said line cdmσ (as γ, θ, σ, &c) shall describe a curve line (as βγ, δθ, λσ, &c) all which will bee perpendicular to ye said line cdmσ, & also parallel one to another & to ye line acg.\n\n2. If acg bee not a circle, there may bee drawne some curve line βδmλ, wch ye moving line cdmδ will always touch in some point or other (as at {illeg} m) & to wch therefore all ye curve lines βγ, δθ, λσ, &c: are perpendiculars.\n\n3. Soe that every point (γ, θ, m, σ, &c:) of ye line cdmσ, when it begineth or ceaseth to touch ye curve line βδmλ, doth yn move perpendicularly to or from it: & therefore ye line γdmσ doth not at all slide upon ye curve line βδ{illeg}|m|λ, but exactly measure it by applying it selfe to it point by point: & therefore ye correspondent parts of ye said lines are equall (viz: βm=γm. δm=θm. δλ=θσ. &c).\n\nResol. Take any Equation for ye nature of ye crooked line acg, & by ye 2d probleme find ye center m of its crookedness at c. That point m is a point of ye required curve line βδ{illeg}mλ. For yt point m whereat cdmσ ye perpendicular to acg doth touch ye curve{illeg} line βδmλ is lesse moved yn any other point of ye said perpendicular, bee|i|ng as it were ye hinge & center upon | about wch ye ye perpendicular turneth | moveth at that moment.\n\nExample 1. If acg is a Parabola whose nature is {xx} −rr=yy (supposing ab=x⊥{illeg}bc=y) is al rx=yy. By Theoreme ye 1st of Problem 2d I find cb+lm=y+$\\frac{4{y}^{3}}{rr}$ . By ye 2d Theoreme, bl=2x+$\\frac{1}{2}$r. And by ye 3d Theoreme $\\frac{\\overline{r+4x}\\sqrt{r+4x}}{2r}=cm$. Soe yt supposing ab=$\\frac{1}{2}$r. bl=3x=z. $lm=\\frac{4{y}^{3}}{rr}=v$. The relation twixt v & z will bee 27rvv=16z3, (for r4vv=16y6=16y3x3=$\\frac{16{z}^{3}{r}^{3}}{27}$) wch is ye nature of ye required line βδmλ. And since cγ=aβ=$\\frac{1}{2}$r. Therefore $\\gamma m=\\frac{r+4x}{2r}\\sqrt{rr+4xr}-\\frac{1}{2}r=\\frac{3r+4z}{18r}\\sqrt{9rr+12rz}-\\frac{r}{2}$. is ye length of its te βδm.\n\nExample 2. Soe if aa=xy, is ye nature of ye line acg. By ye afforesaid Theoreme I find, cb+lm=$\\frac{xx+yy}{2y}$; &, $bl=\\frac{xx+yy}{2x}$; {&} whereby ye nature of ye curve line βδmλ is determined. And lastly I find $cm=\\frac{xx+yy}{2aa}\\sqrt{xx+yy}$ which determine its length.\n\n<59v>\n\nProb: 10. Any curve line being given to find other lines whose lengths may be compared \\to its length or/ to its area, & to compare ym.\n\nResolution. Take any Equation for ye", null, "relation twixt ad & ye perpendicular {illeg} cd=y (whither yt relation bee expressed by an Geometricall Equation or whither it bee ye same wch some streight line beares to a curved one or to its superficies &c). Then (by prop 7) find ye relation twixt ye increa{sic}e or decrease (p & q) of ye lines ad=x, & dc=y. & say (by prop 6) yt {illeg} q∶p∷dc∶dn=$\\frac{py}{q}$ . And soe is ye triangle dnc (rectanguled at c) given & consequently ye Nature of ye curve line acg to wch dc is perpendicular, & cn a tangent.\n\nNow ye nature of ye center (m) of ye perpendiculars motion (wch gives ye nature & length of ye required curve line βm) may be found as in ye 2d or 9th Probleme, But more conveniently thus. Draw any fixed line he∥ad⊥ah=a=ef⊥ad. Also call fd=v. & ye increase \\or decrease/ of (fd) call r. And ye increase or decrease of ye motions p & q, call γ β & γ Now considering yt ye motion (p+r) of ye intersection point e in ye line he is to ye motion (p) of ye intersection point (d) in ye line (ad), as (em) is to (dm) (see prob 2); That is yt ye difference (r) of those motions is to ye motion (p) of ye point (b) soe is (ed) to (dm): First I find ye valor of v. viz $-\\sqrt{pp-qq}$ ∶q∷cn∶cd∷∷ {sic}ef=a∶fd=v=$\\frac{-aq}{\\sqrt{pp-qq}}$ . Or aaqq+vvqq−vvpp=0. Secondly by this Equation I find ye valor of r, viz: (by Prob 7), 2aaqγ+2vvqγ+2rvqq−2rvpp−2vvpβ=0. Thirdly $r=\\frac{aaq\\gamma +vvq\\gamma -vvp\\beta }{ppv-qqv}:p\\colon\\colon ed=\\frac{pv}{q}:dm=\\frac{{p}^{4}zz-ppqqzz}{aaqq\\gamma +vvqq\\gamma -vvpq\\beta }$ . Lastly supposing the motion p to bee uniforme yt its increase or decrease β may vanish, & also substituting ppzz ye valor of aaqq+vvqq in its stead in ye Denominator of dm, ye result will bee $\\frac{pp-qq}{\\gamma }=dm=\\frac{1-qq}{\\gamma }$ , if p=1. And to find ye lines dl & ml, say −p∶q∷dm∶dl=$\\frac{-q+{q}^{3}}{\\gamma }$ . & $p:\\sqrt{pp-qq}\\colon\\colon dm:ml=\\frac{1-qq\\sqrt{1-qq}}{\\gamma }$\n\nSoe yt by the equation expressing ye relation twixt x & y first I se{illeg}|find|e q & yn γ. wch two give me $\\frac{1-qq}{\\gamma }=dm$ &c.\n\nExample 1. If ye relation twixt x & y bee supposed to bee yy−ax=0. Then (by Prop 7) I find, first 2qy−ap=0, Or 2qy−a=0. & secondly 2γy+2qq=0. And substituting these valors of $q=\\frac{a}{2y}$ & γ=$\\frac{-qq}{y}=\\frac{-aa}{4{y}^{3}}$ in their stead in ye Equatio $\\frac{1-qq}{\\gamma }=dm$ , &c: The results will bee $\\frac{aay-4{y}^{3}}{aa}=dm$ . $\\frac{-aa+4yy}{2a}=dl$ . & $\\frac{aa-4yy}{2aa}\\sqrt{4yy-aa}=lm$ . (And adding cd=−y to dm, & ad=x to dl ={illeg}$\\frac{yy}{a}$ to dl, ye result is ad{illeg} cm=$\\frac{-4{y}^{3}}{aa}$ . & al=$\\frac{3yy}{a}-\\frac{a}{2}$ .) Wch determine ye nature & crookednesse of ye line βm. (For if aβ={illeg}$\\frac{a}{4}$ & βl =z=al−ab=al−a aβ=$\\frac{a}{4}$ . βl=z. lm=v. The relation twixt z & v will bee 16z3=27rvv. The length of βm being $m\\gamma =\\frac{4{y}^{3}}{aa}-\\frac{a}{2}=\\frac{3a+4z}{18a}\\sqrt{9aa+12az}-\\frac{1}{2}a$ . {I} as before was found).\n\nExample ye 2d. If x=ad⊥dk=$\\frac{aa}{x}$ , is ye nature of ye", null, "crooked line {illeg} (ye Hyperbola) gkw: And I would find other crooked lines (βm) whose lengths may bee compared wth ye area sdkg (calling as=b⊥gs) of that crooked line gkw. I call <60r> I call {sic} yt area sdkg=ξ, & its motion θ. Now since 1∶dk∷{illeg}p∶θ, (see prob 5. & ye Note on prop 7 in Example 3); Therefore θ{illeg} dk×p=dk=θ=$\\frac{aa}{x}$ . This being knowne I take at pleasure any Equation, in wch ξ is, for ye valor of cd=y.\n\nAs 1st suppose ay=ξ, That (by prop 7) gives aq=θ=$\\frac{aa}{x}$ , Or qx=a{illeg}; wch also (by prop 7) gives γx+qp=0. Which valors of q=$\\frac{a}{x}$ , & γ=$\\frac{-q}{x}=\\frac{-a}{xx}$ ; by helpe of ye Theorems $\\frac{1-qq}{\\gamma }=dm$ &c: doe give $\\frac{xx-aa}{-a}=dm$ . $\\frac{xx-aa}{x}=dl$ . & $\\frac{xx-aa}{-ax}\\sqrt{xx-aa}=lm$ =lm {sic}. wch determines ye nature of ye required curve line βm. The length of yt portion of it wch is intercepted twixt ye point m & the curve line acg being −cm=cd+dm=$\\frac{\\xi +xx-aa}{-a}$ , Or mc=$\\frac{\\xi +xx-aa}{a}$ .\n\n[Note yt in this case although ye area sdkg=ξ cannot bee Geometrically found & therefore ye line acg is a Mechanicall one yet ye desired line βm is a Geometricall one. And ye like will happen in all other such like cases, when |in| ye Equation taken at pleasure to expresse ye relation twixt x, y, & ξ; neither x, y, nor ξ doe multiply \\or divide/ one another, nor it selfe, nor is in any denominator or roote, except x wch may multiply it selfe & bee in \\sometimes/ denominators & rootes, when y or ξ are not in those one|fra|ctions or rootes{sic} \\& herein onely doth this excell the precedent 9th probleme/. Such is this Equation aξ−aby+ax3+$\\frac{axx}{ax-xx}-5xx\\sqrt{ab-xx}=0$ . &c: But not this ξξ=a3y. nor ξ=xy. &c]\n\nSecondly suppose ξ=xy. yt (by prop 7) give θ={q}y+xq=$aax$ , Or xy+xxq=aa, & yt (by prop 7) gives y+qx+2qx+γxx=0. Which two valors of $\\frac{aa\\prime xy}{xx}=q$ , And $\\frac{y+3qx}{\\prime xx}=\\gamma$ ; by meanes of ye Equatio Theoremes $\\frac{1-qq}{\\gamma }=dm$ , {illeg} $\\frac{{q}^{3}-q}{\\gamma }=dl$ , & $\\frac{1-qq}{\\gamma }\\sqrt{1-qq}=lm$ ; doe determine ye nature \\& length/ of ye desired curve line βm.\n\nExample ye 3d. In like manner to find curve lines whose lengths may bee compared to ye length \\gk/ of ye said curve (Hyperbola) gkw. Call gk=ξ, & its motion θ. Now, drawing kh ye tangent to gkw at k, I condsider that ad=x & gk=ξ doe increase in ye proportion of dh to kh; yt is, dh∶kh∷p∶θ. Now finding (by prob 1) yt dh=−x, & $kh=\\frac{-a}{x}\\sqrt{aa+xx}$ ; therefore is $\\frac{kh×p}{dh}=\\frac{kh}{dh}=\\frac{a\\sqrt{aa+xx}}{xx}=\\theta$ . Which being found, I take any equation, in wch ξ is, for the valor of cd=y. & |yn| worke as in ye precedent Example.\n\nNote yt by this &|or| ye Ninth Probleme may bee gathered a Catalogue of whatever lines, whose lengths can bee Geometrically found.\n\n<60v>\n\nProb {illeg} 12. To find ye Length of any given crooked line when{illeg} it may |bee.|\n\nResolution. The length of any streight line to wch ye curve line is cheifly related being called (x), ye length of ye curve line (y), & theire motions (p & q) first (by prob 1) get ye an equation expressing ye relation twixt x & $\\frac{q}{p}$, & yn seeke ye valor of (y) by ye Eight proposition. [Or find a curve line whose area is equall to ye length of ye given line, by Prob 11. And then find that area by Prob 7.]\n\n<61r>\n\nProb 11. To find curve lines whose Areas shall bee Equall (or have any other given relation) to ye length of any given Curve line drawn into a given |right line|\n\nResolution. The length of any streight line, to wch ye given curve line is cheifely referred, being called x, ye length of ye curve line y, |&| their motions of increase p & q. Get The valor of $\\frac{q}{p}$ (te|fo|und by ye first probleme) being ordinately applyed at right angles to x, gives ye nature of a curve line whose area is equall to (y) ye length of ye curve line.\n\nAnd this th|L|ine thus found gives (by prob 6) other lines. whose areas have any other given relation to ye length (y) of ye given curve line\n\n<61v>\n\nProb 13. To find ye nature of a Crooked line whose length is expressed\nby any given Equation, (when it may bee done).\n\nResolution. Suppose ab=x, bc=y, ac=z. & their motions p, q, r.", null, "And let ye relation twixt x & z bee supposed given. Then (by prop 8) finding the relation twixt p & r make $\\overline{rrr-pp}=q$ . (For drawing cd tangent to ac at c & de⊥cb⊥ab: ye lines de, ec, dc, shall bee as p, q, r. but $\\sqrt{dc×dc-de×de}=ec$ , & therefore $\\sqrt{rr-pp}=q$ ). Lastly, ye ratio twixt x & $\\frac{q}{p}$ being thus knowne, seeke y (by prop 8). Which relation twixt ab=x & bc=y determines ye nature of ye crooked line ac=z.\n\n<62r>\n\nOf Gravity.\n\nDefinitn. 1. I call yt point ye center of Motion in any Body, wch always rests when or howsoever yt Body circulates wthout progressive motion. It would a{illeg}|l|ways bee ye same wth ye center of Gravity were ye Rays of Gravity parallel & not converging towards ye center of ye Earth.\n\nLemma 1 \\Def: 2 And ye right lines passing through yt point I call ye axes of Motion or Gravity./\n\nLemma 1 The place & distance of Bodys is determinded by their center of Gravity. Which is ye middle point of a right line circle &|o|r Parallelogram:\n\nLemma 2 Those weights doe equiponderate whose quantitys are reciprocally proportionall to their distances from the common axis of Gravity, supposing their centers of Gravity were to bee in ye same plaine wth yt common axis of Gravity.\n\nProb To find ye center of Gravity in rectilinear plaine figures", null, "1. In ye Triangle acd make ab=bc, & cd=fd. & draw db, & af, their intersection point (e) is its center of Gravity.\n\nIn ye Trapezium abdc, draw ad & cb. Ioyne ye centers of", null, "Gravity e & h, f & g of ye opposite triangles acb & dcb, bad & {illeg} adc wth ye lines eh, fg. Their intersection point n is ye center of Gravity in ye Trapezium. (And so of Pentagons, hexagones &c)\n\nProp|b|: To find such plaine figures wch are equiponderate to any given plaine figure in respect of an axis of Gravity in any given position.\n\nResol That ye natures & positions of ye given", null, "curvilinear plaine (gbc,) & sought plaine (bde) bee such yt they may equiponderate in respect of ye axis (ak;) I suppose x=ab⊥bc=z, & y=ad⊥de=v to bee either perpendicular or parallel or coincident to ye said axis ak: And ye motions whereby x & y doe increase or decrease (i:e: ye motions", null, "of bc, & de to or from ye point a) I call p & q. Now ye ordinatly applyed lines bc=z, & de=v, multiplyed into their motion p & q (yt is, pz, & qv) may signify ye infinitly little parts of those areas (acb, & lde) wch each moment they describe; wch infinitly little parts doe equiponderate (by Lemma 1 & 2), if they multiplied by {illeg} their distances from ye axis ak doe make equall products. (yt is; pxz=qyv, in fig 1: pxz=$\\frac{1}{2}$qvv in fig 2: $\\frac{1}{2}$pzz=qv×fm, in fig 3; supposing dm=me. &) And if all ye respective infinitly little parts doe |equiponderate ye superficies must do so too.|\n\nNow therefore, (ye relation of x & y|z| being given by ye nature of ye curve line cg,) I take at pleasure any Equation for ye relation twixt x & y, & thereby (by prop 7) find p & q, & so by ye cedent Theorem find ye relation twixt y & v, for ye nature of ye sought are plaine lde.\n\nExam: 1. If cg (fig 2) is an Hyperbola, soe yt aa=xz. & I suppose 2x={illeg}y. yn is 2p={illeg}q (prop 7). & {illeg} paa=pxz=$\\frac{1}{2}$qvv=$\\frac{1}{2}$pvv. Or aa=vv. or a=v=de. Soe yt le is a streight line, & lde a parallelogram, wch equiponderates wth ye Hyperbola cgkabc (infinitly extended towards gk) if 2ab=ad. al×al=ab×bc.\n\n<62v>\n\nExample 2. If cg (fig 3) is a circle whose nature is, $\\sqrt{aa-xx}=z$ {illeg}. |&| I suppose at pleasure 3aax−x3=\\6/aay. Then (by prop 7) I find 3aap−3xxp=6aaq. And therefore $\\frac{1}{2}$paa−$\\frac{1}{2}$pxx=$\\frac{pzz}{2}$ ={illeg}qv×fm=(if fd=$\\frac{1}{2}$a,) {illeg}$\\frac{qvv+qav}{2}=\\frac{vv+av}{2}×q=\\frac{vv+av}{2}×\\frac{aap-xxp}{2aa}$ . {illeg} Or $aa×\\overline{paa-pxx}=\\frac{vv+av}{2}×aap-xxp$ . Or 2aa=vv+av. Or $v=-\\frac{1}{2}a♉\\sqrt{\\frac{9aa}{4}}=a$ ; {illeg}. Soe that le is a streight line & alde a parallelogram\n\nExample 3. If abcg is a parallelogram (fig 4) whose nature", null, "is, a=y a=z. & I suppose at pleasure x=yy−b. Then (by prop 7) tis p=2qy. Therefore $\\frac{1}{2}$aap=aaqy=$\\frac{1}{2}$pzz=qvy. Or aa=v. Soe yt aed is a parallelogram.\n\nOr if I suppose at pleasure, x=y3−b. Then is (prop 7) p=3qyy. & therefore $\\frac{1}{2}$aap=$\\frac{3}{2}$ aaqyy=$\\frac{1}{2}$pzz=qvy. Or 3aay=2v. ||\n\nOr if I suppose x=y4−b. yn is p=4qy3 & 2aayy=v. so that aed is a Parabola. [Soe if xx=y5. yn is 2px=5qy4. &, $\\frac{5{a}^{2}qy\\sqrt{y}}{4}=\\frac{5aaq{y}^{4}}{4x}$ =$\\frac{1}{2}$ap=$\\frac{1}{2}$pzz=qvy. Or 5aaqy$\\sqrt{y}$ =4qvy. & 25a4y=16vv. soe yt aed is a p|P|arabola.]\n\nExample {3}|4| If gbc (fig 1) is an Hyperbola whose nature is xx−aa={qy} zz. & I suppose x=y+{illeg}|b|. Then (by prop 7) is p=q. Therefore $px\\sqrt{xx-aa}$ =pxz=qyv=pyv. Or $\\overline{y+b}×\\sqrt{yy+2by+bb-aa}=x\\sqrt{xx-aa}=yv$ . Or $\\overline{yy+2by+bb}$ in $\\overline{yy+2by+bb-aa}=yyvv$ . &c.\n\nOr if I suppose xx=2y. Then is 2px=2q. Therefore $q\\sqrt{xx-aa}$ =pxz=qyv. Or (xx−aa=)2y−aa=yyvv.\n\nOr if I suppose xx=yy+aa. Then (prop 7) is 2px+\\=/2qy{illeg}. Therefore qyz=pxz=qyv. Or $x=\\sqrt{aa}$ $\\sqrt{xx-aa}=$ $y=\\sqrt{xx-aa}=z=v$ . & y=v; so yt aed is a triangle\n\nNote yt This Probleme may bee resolved a{illeg}|lt|hough the lines have a x, z, y, v, & ak \\have/ any other given inclination one to another, but the cedent cases may suffice\n\nNote also yt if I take a Parallelogram for ye knowne superficies (as in ye 3d Example I may thereby gather a Catalogue of all such curvilinear superficies whose weight in respect of ye axis, may bee knowne.\n\nNote also I might have shewn how to find lines whose wh weights in respect of any axis are not onely equall but have also any other given proportion one to another. And yn have made two Problems instead of this, as I did in Probl: 5 & 6: 9 & 10.\n\n<63r>\n\nProb 15. To find ye Gravity of any given plaine in respect of any given axis, given in position\nwhen it may bee done.\n\nResol: Suppose ek to bee ye Axis of Gravity, acb the given plaine,", null, "cb=y, & db=z to bee ordinatly applyed at any angles to ab=x. Bisect cb at m & draw mn⊥ek. Now, since [cb×mn] is ye gravity of ye line [cb], (by lem 1 & 2); if I make cb×mn=db=z, every line db shall designe ye Gravity of its correspondent line cb, yt is, ye superficies adb shall designe ye Gravity of ye superficies acb. Soe yt finding ye quantity of yt superficies adb (by prob 7) I find ye gravity of ye sup{illeg}e|er|ficies acb.\n\nExample 1 If ac is a Parabola; soe yt, ab{illeg} bc={4}, & z=d{a}∥k", null, "parallelTo;ak=axis rx=yy, & ye axis ak is ∥ dcb. &, {illeg} nb⊥ak, & yt, ab∶nb∷d∶e. Then is bc×nb=y×$\\frac{e×ab}{d}=\\frac{ex}{d}\\sqrt{rx}=z$ . Or eerx3=ddzz, is ye nature of ye curve line ad. whose area (were{illeg} abd a right angle would be $\\frac{2e}{5d}{x}^{\\frac{5}{2}}{y}^{\\frac{1}{2}}=\\frac{2e}{5d}\\sqrt{r{x}^{5}}$ but now it) is $\\frac{2ee}{5dd}\\sqrt{r{x}^{5}}$ , (by prob 7) wch is ye weight of ye area acb in respect of ye axis ak.\n\nExamp: 2 If ac is a Circle\n\nProb 16. To find ye Axes of Gravity i|o|f any Plaines\n\nResol. Find ye quantity of ye Plaine (by Prob 7) \\wch call A/ & ye quantity of its gravity in respect of any axis (by prob 15) wch call B{illeg}. & parallell to yt axis draw a line whose distance from it shall bee {illeg} $\\frac{A}{B}$ . That line shall bee an Axis of Gravity of ye given plain\n\nOr If you y cannot find ye quantity of the plane: Then", null, "find its gravitys in respect of two divers axes (AB & AC) wch gravitys call B{illeg} & C & D. & through |(A)| ye intersection of those axes draw a line AD wth this condition yt ye distances (DB & DC) of any one of its points (D) from the said axes (AB & AC), bee in such proportion as \\to/ the gravitys of the plane. That line (AD) shall bee an axis of gravity of ye said plane EF.\n\n<63v>\n\nProb 17 To find ye Center of Gravity of any Plaine, when it may bee\n\nResol Find two axes of Gravity &|b|y the precedent Prop, & their common intersection is ye Center of Gravity desired. If ye figure have any knowne Diameter that {illeg} \\{illeg}/ may bee taken for one of its axes of Gravity.\n\n© 2019 The Newton Project\n\nProfessor Rob Iliffe\nDirector, AHRC Newton Papers Project\n\nScott Mandelbrote,\nFellow & Perne librarian, Peterhouse, Cambridge\n\nFaculty of History, George Street, Oxford, OX1 2RL - newtonproject@history.ox.ac.uk\n\nPrivacy Statement" ]
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https://passemall.com/question/accuplacer/solve-this-system-of-equations-1617w123h20png-6x--10y--14-x-5444952305696768/
[ "", null, "Scan QR code or get instant email to install app\n\nQuestion:\n\n# 1212Solve this system of equations:", null, "-6x + 10y = 14 x + 2y = 5\n\nA (1, 2)\nexplanation\n\n1212The solution is the value or set of values that satisfies each of the equations. Because lines can intersect at only one point, if there is a solution, it must be the point at which the lines intersect. Begin by finding the solution to the system of linear equations. Elimination will be used to solve for the variable x. Multiply the second equation by -5 and combine the two lines to solve for x: (-6x + 10y = 14) + (-5x - 10y = -25), gives -11x = -11, so x = 1. Substitute this value into either linear equation to solve for y: 1 + 2y = 5, so y = 2 To confirm that (1, 2) is a solution, substitute it into the quadratic equation to test if it yields a true statement:", null, ", which becomes 2 = 1 + 3 - 2, which gives 2 = 2, so the only solution is (1, 2)" ]
[ null, "https://passemall.com/wp-content/themes/passemall_theme/assets/images/cdl/tests-by-state-header-background.jpg", null, "https://storage.googleapis.com/micro-enigma-235001.appspot.com/accuplacer/images/1617_w123_h20.png", null, "https://storage.googleapis.com/micro-enigma-235001.appspot.com/accuplacer/images/1538_w148_h20.png", null ]
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https://ww2.mathworks.cn/help/symbolic/sym.erfi.html
[ "# erfi\n\nImaginary error function\n\n## Syntax\n\n``erfi(x)``\n\n## Description\n\nexample\n\n````erfi(x)` returns the imaginary error function of `x`. If `x` is a vector or a matrix, `erfi(x)` returns the imaginary error function of each element of `x`.```\n\n## Examples\n\n### Imaginary Error Function for Floating-Point and Symbolic Numbers\n\nDepending on its arguments, `erfi` can return floating-point or exact symbolic results.\n\nCompute the imaginary error function for these numbers. Because these numbers are not symbolic objects, you get floating-point results.\n\n`s = [erfi(1/2), erfi(1.41), erfi(sqrt(2))]`\n```s = 0.6150 3.7382 3.7731```\n\nCompute the imaginary error function for the same numbers converted to symbolic objects. For most symbolic (exact) numbers, `erfi` returns unresolved symbolic calls.\n\n`s = [erfi(sym(1/2)), erfi(sym(1.41)), erfi(sqrt(sym(2)))]`\n```s = [ erfi(1/2), erfi(141/100), erfi(2^(1/2))]```\n\nUse `vpa` to approximate this result with the 10-digit accuracy:\n\n`vpa(s, 10)`\n```ans = [ 0.6149520947, 3.738199581, 3.773122512]```\n\n### Imaginary Error Function for Variables and Expressions\n\nCompute the imaginary error function for `x` and `sin(x) + x*exp(x)`. For most symbolic variables and expressions, `erfi` returns unresolved symbolic calls.\n\n```syms x f = sin(x) + x*exp(x); erfi(x) erfi(f)```\n```ans = erfi(x) ans = erfi(sin(x) + x*exp(x))```\n\n### Imaginary Error Function for Vectors and Matrices\n\nIf the input argument is a vector or a matrix, `erfi` returns the imaginary error function for each element of that vector or matrix.\n\nCompute the imaginary error function for elements of matrix `M` and vector `V`:\n\n```M = sym([0 inf; 1/3 -inf]); V = sym([1; -i*inf]); erfi(M) erfi(V)```\n```ans = [ 0, Inf] [ erfi(1/3), -Inf] ans = erfi(1) -1i```\n\n### Special Values of Imaginary Error Function\n\nCompute the imaginary error function for x = 0, x = ∞, and x = –∞. Use `sym` to convert `0` and infinities to symbolic objects. The imaginary error function has special values for these parameters:\n\n`[erfi(sym(0)), erfi(sym(inf)), erfi(sym(-inf))]`\n```ans = [ 0, Inf, -Inf]```\n\nCompute the imaginary error function for complex infinities. Use `sym` to convert complex infinities to symbolic objects:\n\n`[erfi(sym(i*inf)), erfi(sym(-i*inf))]`\n```ans = [ 1i, -1i]```\n\n### Handling Expressions That Contain Imaginary Error Function\n\nMany functions, such as `diff` and `int`, can handle expressions containing `erfi`.\n\nCompute the first and second derivatives of the imaginary error function:\n\n```syms x diff(erfi(x), x) diff(erfi(x), x, 2)```\n```ans = (2*exp(x^2))/pi^(1/2) ans = (4*x*exp(x^2))/pi^(1/2)```\n\nCompute the integrals of these expressions:\n\n```int(erfi(x), x) int(erfi(log(x)), x)```\n```ans = x*erfi(x) - exp(x^2)/pi^(1/2) ans = x*erfi(log(x)) - int((2*exp(log(x)^2))/pi^(1/2), x)```\n\n### Plot Imaginary Error Function\n\nPlot the imaginary error function on the interval from -2 to 2.\n\n```syms x fplot(erfi(x),[-2,2]) grid on```", null, "## Input Arguments\n\ncollapse all\n\nInput, specified as a floating-point or symbolic number, variable, expression, function, vector, or matrix.\n\ncollapse all\n\n### Imaginary Error Function\n\nThe imaginary error function is defined as:\n\n`$erfi\\left(x\\right)=-i\\text{\\hspace{0.17em}}erf\\left(ix\\right)=\\frac{2}{\\sqrt{\\pi }}\\underset{0}{\\overset{x}{\\int }}{e}^{{t}^{2}}dt$`\n\n## Tips\n\n• `erfi` returns special values for these parameters:\n\n• `erfi(0) = 0`\n\n• `erfi(inf) = inf`\n\n• `erfi(-inf) = -inf`\n\n• `erfi(i*inf) = i`\n\n• `erfi(-i*inf) = -i`" ]
[ null, "https://ww2.mathworks.cn/help/examples/symbolic/win64/PlotTheImaginaryErrorFunctionExample_01.png", null ]
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https://logicplum.com/knowledge-base/test-statistic/
[ "# What is Test Statistic?\n\nA test statistic is a statistic used in hypothesis testing. A test statistic is defined in a way that from the observed data it can quantify the support or rejection of the null hypothesis. An important property of a test statistic is that the sampling distribution under the null hypothesis must be known and calculable, as this is a necessary condition to calculate the p-value of the results. This p-value represents the agreement between the calculated test statistic and the predicted value.", null, "Figure: A p-value is an area that defines the likelihood of a result happening by chance.\n\nThere are different statistical tests. The table below summarizes the most common ones.\n\n Test statistic Null and alternative hypothesis Hypothesis test t-value H0: The means of two groups are equal. H1: The means of two groups are different. T-test z-value H0: The means of two groups are equal. H1: The means of two groups are different. Z-test F-value H0: The means are equal. H1: The means are not equal. ANOVA Χ2-value H0: The two samples are independent. H1: The two samples are not independent. Chi-squared test\n\n#### Why are Test Statistics Important?\n\nTest statistics play a key role in research and engineering, as they help prove whether the results of a study are due to chance or not. Technically, the difficulty lies in selecting the right statistical test.\n\nThe applications are many. From political surveys to medical studies to product quality control, statistical tests are key to ensure the validity of the results. In politics, they provide reliability to studies done from population samples. In medical studies, they help ensure that medications are effective. And in production, they help maintain quality standards.\n\n#### Tests statistics + LogicPlum\n\nUsing test statistics requires an understanding of the probability distribution that describes the data under study. They also require knowledge about the different hypothesis tests. However, many times industries and researchers lack the necessary mathematical and statistical background.\n\nLogicPlum is the ideal tool for them, as it performs all operations in an automated manner, permitting them to test hundreds of different potential solutions, and selecting the most efficient one for the problem under study. As a result, economists, financial analysts, industries, and laboratories can concentrate on interpreting the model’s results, knowing that the most advanced mathematical techniques have been correctly employed.\n\n##### Guide to Further Reading\n\nA nice guide to statistical tests in Python:\n\nBrownlee, J. 17 Statistical Hypothesis Tests in Python (Cheat Sheet). https://machinelearningmastery.com/statistical-hypothesis-tests-in-python-cheat-sheet/", null, "" ]
[ null, "https://g2p4f9g9.rocketcdn.me/wp-content/plugins/a3-lazy-load/assets/images/lazy_placeholder.gif", null, "https://g2p4f9g9.rocketcdn.me/wp-content/plugins/a3-lazy-load/assets/images/lazy_placeholder.gif", null ]
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https://www.stat.math.ethz.ch/pipermail/r-help/2016-May/438910.html
[ "# [R] Shaded areas in R\n\nDuncan Murdoch murdoch.duncan at gmail.com\nThu May 26 16:32:16 CEST 2016\n\n```On 26/05/2016 5:37 AM, Óscar Jiménez wrote:\n> Hello,\n>\n> I'm working with R language, and plotting some parameters over time. I need\n> to draw a shaded area under the curve of eacj parameter.\n>\n> For that, I might use the polygon (x,y) function, assigning coordinates\n> (x,y) to each vertex of my polygon. To do so, \"x\" and \"y\" must be vectors\n> with numerical values, but since my x-axis is a time series, I cannot\n> assing a numerical value to my \"x\" coordinate, because time variable is a\n> \"character\" variable.\n>\n> Is there any option to use the function polygin (x,y) in this case, or any\n> other function that allows me to draw a shaded area under the curve on a\n> time series basis?\n\nTimes and dates just print like characters, they aren't actually\ncharacters. For example,\n\nx <- Sys.Date() + 1:20\ny <- rnorm(20)\nplot(y ~ x)\npolygon(c(x, x, x), c(y, 0, 0), col=\"gray\")\n\nDuncan Murdoch\n\n```" ]
[ null ]
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https://en.wikipedia.org/wiki/Haar_wavelet
[ "# Haar wavelet\n\nJump to navigation Jump to search\n\nIn mathematics, the Haar wavelet is a sequence of rescaled \"square-shaped\" functions which together form a wavelet family or basis. Wavelet analysis is similar to Fourier analysis in that it allows a target function over an interval to be represented in terms of an orthonormal basis. The Haar sequence is now recognised as the first known wavelet basis and extensively used as a teaching example.\n\nThe Haar sequence was proposed in 1909 by Alfréd Haar. Haar used these functions to give an example of an orthonormal system for the space of square-integrable functions on the unit interval [0, 1]. The study of wavelets, and even the term \"wavelet\", did not come until much later. As a special case of the Daubechies wavelet, the Haar wavelet is also known as Db1.\n\nThe Haar wavelet is also the simplest possible wavelet. The technical disadvantage of the Haar wavelet is that it is not continuous, and therefore not differentiable. This property can, however, be an advantage for the analysis of signals with sudden transitions (discrete signals), such as monitoring of tool failure in machines.\n\nThe Haar wavelet's mother wavelet function $\\psi (t)$", null, "can be described as\n\n$\\psi (t)={\\begin{cases}1\\quad &0\\leq t<{\\frac {1}{2}},\\\\-1&{\\frac {1}{2}}\\leq t<1,\\\\0&{\\mbox{otherwise.}}\\end{cases}}$", null, "Its scaling function $\\varphi (t)$", null, "can be described as\n\n$\\varphi (t)={\\begin{cases}1\\quad &0\\leq t<1,\\\\0&{\\mbox{otherwise.}}\\end{cases}}$", null, "## Haar functions and Haar system\n\nFor every pair n, k of integers in $\\mathbb {Z}$", null, ", the Haar function ψn,k is defined on the real line $\\mathbb {R}$", null, "by the formula\n\n$\\psi _{n,k}(t)=2^{n/2}\\psi (2^{n}t-k),\\quad t\\in \\mathbb {R} .$", null, "This function is supported on the right-open interval In,k = [ k2n, (k+1)2n), i.e., it vanishes outside that interval. It has integral 0 and norm 1 in the Hilbert space L2($\\mathbb {R}$", null, "),\n\n$\\int _{\\mathbb {R} }\\psi _{n,k}(t)\\,dt=0,\\quad \\|\\psi _{n,k}\\|_{L^{2}(\\mathbb {R} )}^{2}=\\int _{\\mathbb {R} }\\psi _{n,k}(t)^{2}\\,dt=1.$", null, "The Haar functions are pairwise orthogonal,\n\n$\\int _{\\mathbb {R} }\\psi _{n_{1},k_{1}}(t)\\psi _{n_{2},k_{2}}(t)\\,dt=\\delta _{n_{1}n_{2}}\\delta _{k_{1}k_{2}},$", null, "where $\\delta _{ij}$", null, "represents the Kronecker delta. Here is the reason for orthogonality: when the two supporting intervals $I_{n_{1},k_{1}}$", null, "and $I_{n_{2},k_{2}}$", null, "are not equal, then they are either disjoint, or else the smaller of the two supports, say $I_{n_{1},k_{1}}$", null, ", is contained in the lower or in the upper half of the other interval, on which the function $\\psi _{n_{2},k_{2}}$", null, "remains constant. It follows in this case that the product of these two Haar functions is a multiple of the first Haar function, hence the product has integral 0.\n\nThe Haar system on the real line is the set of functions\n\n$\\{\\psi _{n,k}(t)\\;:\\;n\\in \\mathbb {Z} ,\\;k\\in \\mathbb {Z} \\}.$", null, "It is complete in L2($\\mathbb {R}$", null, "): The Haar system on the line is an orthonormal basis in L2($\\mathbb {R}$", null, ").\n\n## Haar wavelet properties\n\nThe Haar wavelet has several notable properties:\n\n1. Any continuous real function with compact support can be approximated uniformly by linear combinations of $\\varphi (t),\\varphi (2t),\\varphi (4t),\\dots ,\\varphi (2^{n}t),\\dots$", null, "and their shifted functions. This extends to those function spaces where any function therein can be approximated by continuous functions.\n2. Any continuous real function on [0, 1] can be approximated uniformly on [0, 1] by linear combinations of the constant function 1, $\\psi (t),\\psi (2t),\\psi (4t),\\dots ,\\psi (2^{n}t),\\dots$", null, "and their shifted functions.\n3. Orthogonality in the form\n\n$\\int _{-\\infty }^{\\infty }2^{(n+n_{1})/2}\\psi (2^{n}t-k)\\psi (2^{n_{1}}t-k_{1})\\,dt=\\delta _{nn_{1}}\\delta _{kk_{1}}.$", null, "Here, $\\delta _{ij}$", null, "represents the Kronecker delta. The dual function of ψ(t) is ψ(t) itself.\n\n1. Wavelet/scaling functions with different scale n have a functional relationship: since\n{\\begin{aligned}\\varphi (t)&=\\varphi (2t)+\\varphi (2t-1)\\\\[.2em]\\psi (t)&=\\varphi (2t)-\\varphi (2t-1),\\end{aligned}}", null, "it follows that coefficients of scale n can be calculated by coefficients of scale n+1:\nIf $\\chi _{w}(k,n)=2^{n/2}\\int _{-\\infty }^{\\infty }x(t)\\varphi (2^{n}t-k)\\,dt$", null, "and $\\mathrm {X} _{w}(k,n)=2^{n/2}\\int _{-\\infty }^{\\infty }x(t)\\psi (2^{n}t-k)\\,dt$", null, "then\n$\\chi _{w}(k,n)=2^{-1/2}{\\bigl (}\\chi _{w}(2k,n+1)+\\chi _{w}(2k+1,n+1){\\bigr )}$", null, "$\\mathrm {X} _{w}(k,n)=2^{-1/2}{\\bigl (}\\chi _{w}(2k,n+1)-\\chi _{w}(2k+1,n+1){\\bigr )}.$", null, "## Haar system on the unit interval and related systems\n\nIn this section, the discussion is restricted to the unit interval [0, 1] and to the Haar functions that are supported on [0, 1]. The system of functions considered by Haar in 1910, called the Haar system on [0, 1] in this article, consists of the subset of Haar wavelets defined as\n\n$\\{t\\in [0,1]\\mapsto \\psi _{n,k}(t)\\;:\\;n\\in \\mathbb {N} \\cup \\{0\\},\\;0\\leq k<2^{n}\\},$", null, "with the addition of the constant function 1 on [0, 1].\n\nIn Hilbert space terms, this Haar system on [0, 1] is a complete orthonormal system, i.e., an orthonormal basis, for the space L2([0, 1]) of square integrable functions on the unit interval.\n\nThe Haar system on [0, 1] —with the constant function 1 as first element, followed with the Haar functions ordered according to the lexicographic ordering of couples (n, k)— is further a monotone Schauder basis for the space Lp([0, 1]) when 1 ≤ p < ∞. This basis is unconditional when 1 < p < ∞.\n\nThere is a related Rademacher system consisting of sums of Haar functions,\n\n$r_{n}(t)=2^{-n/2}\\sum _{k=0}^{2^{n}-1}\\psi _{n,k}(t),\\quad t\\in [0,1],\\ n\\geq 0.$", null, "Notice that |rn(t)| = 1 on [0, 1). This is an orthonormal system but it is not complete. In the language of probability theory, the Rademacher sequence is an instance of a sequence of independent Bernoulli random variables with mean 0. The Khintchine inequality expresses the fact that in all the spaces Lp([0, 1]), 1 ≤ p < ∞, the Rademacher sequence is equivalent to the unit vector basis in ℓ2. In particular, the closed linear span of the Rademacher sequence in Lp([0, 1]), 1 ≤ p < ∞, is isomorphic to ℓ2.\n\n### The Faber–Schauder system\n\nThe Faber–Schauder system is the family of continuous functions on [0, 1] consisting of the constant function 1, and of multiples of indefinite integrals of the functions in the Haar system on [0, 1], chosen to have norm 1 in the maximum norm. This system begins with s0 = 1, then s1(t) = t is the indefinite integral vanishing at 0 of the function 1, first element of the Haar system on [0, 1]. Next, for every integer n ≥ 0, functions sn,k are defined by the formula\n\n$s_{n,k}(t)=2^{1+n/2}\\int _{0}^{t}\\psi _{n,k}(u)\\,du,\\quad t\\in [0,1],\\ 0\\leq k<2^{n}.$", null, "These functions sn,k are continuous, piecewise linear, supported by the interval In,k that also supports ψn,k. The function sn,k is equal to 1 at the midpoint xn,k of the interval  In,k, linear on both halves of that interval. It takes values between 0 and 1 everywhere.\n\nThe Faber–Schauder system is a Schauder basis for the space C([0, 1]) of continuous functions on [0, 1]. For every f in C([0, 1]), the partial sum\n\n$f_{n+1}=a_{0}s_{0}+a_{1}s_{1}+\\sum _{m=0}^{n-1}{\\Bigl (}\\sum _{k=0}^{2^{m}-1}a_{m,k}s_{m,k}{\\Bigr )}\\in C([0,1])$", null, "of the series expansion of f in the Faber–Schauder system is the continuous piecewise linear function that agrees with f at the 2n + 1 points k2n, where 0 ≤ k ≤ 2n. Next, the formula\n\n$f_{n+2}-f_{n+1}=\\sum _{k=0}^{2^{n}-1}{\\bigl (}f(x_{n,k})-f_{n+1}(x_{n,k}){\\bigr )}s_{n,k}=\\sum _{k=0}^{2^{n}-1}a_{n,k}s_{n,k}$", null, "gives a way to compute the expansion of f step by step. Since f is uniformly continuous, the sequence {fn} converges uniformly to f. It follows that the Faber–Schauder series expansion of f converges in C([0, 1]), and the sum of this series is equal to f.\n\n### The Franklin system\n\nThe Franklin system is obtained from the Faber–Schauder system by the Gram–Schmidt orthonormalization procedure. Since the Franklin system has the same linear span as that of the Faber–Schauder system, this span is dense in C([0, 1]), hence in L2([0, 1]). The Franklin system is therefore an orthonormal basis for L2([0, 1]), consisting of continuous piecewise linear functions. P. Franklin proved in 1928 that this system is a Schauder basis for C([0, 1]). The Franklin system is also an unconditional Schauder basis for the space Lp([0, 1]) when 1 < p < ∞. The Franklin system provides a Schauder basis in the disk algebra A(D). This was proved in 1974 by Bočkarev, after the existence of a basis for the disk algebra had remained open for more than forty years.\n\nBočkarev's construction of a Schauder basis in A(D) goes as follows: let f be a complex valued Lipschitz function on [0, π]; then f is the sum of a cosine series with absolutely summable coefficients. Let T(f) be the element of A(D) defined by the complex power series with the same coefficients,\n\n$\\left\\{f:x\\in [0,\\pi ]\\rightarrow \\sum _{n=0}^{\\infty }a_{n}\\cos(nx)\\right\\}\\longrightarrow \\left\\{T(f):z\\rightarrow \\sum _{n=0}^{\\infty }a_{n}z^{n},\\quad |z|\\leq 1\\right\\}.$", null, "Bočkarev's basis for A(D) is formed by the images under T of the functions in the Franklin system on [0, π]. Bočkarev's equivalent description for the mapping T starts by extending f to an even Lipschitz function g1 on [−π, π], identified with a Lipschitz function on the unit circle T. Next, let g2 be the conjugate function of g1, and define T(f) to be the function in A(D) whose value on the boundary T of D is equal to g1 + ig2.\n\nWhen dealing with 1-periodic continuous functions, or rather with continuous functions f on [0, 1] such that f(0) = f(1), one removes the function s1(t) = t from the Faber–Schauder system, in order to obtain the periodic Faber–Schauder system. The periodic Franklin system is obtained by orthonormalization from the periodic Faber–-Schauder system. One can prove Bočkarev's result on A(D) by proving that the periodic Franklin system on [0, 2π] is a basis for a Banach space Ar isomorphic to A(D). The space Ar consists of complex continuous functions on the unit circle T whose conjugate function is also continuous.\n\n## Haar matrix\n\nThe 2×2 Haar matrix that is associated with the Haar wavelet is\n\n$H_{2}={\\begin{bmatrix}1&1\\\\1&-1\\end{bmatrix}}.$", null, "Using the discrete wavelet transform, one can transform any sequence $(a_{0},a_{1},\\dots ,a_{2n},a_{2n+1})$", null, "of even length into a sequence of two-component-vectors $\\left(\\left(a_{0},a_{1}\\right),\\dots ,\\left(a_{2n},a_{2n+1}\\right)\\right)$", null, ". If one right-multiplies each vector with the matrix $H_{2}$", null, ", one gets the result $\\left(\\left(s_{0},d_{0}\\right),\\dots ,\\left(s_{n},d_{n}\\right)\\right)$", null, "of one stage of the fast Haar-wavelet transform. Usually one separates the sequences s and d and continues with transforming the sequence s. Sequence s is often referred to as the averages part, whereas d is known as the details part.\n\nIf one has a sequence of length a multiple of four, one can build blocks of 4 elements and transform them in a similar manner with the 4×4 Haar matrix\n\n$H_{4}={\\begin{bmatrix}1&1&1&1\\\\1&1&-1&-1\\\\1&-1&0&0\\\\0&0&1&-1\\end{bmatrix}},$", null, "which combines two stages of the fast Haar-wavelet transform.\n\nCompare with a Walsh matrix, which is a non-localized 1/–1 matrix.\n\nGenerally, the 2N×2N Haar matrix can be derived by the following equation.\n\n$H_{2N}={\\begin{bmatrix}H_{N}\\otimes [1,1]\\\\I_{N}\\otimes [1,-1]\\end{bmatrix}}$", null, "where $I_{N}={\\begin{bmatrix}1&0&\\dots &0\\\\0&1&\\dots &0\\\\\\vdots &\\vdots &\\ddots &\\vdots \\\\0&0&\\dots &1\\end{bmatrix}}$", null, "and $\\otimes$", null, "is the Kronecker product.\n\nThe Kronecker product of $A\\otimes B$", null, ", where $A$", null, "is an m×n matrix and $B$", null, "is a p×q matrix, is expressed as\n\n$A\\otimes B={\\begin{bmatrix}a_{11}B&\\dots &a_{1n}B\\\\\\vdots &\\ddots &\\vdots \\\\a_{m1}B&\\dots &a_{mn}B\\end{bmatrix}}.$", null, "An un-normalized 8-point Haar matrix $H_{8}$", null, "is shown below\n\n$H_{8}={\\begin{bmatrix}1&1&1&1&1&1&1&1\\\\1&1&1&1&-1&-1&-1&-1\\\\1&1&-1&-1&0&0&0&0&\\\\0&0&0&0&1&1&-1&-1\\\\1&-1&0&0&0&0&0&0&\\\\0&0&1&-1&0&0&0&0\\\\0&0&0&0&1&-1&0&0&\\\\0&0&0&0&0&0&1&-1\\end{bmatrix}}.$", null, "Note that, the above matrix is an un-normalized Haar matrix. The Haar matrix required by the Haar transform should be normalized.\n\nFrom the definition of the Haar matrix $H$", null, ", one can observe that, unlike the Fourier transform, $H$", null, "has only real elements (i.e., 1, -1 or 0) and is non-symmetric.\n\nTake the 8-point Haar matrix $H_{8}$", null, "as an example. The first row of $H_{8}$", null, "measures the average value, and the second row of $H_{8}$", null, "measures a low frequency component of the input vector. The next two rows are sensitive to the first and second half of the input vector respectively, which corresponds to moderate frequency components. The remaining four rows are sensitive to the four section of the input vector, which corresponds to high frequency components.\n\n## Haar transform\n\nThe Haar transform is the simplest of the wavelet transforms. This transform cross-multiplies a function against the Haar wavelet with various shifts and stretches, like the Fourier transform cross-multiplies a function against a sine wave with two phases and many stretches.[clarification needed]\n\n### Introduction\n\nThe Haar transform is one of the oldest transform functions, proposed in 1910 by the Hungarian mathematician Alfréd Haar. It is found effective in applications such as signal and image compression in electrical and computer engineering as it provides a simple and computationally efficient approach for analysing the local aspects of a signal.\n\nThe Haar transform is derived from the Haar matrix. An example of a 4x4 Haar transformation matrix is shown below.\n\n$H_{4}={\\frac {1}{2}}{\\begin{bmatrix}1&1&1&1\\\\1&1&-1&-1\\\\{\\sqrt {2}}&-{\\sqrt {2}}&0&0\\\\0&0&{\\sqrt {2}}&-{\\sqrt {2}}\\end{bmatrix}}$", null, "The Haar transform can be thought of as a sampling process in which rows of the transformation matrix act as samples of finer and finer resolution.\n\nCompare with the Walsh transform, which is also 1/–1, but is non-localized.\n\n### Property\n\nThe Haar transform has the following properties\n\n1. No need for multiplications. It requires only additions and there are many elements with zero value in the Haar matrix, so the computation time is short. It is faster than Walsh transform, whose matrix is composed of +1 and −1.\n2. Input and output length are the same. However, the length should be a power of 2, i.e. $N=2^{k},k\\in \\mathbb {N}$", null, ".\n3. It can be used to analyse the localized feature of signals. Due to the orthogonal property of the Haar function, the frequency components of input signal can be analyzed.\n\n### Haar transform and Inverse Haar transform\n\nThe Haar transform yn of an n-input function xn is\n\n$y_{n}=H_{n}x_{n}$", null, "The Haar transform matrix is real and orthogonal. Thus, the inverse Haar transform can be derived by the following equations.\n\n$H=H^{*},H^{-1}=H^{T},{\\text{ i.e. }}HH^{T}=I$", null, "where $I$", null, "is the identity matrix. For example, when n = 4\n$H_{4}^{T}H_{4}={\\frac {1}{2}}{\\begin{bmatrix}1&1&{\\sqrt {2}}&0\\\\1&1&-{\\sqrt {2}}&0\\\\1&-1&0&{\\sqrt {2}}\\\\1&-1&0&-{\\sqrt {2}}\\end{bmatrix}}\\cdot \\;{\\frac {1}{2}}{\\begin{bmatrix}1&1&1&1\\\\1&1&-1&-1\\\\{\\sqrt {2}}&-{\\sqrt {2}}&0&0\\\\0&0&{\\sqrt {2}}&-{\\sqrt {2}}\\end{bmatrix}}={\\begin{bmatrix}1&0&0&0\\\\0&1&0&0\\\\0&0&1&0\\\\0&0&0&1\\end{bmatrix}}$", null, "Thus, the inverse Haar transform is\n\n$x_{n}=H^{T}y_{n}$", null, "### Example\n\nThe Haar transform coefficients of a n=4-point signal $x_{4}=[1,2,3,4]^{T}$", null, "can be found as\n\n$y_{4}=H_{4}x_{4}={\\frac {1}{2}}{\\begin{bmatrix}1&1&1&1\\\\1&1&-1&-1\\\\{\\sqrt {2}}&-{\\sqrt {2}}&0&0\\\\0&0&{\\sqrt {2}}&-{\\sqrt {2}}\\end{bmatrix}}{\\begin{bmatrix}1\\\\2\\\\3\\\\4\\end{bmatrix}}={\\begin{bmatrix}5\\\\-2\\\\-1/{\\sqrt {2}}\\\\-1/{\\sqrt {2}}\\end{bmatrix}}$", null, "The input signal can then be perfectly reconstructed by the inverse Haar transform\n\n${\\hat {x_{4}}}=H_{4}^{T}y_{4}={\\frac {1}{2}}{\\begin{bmatrix}1&1&{\\sqrt {2}}&0\\\\1&1&-{\\sqrt {2}}&0\\\\1&-1&0&{\\sqrt {2}}\\\\1&-1&0&-{\\sqrt {2}}\\end{bmatrix}}{\\begin{bmatrix}5\\\\-2\\\\-1/{\\sqrt {2}}\\\\-1/{\\sqrt {2}}\\end{bmatrix}}={\\begin{bmatrix}1\\\\2\\\\3\\\\4\\end{bmatrix}}$", null, "" ]
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https://doc.qt.io/archives/qt-4.8/qpolygon.html
[ "# QPolygon Class\n\nThe QPolygon class provides a vector of points using integer precision. More...\n\n Header: #include Inherits: QVector Inherited By: Q3PointArray\n\nNote: All functions in this class are reentrant.\n\n## Public Functions\n\n QPolygon() QPolygon(int size) QPolygon(const QPolygon & polygon) QPolygon(const QVector & points) QPolygon(const QRect & rectangle, bool closed = false) ~QPolygon() QRect boundingRect() const bool containsPoint(const QPoint & point, Qt::FillRule fillRule) const QPolygon intersected(const QPolygon & r) const void point(int index, int * x, int * y) const QPoint point(int index) const void putPoints(int index, int nPoints, int firstx, int firsty, ...) void putPoints(int index, int nPoints, const QPolygon & fromPolygon, int fromIndex = 0) void setPoint(int index, int x, int y) void setPoint(int index, const QPoint & point) void setPoints(int nPoints, const int * points) void setPoints(int nPoints, int firstx, int firsty, ...) QPolygon subtracted(const QPolygon & r) const void swap(QPolygon & other) void translate(int dx, int dy) void translate(const QPoint & offset) QPolygon translated(int dx, int dy) const QPolygon translated(const QPoint & offset) const QPolygon united(const QPolygon & r) const operator QVariant() const\n• 66 public functions inherited from QVector\n QDataStream & operator<<(QDataStream & stream, const QPolygon & polygon) QDataStream & operator>>(QDataStream & stream, QPolygon & polygon)\n\n• 2 static public members inherited from QVector\n\n## Detailed Description\n\nThe QPolygon class provides a vector of points using integer precision.\n\nA QPolygon object is a QVector<QPoint>. The easiest way to add points to a QPolygon is to use QVector's streaming operator, as illustrated below:\n\n``` QPolygon polygon;\npolygon << QPoint(10, 20) << QPoint(20, 30);```\n\nIn addition to the functions provided by QVector, QPolygon provides some point-specific functions.\n\nEach point in a polygon can be retrieved by passing its index to the point() function. To populate the polygon, QPolygon provides the setPoint() function to set the point at a given index, the setPoints() function to set all the points in the polygon (resizing it to the given number of points), and the putPoints() function which copies a number of given points into the polygon from a specified index (resizing the polygon if necessary).\n\nQPolygon provides the boundingRect() and translate() functions for geometry functions. Use the QMatrix::map() function for more general transformations of QPolygons.\n\nThe QPolygon class is implicitly shared.\n\n## Member Function Documentation\n\n### QPolygon::QPolygon()\n\nConstructs a polygon with no points.\n\n### QPolygon::QPolygon(int size)\n\nConstructs a polygon of the given size. Creates an empty polygon if size == 0.\n\n### QPolygon::QPolygon(const QPolygon & polygon)\n\nConstructs a copy of the given polygon.\n\n### QPolygon::QPolygon(const QVector<QPoint> & points)\n\nConstructs a polygon containing the specified points.\n\n### QPolygon::QPolygon(const QRect & rectangle, bool closed = false)\n\nConstructs a polygon from the given rectangle. If closed is false, the polygon just contains the four points of the rectangle ordered clockwise, otherwise the polygon's fifth point is set to rectangle.topLeft().\n\nNote that the bottom-right corner of the rectangle is located at (rectangle.x() + rectangle.width(), rectangle.y() + rectangle.height()).\n\n### QPolygon::~QPolygon()\n\nDestroys the polygon.\n\n### QRect QPolygon::boundingRect() const\n\nReturns the bounding rectangle of the polygon, or QRect(0, 0, 0, 0) if the polygon is empty.\n\n### bool QPolygon::containsPoint(const QPoint & point, Qt::FillRule fillRule) const\n\nReturns true if the given point is inside the polygon according to the specified fillRule; otherwise returns false.\n\nThis function was introduced in Qt 4.3.\n\n### QPolygon QPolygon::intersected(const QPolygon & r) const\n\nReturns a polygon which is the intersection of this polygon and r.\n\nSet operations on polygons will treat the polygons as areas. Non-closed polygons will be treated as implicitly closed.\n\nThis function was introduced in Qt 4.3.\n\n### void QPolygon::point(int index, int * x, int * y) const\n\nExtracts the coordinates of the point at the given index to *x and *y (if they are valid pointers).\n\n### QPoint QPolygon::point(int index) const\n\nReturns the point at the given index.\n\n### void QPolygon::putPoints(int index, int nPoints, int firstx, int firsty, ...)\n\nCopies nPoints points from the variable argument list into this polygon from the given index.\n\nThe points are given as a sequence of integers, starting with firstx then firsty, and so on. The polygon is resized if `index+nPoints` exceeds its current size.\n\nThe example code creates a polygon with three points (4,5), (6,7) and (8,9), by expanding the polygon from 1 to 3 points:\n\n``` QPolygon polygon(1);\npolygon = QPoint(4, 5);\npolygon.putPoints(1, 2, 6,7, 8,9);```\n\nThe following code has the same result, but here the putPoints() function overwrites rather than extends:\n\n``` QPolygon polygon(3);\npolygon.putPoints(0, 3, 4,5, 0,0, 8,9);\npolygon.putPoints(1, 1, 6,7);```\n\n### void QPolygon::putPoints(int index, int nPoints, const QPolygon & fromPolygon, int fromIndex = 0)\n\nCopies nPoints points from the given fromIndex ( 0 by default) in fromPolygon into this polygon, starting at the specified index. For example:\n\n``` QPolygon polygon1;\npolygon1.putPoints(0, 3, 1,2, 0,0, 5,6);\n// polygon1 is now the three-point polygon(1,2, 0,0, 5,6);\n\nQPolygon polygon2;\npolygon2.putPoints(0, 3, 4,4, 5,5, 6,6);\n// polygon2 is now (4,4, 5,5, 6,6);\n\npolygon1.putPoints(2, 3, polygon2);\n// polygon1 is now the five-point polygon(1,2, 0,0, 4,4, 5,5, 6,6);```\n\n### void QPolygon::setPoint(int index, int x, int y)\n\nSets the point at the given index to the point specified by (x, y).\n\n### void QPolygon::setPoint(int index, const QPoint & point)\n\nSets the point at the given index to the given point.\n\n### void QPolygon::setPoints(int nPoints, const int * points)\n\nResizes the polygon to nPoints and populates it with the given points.\n\nThe example code creates a polygon with two points (10, 20) and (30, 40):\n\n``` static const int points[] = { 10, 20, 30, 40 };\nQPolygon polygon;\npolygon.setPoints(2, points);```\n\n### void QPolygon::setPoints(int nPoints, int firstx, int firsty, ...)\n\nResizes the polygon to nPoints and populates it with the points specified by the variable argument list. The points are given as a sequence of integers, starting with firstx then firsty, and so on.\n\nThe example code creates a polygon with two points (10, 20) and (30, 40):\n\n``` QPolygon polygon;\npolygon.setPoints(2, 10, 20, 30, 40);```\n\n### QPolygon QPolygon::subtracted(const QPolygon & r) const\n\nReturns a polygon which is r subtracted from this polygon.\n\nSet operations on polygons will treat the polygons as areas. Non-closed polygons will be treated as implicitly closed.\n\nThis function was introduced in Qt 4.3.\n\n### void QPolygon::swap(QPolygon & other)\n\nSwaps polygon other with this polygon. This operation is very fast and never fails.\n\nThis function was introduced in Qt 4.8.\n\n### void QPolygon::translate(int dx, int dy)\n\nTranslates all points in the polygon by (dx, dy).\n\n### void QPolygon::translate(const QPoint & offset)\n\nTranslates all points in the polygon by the given offset.\n\n### QPolygon QPolygon::translated(int dx, int dy) const\n\nReturns a copy of the polygon that is translated by (dx, dy).\n\nThis function was introduced in Qt 4.6.\n\n### QPolygon QPolygon::translated(const QPoint & offset) const\n\nReturns a copy of the polygon that is translated by the given offset.\n\nThis function was introduced in Qt 4.6.\n\n### QPolygon QPolygon::united(const QPolygon & r) const\n\nReturns a polygon which is the union of this polygon and r.\n\nSet operations on polygons, will treat the polygons as areas, and implicitly close the polygon.\n\nThis function was introduced in Qt 4.3.\n\n### QPolygon::operator QVariant() const\n\nReturns the polygon as a QVariant\n\n## Related Non-Members\n\n### QDataStream & operator<<(QDataStream & stream, const QPolygon & polygon)\n\nWrites the given polygon to the given stream, and returns a reference to the stream.\n\nThis function was introduced in Qt 4.4." ]
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https://patents.google.com/patent/CN105180963B/en
[ "# CN105180963B - Unmanned plane telemetry parameter modification method based on online calibration - Google Patents\n\nUnmanned plane telemetry parameter modification method based on online calibration Download PDF\n\n## Info\n\nPublication number\nCN105180963B\nCN105180963B CN201510433736.2A CN201510433736A CN105180963B CN 105180963 B CN105180963 B CN 105180963B CN 201510433736 A CN201510433736 A CN 201510433736A CN 105180963 B CN105180963 B CN 105180963B\nAuthority\nCN\nChina\nPrior art keywords\nerror\nunmanned plane\ncontrol point\nequation\nimage\nPrior art date\nApplication number\nCN201510433736.2A\nOther languages\nChinese (zh)\nOther versions\nCN105180963A (en\nInventor\n\nOriginal Assignee\n\nPriority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)\nFiling date\nPublication date\nApplication filed by 北京航空航天大学 filed Critical 北京航空航天大学\nPriority to CN201510433736.2A priority Critical patent/CN105180963B/en\nPublication of CN105180963A publication Critical patent/CN105180963A/en\nApplication granted granted Critical\nPublication of CN105180963B publication Critical patent/CN105180963B/en\n\n## Classifications\n\n• GPHYSICS\n• G01MEASURING; TESTING\n• G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY\n• G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass\n\n## Abstract\n\nThe invention discloses a kind of unmanned plane telemetry parameter modification method based on online calibration, belong to digital video image processing technology field.This method is first depending on the information such as flying height and the focal length of unmanned plane and installs ground control point, flown in the air route according to planning and the image to obtaining screened so as to obtain representative a small amount of view data, the error analysis of each telemetry parameter of unmanned plane is carried out according to the thought of space resection to obtained image afterwards, so as to obtain corresponding error prediction model.The present invention has been obtained establishing the view data needed for error prediction model using the thought of online calibration, and so as to obtain the forecast model of each telemetry parameter of unmanned plane, each telemetry parameter is modified.The step of this is operated after being allowed to using the telemetry parameter of unmanned plane improves certain precision.\n\n## Description\n\nUnmanned plane telemetry parameter modification method based on online calibration\n\nTechnical field\n\nThe invention belongs to digital video image processing technology field, and in particular to a kind of unmanned plane based on online calibration is distant Survey parameter correction method.\n\nBackground technology\n\nUnmanned plane is all with a wide range of applications in terms of military and civilian, is all lot of domestic and international mechanism for a long time With the hot research project of tissue.\n\nScouting is the inherent mission of unmanned plane, and unmanned plane reconnaissance image has turned into the important of fast and effective acquisition information Means, more and more important effect is played in all previous local war.Although using unmanned plane reconnaissance image it can be found that and Target is identified, but because imaging moment is influenceed by various external factors, causes each telemetry parameter of unmanned plane to exist and misses Difference, and do not have accurate geographical coordinate, so as to the precision of the operations such as the target positioning that is unable to after limit value.Therefore, to fill Distribution waves the fighting efficiency of unmanned plane, it is necessary to take certain technological means to be effectively treated the reconnaissance image of acquisition, corrects The error of each telemetry parameter of unmanned plane, so as to provide accurate measurement parameter for follow-up calculating.\n\nThe content of the invention\n\nThe present invention proposes the unmanned plane telemetry parameter modification method based on online calibration, it is therefore an objective to corrects the distant of unmanned plane The error of parameter is surveyed, so as to provide accurate measurement parameter for follow-up calculating.Pressed first before unmanned plane execution task Flown according to both tramp-liners, and obtain multiple images for including ground control point, recycle list as the thought of resection, it is right The longitude and latitude of unmanned plane, height, carriage angle and platform attitude angle carry out error analysis, so as to reach each remote measurement ginseng of amendment Several purposes.\n\nUnmanned plane telemetry parameter modification method based on online calibration, including following steps:\n\nThe first step, flight course planning is carried out according to the distribution situation of ground control point;\n\nAccording to the distribution situation of ground control point, unmanned plane is made to hold the area comprising at least four ground control point Continuous shooting, so as to obtain the shooting image in the case of unmanned plane multi-angle.It is required that the distribution of ground control point in the picture Disperse as far as possible, each posture of unmanned plane includes whole span as far as possible.\n\n1) control point is distributed:\n\nDue on the premise of identical height and focal length are constant, in the case that unmanned plane is regarded under vertical, corresponding to image True geographic range is minimum, therefore, as long as the distribution situation at control point ensures that nothing depending in the case of under analyzing vertically It is man-machine ground control point to be photographed in picture totally under any attitude.To ensure that the distribution at control point more divides Dissipate, image is now simply divided into the form of nine grids, as shown in Figure 1.Because this method needs at least four ground control point, Therefore, this 4 ground control points are individually positioned in 1~4 part by we.\n\n2) course line is planned, ensures posture coverage:\n\nBecause unmanned plane is during execution task, aircraft altitude, aircraft roll angle and aircraft pitch angle are all smaller, because This needs emphasis to consider vector angle and platform deflection and the platform angle of site.Fig. 2 gives an air strips rule The example drawn.According to the airline operation, it can cause vector angle and platform deflection is satisfied by 360 ° of excursion, put down The platform angle of site meets almost 90 ° of excursion;\n\nSecond step, image are chosen and record corresponding telemetry intelligence (TELINT);\n\nThe multiple image of representative angle is chosen in the image obtained from planning air strips.Need to record simultaneously The every two field picture obtained corresponds to the aircraft telemetry intelligence (TELINT) at moment, specifically include the longitude of aircraft, latitude, height, aircraft pitch angle, Aircraft roll angle, vector angle, the platform angle of site and platform azimuth.It is worth noting that aircraft telemetry parameter and image Corresponding relation is particularly significant, and real-time is higher, and error measure afterwards is more accurate;\n\n3rd step, obtain the pixel coordinate at control point;\n\nUsing image matching technology by the multiple image of acquisition respectively with comprising ground control point benchmark image carry out Match somebody with somebody, so as to obtain ground control point corresponding pixel coordinate information in image is investigated;\n\n4th step, the error analysis based on space resection;\n\nInitial value is used as by the use of the corresponding aircraft telemetry parameter of image.Error equation is listed according to collinearity equation, utilized Multiple control points obtain multigroup error equation, and obtain normal equation according to least square method, so as to try to achieve unmanned plane remote measurement ginseng Several corrections.Wherein the coefficient of error equation is represented by focal length, control point pixel coordinate and aircraft telemetry parameter;\n\n5th step, the error obtained according to multiple image carry out error prediction model foundation;\n\nAccording to corresponding when the multiple image chosen on planning air strips obtains each posture of unmanned plane in different values Error.The error obtained according to multiple image, the error prediction of each telemetry parameter of unmanned plane is established using least square method Model.\n\nThe advantage of the invention is that:\n\n(1) due to being to carry out error measure before each execution task, so obtained error is applicable the environment Property is strong;\n\n(2) longitude and latitude of unmanned plane and the error of attitude angle are have modified, so as to improve positioning precision.\n\nBrief description of the drawings\n\nFig. 1 is the ground control point arrangement schematic diagram of the present invention;\n\nFig. 2 is the planning route map of the present invention;\n\nFig. 3 is flow chart of the method for the present invention;\n\nFig. 4 is that the flow chart of telemetry parameter error component is sought in the utilization space resection of the present invention.\n\nEmbodiment\n\nThe embodiment of the present invention is described in detail below in conjunction with accompanying drawing.\n\nThe present invention is a kind of unmanned plane telemetry parameter modification method based on online calibration, and flow such as Fig. 3 shows, first, when Unmanned plane have flight take photo by plane task when, first flown in the overhead for arranging control point region according to the air route of advance planning OK, the Aerial Images for including ground control point under several different postures are obtained.The invention afterwards believes resection in aircraft Breath combine, so as under aircraft vertical depending on situation be generalized to more extensive aircraft flight and shooting situation.For obtaining Each telemetry parameter error, the invention is returned using the thought of least square fitting, so as to realize to follow-up remote measurement The error compensation of parameter, the present invention include following steps:\n\nThe first step, flight course planning is carried out according to the distribution situation of ground control point;\n\nAccording to the distribution situation of ground control point, unmanned plane is made to hold the area comprising at least four ground control point Continuous shooting, so as to obtain the shooting image in the case of unmanned plane multi-angle.\n\nIt is specifically described below and how arranges ground control point, and proposes that one kind can ensure each attitude angle covering one of aircraft Determine the flight course planning scheme of excursion:\n\n1) control point is arranged:\n\nDue on the premise of identical height and focal length are constant, in the case that unmanned plane is regarded under vertical, corresponding to image True geographic range is minimum, therefore, as long as the distribution situation at control point ensures that nothing depending in the case of under analyzing vertically It is man-machine under any attitude ground control point to be made to photograph totally in picture.If the camera focus of unmanned plane is f, pixel Size is μ, and the image a height of W*L of wide * of shooting, the working depth of aircraft is H.In the case of then regarding under vertical, image is covered The geographic range of lid is (W*H* μ/f) * (L*H* μ/f).To ensure that the distribution at control point is more scattered, now image is simply divided Into the form of nine grids, as shown in Figure 1.Because this method needs at least four ground control point, therefore, by this 4 ground controls Point is individually positioned in 1~4 part.It is reflected on true ground i.e., can in the case where No. 1 control point is determined With in its east sideIn the range of dispose No. 2 control points.Similarly in No. 1 control point southern sideIn the range of dispose No. 3 control points.Again No. 4 control points are determined by No. 2 and No. 3 control points i.e. Can.\n\n2) course line is planned, ensures posture coverage:\n\nMake vector angle and platform deflection be with due north angle, clockwise for just, the platform angle of site is and level Face angle, vertically lower apparent time is 90 °.Because unmanned plane is during execution task, aircraft altitude, aircraft roll angle and aircraft The angle of pitch is all smaller, therefore only needs emphasis to consider vector angle and platform deflection and the platform angle of site.Fig. 2 gives The example of an air strips planning is gone out.In the flight course from 1 to 5, vector angle is held essentially constant, the orientation of platform From close to 90 ° to close to 270 °, the platform angle of site is returned to low-angle from a low-angle to 90 ° at angle.In the flight from 5 to 14 During, vector angle returns to 90 ° from 90 ° after 360 ° of rotations, and platform deflection is from the change close to 270 ° of 360 ° of processes Change is returned near 270 °, and the platform angle of site is also from a small angle variation to close to 90 °.Therefore, can according to the airline operation To cause vector angle and platform deflection is satisfied by 360 ° of excursion, the platform angle of site meets almost 90 ° of change Scope;\n\nSecond step, image are chosen and record corresponding telemetry intelligence (TELINT);\n\nThe multiple image of representative angle is chosen in the image obtained from planning air strips, specific method can be From image sequence a two field picture is obtained every certain frame number.The image of selection is more, and the data area of covering is bigger, Zhi Houxuan The error compensation taken is more accurate, but also more wastes time and energy simultaneously.The every two field picture for recording acquisition is needed to correspond to the moment simultaneously Aircraft telemetry intelligence (TELINT), specifically include the longitude of aircraft, latitude, height, aircraft pitch angle, aircraft roll angle, vector angle, flat The platform angle of site and platform azimuth.It is worth noting that the corresponding relation of aircraft telemetry parameter and image is particularly significant, real-time Higher, error measure afterwards is more accurate.Here image selection can be carried out according to 1~No. 14 Aircraft point shown in Fig. 2, Can so ensure that vector angle and platform deflection can take a data every more than 20 degree, the platform angle of site every 10 ° or so take a data.But in order to avoid some accidental mistakes, it can continuously take multiframe at each aircraft destination Data.\n\n3rd step, obtain the pixel coordinate at control point;\n\nAccording to ground control point, its corresponding image pixel coordinates is obtained.The process can be marked manually, can also profit The multiple image of acquisition is matched with the benchmark image comprising ground control point respectively with image matching technology, so as to obtain Ground control point corresponding pixel coordinate information in image is investigated;\n\n4th step, the error analysis based on space resection;\n\nBy the use of the corresponding aircraft telemetry parameter of image as initial value, error equation is listed according to collinearity equation, utilized Multiple control points obtain multigroup error equation, and obtain normal equation according to least square method, so as to try to achieve unmanned plane remote measurement ginseng Several corrections, Fig. 4 are the flow chart of space resection.Wherein the coefficient of error equation is sat by focal length, control point pixel It is marked with and aircraft telemetry parameter represents.Specifically include following steps:\n\nIf geodetic coordinates corresponding to ground control point is (X, Y, Z), geodetic coordinates corresponding to the high information of longitude and latitude of unmanned plane For (Xs, Ys, Zs), camera focus f, x, y are that image pixel coordinates corresponding to ground control point are right under platform for video camera coordinate system The value answered, if platform azimuth is κ1, the platform angle of site is ω1, aircraft pitch angle is φ2, aircraft roll angle is ω2, Aircraft It is κ to angle2\n\n1) spin matrix R is calculated according to aspect information:\n\nThe transformational relation of platform for video camera coordinate and northeast day coordinate is in image:\n\nWherein:Represent coordinate value of the picture point (x, y) under northeast day coordinate system, RX,RY,RZRepresent around X, Y, Z axis The spin matrix of corresponding attitude angle is rotated, R is represented from Camera Platform coordinate system to the transformation matrix of northeast day coordinate system, a1~ c3Represent spin matrix R each value.\n\n2) approximation (x) of the pixel coordinate at control point, (y) are calculated according to collinearity condition equation;\n\nIn formula:λ is scale factor, then is write as matrix form and be\n\nBecause R is orthogonal matrix, then RΤ=R-1, so as to obtain relation\n\nAnd then obtain the imaging equation of central projection, also known as collinearity condition equation:\n\nBy the use of the telemetry parameter of unmanned plane as initial value, bring collinearity condition equation into and obtain the near of control point picpointed coordinate Like value (x), (y).\n\n3) error equation is obtained according to collinearity equation\n\nBy the Linearization of Collinearity Equations and a sub-minimum item is taken to obtain:\n\nThe geodetic coordinates at control point is considered as true value, and corresponding picpointed coordinate is considered as observation, then according to observation+ The principle of observation correction=approximation+approximation correction, makes vx, vyFor x, y observation correction obtains:\n\nThe error equation of each point can thus be listed\n\nIf by each coefficient a of above formula11,..., a28Represent, then can be write as\n\nWherein:lx,lyRepresent x, the difference between y observation and approximation.\n\nIt is expressed as with matrix form:\n\nV=AX-l\n\nIn formula:\n\nV=[vx,vy]Τ\n\nWherein A is coefficient matrix, and X is correction matrix number to be asked, and l is error matrix\n\n4) coefficient of each correction is calculated\n\nIt is convenient for writing, be by the molecule in collinearity equation, denominator tabular form:\n\nIt can then calculate\n\nSimilarly, coefficient can be calculated:\n\nSeparately have:\n\nWherein, due to\n\nSo have\n\n5) control point calculates one by one, obtains normal equation;\n\nIf there is n control point, n grouping error equations [V can be listed1 V2 … Vn]Τ, forming overall error equation is:\n\nV=AX-L\n\nIn formula:\n\n, can row normal equation according to least square method indirect adjustment principle\n\nAΤAX=AΤL\n\nSo as to which the vectorial solution for obtaining unknown number is\n\nX=(AΤA)-1AΤL\n\nThat is, correction dX is tried to achieves、dYs、dZs、dω1、dκ12、dκ2\n\n6) iteration, until corrected value is less than a certain prescribed limits, so as to obtain final error\n\nBy the improvement number tried to achieve every time compared with limit value, if being unsatisfactory for requiring, by formula\n\nWherein:Xs,…,k2Represent final revised parameter value;Xs0,…,k20Represent the initial value of parameters, dXsi, dYsi,…,dk2iRepresent the correction for the parameters that ith iteration obtains.\n\nIt is iterated, until correction, which is less than, limits poor, stopping calculating.Then there is the final error to be\n\nWherein, Δ Xs,…,Δκ2Represent the correction of parameters final result.\n\n5th step, the error obtained according to multiple image carry out error prediction model foundation;\n\nAccording to corresponding when the multiple image chosen on planning air strips obtains each posture of unmanned plane in different values Error.Due to when planning air strips, it has to be considered that the coverage of each attitude angle, therefore need to only obtain some and compare Representative image and telemetry parameter, it is possible to carry out the foundation of error prediction model.Angle during due to planning air strips It is all gradual change to change, therefore a relatively simple method, exactly takes a two field picture every certain frame number, can be built with satisfaction Mould requirement.\n\nThe measuring system of longitude and latitude and height in view of unmanned plane and measure the posture of unmanned plane and be two and independent be System, therefore, can be predicted to its error respectively.\n\n1) unmanned plane longitude and latitude and the error prediction of height\n\nBecause the navigation system that unmanned plane longitude and latitude and height mainly have unmanned plane provides, therefore its error and unmanned plane institute The environment at place is relevant.On the other hand, because the longitude and latitude for providing unmanned plane GPS is recognized as the longitude and latitude of optical centre, therefore One is generated from optical centre to the error of unmanned plane GPS physical locations.Therefore, if its error prediction formula is:\n\nWhereinThe constant term of error prediction model, a are represented respectively11~a33Represent that forecast model is each respectively The coefficient of parameter.\n\nFor Δ XsBeing write as matrix form is:\n\nΔXs=AX\n\nIn formula:\n\nN width images are then utilized, can be obtained on Δ XsN equation, be expressed as Δ Xsi=AiX, can with matrix To be expressed as:\n\nΔXs=AX\n\nWherein:\n\nSo as to which according to least square method, normal equation can be listed\n\nAΤAX=AΤΔXs\n\nThen the vectorial solution of unknown number is:\n\nX=(AΤA)-1AΤΔXs\n\nΔ Y can similarly be obtainedsWith Δ ZsUnknown parameter coefficient, so as to obtain on unmanned plane longitude and latitude and height big Error compensation formula under ground coordinate system:\n\n2) error compensation of unmanned plane and platform stance calculates\n\nBecause the influence of measurement of the platform attitude angle to the flight attitude angle of unmanned plane is smaller, therefore, in analysis unmanned plane Aspect error when, need to only consider the angle of pitch, aircraft roll angle and vector angle of aircraft.And for platform appearance The error of state, the posture of unmanned plane have a certain impact to it, thus should using UAV Attitude and platform stance together as The influence factor of platform stance error considers.\n\nTherefore, for the attitude error of unmanned plane, we set its error prediction formula as:\n\nWhereinThe constant term of error prediction model, b are represented respectively11~b33Represent that forecast model is each respectively The coefficient of parameter.N width images are recycled, it is right respectivelyΔω2、Δκ2N equation is listed, obtains normal equation, is obtained unknown Number, so as to obtainω2、κ2Compensation formula:\n\nFor platform attitude angle, if its error prediction formula is:\n\nN width images are recycled, respectively to Δ ω1、Δκ1N equation is listed, obtains normal equation, obtains unknown number, so as to To ω1、κ1Compensation formula:\n\nWhereinThe constant term of error prediction model, c are represented respectively11~c25Forecast model parameters are represented respectively Coefficient.\n\n, can will be normal in error prediction formula here it is worth noting that in the case of the image quantity taken Several I compensate as prediction error:\n\nAnd enriched in amount of images, there is preferable representativeness to be, can be to be compensated using error prediction formula.\n\nIn order to correct the error of the telemetry parameter of unmanned plane, it is distant that the present invention proposes a kind of unmanned plane based on online calibration Survey parameter correction method.This method needs to be flown according to both tramp-liners before execution task, and obtains multiple and include ground The image at face control point, so as to using list as the thought of resection analyze unmanned plane longitude and latitude is high and each attitude angle Error.Go out the error prediction formula of parameters using least square fitting afterwards, error benefit is carried out for follow-up telemetry parameter Repay.\n\n## Claims (3)\n\n1. a kind of unmanned plane telemetry parameter modification method based on online calibration, including following steps:\nThe first step, flight course planning is carried out according to the distribution situation of ground control point;\nAccording to the distribution situation of ground control point, unmanned plane is made to carry out continuing bat to the area comprising at least four ground control point Take the photograph, obtain the shooting image in the case of unmanned plane multi-angle;\nSecond step, image are chosen and record corresponding telemetry intelligence (TELINT);\nThe multiple image of user's set angle is chosen in the image obtained from planning air strips, is specially:It is every from image sequence A two field picture is obtained every certain frame number;The every two field picture for recording acquisition simultaneously corresponds to the aircraft telemetry intelligence (TELINT) at moment, aircraft remote measurement Longitude of the information including aircraft, latitude, height, aircraft pitch angle, aircraft roll angle, vector angle, platform angle of site peace Platform azimuth;\n3rd step, obtain the pixel coordinate at control point;\nAccording to ground control point, its corresponding image pixel coordinates is obtained;\n4th step, the error analysis based on space resection;\nBy the use of the corresponding aircraft telemetry parameter of image as initial value, error equation is listed according to collinearity equation, utilization is multiple Control point obtains multigroup error equation, and obtains normal equation according to least square method, tries to achieve the correction of unmanned plane telemetry parameter Number;\n5th step, the error obtained according to multiple image carry out error prediction model foundation;\nSpecifically:\n1) unmanned plane longitude and latitude and the error prediction of height\nError prediction formula is:\nWherein:Xs, Ys, Zs, represent final revised parameter value;Wherein, Δ Xs,ΔYs,ΔZsRepresent that parameters most terminate The correction of fruit;\nWhereinThe constant term of error prediction model, a are represented respectively11~a33Forecast model parameters are represented respectively Coefficient;For Δ XsBeing write as matrix form is:\nΔXs=AX\nIn formula:\nA=[1 Xs Ys Zs]\nWherein:A is coefficient matrix, and X is correction matrix number to be asked;\nN width images are then utilized, are obtained on Δ XsN equation, be expressed asIt is expressed in matrix as:\nΔXs=AX\nWherein:\nA=[A1 A2 … An]T\nSo as to according to least square method, list normal equation\nATAX=ATΔXs\nThen the vectorial solution of unknown number is:\nX=(ATA)-1ATΔXs\nSimilarly obtain Δ YsWith Δ ZsUnknown parameter coefficient, so as to obtain on unmanned plane longitude and latitude and height in earth coordinates Under error compensation formula:\nWherein:Xs0,Ys0,Zs0Represent the initial value of parameters;\n2) error compensation of unmanned plane and platform stance calculates\nThe attitude error predictor formula of unmanned plane is:\nWherein:ω2,k2Represent final revised parameter value;Wherein,Δω2,Δκ2Represent that parameters most terminate The correction of fruit;The constant term of error prediction model, b are represented respectively11~b33The each ginseng of forecast model is represented respectively Several coefficients;It is right respectively using n width imagesΔω2、Δκ2N equation is listed, obtains normal equation, obtains unknown number, from And obtainω2、κ2Compensation formula:\nWherein:ω20,k20Represent the initial value of parameters;\nFor platform attitude angle, if its error prediction formula is:\nWherein:ω1,k1Represent final revised parameter value;Wherein, Δ ω1Δκ1Represent the correction of parameters final result Number;Using n width images, respectively to Δ ω1、Δκ1N equation is listed, obtains normal equation, obtains unknown number, so as to obtain ω1、 κ1Compensation formula:\nWherein:ω10,k10The initial value of parameters is represented,The constant term of error prediction model, c are represented respectively11~c25 The coefficient of forecast model parameters is represented respectively;In the case of the image quantity taken, by error prediction formula Constant term I as prediction error compensate:\nIn the case that the amount of images taken is more, compensated using error prediction formula;\n2. a kind of unmanned plane telemetry parameter modification method based on online calibration according to claim 1, described first Step specifically includes:\n1) control point is arranged;\nIf the camera focus of unmanned plane is f, pixel dimension μ, the image a height of W*L of wide * of shooting, the working depth of aircraft is H, In the case of regarding under vertical, the geographic range that image is covered is (W*H* μ/f) * (L*H* μ/f), divides the image into nine grids Form, 4 ground control points are individually positioned in the position at four angles of nine grids, the upper left corner is set to No. 1 control point, The upper right corner is No. 2 control points, and the lower left corner is set to No. 3 control points, and the lower right corner is No. 4 control points, it is first determined No. 1 control point Position, in No. 1 control point east sideIn the range of dispose No. 2 control points, in No. 1 control point south SideIn the range of dispose No. 3 control points, then determine No. 4 by No. 2 control points and No. 3 control points Control point;\n2) course line is planned, ensures posture coverage;\nPlan course line so that vector angle and platform deflection be with due north angle, clockwise for just, the platform angle of site is With horizontal plane angle, vertically lower apparent time is 90 °.\n3. a kind of unmanned plane telemetry parameter modification method based on online calibration according to claim 1, the described the 4th Step specifically includes:\nIf geodetic coordinates corresponding to ground control point is (X, Y, Z), geodetic coordinates corresponding to the high information of longitude and latitude of unmanned plane is (Xs, Ys, Zs), camera focus f, x, y are image pixel coordinates corresponding to ground control point corresponding under platform for video camera coordinate system Value, if platform azimuth is κ1, the platform angle of site is ω1, aircraft pitch angle isAircraft roll angle is ω2, vector angle For κ2\n1) spin matrix R is calculated according to aspect information:\nThe transformational relation of platform for video camera coordinate and northeast day coordinate is in image:\nWherein:Represent coordinate value of the picture point (x, y) under northeast day coordinate system, a1~c3Represent that spin matrix R's is each Value, RX,RY,RZExpression rotates the spin matrix of corresponding attitude angle around X, Y, Z axis, and R is represented from Camera Platform coordinate system to northeast The transformation matrix of its coordinate system;\n2) approximation (x) of the pixel coordinate at control point, (y) are calculated according to collinearity condition equation;\nIn formula:λ is scale factor, then is write as matrix form and be\nBecause R is orthogonal matrix, then RT=R-1, so as to obtain relation\nAnd then obtain the imaging equation of central projection, also known as collinearity condition equation:\nBy the use of the telemetry parameter of unmanned plane as initial value, bring collinearity condition equation into and obtain the approximation of control point picpointed coordinate (x)、(y);\n3) error equation is obtained according to collinearity equation\nBy the Linearization of Collinearity Equations and a sub-minimum item is taken to obtain:\nThe geodetic coordinates at control point is considered as true value, and corresponding picpointed coordinate is considered as observation, then according to observation+observation It is worth the principle of correction=approximation+approximation correction, makes vx, vyFor x, y observation correction obtains:\nList the error equation of each point\nIf by each coefficient a of above formula11..., a28Represent, then write as\nWherein:lx,lyRepresent x, the difference between y observation and approximation;\nIt is expressed as with matrix form:\nV=AX-l\nIn formula:\nV=[vx,vy]T\nL=[lx ly]T\nWherein l is error matrix\n4) coefficient of each correction is calculated\nIt is by the molecule in collinearity equation, denominator tabular form:\nThen calculate\nSimilarly, coefficient is calculated:\nSeparately have:\nWherein, due to\nSo have\n5) control point calculates one by one, obtains normal equation;\nIf there is n control point, n grouping error equations [V is listed1 V2 … Vn]T, forming overall error equation is:\nV=AX-L\nIn formula:\nV=[V1 V2 … Vn]T\nA=[A1 A2 … An]T\nL=[l1 l2 … ln]T\nAccording to least square method indirect adjustment principle, row normal equation\nATAX=ATL\nSo as to which the vectorial solution for obtaining unknown number is\nX=(ATA)-1ATL\nThat is, correction dX is tried to achieves、dYs、dZs、dω1、dκ12、dκ2\n6) iteration, until corrected value is less than a certain prescribed limits, so as to obtain final error\nBy the improvement number tried to achieve every time compared with limit value, if being unsatisfactory for requiring, by formula\nWherein:dXsi,dYsi,…,dk2iRepresent the correction for the parameters that ith iteration obtains;\nIt is iterated, until correction, which is less than, limits poor, stopping calculating;Then there is the final error to be\nCN201510433736.2A 2015-07-22 2015-07-22 Unmanned plane telemetry parameter modification method based on online calibration CN105180963B (en)\n\n## Priority Applications (1)\n\nApplication Number Priority Date Filing Date Title\nCN201510433736.2A CN105180963B (en) 2015-07-22 2015-07-22 Unmanned plane telemetry parameter modification method based on online calibration\n\n## Applications Claiming Priority (1)\n\nApplication Number Priority Date Filing Date Title\nCN201510433736.2A CN105180963B (en) 2015-07-22 2015-07-22 Unmanned plane telemetry parameter modification method based on online calibration\n\n## Publications (2)\n\nPublication Number Publication Date\nCN105180963A CN105180963A (en) 2015-12-23\nCN105180963B true CN105180963B (en) 2018-02-16\n\n# Family\n\n## Family Applications (1)\n\nApplication Number Title Priority Date Filing Date\nCN201510433736.2A CN105180963B (en) 2015-07-22 2015-07-22 Unmanned plane telemetry parameter modification method based on online calibration\n\n## Country Status (1)\n\nCN (1) CN105180963B (en)\n\n## Families Citing this family (3)\n\n* Cited by examiner, † Cited by third party\nPublication number Priority date Publication date Assignee Title\nCN107192376B (en) * 2017-04-28 2019-05-24 北京航空航天大学 Unmanned plane multiple image target positioning correction method based on interframe continuity\nCN107272733A (en) * 2017-06-13 2017-10-20 深圳市伊特利网络科技有限公司 The unmanned aerial vehicle (UAV) control method and system of terminal positioning\nCN108263606A (en) * 2018-01-29 2018-07-10 四川尚航智能科技有限公司 One kind is based on VTOL fixed-wing unmanned plane and its natural gas line cruising inspection system, method\n\n## Citations (5)\n\n* Cited by examiner, † Cited by third party\nPublication number Priority date Publication date Assignee Title\nCN101126639A (en) * 2007-09-18 2008-02-20 武汉大学 Quick low altitude remote sensing image automatic matching and airborne triangulation method\nCN102190081A (en) * 2010-03-04 2011-09-21 南京航空航天大学 Vision-based fixed point robust control method for airship\nCN103129752A (en) * 2013-02-28 2013-06-05 中国资源卫星应用中心 Dynamic compensation method for attitude angle errors of optical remote sensing satellite based on ground navigation\nCN103345737A (en) * 2013-06-04 2013-10-09 北京航空航天大学 UAV high resolution image geometric correction method based on error compensation\nCN103679711A (en) * 2013-11-29 2014-03-26 航天恒星科技有限公司 Method for calibrating in-orbit exterior orientation parameters of push-broom optical cameras of remote sensing satellite linear arrays\n\n## Patent Citations (5)\n\n* Cited by examiner, † Cited by third party\nPublication number Priority date Publication date Assignee Title\nCN101126639A (en) * 2007-09-18 2008-02-20 武汉大学 Quick low altitude remote sensing image automatic matching and airborne triangulation method\nCN102190081A (en) * 2010-03-04 2011-09-21 南京航空航天大学 Vision-based fixed point robust control method for airship\nCN103129752A (en) * 2013-02-28 2013-06-05 中国资源卫星应用中心 Dynamic compensation method for attitude angle errors of optical remote sensing satellite based on ground navigation\nCN103345737A (en) * 2013-06-04 2013-10-09 北京航空航天大学 UAV high resolution image geometric correction method based on error compensation\nCN103679711A (en) * 2013-11-29 2014-03-26 航天恒星科技有限公司 Method for calibrating in-orbit exterior orientation parameters of push-broom optical cameras of remote sensing satellite linear arrays\n\n## Also Published As\n\nPublication number Publication date\nCN105180963A (en) 2015-12-23\n\n## Similar Documents\n\nPublication Publication Date Title\nSugiura et al. Remote-sensing technology for vegetation monitoring using an unmanned helicopter\nXiang et al. Method for automatic georeferencing aerial remote sensing (RS) images from an unmanned aerial vehicle (UAV) platform\nXiang et al. Development of a low-cost agricultural remote sensing system based on an autonomous unmanned aerial vehicle (UAV)\nEisenbeiss A mini unmanned aerial vehicle (UAV): system overview and image acquisition\nLucieer et al. HyperUAS—Imaging spectroscopy from a multirotor unmanned aircraft system\nVallet et al. Photogrammetric performance of an ultra light weight swinglet UAV\nHu et al. Understanding the rational function model: methods and applications\nGómez-Candón et al. Assessing the accuracy of mosaics from unmanned aerial vehicle (UAV) imagery for precision agriculture purposes in wheat\nUS9898821B2 (en) Determination of object data by template-based UAV control\nWO2009093587A1 (en) Orthophotographic image creating method and imaging device\nUS10203692B2 (en) Structure from motion (SfM) processing for unmanned aerial vehicle (UAV)\nRinaudo et al. Archaeological site monitoring: UAV photogrammetry can be an answer\nEisenbeiss et al. Investigation of UAV systems and flight modes for photogrammetric applications\nUS9336568B2 (en) Unmanned aerial vehicle image processing system and method\nGrenzdörffer et al. The photogrammetric potential of low-cost UAVs in forestry and agriculture\nZhou Near real-time orthorectification and mosaic of small UAV video flow for time-critical event response\nFernández‐Hernandez et al. Image‐based modelling from unmanned aerial vehicle (UAV) photogrammetry: an effective, low‐cost tool for archaeological applications\nUS20120114229A1 (en) Orthorectification and mosaic of video flow\nSamad et al. The potential of Unmanned Aerial Vehicle (UAV) for civilian and mapping application\nEisenbeiss The autonomous mini helicopter: a powerful platform for mobile mapping\nUS9013576B2 (en) Aerial photograph image pickup method and aerial photograph image pickup apparatus\nDelacourt et al. DRELIO: An unmanned helicopter for imaging coastal areas\nRuzgienė et al. The surface modelling based on UAV Photogrammetry and qualitative estimation\nUS9194954B2 (en) Method for geo-referencing an imaged area\nGurtner et al. Investigation of fish-eye lenses for small-UAV aerial photography\n\n## Legal Events\n\nDate Code Title Description\nPB01 Publication\nC06 Publication\nSE01 Entry into force of request for substantive examination\nC10 Entry into substantive examination\nGR01 Patent grant\nGR01 Patent grant" ]
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https://openaccesspub.org/editor-profile/bidyut-bikash-gogoi-2126
[ "### Journal of Precision Agriculture\n\nThe Open Access Pub has the reputation for quick reviewing and publishing original research articles. The editorial boards of our journals have many dedicated and reputed scientists as editorial members. Their support helps many researchers from all countries to enhance their research between scientists of various communities. This platform plays a crucial role in promoting science networks and exchanges.", null, "India\n\nIndian Space Research Organization, Satellite Centre (ISAC), Bengaluru\n\n# Bidyut Bikash Gogoi\n\nIndian Space Research Organization,\n\nSatellite Centre (ISAC),\n\nBengaluru\n\n#### Research Interests:\n\nFluid Mechanics, Modeling and Simulation, Computational Fluid Dynamics, Numerical Simulation, Numerical Modeling, Numerical Analysis, Engineering, Applied and Computational Mathematics, Mechanical Engineering, Mathematical Analysis, Thermal Engineering, MATLAB, Computational Fluid Mechanics, Applied Mathematics, Heat Transfer, Numerical Mathematics, Nonlinear Dynamics, Computational Simulation, Numerics, Computational Mathematics, Stability, Stability Analysis, Finite Difference, Gas Dynamics, Fluid, Fluid Flow, Mathematical Computing, Numerical Methods, Finite-Difference Schemes, Heat & Mass Transfer, Mathematical Biology, Scientific Computation, Numerical Integration, Computing in Mathematics, Nonlinear Physics, Finite Difference Method, Scientific Computing (Computational Science), Industrial Mathematics, Nonlinear Partial Differential Equations, Lattice Boltzmann Method, Space Geodesy, Numerical Heat Transfer, Higher Order Compact Methods\n\n#### Biography:\n\nPublications:\n\n1. HOC Simulation of Double-diffusive Natural Convection in a Rectangular Cavity.\n2. Magic Squares : History, Construction and Applications.\n3. A Very Efficient Class of HOC Schemes for the One-Dimensional Euler Equations of Gas Dynamics.\n4. Global two-dimensional stability of the staggered cavity flow with an HOC approach.\n5. An accurate predictor-corrector Higher order compact solver for the 2D Riemann problem.\n6. Global 2D stability analysis of the cross lid-driven cavity flow with a streamfunction-vorticity approach.\n7. A Biharmonic Approach for the Global Stability Analysis of 2D Incompressible Viscous Flows.\n8. An accurate predictor-corrector HOC solver for the two dimensional Riemann problem of Gas Dynamics.\n9. Lattice Boltzmann Simulation of Transient Natural Convection in a Staggered Cavity with Four Vertically Heated Walls.\n10. NAVIC Time Transfer with Satellite Common View: An Analysis on Choosing Different Reference Times." ]
[ null, "https://openaccesspub.org/uploads/171215100632BidyutGogoi.jpg", null ]
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https://jminded.com/binary-search-algorithm-implementation-with-recursion-in-java/
[ "# Binary Search Algorithm implementation with Recursion in Java\n\nLet me explain the Binary Search algorithm through a well known example of Dictionary. Let us consider, searching a word in a dictionary, in general we directly go to some approximate page [say middle page] start searching from that point. If the name that we are searching is same, then we are done with the search. If the page is before the selected pages then apply the same process[call the method to itself with different arguments to do the process]  for the first half otherwise apply the same process to the second half [call the method to itself, with second half related arguments]. Binary Search also works in similar fashion considering one half of the list and throwing the other half. Algorithm following such a strategy is called Binary Search.\n\nRecurrence for binary search algorithm T(n)=T(n/2)+Θ(1)+Sack Overhead  , this is because we are always considering one half of the input list throwing out the other half and as we are using Recursion, a function calling to it self, It uses Stack space pushing and popping of activation records of method calls.\n\nTo solve this Recurrence relation if we use Divide and Conquer Master theorem, we get, T(n)=O(logn) +Stack Overhead\nTime complexity : O(logn)  :: Space complexity : O(logn)  [for Recursive algorithm]\n\nAs stack overhead is involved, this algorithm must be little slower than iterative approach.\n\n### Binary Search Algorithm implementation with Recursion\n\n```package com.jminded.algorithms.search;\n\npublic class BinarySearchRecursiveAlgorithm {\n\n/**\n* @param args\n*/\npublic static void main(String[] args) {\n// TODO Auto-generated method stub\nint[] arr={0,1,2,4,5,6,7};\nint searchIndex=binarySearch(arr,3,0,arr.length);\nSystem.out.println(\"Element at search index \"+searchIndex);\nsearchIndex=binarySearch(arr, 7,0,arr.length);\nSystem.out.println(\"Element at search index \"+searchIndex);\n}\n/**\n* <p>Binary Search Recursive Algorithm</p>\n* @param a\n* @param number\n* @param low\n* @param high\n* @return search Index\n* Recurrence relation :: T(n/2)+O(1)\n* Time Complexity :: O(logn)\n*\n*/\npublic static int binarySearch(int[] a,int number,int low,int high){\nint mid=low+(high-low)/2;\nif(low>high){\nreturn -1;\n}else{\nif(a[mid]==number)\nreturn mid;\nelse if(a[mid]<number) //recursive case.\nreturn binarySearch(a, number, mid+1, high);\nelse\nreturn binarySearch(a, number, low, mid-1);\n}\n\n}\n\n}```" ]
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https://datacube-core.readthedocs.io/en/latest/dev/api/generate/datacube.utils.geometry.Geometry.html
[ "# datacube.utils.geometry.Geometry¶\n\nclass datacube.utils.geometry.Geometry(geo, crs=None)[source]\n\n2D Geometry with CRS\n\nInstantiate with a GeoJSON structure\n\nIf 3D coordinates are supplied, they are converted to 2D by dropping the Z points.\n\n__init__(geo, crs=None)[source]\n\nInitialize self. See help(type(self)) for accurate signature.\n\nMethods\n\n __init__(geo[, crs]) Initialize self. buffer(distance[, quadsecs]) contains(*args) Contains(Geometry self, Geometry other) -> bool crosses(*args) Crosses(Geometry self, Geometry other) -> bool difference(*args) Difference(Geometry self, Geometry other) -> Geometry disjoint(*args) Disjoint(Geometry self, Geometry other) -> bool interpolate(distance) Returns a point distance units along the line or None if underlying geometry doesn’t support this operation. intersection(*args) Intersection(Geometry self, Geometry other) -> Geometry intersects(*args) Intersects(Geometry self, Geometry other) -> bool overlaps(*args) Overlaps(Geometry self, Geometry other) -> bool segmented(resolution) Possibly add more points to the geometry so that no edge is longer than resolution simplify(tolerance) symmetric_difference(*args) SymDifference(Geometry self, Geometry other) -> Geometry to_crs(crs[, resolution, wrapdateline]) Convert geometry to a different Coordinate Reference System touches(*args) Touches(Geometry self, Geometry other) -> bool union(*args) Union(Geometry self, Geometry other) -> Geometry within(*args) Within(Geometry self, Geometry other) -> bool\n\nAttributes\n\n area boundary boundingbox centroid convex_hull coords envelope is_empty is_valid json length points type wkt" ]
[ null ]
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https://www.vedantu.com/formula/strain-formula
[ "# Strain Formula\n\n## What is the Formula of Strain?\n\nStrain is a deformation measurement that represents the displacement of particles in the body in relation to a reference length. Strain is defined as a change in the shape or size of a body caused by a deforming force.\n\nThe strain equation is represented by the Greek letter epsilon (ε).\n\nε = $\\frac{\\text{Change in dimension}}{Original dimension}$ = $\\frac{\\Delta x}{x}$\n\nSince strain is a ratio of two similar quantities, it is dimensionless.\n\n### Strain Example:\n\nWhen a body is subjected to a tension force along its length then there develops stress due to which the body experiences a longitudinal strain along the length. Similarly when the same body is subjected to loading in all directions then the body will experience a volumetric strain. If the body is loaded parallel to the axis then shearing occurs which results in shearing strain.\n\n## Types of Strain\n\nThere are three types of strain:\n\n• Longitudinal strain\n\n• Volumetric strain\n\n• Shearing strain\n\n### Longitudinal Strain\n\nThe strain produced by a deforming force that only changes length is known as longitudinal strain. The ratio of the change in length to the initial length is used to calculate the longitudinal strain formula.\n\nThe longitudinal strain formula physics is given as follows:\n\nε$_{L}$ = $\\frac{\\text{Change in length}}{Original length}$ = $\\frac{\\Delta L}{L}$\n\n### Volumetric Strain\n\nThe strain is called volume strain when the deforming force changes volume. The ratio of change in volume to the original volume is used to calculate the volumetric strain formula.\n\nThe volumetric strain formula physics is given as follows:\n\nε$_{v}$ = $\\frac{\\text{Change in volume}}{Original volume}$ = $\\frac{\\Delta v}{v}$\n\n### Shearing Strain\n\nShearing strain occurs when a deforming force causes a change in the shape of the body. It's calculated as the difference between the original location and the displacement of the surface in direct contact with the applied shear stress. Shear strain is represented by the lowercase Greek letter gamma (ℽ) or Greek letter epsilon (ε).\n\nThe shear strain formula physics is given as follows:\n\nγ = ε$_{s}$ = $\\frac{\\text{Change in volume}}{Original volume}$ = $\\frac{\\Delta v}{v}$\n\n### Solved Examples on Strain Formula\n\n1) Calculate the Longitudinal Strain if the Original Length of the Body is 10cm and After Stretching the Length of the Body Is 10.2 Cm.\n\nAns: Here the original length is L = 10cm.\n\nTo calculate the change in length, we have to subtract the final length from the original length. So the change in length is,\n\n$\\Delta$L = 10.2 - 10 = 0.2 cm\n\nNow the longitudinal strain formula is given as follows:\n\nε$_{L}$ = $\\frac{\\text{Change in length}}{Original length}$ = $\\frac{\\Delta L}{L}$\n\nSubstituting the values we get,\n\nε$_{L}$ = $\\frac{0.2}{10}$ = 0.02 cm\n\nTherefore, the longitudinal strain is 0.02 cm.\n\n2) If the Longitudinal Strain of the Body is 0.0125 and the Original Length is 8 Cm. Calculate the Change in Length of the Body.\n\nAns: Here the longitudinal strain is ε$_{L}$ = 0.0125.\n\nThe original length is L = 8 cm.\n\nTo calculate the change in length we will use the longitudinal strain equation\n\nε$_{L}$ = $\\frac{\\text{Change in length}}{Original length}$ = $\\frac{\\Delta L}{L}$\n\nSubstituting the values we get,\n\n0.0125 = $\\frac{\\Delta L}{8}$\n\n0.0125 x 8 = $\\Delta$L\n\n$\\Delta$L = 0.1 cm\n\nTherefore, the change in length of the body is 0.1 cm.\n\n3) Calculate the Original Length of the Body if the Longitudinal Strain is 0.015 and the Change in Length is 0.3 Cm.\n\nAns: Here the longitudinal strain is ε$_{L}$ = 0.015.\n\nChange in length is $\\Delta$L = 0.3 cm\n\nTo calculate the original length we will use the longitudinal strain equation\n\nε$_{L}$ = $\\frac{\\text{Change in length}}{Original length}$ = $\\frac{\\Delta L}{L}$\n\nSubstituting the values we get\n\n0.015 = $\\frac{0.3}{L}$\n\nL = $\\frac{0.3}{0.015}$\n\nL = 20 cm.\n\nTherefore, the original length of the body is 20 cm.\n\n### Conclusion\n\nStrain is a word used to describe deformation in terms of relative particle displacement in the body, excluding rigid-body motions. External loads, body forces such as gravity or electromagnetic forces, changes in temperature, moisture content, or chemical reactions, among other things, can induce deformation. A deformation field occurs in a continuous body as a result of a stress field caused by applied forces or as a result of changes in the temperature field inside the body. Constitutive equations represent the relationship between stresses and induced strains and are used to solve a variety of structural problems.\n\nQ1: What is a Strain?\n\nAns: Strain is a term used to describe the result of stress. The strain is a measurement of how much the body has distorted in comparison to its original shape as a result of the force's action. The strain is represented by the Greek letter epsilon (ε).\n\nQ2: What is the Strain Equation?\n\nAns: Strain is defined as a change in the shape or size of a body caused by a deforming force.\n\nIt is given by the formula\n\nε = Change in dimension/Original dimension = Δx/x\n\nQ3: What are the Types of Strain?\n\nAns: There are three types of strain:\n\nLongitudinal Strain\n\nεL = Change in length/Original length = ΔL/L\n\nVolumetric Strain\n\nεV = Change in volume/Original volume = Δv/v\n\nShearing Strain\n\nγ = εs = Change in volume/Original volume = Δv/v" ]
[ null ]
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https://en.wikipedia.org/wiki/Leech_lattice
[ "# Leech lattice\n\nIn mathematics, the Leech lattice is an even unimodular lattice Λ24 in 24-dimensional Euclidean space, which is one of the best models for the kissing number problem. It was discovered by John Leech (1967). It may also have been discovered (but not published) by Ernst Witt in 1940.\n\n## Characterization\n\nThe Leech lattice Λ24 is the unique lattice in E24 with the following list of properties:\n\n• It is unimodular; i.e., it can be generated by the columns of a certain 24×24 matrix with determinant 1.\n• It is even; i.e., the square of the length of each vector in Λ24 is an even integer.\n• The length of every non-zero vector in Λ24 is at least 2.\n\nThe last condition is equivalent to the condition that unit balls centered at the points of Λ24 do not overlap. Each is tangent to 196,560 neighbors, and this is known to be the largest number of non-overlapping 24-dimensional unit balls that can simultaneously touch a single unit ball (compare with 6 in dimension 2, as the maximum number of pennies which can touch a central penny; see kissing number). This arrangement of 196,560 unit balls centred about another unit ball is so efficient that there is no room to move any of the balls; this configuration, together with its mirror-image, is the only 24-dimensional arrangement where 196,560 unit balls simultaneously touch another. This property is also true in 1, 2 and 8 dimensions, with 2, 6 and 240 unit balls, respectively, based on the integer lattice, hexagonal tiling and E8 lattice, respectively.\n\nIt has no root system and in fact is the first unimodular lattice with no roots (vectors of norm less than 4), and therefore has a centre density of 1. By multiplying this value by the volume of a unit ball in 24 dimensions, ${\\tfrac {\\pi ^{12}}{12!}}$", null, ", one can derive its absolute density.\n\nConway (1983) showed that the Leech lattice is isometric to the set of simple roots (or the Dynkin diagram) of the reflection group of the 26-dimensional even Lorentzian unimodular lattice II25,1. By comparison, the Dynkin diagrams of II9,1 and II17,1 are finite.\n\n## Applications\n\nThe binary Golay code, independently developed in 1949, is an application in coding theory. More specifically, it is an error-correcting code capable of correcting up to three errors in each 24-bit word, and detecting a fourth. It was used to communicate with the Voyager probes, as it is much more compact than the previously-used Hadamard code.\n\nQuantizers, or analog-to-digital converters, can use lattices to minimise the average root-mean-square error. Most quantizers are based on the one-dimensional integer lattice, but using multi-dimensional lattices reduces the RMS error. The Leech lattice is a good solution to this problem, as the Voronoi cells have a low second moment.\n\nThe vertex algebra of the two-dimensional conformal field theory describing bosonic string theory, compactified on the 24-dimensional quotient torus R2424 and orbifolded by a two-element reflection group, provides an explicit construction of the Griess algebra that has the monster group as its automorphism group. This monster vertex algebra was also used to prove the monstrous moonshine conjectures.\n\n## Constructions\n\nThe Leech lattice can be constructed in a variety of ways. As with all lattices, it can be constructed by taking the integral span of the columns of its generator matrix, a 24×24 matrix with determinant 1.\n\nLeech generator matrix\n\nA 24x24 generator (in row convention) for the Leech Lattice is given by the following matrix divided by ${\\sqrt {8}}$", null, ":\n\n 8 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n2 2 2 2 2 2 2 2 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 0 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 0 0 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 0 0 0 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0 0 0\n2 2 2 2 0 0 0 0 2 2 2 2 0 0 0 0 0 0 0 0 0 0 0 0\n4 0 0 0 0 0 0 0 0 0 0 0 4 0 0 0 0 0 0 0 0 0 0 0\n2 2 0 0 2 2 0 0 2 2 0 0 2 2 0 0 0 0 0 0 0 0 0 0\n2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 0 0 0 0 0 0 0 0\n2 0 0 2 2 0 0 2 2 0 0 2 2 0 0 2 0 0 0 0 0 0 0 0\n4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4 0 0 0 0 0 0 0\n2 0 2 0 2 0 0 2 2 2 0 0 0 0 0 0 2 2 0 0 0 0 0 0\n2 0 0 2 2 2 0 0 2 0 2 0 0 0 0 0 2 0 2 0 0 0 0 0\n2 2 0 0 2 0 2 0 2 0 0 2 0 0 0 0 2 0 0 2 0 0 0 0\n0 2 2 2 2 0 0 0 2 0 0 0 2 0 0 0 2 0 0 0 2 0 0 0\n0 0 0 0 0 0 0 0 2 2 0 0 2 2 0 0 2 2 0 0 2 2 0 0\n0 0 0 0 0 0 0 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0\n−3 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1\n\n\n\n### Using the binary Golay code\n\nThe Leech lattice can be explicitly constructed as the set of vectors of the form 2−3/2(a1, a2, ..., a24) where the ai are integers such that\n\n$a_{1}+a_{2}+\\cdots +a_{24}\\equiv 4a_{1}\\equiv 4a_{2}\\equiv \\cdots \\equiv 4a_{24}{\\pmod {8}}$", null, "and for each fixed residue class modulo 4, the 24 bit word, whose 1s correspond to the coordinates i such that ai belongs to this residue class, is a word in the binary Golay code. The Golay code, together with the related Witt design, features in a construction for the 196560 minimal vectors in the Leech lattice.\n\n### Using the Lorentzian lattice II25,1\n\nThe Leech lattice can also be constructed as $w^{\\perp }/w$", null, "where w is the Weyl vector:\n\n$(0,1,2,3,\\dots ,22,23,24;70)$", null, "in the 26-dimensional even Lorentzian unimodular lattice II25,1. The existence of such an integral vector of norm zero relies on the fact that 12 + 22 + ... + 242 is a perfect square (in fact 702); the number 24 is the only integer bigger than 1 with this property. This was conjectured by Édouard Lucas, but the proof came much later, based on elliptic functions.\n\nThe vector $(0,1,2,3,\\dots ,22,23,24)$", null, "in this construction is really the Weyl vector of the even sublattice D24 of the odd unimodular lattice I25. More generally, if L is any positive definite unimodular lattice of dimension 25 with at least 4 vectors of norm 1, then the Weyl vector of its norm 2 roots has integral length, and there is a similar construction of the Leech lattice using L and this Weyl vector.\n\n### Based on other lattices\n\nConway & Sloane (1982) described another 23 constructions for the Leech lattice, each based on a Niemeier lattice. It can also be constructed by using three copies of the E8 lattice, in the same way that the binary Golay code can be constructed using three copies of the extended Hamming code, H8. This construction is known as the Turyn construction of the Leech lattice.\n\n### As a laminated lattice\n\nStarting with a single point, Λ0, one can stack copies of the lattice Λn to form an (n + 1)-dimensional lattice, Λn+1, without reducing the minimal distance between points. Λ1 corresponds to the integer lattice, Λ2 is to the hexagonal lattice, and Λ3 is the face-centered cubic packing. Conway & Sloane (1982b) showed that the Leech lattice is the unique laminated lattice in 24 dimensions.\n\n### As a complex lattice\n\nThe Leech lattice is also a 12-dimensional lattice over the Eisenstein integers. This is known as the complex Leech lattice, and is isomorphic to the 24-dimensional real Leech lattice. In the complex construction of the Leech lattice, the binary Golay code is replaced with the ternary Golay code, and the Mathieu group M24 is replaced with the Mathieu group M12. The E6 lattice, E8 lattice and Coxeter–Todd lattice also have constructions as complex lattices, over either the Eisenstein or Gaussian integers.\n\n### Using the icosian ring\n\nThe Leech lattice can also be constructed using the ring of icosians. The icosian ring is abstractly isomorphic to the E8 lattice, three copies of which can be used to construct the Leech lattice using the Turyn construction.\n\n### Witt's construction\n\nIn 1972 Witt gave the following construction, which he said he found in 1940 January 28. Suppose that H is an n by n Hadamard matrix, where n=4ab. Then the matrix ${\\begin{pmatrix}Ia&H/2\\\\H/2&Ib\\end{pmatrix}}$", null, "defines a bilinear form in 2n dimensions, whose kernel has n dimensions. The quotient by this kernel is a nonsinguar bilinear form taking values in (1/2)Z. It has 3 sublattices of index 2 that are integral bilinear forms. Witt obtained the Leech lattice as one of these three sublattices by taking a=2, b=3, and taking H to be the 24 by 24 matrix (indexed by Z/23Z ∪ ∞) with entries Χ(m+n) where Χ(∞)=1, Χ(0)=−1, Χ(n)=is the quadratic residue symbol mod 23 for nonzero n. This matrix H is a Paley matrix with some insignificant sign changes.\n\n### Using a Paley matrix\n\nChapman (2001) described a construction using a skew Hadamard matrix of Paley type. The Niemeier lattice with root system $D_{24}$", null, "can be made into a module for the ring of integers of the field $\\mathbb {Q} ({\\sqrt {-23}})$", null, ". Multiplying this Niemeier lattice by a non-principal ideal of the ring of integers gives the Leech lattice.\n\n### Using octonions\n\nIf L is the set of octonions with coordinates on the $E_{8}$", null, "lattice, then the Leech lattice is the set of triplets $(x,y,z)$", null, "such that\n\n$x,y,z\\in L$", null, "$x+y,y+z,x+z\\in L{\\bar {s}}$", null, "$x+y+z\\in Ls$", null, "where $s{\\bar {s}}={\\frac {1}{2}}(s_{x}{\\bar {s}}_{x}+s_{y}{\\bar {s}}_{y}+s_{z}{\\bar {s}}_{z})=2$", null, ".\n\n## Symmetries\n\nThe Leech lattice is highly symmetrical. Its automorphism group is the Conway group Co0, which is of order 8 315 553 613 086 720 000. The center of Co0 has two elements, and the quotient of Co0 by this center is the Conway group Co1, a finite simple group. Many other sporadic groups, such as the remaining Conway groups and Mathieu groups, can be constructed as the stabilizers of various configurations of vectors in the Leech lattice.\n\nDespite having such a high rotational symmetry group, the Leech lattice does not possess any hyperplanes of reflection symmetry. In other words, the Leech lattice is chiral. It also has far fewer symmetries than the 24-dimensional hypercube and simplex.\n\nThe automorphism group was first described by John Conway. The 398034000 vectors of norm 8 fall into 8292375 'crosses' of 48 vectors. Each cross contains 24 mutually orthogonal vectors and their negatives, and thus describe the vertices of a 24-dimensional orthoplex. Each of these crosses can be taken to be the coordinate system of the lattice, and has the same symmetry of the Golay code, namely 212 × |M24|. Hence the full automorphism group of the Leech lattice has order 8292375 × 4096 × 244823040, or 8 315 553 613 086 720 000.\n\n## Geometry\n\nConway, Parker & Sloane (1982) showed that the covering radius of the Leech lattice is ${\\sqrt {2}}$", null, "; in other words, if we put a closed ball of this radius around each lattice point, then these just cover Euclidean space. The points at distance at least ${\\sqrt {2}}$", null, "from all lattice points are called the deep holes of the Leech lattice. There are 23 orbits of them under the automorphism group of the Leech lattice, and these orbits correspond to the 23 Niemeier lattices other than the Leech lattice: the set of vertices of deep hole is isometric to the affine Dynkin diagram of the corresponding Niemeier lattice.\n\nThe Leech lattice has a density of ${\\tfrac {\\pi ^{12}}{12!}}\\approx 0.001930\\ldots$", null, ". Cohn & Kumar (2009) showed that it gives the densest lattice packing of balls in 24-dimensional space. Henry Cohn, Abhinav Kumar, and Stephen D. Miller et al. (2016) improved this by showing that it is the densest sphere packing, even among non-lattice packings.\n\nThe 196560 minimal vectors are of three different varieties, known as shapes:\n\n• 1104 vectors of shape (42,022), for all permutations and sign choices;\n• 97152 vectors of shape (28,016), where the '2's correspond to octads in the Golay code, and there is an even number of minus signs;\n• 98304 vectors of shape (-3,123), where the changes of signs come from the Golay code, and the '3' can appear in any position.\n\nThe ternary Golay code, binary Golay code and Leech lattice give very efficient 24-dimensional spherical codes of 729, 4096 and 196560 points, respectively. Spherical codes are higher-dimensional analogues of Tammes problem, which arose as an attempt to explain the distribution of pores on pollen grains. These are distributed as to maximise the minimal angle between them. In two dimensions, the problem is trivial, but in three dimensions and higher it is not. An example of a spherical code in three dimensions is the set of the 12 vertices of the regular icosahedron.\n\n## Theta series\n\nOne can associate to any (positive-definite) lattice Λ a theta function given by\n\n$\\Theta _{\\Lambda }(\\tau )=\\sum _{x\\in \\Lambda }e^{i\\pi \\tau \\|x\\|^{2}}\\qquad \\operatorname {Im} \\tau >0.$", null, "The theta function of a lattice is then a holomorphic function on the upper half-plane. Furthermore, the theta function of an even unimodular lattice of rank n is actually a modular form of weight n/2 for the full modular group PSL(2,Z). The theta function of an integral lattice is often written as a power series in $q=e^{2i\\pi \\tau }$", null, "so that the coefficient of qn gives the number of lattice vectors of squared norm 2n. In the Leech lattice, there are 196560 vectors of squared norm 4, 16773120 vectors of squared norm 6, 398034000 vectors of squared norm 8 and so on. The theta series of the Leech lattice is\n\n{\\begin{aligned}\\Theta _{\\Lambda _{24}}(\\tau )&=E_{12}(\\tau )-{\\frac {65520}{691}}\\Delta (\\tau )\\\\[5pt]&=1+\\sum _{m=1}^{\\infty }{\\frac {65520}{691}}\\left(\\sigma _{11}(m)-\\tau (m)\\right)q^{m}\\\\[5pt]&=1+196560q^{2}+16773120q^{3}+398034000q^{4}+\\cdots ,\\end{aligned}}", null, "where $E_{12}(\\tau )$", null, "is the normalized Eisenstein series of weight 12, $\\Delta (\\tau )$", null, "is the modular discriminant, $\\sigma _{11}(n)$", null, "is the divisor function for exponent 11, and $\\tau (n)$", null, "is the Ramanujan tau function. It follows that for m≥1 the number of vectors of squared norm 2m is\n\n${\\frac {65520}{691}}\\left(\\sigma _{11}(m)-\\tau (m)\\right).$", null, "## History\n\nMany of the cross-sections of the Leech lattice, including the Coxeter–Todd lattice and Barnes–Wall lattice, in 12 and 16 dimensions, were found much earlier than the Leech lattice. O'Connor & Pall (1944) discovered a related odd unimodular lattice in 24 dimensions, now called the odd Leech lattice, one of whose two even neighbors is the Leech lattice. The Leech lattice was discovered in 1965 by John Leech (1967, 2.31, p. 262), by improving some earlier sphere packings he found (Leech 1964).\n\nConway (1968) calculated the order of the automorphism group of the Leech lattice, and, working with John G. Thompson, discovered three new sporadic groups as a by-product: the Conway groups, Co1, Co2, Co3. They also showed that four other (then) recently announced sporadic groups, namely, Higman-Sims, Suzuki, McLaughlin, and the Janko group J2 could be found inside the Conway groups using the geometry of the Leech lattice. (Ronan, p. 155)\n\nBei dem Versuch, eine Form aus einer solchen Klasse wirklich anzugeben, fand ich mehr als 10 verschiedene Klassen in Γ24\n\nWitt (1941, p. 324)\n\nWitt (1941, p. 324), has a single rather cryptic sentence mentioning that he found more than 10 even unimodular lattices in 24 dimensions without giving further details. Witt (1998, p. 328–329) stated that he found 9 of these lattices earlier in 1938, and found two more, the Niemeier lattice with A24\n1\nroot system and the Leech lattice (and also the odd Leech lattice), in 1940." ]
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https://mathematics.pitt.edu/research-areas/numerical-analysis-and-scientific-computing
[ "# Numerical Analysis and Scientific Computing\n\nThe diversity of this group is reflected in its research interests, which range over such areas as numerical analysis of partial differential equations, adaptive methods for scientific computing, computational methods of fluid dynamics and turbulence, numerical solution of nonlinear problems arising from porous media flow and transport, optimal control, and simulation of stochastic reaction diffusion systems. There are weekly seminars, as well as lectures and workshops at the Pittsburgh Supercomputing Center, on current trends in scientific supercomputing.\n\n### Burhkardt's Research (Part-Time Faculty)\n\nJohn Burkardt's research has usually involved collaboration with numerical analysts.  The scientist usually has a general idea of how to solve a problem, but John's task is to design and implement a corresonding computer program.  The program accepts a description of the problem to be solved, and creates reports or pictures of the results.  Since this is usually an experimental process, the program must be repeatedly corrected or refined.  This is done by working with the scientist to choose test cases, decide whether the program is working effectively, find remedies when the program fails, and search for improvements that make the program more accurate, faster, or able to solve a wider range of problems.  His research projects have addressed the probems found here.\n\nMany of the research programs he has worked on are available at https://people.sc.fsu.edu/~jburkardt/.\n\n### Layton's Research (Professor)\n\nDr. Layton's research involves modeling the large eddies (such as storm fronts, hurricanes and tornadoes in the atmosphere) in turbulent flow, predicting their motion in computational experiments and validating mathematically the large eddy models and algorithms developed. Current approaches to LES seem to be presently confronting some barriers to resolution, accuracy and predictability. It seems likely that many of these barriers can be traced to the mathematical foundation of the models used, the boundary conditions imposed and the algorithms employed for the simulations. The goal of Dr. Layton's research is to develop these mathematical foundations as a guide for practical computation. This research promises to make it possible to extend the range of accuracy and reliability of predictions important to applications, such as those described above, where technological progress requires confronting turbulence! In all these aspects of analysis, modeling, algorithm development, numerical analysis and experimentation, common themes include: Mathematical analysis as a guide to practical computation and Numerical analysis as a guide to understanding phenomena rather than \"solving equations\".\n\n### Neilan's Research (Assoc. Professor, Colloquium Chair)\n\nDr. Neilan's research interests include finite element methods and their convergence analysis for fully nonlinear partial differential equations. His current focus is on the construction and analysis of reliable and efficient numerical methods for the Monge-Ampere equation though the use of simple and practical finite elements.  Other research interests of his include the numerical approximation of fluid flow (Stokes/Navier Stokes/Brinkman), the design and implementation of fourth and sixth order elliptic PDEs that arise in, e.g.,  plate bending and phase-field problems,  the theory and construction of nonconforming finite element methods, and singular perturbation problems.\n\n### Trenchea's Research (Assoc. Professor)\n\nDr. Trenchea’s expertise lies in the numerical analysis of semidiscrete and fully discrete space-time discretizations of control problems, convergence and error estimates, and the development of numerical algorithms for finding the optimal solutions. He is an expert on control theory in the abstract infinite dimensional space framework, the use of analysis and control theory for proving existence of optimal solutions (i.e., solutions that minimize the cost functional and satisfy the state equation), and getting necessary conditions of optimality for the continuous control problem.\n\n### Yotov's Research (Professor)\n\nDr. Yotov’s research interests are in the numerical analysis and solution of partial differential equations and large scale scientific computing with applications to fluid flow and transport. His current research focus is on the design and analysis of accurate multiscale adaptive discretization techniques (mixed finite elements, finite volumes, finite differences) and efficient linear and nonlinear iterative solvers (domain decomposition, multigrid, Newton-Krylov methods) for massively parallel simulations of coupled multiphase porous media and surface flows. Other areas of research interest include estimation of uncertainty in stochastic systems and mathematical and computational modeling for biomedical applications. Dr. Yotov is also an adjunct faculty at the McGowan Institute for Regenerative Medicine." ]
[ null ]
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http://gluon.ai/_sources/chapter_computational-performance/async-computation.rst.txt
[ ".. _sec_async: Asynchronous Computation ======================== Today’s computers are highly parallel systems, consisting of multiple CPU cores (often multiple threads per core), multiple processing elements per GPU, and often multiple GPUs per device. In short, we can process many different things at the same time, often on different devices. Unfortunately Python is not a great way of writing parallel and asynchronous code, at least not without some extra help. After all, Python is single-threaded and this is unlikely to change in the future. Deep learning frameworks such as MXNet and TensorFlow adopt an *asynchronous programming* model to improve performance, while PyTorch uses Python’s own scheduler leading to a different performance trade-off. For PyTorch, by default, GPU operations are asynchronous. When you call a function that uses the GPU, the operations are enqueued to the particular device, but not necessarily executed until later. This allows us to execute more computations in parallel, including operations on the CPU or other GPUs. Hence, understanding how asynchronous programming works helps us to develop more efficient programs, by proactively reducing computational requirements and mutual dependencies. This allows us to reduce memory overhead and increase processor utilization. .. raw:: html\n.. raw:: html\n.. code:: python import os import subprocess import numpy from mxnet import autograd, gluon, np, npx from mxnet.gluon import nn from d2l import mxnet as d2l npx.set_np() .. raw:: html\n.. raw:: html\n.. code:: python import os import subprocess import numpy import torch from torch import nn from d2l import torch as d2l .. raw:: html\n.. raw:: html\nAsynchrony via Backend ---------------------- .. raw:: html\n.. raw:: html\nFor a warmup consider the following toy problem: we want to generate a random matrix and multiply it. Let us do that both in NumPy and in ``mxnet.np`` to see the difference. .. code:: python with d2l.Benchmark('numpy'): for _ in range(10): a = numpy.random.normal(size=(1000, 1000)) b = numpy.dot(a, a) with d2l.Benchmark('mxnet.np'): for _ in range(10): a = np.random.normal(size=(1000, 1000)) b = np.dot(a, a) .. parsed-literal:: :class: output numpy: 1.1620 sec mxnet.np: 0.0272 sec The benchmark output via MXNet is orders of magnitude faster. Since both are executed on the same processor something else must be going on. Forcing MXNet to finish all the backend computation prior to returning shows what happened previously: computation is executed by the backend while the frontend returns control to Python. .. code:: python with d2l.Benchmark(): for _ in range(10): a = np.random.normal(size=(1000, 1000)) b = np.dot(a, a) npx.waitall() .. parsed-literal:: :class: output Done: 1.1487 sec Broadly speaking, MXNet has a frontend for direct interactions with users, e.g., via Python, as well as a backend used by the system to perform the computation. As shown in :numref:`fig_frontends`, users can write MXNet programs in various frontend languages, such as Python, R, Scala, and C++. Regardless of the frontend programming language used, the execution of MXNet programs occurs primarily in the backend of C++ implementations. Operations issued by the frontend language are passed on to the backend for execution. The backend manages its own threads that continuously collect and execute queued tasks. Note that for this to work the backend must be able to keep track of the dependencies between various steps in the computational graph. Hence, it is not possible to parallelize operations that depend on each other. .. raw:: html\n.. raw:: html\nFor a warmup consider the following toy problem: we want to generate a random matrix and multiply it. Let us do that both in NumPy and in PyTorch tensor to see the difference. Note that PyTorch ``tensor`` is defined on a GPU. .. code:: python # Warmup for GPU computation device = d2l.try_gpu() a = torch.randn(size=(1000, 1000), device=device) b = torch.mm(a, a) with d2l.Benchmark('numpy'): for _ in range(10): a = numpy.random.normal(size=(1000, 1000)) b = numpy.dot(a, a) with d2l.Benchmark('torch'): for _ in range(10): a = torch.randn(size=(1000, 1000), device=device) b = torch.mm(a, a) .. parsed-literal:: :class: output numpy: 0.9222 sec torch: 0.0011 sec The benchmark output via PyTorch is orders of magnitude faster. NumPy dot product is executed on the CPU processor while PyTorch matrix multiplication is executed on GPU and hence the latter is expected to be much faster. But the huge time difference suggests something else must be going on. By default, GPU operations are asynchronous in PyTorch. Forcing PyTorch to finish all computation prior to returning shows what happened previously: computation is being executed by the backend while the frontend returns control to Python. .. code:: python with d2l.Benchmark(): for _ in range(10): a = torch.randn(size=(1000, 1000), device=device) b = torch.mm(a, a) torch.cuda.synchronize(device) .. parsed-literal:: :class: output Done: 0.0024 sec Broadly speaking, PyTorch has a frontend for direct interaction with the users, e.g., via Python, as well as a backend used by the system to perform the computation. As shown in :numref:`fig_frontends`, users can write PyTorch programs in various frontend languages, such as Python and C++. Regardless of the frontend programming language used, the execution of PyTorch programs occurs primarily in the backend of C++ implementations. Operations issued by the frontend language are passed on to the backend for execution. The backend manages its own threads that continuously collect and execute queued tasks. Note that for this to work the backend must be able to keep track of the dependencies between various steps in the computational graph. Hence, it is not possible to parallelize operations that depend on each other. .. raw:: html\n.. raw:: html\n.. _fig_frontends: .. figure:: ../img/frontends.png :width: 300px Programming language frontends and deep learning framework backends. Let us look at another toy example to understand the dependency graph a bit better. .. raw:: html\n.. raw:: html\n.. code:: python x = np.ones((1, 2)) y = np.ones((1, 2)) z = x * y + 2 z .. parsed-literal:: :class: output array([[3., 3.]]) .. raw:: html\n.. raw:: html\n.. code:: python x = torch.ones((1, 2), device=device) y = torch.ones((1, 2), device=device) z = x * y + 2 z .. parsed-literal:: :class: output tensor([[3., 3.]], device='cuda:0') .. raw:: html\n.. raw:: html\n.. _fig_asyncgraph: .. figure:: ../img/asyncgraph.svg The backend tracks dependencies between various steps in the computational graph. The code snippet above is also illustrated in :numref:`fig_asyncgraph`. Whenever the Python frontend thread executes one of the first three statements, it simply returns the task to the backend queue. When the last statement’s results need to be *printed*, the Python frontend thread will wait for the C++ backend thread to finish computing the result of the variable ``z``. One benefit of this design is that the Python frontend thread does not need to perform actual computations. Thus, there is little impact on the program’s overall performance, regardless of Python’s performance. :numref:`fig_threading` illustrates how frontend and backend interact. .. _fig_threading: .. figure:: ../img/threading.svg Interactions of the frontend and backend. Barriers and Blockers --------------------- .. raw:: html\nmxnet\n.. raw:: html\nThere are a number of operations that will force Python to wait for completion: - Most obviously ``npx.waitall()`` waits until all computation has completed, regardless of when the compute instructions were issued. In practice it is a bad idea to use this operator unless absolutely necessary since it can lead to poor performance. - If we just want to wait until a specific variable is available we can call ``z.wait_to_read()``. In this case MXNet blocks return to Python until the variable ``z`` has been computed. Other computation may well continue afterwards. Let us see how this works in practice. .. code:: python with d2l.Benchmark('waitall'): b = np.dot(a, a) npx.waitall() with d2l.Benchmark('wait_to_read'): b = np.dot(a, a) b.wait_to_read() .. parsed-literal:: :class: output waitall: 0.0219 sec wait_to_read: 0.0106 sec Both operations take approximately the same time to complete. Besides the obvious blocking operations we recommend that you are aware of *implicit* blockers. Printing a variable clearly requires the variable to be available and is thus a blocker. Last, conversions to NumPy via ``z.asnumpy()`` and conversions to scalars via ``z.item()`` are blocking, since NumPy has no notion of asynchrony. It needs access to the values just like the ``print`` function. Copying small amounts of data frequently from MXNet’s scope to NumPy and back can destroy performance of an otherwise efficient code, since each such operation requires the computational graph to evaluate all intermediate results needed to get the relevant term *before* anything else can be done. .. code:: python with d2l.Benchmark('numpy conversion'): b = np.dot(a, a) b.asnumpy() with d2l.Benchmark('scalar conversion'): b = np.dot(a, a) b.sum().item() .. parsed-literal:: :class: output numpy conversion: 0.0288 sec scalar conversion: 0.0280 sec .. raw:: html\n.. raw:: html\nImproving Computation --------------------- .. raw:: html\nmxnet\n.. raw:: html" ]
[ null ]
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https://physics.stackexchange.com/questions/588734/in-the-entropy-formula-how-do-we-know-which-one-is-a-valid-microstate-for-a-par
[ "# In the entropy formula, how do we know which one is a valid microstate for a particular macrostate?\n\nConsider a very long vertical cylinder containing air in thermodynamic equilibrium. Observe that the air column is necessarily bottom heavy. The macrostate is described in part by a pressure gradient that is due to gravity. All corresponding microstates for this particular macrostate will have a matching density distribution. It seems that a top heavy distribution of the air molecules is not a valid microstate of that macrostate. And neither is a uniform density distribution along the cylinder length. When gravity is reversed, the density distribution also reverses.\n\nWhen the gravity force is removed or equalized along the cylinder's length by turning it horizontal, it seems the density distribution necessarily becomes uniform in equilibrium. A microstate where all the air molecules are concentrated in one area appears to not be a valid microstate of that macrostate because the density gradient causes a pressure gradient (all else equal) that is different than the uniform pressure of the uniform density system, hence the two macrostates are not identical.\n\nCan we therefore say that entropy forbids density fluctuations in a gas-filled system in thermodynamic equilibrium? In other words, can we say that the only valid microstates of a particular macrostate are those that always match the macrostate parameters?\n\nRemember that macro state parameters are derivable from the distribution of micro states. Concretely, macro state parameters like pressure, density etc are averages over micro states of like velocity, number density etc.\n\nIt is not true that for a gas in a gravitational field, the uniform density micro state does not contribute because it does not reproduce the correct bulk parameter. Instead the statistical interpretation would be that this micro state occurs with a very low probability in comparison to the micro state that is bottom heavy, which occurs with a very high probability. Therefore when one averages over all possible micro states, the average is dominated by the bottom heavy configurations thereby reproducing the correct macrostate parameter.\n\n• Interesting. However, how are the macrostates averages over microstates? If there were any fluctuations, won't we measure them in the macrostates? But the whole point of a macrostate is that it's perfectly described by its static parameters. And that the system is in thermodynamic equilibrium. Furthermore, does it make sense to be able to extract work from a transition between microstates of the same macrostate (such as from top-heavy to bottom-heavy state)? Oct 22, 2020 at 17:30\n\nIt depends on the setup which constraints are put on the microstate. For example the microcanonical ensemble assumes that the system is entirely isolated from the environmnent so necessarily energy has to be conserved. The microcanonical ensemble doesn't forbid the state where all particles are at the top as long as energy is conserved. So some of the system's kinetic energy has to be converted into potential energy. In the canonical ensemble it is only assumed that the system is in contact with a heat bath so energy is not necessarily conserved for the system.\n\nThe microstate where most of the particles are at the top is a valid microstate. In fact in the microcanonical ensemble each microstate has equal probability. But there are a lot more microstates where the particles are distributed in a more sensical way (more at the bottom, less at the top). Similarly if you toss a million coins the outcome of all heads is a valid microstate. But since the probability of getting all heads is $$1/2^{1000\\,000}\\approx 10^{-300\\,000}$$ I can tell you that this will not happen in our lifetimes. The chance of getting exactly half a million is $$\\sim 0.0008$$ which is a lot higher. Since gasses often contain at least a mole $$\\sim6\\cdot 10^{23}$$ of molecules we can guarantee that the gas will always be in a 'sensical' microstate even though nonsensical ones are still possible. So no, density fluctuations are possible and thermodynamics even makes predictions about these fluctuations.\n\nWhat do I mean by sensical states? With sensical I mean a state that is in thermodynamical equilibrium which in term means the entropy is maxized. Maximum entropy means a maximum number of microstates by Boltzmann's law. I can force the system in a non-equilibrium state by turning the bottle upside down but the second law of thermodynamics says the entropy always has to increase (or stay the same). Once the entropy is maximized we can say it's in thermodynamical equilibrium and we can use the machinery of thermodynamics since technically thermodynamics only considers systems in equilibrium.\n\n• How can the top-heavy microstate be valid when the pressure gradient of that microstate doesn't match that of the macrostate? And how can the coin analogy be valid when they're not subject to gravity, and when those events are IID as apposed to air molecules which clearly interact with one another? Oct 22, 2020 at 17:20" ]
[ null ]
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https://socratic.org/precalculus/matrix-algebra/determinant-of-a-square-matrix
[ "# Determinant of a Square Matrix\n\n## Key Questions\n\n• Without any other information, all we can say is:\n\n$\\det \\left({A}^{- 1}\\right) = \\frac{1}{\\det \\left(A\\right)}$\n\nI hope that this was helpful.\n\n• Every SQUARE matrix $n \\times n$ has a determinant.\nThe determinant $| A |$ of a square matrix $A$ is a number that helps you to decide:\n\n1) What kind of solutions a system (from whose coefficients you built the square matrix $A$) can have (unique, no solutions or an infinite number of solutions);\n\n2) If your matrix $A$, considered as an operator that produce transformations on vectors (making them bigger, flipping them, reducing them...etc.), can have an inverse (operating an inverse transformation) and what is the size of the transformation produced by $A$.\n\nYou can have a look to System of Linear Equations and Eigenvalues/Eigenvectors.\n\n• Assuming that we have a square matrix, then the determinant of the matrix is the determinant with the same elements.\n\nEg if we have a $2 \\times 2$ matrix:\n\n$\\boldsymbol{A} = \\left(\\begin{matrix}a & b \\\\ c & d\\end{matrix}\\right)$\n\nThe the associated determinant given by\n\n$D = | \\boldsymbol{A} | = | \\left(a , b\\right) , \\left(c , d\\right) | = a d - b c$\n\n• The determinant of a matrix $A$ helps you to find the inverse matrix ${A}^{- 1}$.\n\nYou can know a few things with it :\n\n• $A$ is invertible if and only if $D e t \\left(A\\right) \\ne 0$.\n\n• $D e t \\left({A}^{- 1}\\right) = \\frac{1}{D e t \\left(A\\right)}$\n\n• A^(-1) = 1/(Det(A)) * \"\"^t((-1)^(i+j)*M_(ij)),\n\nwhere $t$ means the transpose matrix of $\\left({\\left(- 1\\right)}^{i + j} \\cdot {M}_{i j}\\right)$,\n\nwhere $i$ is the n° of the line, $j$ is the n° of the column of $A$,\n\nwhere ${\\left(- 1\\right)}^{i + j}$ is the cofactor in the $i$-th row and $j$-th column of $A$,\n\nand where ${M}_{i j}$ is the minor in the $i$-th row and $j$-th column of $A$." ]
[ null ]
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https://eng.kakprosto.ru/how-122461-how-to-find-angle-if-you-know-the-sine
[ "Advice 1: How to find angle if you know the sine\n\nThe sine and cosine pair of the basic trigonometric functions, which indirectly Express the measure of an angle in degrees. All of these functions there are more than a dozen, and among them there are those that allow, for instance, to recover the sine value of an angle in degrees. For practical work with them, you can use a software calculator or network services.", null, "Instruction\n1\nUse the inverse sine to calculate the angle in degrees, if you know the sine of this angle. If the angle denoted by the letter α, in General form, this can be written as: α = arcsin(sin(α)).\n2\nIf you have the ability to use the computer for practical calculations it is easiest to use the built in calculator operating system. In the last two versions of Windows it can be run like this: press the Windows key, type the letters \"ka\" and press Enter. In earlier releases of this OS the link \"Calculator\" look at the subsection \"Standard\" under \"All programs\" in the main menu system.\n3\nAfter starting the application, switch to a mode that allows you to work with trigonometric functions. You can do this by selecting the string \"Engineering\" in the \"View\" menu of the calculator or by pressing Alt + 2.\n4\nEnter the value of the sine. By default, the calculator interface is no button to calculate the inverse sine. To be able to use this feature, you need to invert the values of the default button - click on the Inv button in the program window. In earlier versions, this button replaces the checkbox with the same name - put a checkmark.\n5\nClick on the button calculate sine - inverting functions symbol will change to sin⁻1. The calculator will calculate the angle and display its value.\n6\nCan be used in the calculations, and various online services, which is more than enough on the Internet. For example, go to the page http://planetcalc.com/326/, scroll it down a bit and in the Input field enter the value of the sine. To start the calculation procedure here is the orange button labeled Calculate - click it. The result of the calculation you will find in the first row of the table under this button. In addition to the arcsine and it displays the value of the arc cosine, arc tangent and arc cotangent of the entered value.\n\nAdvice 2 : How to find the cosine, the sine of knowing\n\nIn order to obtain a formula linking the sine and cosine of the angle, it is necessary to give or to recall some definitions. So, the sine of an angle is the ratio (quotient of the) opposite side of a right triangle to the hypotenuse. Tothe sine of an angle is the ratio adjacent side to the hypotenuse.", null, "Instruction\n1\nDraw a right triangle ABC, where angle ABC is a straight line (Fig.1). Consider the ratio of the sineand cosineand angle CAB. According to the above definition\nsin CAB=BC/AC cos CAB=AB/AC.\n2\nRemember the Pythagorean theorem - AB^2 + BC^2 = AC^2, where ^2 is the operation of squaring.\nDivide left and right side of the equation by the square of the hypotenuse AC. Then the previous equation will look like this:\nAB^2/AC^2 + BC^2 AC^2 = 1.\n3\nFor convenience, we rewrite the equation obtained in step 2, as follows:\n(AB/AC)^2 + (BC/AC)^2 = 1.\nAccording to the definitions given in step 1, we get:\ncos^2(CAB) + sin^2(CAB) = 1, i.e.\ncos(CAB)=SQRT(1-sin^2(CAB)), where SQRT is the operation of taking the square root.\nThe magnitude of the sine and cosine of any angle cannot be greater than 1.\n\nAdvice 3 : How to find the tangent using the cosine\n\nCosine, and sine, referred to as \"direct\" trigonometric functions. The tangent (along with the cotangent) is referred to the other pair, called \"derivatives\". There are several definitions of these functions that make possible finding the tangent of a specified angle for a known cosine value from the same value.", null, "Instruction\n1\nSubtract from unity the quotient of the units on the squared value of the cosine of the specified angle, and from the result, extract the square root, this will be the value of the tangent of the angle, expressed via its cosine: tg(α)=√(1-1/(cos(α))2). In this case, note that in the formula for the cosine is in the denominator of the fraction. The impossibility of division by zero eliminates the use of this expression for angles equal to 90°, and differs from this value by multiples of 180° (270°, 450°, -90° etc.).\n2\nThere is an alternative method of calculating the tangent at the known value of the cosine. It can be used, if not set a limit on the use of other trigonometric functions. To implement this method, first determine the angle for a known cosine value - this can be done using the inverse cosine. Then just calculate the tangent for the angle values. In General this algorithm can be written as: tg(α)=tg(arccos(cos(α))).\n3\nThere are even more exotic option using the definition of cosine and tangent of acute angles using right triangle. The cosine in this definition corresponds to the ratio of the length adjacent to the considered corner of the leg to the length of the hypotenuse. Knowing the cosine ratio to find the corresponding lengths of these two sides. For example, if cos(α)=0.5, then the adjacent side can be taken equal to 10 cm and the hypotenuse is 20cm. The specific numbers here do not matter - the same and right decision you will get to any values having the same ratio. Then by the Pythagorean theorem determine the length of the missing side opposite leg. It will be equal to the square root of the difference between the lengths squared of the hypotenuse and the known leg: √(202-102)=√300. The tangent is, by definition, corresponds to the ratio of the lengths opposite and adjacent sides (√300/10) - calculate it and get the tangent value found using the classic definition of cosine.\nSearch", null, "" ]
[ null, "https://st03.kakprosto.ru/tumb/680/images/article/2012/3/20/1_5254fede29c515254fede29ca8.jpg", null, "https://st03.kakprosto.ru/tumb/680/images/article/2011/7/27/1_5254fc746512b5254fc746516a.jpg", null, "https://st03.kakprosto.ru/tumb/680/images/article/2011/12/16/1_5254fe2c7828a5254fe2c782c8.jpg", null, "https://tms.dmp.wi-fi.ru/", null ]
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https://abstracts.societyforscience.org/Home/FullAbstract?ISEFYears=2018%2C&Category=Any%20Category&AllAbstracts=True&FairCountry=Any%20Country&FairState=Any%20State&ProjectId=15645
[ "# Abstract Search\n\n## Extreme Point in the Triangle Plane\n\nBooth Id:\nMATH051\n\nCategory:\nMathematics\n\nYear:\n2018\n\nFinalist Names:\nBatarin, Egor (School: Lyceum 1523)\n\nAbstract:\nThe present work is used to set a mathematical problem to discover absolute barycentric coordinates of locus $P^n_{min}$ in the triangle plane, featured with the $n^{\\text{th}}$ powers of distances from points of this locus to the straight lines containing the triangle sides having minimum sum value. The accomplished research was used to resolve this problem, in the course of which, the search of barycentric coordinates of the extremum point, for $n\\geqslant 1$ has been discovered. It's shown, that in case $n=1$ the answer for the problem depends on type of the triangle. In the case $n>1$ $P^n_{min}$ is the single point, which lies strictly inside the triangle and having absolute barycentric coordinates: $$\\left( \\begin{array}{lcr} \\displaystyle \\frac{a^\\frac{n}{n-1}}{a^\\frac{n}{n-1} + b^\\frac{n}{n-1} + c^\\frac{n}{n-1}}; & \\displaystyle \\frac{b^\\frac{n}{n-1}}{a^\\frac{n}{n-1} + b^\\frac{n}{n-1} + c^\\frac{n}{n-1}}; & \\displaystyle \\frac{c^\\frac{n}{n-1}}{a^\\frac{n}{n-1} + b^\\frac{n}{n-1} + c^\\frac{n}{n-1}} \\end{array} \\right).$$ The theorem have cases which are gained for the first time: \\begin{itemize} \\item[1)] in regular triangle $P^n_{min}$ coincides with its center for $n>1$; \\item[2)] $P^n_{min}$ for $n\\rightarrow\\infty$ coincides with incenter. \\end{itemize} As the result of the research, for the first time, it was possible to gain expressions for the absolute barycentric coordinates of the extremum point. The research may be used in the optimization theory and physics." ]
[ null ]
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http://web.mit.edu/r/current/lib/R/library/SparseM/html/slm.html
[ "slm {SparseM} R Documentation\n\n## Fit a linear regression model using sparse matrix algebra\n\n### Description\n\nThis is a function to illustrate the use of sparse linear algebra to solve a linear least squares problem using Cholesky decomposition. The syntax and output attempt to emulate `lm()` but may fail to do so fully satisfactorily. Ideally, this would eventually become a method for `lm`. The main obstacle to this step is that it would be necessary to have a model.matrix function that returned an object in sparse csr form. For the present, the objects represented in the formula must be in dense form. If the user wishes to specify fitting with a design matrix that is already in sparse form, then the lower level function `slm.fit()` should be used.\n\n### Usage\n\n```slm(formula, data, weights, na.action, method = \"csr\", contrasts = NULL, ...)\n```\n\n### Arguments\n\n `formula` a formula object, with the response on the left of a `~` operator, and the terms, separated by `+` operators, on the right. As in `lm()`, the response variable in the formula can be matrix valued. `data` a data.frame in which to interpret the variables named in the formula, or in the subset and the weights argument. If this is missing, then the variables in the formula should be on the search list. This may also be a single number to handle some special cases – see below for details. `weights` vector of observation weights; if supplied, the algorithm fits to minimize the sum of the weights multiplied into the absolute residuals. The length of weights must be the same as the number of observations. The weights must be nonnegative and it is strongly recommended that they be strictly positive, since zero weights are ambiguous. `na.action` a function to filter missing data. This is applied to the model.frame after any subset argument has been used. The default (with `na.fail`) is to create an error if any missing values are found. A possible alternative is `na.omit`, which deletes observations that contain one or more missing values. `method` there is only one method based on Cholesky factorization `contrasts` a list giving contrasts for some or all of the factors default = `NULL` appearing in the model formula. The elements of the list should have the same name as the variable and should be either a contrast matrix (specifically, any full-rank matrix with as many rows as there are levels in the factor), or else a function to compute such a matrix given the number of levels. `...` additional arguments for the fitting routines\n\n### Value\n\nA list of class `slm` consisting of:\n\n `coefficients` estimated coefficients `chol` cholesky object from fitting `residuals` residuals `fitted` fitted values `terms` terms `call` call\n\n...\n\nRoger Koenker\n\n### References\n\nKoenker, R and Ng, P. (2002). SparseM: A Sparse Matrix Package for R,\nhttp://www.econ.uiuc.edu/~roger/research\n\n`slm.methods` for methods `summary`, `print`, `fitted`, `residuals` and `coef` associated with class `slm`, and `slm.fit` for lower level fitting functions. The latter functions are of special interest if you would like to pass a sparse form of the design matrix directly to the fitting process.\n\n### Examples\n\n```data(lsq)\nX <- model.matrix(lsq) #extract the design matrix\ny <- model.response(lsq) # extract the rhs\nX1 <- as.matrix(X)\nslm.time <- system.time(slm(y~X1-1) -> slm.o) # pretty fast\nlm.time <- system.time(lm(y~X1-1) -> lm.o) # very slow\ncat(\"slm time =\",slm.time,\"\\n\")\ncat(\"slm Results: Reported Coefficients Truncated to 5 \",\"\\n\")\nsum.slm <- summary(slm.o)\nsum.slm\\$coef <- sum.slm\\$coef[1:5,]\nsum.slm\ncat(\"lm time =\",lm.time,\"\\n\")\ncat(\"lm Results: Reported Coefficients Truncated to 5 \",\"\\n\")\nsum.lm <- summary(lm.o)\nsum.lm\\$coef <- sum.lm\\$coef[1:5,]\nsum.lm\n```\n\n[Package SparseM version 1.77 Index]" ]
[ null ]
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https://giasutamtaiduc.com/point-of-intersection-formula.html
[ "# ✅ Point of intersection formula ⭐️⭐️⭐️⭐️⭐️\n\n5/5 - (1 bình chọn)\n\nPoint of intersection means the point at which two lines intersect. These two lines are represented by the equation a1x+ b1y + c1= 0  and a2x+ b2y + c2 = 0, respectively. Given figure illustrate the point of intersection of two lines.\n\nWe can find the point of intersection of three or more lines also. By solving the two equations, we can find the solution for the point of intersection of two lines.\n\nThe formula of the point of Intersection of two lines is:\n\nMục Lục\n\n### Solved Example\n\nQuestion: Find out the point of intersection of two lines x + 2y + 1 = 0 and 2x + 3y + 5 = 0.\n\nSolution:\n\nGiven straight line equations are:\n\nx + 2y + 1 = 0 and 2x + 3y + 5 = 0\n\nHere,\na1 = 1, b1 = 2, c1 = 1\n\na2 = 2, b2 = 3, c2 = 5\n\nIntersection point can be calculated using this formula,\n\n## Point of Intersection Formula\n\nThe point of intersection formula is used to find the point of intersection of two lines, meaning the meeting point of two lines. These two lines can be represented by the equation a1x+b1y+c1=0  and a2x+b2y+c2=0, respectively. It is possible to find the point of intersection of three or more lines. By solving the two equations, we can find the solution for the point of intersection of two lines. Let us learn about the point of intersection formula with a few solved examples.\n\n## What Is Point of Intersection Formula?\n\nConsider 2 straight lines a1x+b1y+c1=0, and a2x+b2y+c2=0 which are intersecting at point (x,y) as shown in figure. So, we have to find a line intersection formula to find these points of intersection (x,y). These points satisfy both the equations. By solving these two equations we can find the point where two lines intersect. The formula of the point of Intersection of two lines is:\n\nLet us have a look at a few solved examples to understand the point of intersection formula better.\n\n## Solved Examples Using Point of Intersection Formula\n\nExample 1: Using point of intersection formula, find the point of intersection of two lines 2x + 4y + 2 = 0 and 2x + 3y + 5 = 0.\n\nSolution:\n\nGiven straight line equations are:\n2x + 4y + 2 = 0 and 2x + 3y + 5 = 0\nHere,\na1=2,b1=4,c1=2\na2=2,b2=3,c2=5\nIntersection point can be calculated using the point of intersection formula,\n\nAnswer: Thus, the point of intersection is (-7,3).\n\nExample 2: What will be the point of Intersection of the given two lines 2x+4y+6=0\n\nand 6x+9y+12=0\n\nSolution:\n\nThe two line equations are given as 2x+4y+6=0 and 6x+9y+12=0.\nComparing these two equations with a1x+b1y+c1anda2x+b2y+c2\nWe get a1=2,b1=4,c1=6\na2=6,b2=9,c2=12\nPoint of intersection formula is given as\n\n## Point of Intersection Formula – Two Lines Formula and Solved Problems\n\nIn mathematics, we refer to the point of intersection where a point meets two lines or curves. The intersection of lines may be an empty set, a point, or a line in Euclidean geometry. A required criterion for two lines to intersect is that they should be in the same plane and are not skew lines. The intersection formula gives the point at which these lines are meeting.\n\n### Point of Intersection of Two Lines Formula\n\nConsider 2 straight lines\n\na1x+b1y+c1 and\n\na2x+b2y+c2\n\nwhich are intersecting at point (x,y) as shown in figure. So, we have to find a line intersection formula to find these points of intersection (x,y). These points satisfy both the equations.\n\nBy solving these two equations we can find the intersection of two lines formula.\n\nThe formula for the point of intersection of two lines will be as follows:\n\nSo, this is the point of intersection formula of 2 lines when intersecting at one point.\n\nA Intersection B Intersection C Formula\n\nIf we have 3 sets A,B and C. A intersection B intersection C formula will be as follows:\n\nThe point of intersection formula is used to find the meeting point of two lines, also known as the point of intersection. The equation can be used to represent these two lines\n\na1x+b1y+c1=0\n\nand\n\na2x+b2y+c2=0\n\nrespectively. The point of intersection of three or more lines can be found. We can discover the solution for the point of intersection of two lines by solving the two equations. Let’s look at some solved examples of the point of intersection formula.\n\nTwo straight lines will intersect at a point if they are not parallel. The point of intersection is the meeting point of two straight lines.\n\nIf two crossing straight lines have the same equations, the intersection point can be found by solving both equations at the same time.\n\nOn a two-dimensional graph, straight lines intersect at just one location, which is described by a single set of display style x-coordinates and display style y-coordinates. You know the display style x-coordinates and display style y-coordinates must fulfil both equations since both lines pass through that location.\n\n### Intersection Point\n\nHave you ever been driving and come across a traffic sign like this?\n\nThis is an intersection traffic sign, and it means you’re approaching a place where two roads connect. Two lines cross and meet in the centre of the intersection traffic sign, as you can see. This is where their paths cross. The intersection of two lines or curves is referred to as a point of intersection in mathematics.\n\nThe intersection of two curves is noteworthy because it is the point at which the two curves have the same value. This can come in handy in a variety of situations. Let’s imagine we’re dealing with an equation that represents a company’s revenue and another that represents the company’s expense. The point of intersection of the curves corresponding to these two equations is where revenue equals cost; this is the company’s breakeven point.\n\n### Application for a Map of Points of Intersection\n\nReview\n\n• A point of intersection is the meeting point of two lines or curves.\n• By graphing the curves on the same graph and finding their points of intersection, we can discover a point of junction graphically.\n• The following steps can be used to find a point of intersection algebraically:\n• For one of the variables, call it y, and solve each equation.\n• Set the equations for y discovered in the first step to the same value, then solve for the other variable, which we’ll call x. This is the x-value of the junction point.\n• In any of the original equations, plug in the x-value of the site of intersection and solve for y. This is the point of intersection y-variable.\n\nQuestion 1: Find the point of intersection of line 3x + 4y + 5 = 0, 2x + 5y +7 = 0.\n\nSolution:\n\nThe point of intersection of two lines is given by :\n\n(x, y) = ((b1*c2−b2*c1)/(a1*b2−a2*b1), (c1*a2−c2*a1)/(a1*b2−a2*b1))\n\na1 = 3, b1 = 4, c1 = 5\n\na2 = 2, b2 = 5, c2 = 7\n\n(x,y) = ((28-25)/(15-8), (10-21)/(15-8))\n\n(x,y) = (3/7,-11/7)\n\nQuestion 2: Find the point of intersection of line 9x + 3y + 3 = 0, 4x + 5y + 6 = 0.\n\nSolution:\n\nThe point of intersection of two lines is given by :\n\n(x,y) = ((b1*c2−b2*c1)/(a1*b2−a2*b1), (c1*a2−c2*a1)/(a1*b2−a2*b1))\n\na1 = 9, b1 = 3, c1 = 3\n\na2 = 4, b2 = 5, c2 = 6\n\n(x, y) = ((18-15)/(45-15), (54-12)/(45-15))\n\n(x, y) = (1/10, 7/5)\n\nQuestion 3: Check if the two lines are parallel or not  2x + 4y + 6 = 0, 4x + 8y + 6 = 0\n\nSolution:\n\nTo check whether the lines are parallel or not we need to check a1/b1 = a2/b2\n\na1 = 2, b1 = 4\n\na2 = 4, b2 = 8\n\n2/4 = 4/8\n\n1/2 = 1/2\n\nSince the condition is satisfied the lines are parallel and can’t intersect each other.\n\nQuestion 4: Check if the two lines are parallel or not  3x + 4y + 8 = 0, 4x + 8y + 6 = 0\n\nSolution:\n\nTo check whether the lines are parallel or not we need to check a1/b1 = a2/b2\n\na1 = 3, b1 = 4\n\na2 = 4, b2 = 8\n\n3/4 is not equal to 4/8\n\nSince the condition is not satisfied the lines are not parallel.\n\nQuestion 5: Check whether the point (3, 5) is point of intersection of lines 2x + 3y – 21 = 0, x + 2y – 13 = 0.\n\nSolution:\n\nA point to be a point of intersection it should satisfy both the lines.\n\nSubstituting (x,y) = (3,5) in both the lines\n\nCheck for equation 1: 2*3 + 3*5 – 21 =0 —-> satisfied\n\nCheck for equation 2: 3 + 2* 5 -13 =0 —-> satisfied\n\nSince both the equations are satisfied it is a point of intersection of both the lines.\n\nQuestion 6: Check whether the point (2, 5) is point of intersection of lines x + 3y – 17 = 0, x + y – 13 = 0\n\nSolution:\n\nA point to be a point of intersection it should satisfy both the lines.\n\nSubstituting (x,y) = (2,5) in both the lines\n\nCheck for equation 1: 2+ 3*5 – 17 =0 —-> satisfied\n\nCheck for equation 2: 7 -13 = -6  —>not satisfied\n\nSince both the equations are not satisfied it is not a point of intersection of both the lines.\n\nQuestion 7: Find the point of intersection of lines x = -2 and 3x + y + 4 = 0\n\nSolution:\n\nOn substituting x = -2 in 3x + y + 4 = 0\n\n-6 + y + 4 = 0;\n\ny = 2;\n\nSo the point of intersection is (x,y) = (-2,2)\n\nGIA SƯ TOÁN BẰNG TIẾNG ANH\n\nGIA SƯ DẠY SAT\n\nMath Formulas" ]
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https://beta.geogebra.org/m/JvuyGuu2
[ "# Exploring Dilations\n\nTopic:\nDilation\nIn this construction, we have created a dilation of polygon ABCDE from center O, by the scale factor indicated on the slider (r).\n\nCompare the lengths of AB and A'B'. How does the ratio AB/A'B' compare to the scale factor r (the slider)?\n\nNow change the value of r by moving the slider. Does the length of A'B' change as you would expect?\n\nExplore this construction by moving point O. Can you find a way to place ABCD completely in the interior of A'B'C'D'?" ]
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https://www.mathworks.com/matlabcentral/answers/514154-vectorization-of-loops-with-matrix-multiplications?s_tid=prof_contriblnk
[ "# Vectorization of Loops with Matrix Multiplications\n\n1 view (last 30 days)\nTommaso Belluzzo on 30 Mar 2020\nAnswered: Matt Shellhammer on 31 Mar 2020\nHi all. I have the following code which is being repeated many times with different time series and this is producing a huge bottleneck on my code:\n%% Example Data\nt = 252;\nh = randn(252,2);\nl = round(0.1 * t,0);\n%% Loop\nfor i = 1:(l - 1)\no_tmp = h(1,:).' * h(1+i,:);\nfor j = 2:(t - i)\no_tmp = o_tmp + h(j,:).' * h(j+i,:);\nend\no_tmp = o_tmp / (t - i);\nend\nI would like ti know if there is a suitable way to improve it, maybe by vectorizing all computations or just some of them. Any suggestion is more than welcome. Thanks in advance for your help!\nDavid Hill on 30 Mar 2020\nIt would help if you explained what you are trying to do (big picture).\n\nMatt Shellhammer on 31 Mar 2020\n%% Example Data\nt = 252;\nh = randn(252,2);\nl = round(0.1 * t,0);\n%% Loop\nfor i = 1:(l - 1)\no_tmp = (h(1:(t-i),:).' * h((1+i):t,:))/(t-i);\nend\n\n### Categories\n\nFind more on Loops and Conditional Statements in Help Center and File Exchange\n\nR2018a\n\n### Community Treasure Hunt\n\nFind the treasures in MATLAB Central and discover how the community can help you!\n\nStart Hunting!" ]
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https://www.physicsforums.com/threads/magnetic-field-in-biot-savart-law.149387/
[ "# Magnetic Field in BIOT-SAVART law\n\n#### alireza.ramezan\n\nI have a question about the magnrtic force of steady curent .\nIn Biot - Savart law to evalute of B (magnetic Field ) , below the Integral we have to do a cross product Idl'*(r-r')/|r-r'|^3 that r and r' are the vector position of the field and source . How we can evaluate this Integral if the vector r-r' is zero . ?\nfor example if we have a U shape Incomplete circuit and put a metal bar as the fourth side to complete it , when a stationary current I circualtes in square , a force will exert on the bar . if we would like to evaluate the force exerted by three sides on the fourth one , we will encounter this problem for the toppest and the lowest point of fourth one , on corners .Because vector r-r' =0 and B approches to infinity . Please help me .\n\nLast edited:\nRelated Advanced Physics Homework Help News on Phys.org\n\n#### Mindscrape\n\nIf you have a square shape current loop you can use superposition (i.e. the additive linearity operator).\n\n#### StatMechGuy\n\nIf you have a totally localized current distribution, you'll get divergences, same as if you have point charges in electrostatics, i.e. in Coulomb's Law. Try solving the magnetic field for a cylindrical charge distribution and see what you get.\n\n#### StatMechGuy\n\nWell, just work it out. The Biot-Savart law is pretty much equivalent to Ampere's law, so I'll work out the most trivial example of Ampere's law.\n\nIf you have an infinitely long wire with a current I running through it, and it has no spacial extent, then if I make a circle centered on the wire, I find that\n$$\\oint \\mathbf{B} \\cdot d \\mathbf{l} = \\mu_0 I$$\n$$B (2 \\pi r) = \\mu_0 I$$\nfrom which we see that the magnetic field is infinite at r = 0.\n\nNow let's work the same problem, only this time with a wire of radius a and constant current density J. Outside the wire, we get the same result from Ampere's law:\n$$B = \\frac{m_0}{2 \\pi} \\frac{\\pi a^2 J}{r}$$\nBut inside, the magnetic field is different. Inside, the current enclosed in the loop is given by $$I = \\pi r^2 J$$, which means that\n$$B = \\frac{\\mu_0}{2 \\pi} \\pi r J$$\nThe magnetic field is nice and well-behaved inside the wire! But what's the difference?\n\nWell, in the first case, the current density can be described as a delta-function, so that $$\\nabla \\times \\mathbf{B} = \\mu_0 I \\delta(x)\\delta(y)$$ if, say, the wire is resting on the z-axis. These delta-functions are wildly singular, and in fact this differential equation looks very similar to that of a point electrostatic charge $$\\nabla \\cdot \\mathbf{E} = q \\delta(\\mathbf{r}) / \\epsilon_0$$\n\nIn the second case, the current distribution can be described by step-functions, which although their derivatives are discontinuous, the actual functions are finite and well-behaved everywhere. This is the origin of the difference, and why the magnetic field would diverge for a wire of zero physical extent.\n\nLast edited:" ]
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https://www.degruyter.com/search?pageSize=10&q=%22Tate+pairing%22&sort=relevance&t=MT-10
[ "# Search Results\n\n## You are looking at 1 - 10 of 17 items :\n\n• \"Tate pairing\"\n• Numerical and Computational Mathematics\nClear All", null, "", null, "## Abstract\n\nThis paper proposes the computation of the Tate pairing, Ate pairing and its variations on the special Jacobi quartic elliptic curve $Y2=dX4+Z4$. We improve the doubling and addition steps in Miller's algorithm to compute the Tate pairing. We use the birational equivalence between Jacobi quartic curves and Weierstrass curves, together with a specific point representation to obtain the best result to date among curves with quartic twists. For the doubling and addition steps in Miller's algorithm for the computation of the Tate pairing, we obtain a theoretical gain up to $27%$ and $39%$, depending on the embedding degree and the extension field arithmetic, with respect to Weierstrass curves and previous results on Jacobi quartic curves. Furthermore and for the first time, we compute and implement Ate, twisted Ate and optimal pairings on the Jacobi quartic curves. Our results are up to $27%$ more efficient compared to the case of Weierstrass curves with quartic twists.\n\nOPEN ACCESS\n\nthis pairing in cryptographic applications. Keywords. Tate pairing, Weil pairing, self-pairing, pairing based cryptography. 2010 Mathematics Subject Classification. 14G50, 11T71, 11G20, 14Q05. 1 Introduction A pairing is a non-degenerate bilinear map e W G1 G2 7! GT where G1;G2;GT are cyclic groups of prime order r (the first two are usually written additively, and the third multiplicatively). Such groups are found from elliptic or hyperelliptic curves and the pairing is usually the Tate–Lichtenbaum pairing or one of its variants. Pairings have found many\n\n-adic representation, 9 Perrin-Riou's \"logarithme elargi\", 165 pseudo-isomorphism of lwasawa mod- ules, 40 pseudo-null lwasawa module, 40 representation, p-adic, 9 rigidity, 176 Selmer group, 21 Selmer group of an abelian variety, 27 Selmer sequence, 132 semilocal Galois cohomology, 93, 202 singular cohomology classes, 14 Stickelberger element, 56 symmetric square of an elliptic curve, 73, 170 Tate pairing, 18 Teichmiiller character, 54 Thaine, Francisco, 3 twist (by arbitrary characters), 123 twist (by characters of finite order), 44 twisting homomorphism, 119\n\ncohomology groups. In §1.4 we state without proof the results we need concerning the Tate pair- ing on local cohomology groups, and we study how our special subgroups behave with respect to this pairing. In §1.5 and §1.6 we define Selmer groups and give the basic examples of ideal class groups and Selmer groups of elliptic curves and abelian varieties. Then in §1.7, using Poitou-Tate global duality and the local orthogonality results from §1.4, we derive our main tool (Theorem 1.7.3) for bounding the size of Selmer groups. 1.1. p-adic Representations Definition 1\n\ncommutative diagram in which all the maps are isomorphisms where AE is the formal group logarithm, and the bottom right isomorphism is defined in [T3] Theorem 4.2. Using these identifications we will also view AE as a homomorphism from E(Qn,p) to Qn,p· Since V !::! V*, the local Tate pairing gives the second isomorphism in Hom(E(Qn,p), Qp) !::! Hom(H}(Qn,p, V), Qp) !::! H!(Qn,p, V). Thus there is a dual exponential map (see [Kal] §11.1.2) expE; : H!(Qn,p, V) ~ Cotan(E;Qn,p) = Qn,pWE. Write exp~E : Hi (Qn,p, V) ~ Qn,p for the composition wE; o expE;. Since Hi\n\nconse- quence, pairings became very popular in asymmetric cryptography and computing RNS in Fpk and pairings 65 them as fast as possible is very important. Let us first briefly recall the state of the art in this field and then explain how an RNS arithmetic can be helpful. 4.2 The Tate pairing The most popular pairing used in cryptography is the Tate pairing. We present it here in a simplified and reduced form because it is the one usually used in cryp- tographic applications. More details and generalities can be found in [16, 23]. In this paper we assume that E is an\n\ngroup of points of order r defined over the ground field Fq. Hence, we consider a non-degenerate bilinear pairing of the form e : E(Fq)[r]× E(Fq)[r]→ µr ⊆ F∗qk . We may obtain such a pairing from the Weil pairing or Tate pairing twisted by an endomorphism ψ called a distortion map [21, 22]. For example, if the Tate pairing is used then we define e(P,Q) = fr,P (ψ(Q))(q k−1)/r where fr,P is a function on E with divisor (fr,P ) = r(P ) − r(0) (see or for more details about pairings). The value fr,P (ψ(Q)) may be computed using Miller’s algorithm . 2\n\nfor each n > 0. Let r be a prime dividing #Jac(C)(Fq) and coprime to p. We define the embedding degree to be the smallest positive integer k such that r divides qk − 1; note that Fqk is the field generated over Fq by adjoining the group µr of rth roots of unity in Fq. Throughout, er : Jac(C)[r]× Jac(C)[r]→ µr ⊂ F∗qk denotes a non-degenerate, bilinear, and Galois-invariant pairing on Jac(C)[r], such as the Weil pairing or the reduced Tate pairing; we refer the reader to [1, 2, 8, 7, 16, 17] for details on pairings and pairing-based cryptography. An elliptic curve E\n\n–Rück attack and MOV attack use the Tate pairing and Weil pairing, respectively, to map the discrete logarithm problem on the curve’s Jaco- bian defined over Fq to the discrete logarithm in the multiplicative group of the exten- 20 Laura Hitt sion field Fqk , for some integer k, where there are more efficient methods for solving the DLP. This extension degree k is known as the embedding degree. We will say a curve C has embedding degree k with respect to an integer N if and only if a subgroup of order N of its Jacobian JC does. So for pairing-based cryptosystems, it is impor\n\nOPEN ACCESS\n\nhttp://arxiv.org/abs/1409.0846 E. Fouvry and H. Iwaniec, Gaussian primes, Acta Arith. 79 (1997), no. 3, 249–287. 10.4064/aa-79-3-249-287 Fouvry E. Iwaniec H. Gaussian primes Acta Arith. 79 1997 3 249 287 G. Frey, M. Müller and H.-G. Rück, The Tate pairing and the discrete logarithm applied to elliptic curve cryptosystems, IEEE Trans. Inform. Theory 45 (1999), no. 5, 1717–1719. 10.1109/18.771254 Frey G. Müller M. Rück H.-G. The Tate pairing and the discrete logarithm applied to elliptic curve cryptosystems IEEE Trans. Inform. Theory 45 1999 5 1717", null, "", null, "" ]
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https://physics.stackexchange.com/questions/250148/binding-energy-per-nucleon-in-radioisotopes-of-hydrogen
[ "# Binding energy per nucleon in radioisotopes of hydrogen\n\nI understand that greater binding energy per nucleon implies a more stable atom and atoms undergo nuclear fusion and fission to attain higher binding energy per nucleon. The binding energy per nucleon curve (https://en.wikipedia.org/wiki/File:Binding_energy_curve_-_common_isotopes.svg) shows that radioactive isotopes of hydrogen (deuterium and tritium) are more stable than hydrogen itself. Is this not incorrect? Is my assumption of greater binding energy per nucleon $=>$ more stable atom incorrect?\n\n## 1 Answer\n\n$^1_1H$ is a special case as the proton does not have any other nucleons to bind onto. I suppose that you could call the binding energy per nucleon zero which means that you require no energy to split up the nucleus of $^1_1H$ into its constituent parts?\n\nNote also that the binding energy per nucleon is not necessarily the full measure of whether a nucleus is stable or not.\n\n$^2_1H$ has a binding energy per nucleon of 1.11 MeV and is a stable isotope of hydrogen whereas $^3_1H$ has a binding energy per nucleon of 2.83 MeV and is an unstable isotope of hydrogen with a half life of 12.32 years." ]
[ null ]
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https://www.actapress.com/Abstract.aspx?paperId=22321
[ "## The Parallel Algorithm for an Improved SUMT Method for Equality Constrained Optimization\n\nJ.-J. Chen, L. Jia, J.-C. Chen, W.-W. Cheng (USA), and H.-M. Lee (Taiwan)\n\n### Keywords\n\nSUMT method, constrained optimization, penalty function, quasi-Newton method, Armijo line search, BFGS. r : penalty parameter gƒ (x) : gradient of f(x) Jc(x): Jc(x) = [∂ci(x)/∂xj],the constraints Jacobian\n\n### Abstract\n\n: This paper presents a detailed derivation and description of an improved SUMT method for solving equality constrained optimization problem. The method is based upon the quadratic penalty function, but uses orthogonal transformations, derived from the Jacobian matrix of the constraints, to deal with the numerical ill conditioning that affects the methods of this type. The newly developed parallel algorithm is issued to find the optimal n-ary dimension variables for the constrained function. At each iteration of the new algorithm, the orthogonal search direction is determined by a quasi Newton method which can avoid the necessity of solving a set of equations and the step-length is chosen by a Armijo line search. The matrix which approaches the inverse of the projected Hessian of composite function is updated by means of the BFGS formula from iteration to iteration. As the penalty parameter approaches zero, the projected inverse Hessian has a special structure which can guarantee us to obtain the search direction accurately even if the Hessian of composite function is ill-conditioned in the former SUMT methods. where c(x)T c(x)/(2r) is the quadratic penalty term and r is the penalty parameter. It is known that if x* is the solution of (1) and x*(r) is the unconstrained minimum of (2), then under mild conditions [4, 10, 11], lim x* (r) = x* r→0 Thus, we deal with the unconstrained problem minimize φ (x,r) (2) instead of (1). The method we use to solve (2) will generate a sequence that converges (as r→0) to solution x* of the original problem (1). 2 Basic Idea In order to simplify our discussion, we introduce the following notation: f(x) : objective function c(x) : [ci(x)], the constraints vector φ (x, r) : composite function (φ (x, r) = f(x) + c(x) T c(x)/(2r))" ]
[ null ]
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https://wiki.inria.fr/wikis/popix/index.php?title=Overview&diff=prev&oldid=7173
[ "# Difference between revisions of \"Overview\"\n\n$\\def\\simulix{\\mathsf{simulix} }$ The desire to model a biological or physical phenomenon often arises when we are able to record some observations issued from that phenomenon. Nothing would be more natural therefore than to begin this introduction by looking at some observed data.\n\n This first plot displays the viral load of four patients with hepatitis C who started a treatment at time $t=0$.", null, "This second example involves weight data for rats measured over 14 weeks, for a sub-chronic toxicity study related to the question of genetically modified corn.", null, "In this third example, data are fluorescence intensities measured over time in a cellular biology experiment.", null, "Note that repeated measurements are not necessarily always functions of time. For example, we may be interested in corn production as a function of fertilizer quantity.", null, "Even though these examples come from quite different domains, in each case the data is made up of repeated measurements on several individuals from a population. What we will call a \"population approach\" is therefore relevant for characterizing and modeling this data. The modeling goal is thus twofold: characterize the biological or physical phenomena observed for each individual, and secondly, the variability seen between individuals.\n\nIn the example with the rats, the model needs to integrate a growth model that describes how a rat's weight increases with time, and a statistical model that describes why these kinetics can vary from one rat to another. The goal is thus to finish with a \"typical\" curve for the population (in red) and to be able to explain the variability in the individual's curves (in green) around this population curve.", null, "The model will explain some of this variability by individual covariates such as sex or diet (rats 1 and 3 are male while rats 2 and 4 are female), but some of the variability will remain unexplained and will be considered as random. Integrating into the same model effects considered fixed and others considered random leads naturally to the use of mixed-effects models.\n\nAn alternative yet equivalent approach considers this model as a hierarchical one: each curve is described by a single model, and the variability between individual models is described by a population model. In the case of parametric models, this means that the observations for a given individual are described by a model of the observations that depends on a vector of individual parameters: this is the classic individual approach. The population approach is then a direct extension of the individual approach: we add a component to the model that describes the variability of the individual parameters within the population.\n\nA model can thus be seen as a joint probability distribution, which can easily be extended to the case where other variables in the model are considered as random variables: covariates, population parameters, the design, etc. The hierarchical structure of the model leads to a natural decomposition of the joint distribution into a product of conditional and marginal distributions.\n\nModels for individual parameters and models for observations are described in the Models chapter. In particular, models for continuous observations, categorical, count and survival data are presented and illustrated by various examples. Extensions for mixture models, hidden Markov models and stochastic differential equation-based models are also presented.\n\nThe Tasks & Tools chapter presents practical examples of using these models: exploration and visualization, estimation, model diagnostics, model selection and simulation. All approaches and proposed methods are rigorously detailed in the Methods chapter.\n\nThe main purpose of a model is to be used. Mathematical modeling and statistics remain useful tools for many disciplines (biology, agronomy, environmental studies, pharmacology, etc.), but it is important that these tools are used properly. The various software packages used in this wiki have been developed with this in mind: they serve the modeler well, while fully complying with a coherent mathematical formalism and using well-known and theoretically justified methods.\n\nTools for model exploration ($\\mlxplore$), modeling ($\\monolix$) and simulation ($\\simulix$) use the same model coding language $\\mlxtran$. This allows us to define a complete workflow using the same model implementation, i.e., to run several different tasks based on the same model.\n\n$\\mlxtran$ is extremely flexible and well-adapted to implementing complex mixed-effects models. With $\\mlxtran$ we can easily write ODE-based models, implement pharmacokinetic models with complex administration schedules, include inter-individual variability in parameters, define statistical models for covariates, etc. Another crucial property of $\\mlxtran$ is that it rigorously adopts the model representation formalism proposed in $\\wikipopix$. In other words, the model implementation is fully consistent with its mathematical representation.\n\n$\\mlxplore$ provides a clear graphical interface that allows us to visualize not only the structural model but also the statistical model, which is of fundamental importance in the population approach. We can visualize for instance the impact of covariates and inter-individual variability of model parameters on predictions.\n\nThe algorithms implemented in $\\monolix$ (Stochastic Approximation of EM, MCMC, Simulated Annealing, Importance Sampling, etc.) are extremely efficient for a wide variety of complex models. Furthermore, convergence of SAEM and its extensions (mixture models, hidden Markov models, SDE-based models, censored data, etc.) has been rigorously proved and published in statistical journals.\n\n$\\simulix$ is a model computation engine which enables us to simulate a $\\mlxtran$ model from within various environments. $\\simulix$ is now available for the Matlab and R platforms, allowing any user to combine the flexibility of R and Matlab scripts with the power of $\\mlxtran$ in order to easily encode complex models and simulate data.\n\nFor these reasons, $\\wikipopix$ and these tools can be used with confidence for training and teaching. This is even more the case because $\\mlxplore$, $\\monolix$ and $\\simulix$ are free for academic research and education purposes." ]
[ null, "https://wiki.inria.fr/wikis/popix/images/1/10/NEWintro1.png", null, "https://wiki.inria.fr/wikis/popix/images/7/75/NEWintro2.png", null, "https://wiki.inria.fr/wikis/popix/images/1/10/NEWintro3.png", null, "https://wiki.inria.fr/wikis/popix/images/1/12/NEWintro4.png", null, "https://wiki.inria.fr/wikis/popix/images/8/86/NEWintro5.png", null ]
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https://www.actapress.com/Abstract.aspx?paperId=33829
[ "## Efficient System-Level Statistical Design of Analog Systems via Variance Minimization\n\nH. Chang and H. Tang (USA)\n\n### Keywords\n\nSystemlevel design, Statistical design, Variance minimiza tion, Worstcase design, Analog systems, Symbolic analy sis\n\n### Abstract\n\nDue to increasing system complexity, statistical design has to be performed at both system-level and circuit-level. This paper presents an efficient method for system-level statis tical design of analog systems. In particular, the method considers system performances that can be obtained from symbolic analysis, which are then linearized at the nominal design point with first-order Taylor series expansion. As suming that all system-level design parameters are Gaus sian random variables, the system performances are also Gaussian variables. To maximize yield, it is equivalent to minimizing performance variances. The overall statistical design problem is formulated as a nonlinear programming problem and is solved efficiently." ]
[ null ]
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https://planetmath.org/EmptySet
[ "# empty set\n\nAn is a set $\\emptyset$ that contains no elements. The Zermelo-Fraenkel Axioms", null, "", null, "of set theory", null, "", null, "imply that there exists an empty set. One constructs an empty set by starting with any set $X$ and then applying the axiom of separation to form the empty set $\\emptyset:=\\{x\\in X\\mid x\\neq x\\}$.\n\nAn empty set is a subset of every other set, and any two empty sets are equal. Alternative notations", null, "", null, "", null, "", null, "", null, "for the empty set include $\\{\\}$ and $\\varnothing$.\n\nTitle empty set EmptySet 2013-03-22 11:49:55 2013-03-22 11:49:55 djao (24) djao (24) 8 djao (24) Definition msc 03-00 msc 65H05 msc 65H10 null set" ]
[ null, "http://mathworld.wolfram.com/favicon_mathworld.png", null, "http://planetmath.org/sites/default/files/fab-favicon.ico", null, "http://mathworld.wolfram.com/favicon_mathworld.png", null, "http://planetmath.org/sites/default/files/fab-favicon.ico", null, "http://dlmf.nist.gov/style/DLMF-16.png", null, "http://dlmf.nist.gov/style/DLMF-16.png", null, "http://dlmf.nist.gov/style/DLMF-16.png", null, "http://dlmf.nist.gov/style/DLMF-16.png", null, "http://dlmf.nist.gov/style/DLMF-16.png", null ]
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https://essayhomeworks.com/if-a4-b5-and-m/
[ "# if a=4 , b=5 , and m\n\nif a=4 , b=5 , and m<A = 30 , the number of distinct triangles that may be constructed" ]
[ null ]
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https://oeis.org/A328352/internal
[ "The OEIS Foundation is supported by donations from users of the OEIS and by a grant from the Simons Foundation.", null, "Hints (Greetings from The On-Line Encyclopedia of Integer Sequences!)\n A328352 Similar to A328350, but for 5 digits rather then 3. 8\n\n%I\n\n%S 0,1,56,2831,141706,7086081,354307956,17715417331,885770964206,\n\n%T 44288548698581,2214427437370456,110721371880729831,\n\n%U 5536068594097526706,276803429705181511081,13840171485260601432956,692008574263037701042331,34600428713151923199089206,1730021435657596350689323581\n\n%N Similar to A328350, but for 5 digits rather then 3.\n\n%C This sequence is the building block for the calculation of the sums of positive integers whose decimal expansion only uses five distinct, nonzero digits: see the attached pdf document.\n\n%H Pierre-Alain Sallard, <a href=\"/A328352/b328352.txt\">Table of n, a(n) for n = 0..50</a>\n\n%H Pierre-Alain Sallard, <a href=\"/A328352/a328352.pdf\">Integers sequences A328348 and A328350 to A328356</a>\n\n%F a(n) = (40*50^n - 49*5^n + 9) / 1764.\n\n%F a(n) = 51*a(n-1) - 50*a(n-2) + 5^(n-1) for n > 1.\n\n%F G.f.: x / (1 - 56*x + 305*x^2 - 250*x^3).\n\n%F a(n) = 56*a(n-1) - 305*a(n-2) + 250*a(n-3) for n > 2.\n\n%e For n=2, the sum of all positive integers whose decimal notation is only made of the 3,4,5,6 and 7 digit with at most n=2 such digits, i.e. the sum 3+4+5+6+7+33+34+35+36+37+43+44+45+46+47+53+54+55+56+57+63+64+65+66+67+73+74+75+76+77 is equal to a(2)*(3+4+5+6+7) = 56*25 = 1400.\n\n%e The formula is valid for any other 5-tuple of digits, as soon as the 5 digits are different from each other. Always with n=2 but let's say with the 5,6,7,8 and 9 digits, the sum 5+6+7+8+9+55+56+57+58+59+65+66+67+68+69+75+76+77+78+79+85+86+87+88+89+95+96+97+98+99 is equal to a(2)*(5+6+7+8+9) = 56*35 = 1960.\n\n%o (Python) [(40*50**n-49*5**n+9)//1764 for n in range(12)]\n\n%Y Cf. A328348, A328350, A328351, A328353, A328354, A328355, A328356.\n\n%K nonn,base\n\n%O 0,3\n\n%A _Pierre-Alain Sallard_, Nov 26 2019\n\nLookup | Welcome | Wiki | Register | Music | Plot 2 | Demos | Index | Browse | More | WebCam\nContribute new seq. or comment | Format | Style Sheet | Transforms | Superseeker | Recent\nThe OEIS Community | Maintained by The OEIS Foundation Inc.\n\nLast modified October 23 11:52 EDT 2021. Contains 348212 sequences. (Running on oeis4.)" ]
[ null, "https://oeis.org/banner2021.jpg", null ]
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https://ciqukasulon.olivierlile.com/write-a-formula-for-the-area-of-a-circle-as-a-function-of-its-radius-23747bh.html
[ "# Write a formula for the area of a circle as a function of its radius\n\nAt first sight it would seem a divisor could end in 3 or 7, but this never happens. In particular, every inscribed angle that subtends a diameter is a right angle since the central angle is degrees.\n\nThe prime factorization of 18, for example, is 3 x 3 x 2. What you do is this: Missing over primitive procedures. Nick Hobson points out that you can \"Take any triangular number and append the digit 1. Is there any way to maybe make a larger picture when the numbers are larger.\n\nDo this for all parts of the cube, and you will use all the numbers from 1 to 26 without any repetitions.\n\nConsecutive integers are integers in order from least to greatest, for example 1,2,3. The three pairs are: A circle's circumference and radius are proportional.\n\nThe SAT loves to use them, so know them by heart and save yourself the trouble of calculating all those roots. If two angles are inscribed on the same chord and on opposite sides of the chord, then they are supplementary.\n\nA clip limit smaller than 1 results in standard non-contrast limited AHE. Typically it is a either a single row or column image of replacement color values. Visualize that your left pinky finger represents 1, the next finger 2, and so on left to right, until your right pinky finger represents The principal task of angle measurement is to create a system that captures this radius-invariance.\n\nThe area enclosed and the square of its radius are proportional. Remember that -3 is less than -2, not the other way around sounds simple but is a common mistake. Be aware of strange tricks with negatives, and that negatives taken to EVEN powers are positive and that negatives taken to ODD powers are negative.\n\nThe number π (/ p aɪ /) is a mathematical olivierlile.comally defined as the ratio of a circle's circumference to its diameter, it now has various equivalent definitions and appears in many formulas in all areas of mathematics and olivierlile.com is approximately equal to It has been represented by the Greek letter \"π\" since the midth century, though it is also sometimes spelled out.\n\nPixel Circle and Oval Generator for help building shapes in games such as Minecraft or Terraria. Notice that the entire table above is enclosed in opening and closing. T A B L E > tags, and each row is enclosed in opening/closing T R > (table row) and T D > (table data) tags. A minimal format to create a web page is shown below.\n\nNotice that the title is nested between \"head\" tags, and the entire document is nested within \"HTML\" tags. Math homework help. Hotmath explains math textbook homework problems with step-by-step math answers for algebra, geometry, and calculus. Online tutoring available for math help.\n\nNote. There is a subtlety when the sequence is being modified by the loop (this can only occur for mutable sequences, e.g. lists).", null, "An internal counter is used to keep track of which item is used next, and this is incremented on each iteration. This article describes approaches for efficient isotropic two-dimensional convolution with disc-like and arbitrary circularly symmetric convolution kernels, and also discusses lens blur effects.\n\nKeywords: depth of field, circle of confusion, bokeh, circular blur, lens blur, hexagonal blur, octagonal blur, real-time, DOF Gaussian function approach. The circularly symmetric 2-d Gaussian kernel.", null, "Write a formula for the area of a circle as a function of its radius\nRated 5/5 based on 24 review\nTau Day | No, really, pi is wrong: The Tau Manifesto by Michael Hartl" ]
[ null, "http://scienceblogs.com/startswithabang/files/2012/03/Circle_Area.png", null, "https://i.stack.imgur.com/6Adtg.png", null ]
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https://millenia.cars.aps.anl.gov/pipermail/ifeffit/attachments/20150306/0ba91446/attachment.html
[ "<HTML><BODY>Good afternoon or other time of day again,<br>I don't know how to add message to the thread (I use online mail service), so will write additions here, sorry, may be somebody will correct me.<br>The chi_square definition in FEFFIT manual is chi_square=N_idp/N_data*sum((dat-model)^2/epsilon_k^2), and to this sum IFEFFIT adds restraint^2 (as of source code). But with 0 restraint I didn't get the right value. If there is 2*N_data, I get the right order, but not exactly the same value (0.6 and 0.8 for instance). chi_reduced=chi_square/(N_idp-N_param) by definition, and it is exact. (N_idp=18, N_param=4 in my case, eps_k=3.6e-3 from FT high-frequency compared with mu0 calculation in real spectrum. I'm not sure about small values, but the test is generated oxygen sphere without noise, so only systematic errors. I will correct it anyhow, but can it be a problem I'm not sure)<br>I found that I need to set Rmin and Rmax for N_idp calculus even if I fit in k space, but it doesn't help.<br>The adding of real part of fit chi (that exists, I don't know why) with 0 data made things only worse.<br>I try to find maths in source code, but it is big, and I can not find all definitions and understand quickly what is the beginning and what is the chain of calls I need. Are files in feffit and lib directories used together? That seems that the fit vector that is LS-fitted is (dat-model)/weight and restraint components, but what of weight. In fitnls.f file there are<br><br>weight(id) = sigdtk(id) * sigdtk(id) / sigwgt(id)              !in k space case. Is it epsilon_k**2 if user-defined epsilon_k? what is this normalization?<br>weight(id) = sqrt ( nptfit(id) * weight(id) / xinfo(id))       !nptfit=N_data without 2 from kmin to kmax? xinfo=N_idp ifeffit variable? <br>                                                !We sum chi_square in m_fit points, is it the same? in fft file there was 2*N_data even in k space?<br><br>So can I think that weight=sqrt(N_data/N_idp)*epsilon_k, or not? I didn't get the chi_square right with this formula. Also, dat-model is multiplied by window, but I make Hanning window with dk=0 and it doesn't help.<br><br>It is the main question I wish to find the answer now, because need to make this calculus to publish, for results in my compounds to be confident. I thought of suggesting that chi_square is different only by norm and restraint is added to chi_square and to calculate and renormalize errors and A parameter in restraint for calculation. But it can be a problem if is not proportional, and I'm not sure if A renormalization can help...<br> <br>The question of extending the method can wait a while.<br><br>I will be very thankful if somebody could help...<br><br><br>Thanks sincerely,<br>O.V. Kashurnikova,<br>XAFS group of the MEPhI, Moscow (Moscow Engeneering-Physics Institute)<br></BODY></HTML>" ]
[ null ]
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https://www.luogu.com.cn/problem/T82700
[ "# [HMI-1]简单平面几何1\n\n## 题目描述\n\n【例1.1】已知一正方形\\$ABCD\\$,几何中心为\\$E\\$。 连接\\$AE,BE,CE,DE\\$,作\\$FE=1/a_{1}AE,GE=1/a_{2}BE,HE=1/a_{3}CE,IE=1/a_{4}DE\\$ \\$JE=1/a_{5}FE,KE=1/a_{6}GE,LE=1/a_{7}GE,ME=1/a_{8}IE\\$ 连接\\$FK,GL,HM,IJ\\$,连接4个线段的中点,组成四边形A 连接\\$JK,KL,LM,MJ\\$,求ABCD面积比四边形A与四边形JKLM的重叠面积的比值 以下为a1=a2=...=a8=2时的图形,中间的八边形即所求图形 ![](https://cdn.luogu.com.cn/upload/pic/66882.png)\n\n## 输入输出样例\n\n### 输入样例 #1\n\n``2 2 2 2 1 1 1 1``\n\n### 输出样例 #1\n\n``4.00000``\n\n## 说明\n\n1<=\\$a_{1},a_{2},...,a_{8}\\$<=10" ]
[ null ]
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http://www.eden69.net/productlist/p91.html
[ "# 彩69彩票", null, "", null, "", null, "", null, "# 花岗岩破碎生产线\n\n【加工物料】:花岗岩\n【生产能力】:50-500t/h\n【配套设备】:颚式破碎机、圆锥破碎机、制砂机、振动给料机、洗砂机、振动筛等配套设备\n\n### 花岗岩破碎生产线介绍", null, "### 花岗岩破碎生产线设备——破碎设备\n\n1、颚式破碎机", null, "2、圆锥破碎机", null, "### 花岗岩破碎生产线设备——圆振动筛", null, "### 花岗岩破碎生产线设备——皮带输送机", null, "### 花岗岩破碎生产线设备——振动给料机", null, "```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`\n\n```\n\n```\n`\t`" ]
[ null, "http://www.eden69.net/productlist/proimg/al_m_big_20180614154325.jpg", null, "http://www.eden69.net/productlist/images/back1.png", null, "http://www.eden69.net/productlist/images/phone-home.png", null, "http://www.eden69.net/productlist/proimg/al_big_20180614154325.jpg", null, "http://www.eden69.net/productlist/uploads/image/20180517/20180517053211_96451.jpg", null, "http://www.eden69.net/productlist/uploads/image/20180517/20180517053219_78985.jpg", null, "http://www.eden69.net/productlist/uploads/image/20180517/20180517083054_24977.jpg", null, "http://www.eden69.net/productlist/uploads/image/20180517/20180517053233_59490.jpg", null, "http://www.eden69.net/productlist/uploads/image/20180517/20180517053241_67919.jpg", null, "http://www.eden69.net/productlist/uploads/image/20180517/20180517053250_12178.jpg", null ]
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https://commons.apache.org/proper/commons-math/apidocs/org/apache/commons/math4/linear/SingularValueDecomposition.html
[ "org.apache.commons.math4.linear\n\n## Class SingularValueDecomposition\n\n• public class SingularValueDecomposition\nextends Object\nCalculates the compact Singular Value Decomposition of a matrix.\n\nThe Singular Value Decomposition of matrix A is a set of three matrices: U, Σ and V such that A = U × Σ × VT. Let A be a m × n matrix, then U is a m × p orthogonal matrix, Σ is a p × p diagonal matrix with positive or null elements, V is a p × n orthogonal matrix (hence VT is also orthogonal) where p=min(m,n).\n\nThis class is similar to the class with similar name from the JAMA library, with the following changes:\n\nSince:\n2.0 (changed to concrete class in 3.0)\nMathWorld, Wikipedia\n• ### Constructor Summary\n\nConstructors\nConstructor and Description\nSingularValueDecomposition(RealMatrix matrix)\nCalculates the compact Singular Value Decomposition of the given matrix.\n• ### Method Summary\n\nAll Methods\nModifier and Type Method and Description\ndouble getConditionNumber()\nReturn the condition number of the matrix.\nRealMatrix getCovariance(double minSingularValue)\nReturns the n × n covariance matrix.\ndouble getInverseConditionNumber()\nComputes the inverse of the condition number.\ndouble getNorm()\nReturns the L2 norm of the matrix.\nint getRank()\nReturn the effective numerical matrix rank.\nRealMatrix getS()\nReturns the diagonal matrix Σ of the decomposition.\ndouble[] getSingularValues()\nReturns the diagonal elements of the matrix Σ of the decomposition.\nDecompositionSolver getSolver()\nGet a solver for finding the A × X = B solution in least square sense.\nRealMatrix getU()\nReturns the matrix U of the decomposition.\nRealMatrix getUT()\nReturns the transpose of the matrix U of the decomposition.\nRealMatrix getV()\nReturns the matrix V of the decomposition.\nRealMatrix getVT()\nReturns the transpose of the matrix V of the decomposition.\n• ### Methods inherited from class java.lang.Object\n\nclone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait\n• ### Constructor Detail\n\n• #### SingularValueDecomposition\n\npublic SingularValueDecomposition(RealMatrix matrix)\nCalculates the compact Singular Value Decomposition of the given matrix.\nParameters:\nmatrix - Matrix to decompose.\n• ### Method Detail\n\n• #### getU\n\npublic RealMatrix getU()\nReturns the matrix U of the decomposition.\n\nU is an orthogonal matrix, i.e. its transpose is also its inverse.\n\nReturns:\nthe U matrix\ngetUT()\n• #### getUT\n\npublic RealMatrix getUT()\nReturns the transpose of the matrix U of the decomposition.\n\nU is an orthogonal matrix, i.e. its transpose is also its inverse.\n\nReturns:\nthe U matrix (or null if decomposed matrix is singular)\ngetU()\n• #### getS\n\npublic RealMatrix getS()\nReturns the diagonal matrix Σ of the decomposition.\n\nΣ is a diagonal matrix. The singular values are provided in non-increasing order, for compatibility with Jama.\n\nReturns:\nthe Σ matrix\n• #### getSingularValues\n\npublic double[] getSingularValues()\nReturns the diagonal elements of the matrix Σ of the decomposition.\n\nThe singular values are provided in non-increasing order, for compatibility with Jama.\n\nReturns:\nthe diagonal elements of the Σ matrix\n• #### getV\n\npublic RealMatrix getV()\nReturns the matrix V of the decomposition.\n\nV is an orthogonal matrix, i.e. its transpose is also its inverse.\n\nReturns:\nthe V matrix (or null if decomposed matrix is singular)\ngetVT()\n• #### getVT\n\npublic RealMatrix getVT()\nReturns the transpose of the matrix V of the decomposition.\n\nV is an orthogonal matrix, i.e. its transpose is also its inverse.\n\nReturns:\nthe V matrix (or null if decomposed matrix is singular)\ngetV()\n• #### getCovariance\n\npublic RealMatrix getCovariance(double minSingularValue)\nReturns the n × n covariance matrix.\n\nThe covariance matrix is V × J × VT where J is the diagonal matrix of the inverse of the squares of the singular values.\n\nParameters:\nminSingularValue - value below which singular values are ignored (a 0 or negative value implies all singular value will be used)\nReturns:\ncovariance matrix\nThrows:\nIllegalArgumentException - if minSingularValue is larger than the largest singular value, meaning all singular values are ignored\n• #### getNorm\n\npublic double getNorm()\nReturns the L2 norm of the matrix.\n\nThe L2 norm is max(|A × u|2 / |u|2), where |.|2 denotes the vectorial 2-norm (i.e. the traditional euclidean norm).\n\nReturns:\nnorm\n• #### getConditionNumber\n\npublic double getConditionNumber()\nReturn the condition number of the matrix.\nReturns:\ncondition number of the matrix\n• #### getInverseConditionNumber\n\npublic double getInverseConditionNumber()\nComputes the inverse of the condition number. In cases of rank deficiency, the condition number will become undefined.\nReturns:\nthe inverse of the condition number.\n• #### getRank\n\npublic int getRank()\nReturn the effective numerical matrix rank.\n\nThe effective numerical rank is the number of non-negligible singular values. The threshold used to identify non-negligible terms is max(m,n) × ulp(s1) where ulp(s1) is the least significant bit of the largest singular value.\n\nReturns:\neffective numerical matrix rank\n• #### getSolver\n\npublic DecompositionSolver getSolver()\nGet a solver for finding the A × X = B solution in least square sense.\nReturns:\na solver" ]
[ null ]
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https://courses.maths.ox.ac.uk/node/43902
[ "M3: Statistics and Data Analysis - Material for the year 2019-2020\n\nPrimary tabs\n\n2019-2020\nLecturer(s):\nProf. Christl Donnelly\nCourse Term:\nTrinity\nCourse Lecture Information:\n\n16 lectures\n\nCourse Overview:\n\nThe course introduces the concept of likelihood for a probabilistic model and its use in estimating unknown model parameters. Models covered will include linear regression with one or two regressors. In many examples confidence intervals may be found by using the Central Limit Theorem (statement only). Model checking and outlier detection are core concepts that are broadly relevant across many aspects of mathematical modelling and will be explored here in the context of regression with one or two regressors. Regression models are an example of supervised learning, however a large part of statistics and data analysis can be classified as unsupervised learning, i.e. finding structure in data sets, e.g. data from financial markets, medical imaging, retail, population genetics, social networks. Techniques for finding structure in datasets are relevant to many parts of applied maths, specifically this course will cover principal components analysis and clustering techniques.\n\nLearning Outcomes:\n\nStudents should have an understanding of likelihood, the use of maximum likelihood to find estimators, and some properties of the resulting estimators. They should have an understanding of confidence intervals and their construction using the Central Limit Theorem. They should have an understanding of linear regression with one or two regressors, and of finding structure in data sets using principal components and some clustering techniques.\n\nCourse Syllabus:\nCourse Synopsis:\n\nRandom samples, concept of a statistic and its distribution, sample mean as a measure of location and sample variance as a measure of spread.\n\nConcept of likelihood; examples of likelihood for simple distributions. Estimation for a single unknown parameter by maximising likelihood. Examples drawn from: Bernoulli, binomial, geometric, Poisson, exponential (parametrized by mean), normal (mean only, variance known). Data to include simple surveys, opinion polls, archaeological studies, etc. Properties of estimators---unbiasedness, Mean Squared Error = (bias$^{2}$ + variance). Statement of Central Limit Theorem (excluding proof). Confidence intervals using CLT. Simple straight line fit, $Y_{t}=a+bx_{t}+\\varepsilon_{t}$, with $\\varepsilon _{t}$ normal independent errors of zero mean and common known variance. Estimators for $a$, $b$ by maximising likelihood using partial differentiation, unbiasedness and calculation of variance as linear sums of $Y_{t}$. (No confidence intervals). Examples (use scatter plots to show suitability of linear regression).\n\nLinear regression with 2 regressors. Special case of quadratic regression $Y_t = a + bx_t + cx^2_t + \\epsilon_t$. Model diagnostics and outlier detection. Residual plots. Heteroscedasticity.\nOutliers and studentized residuals. High-leverage points and leverage statistics. [2.5]\n\nIntroduction to unsupervised learning with real world examples. Principal components analysis (PCA). Proof that PCs maximize directions of maximum variance and are orthogonal using Lagrange multipliers. PCA as eigendecomposition of covariance matrix. Eigenvalues as variances. Choosing number of PCs. The multivariate normal distribution pdf. Examples of PCA on multivariate normal data and clustered data. \n\nClustering techniques; K-means clustering. Minimization of within-cluster variance. K-means algorithm and proof that it will decrease objective function. Local versus global optima and use of random initializations. Hierarchical clustering techniques. Agglomerative clustering using complete, average and single linkage [2.5]" ]
[ null ]
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https://www.meritnation.com/ask-answer/question/why-3-equation-is-not-balanced-and-only-the-upper-two-equati/study-of-compounds/13947053
[ "Why 3 equation is not balanced and only the upper two equations are balanced why is it so? It is inside the chapter and I want to know that why they had done this?", null, "Dear Student,\n\nAs such it is expected that the chemical equation should be balanced. However, in this case I suppose they must have missed balancing it.\n\nHere is the balanced equation:\nMg + 2HCl (dilute) --> MgCl2 + H2\n\nRegards\n\n• 0\nWhat are you looking for?" ]
[ null, "https://s3mn.mnimgs.com/img/shared/content_ck_images/ck_5d85e37f33898.png", null ]
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