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|
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
beef3bbb79c2525e79e3151d2827bb56dbfb4145
|
04236ab1161ec860ab3b1d0c3225fcbdc54923a3
|
/2012.d/3-remez.d/tcheby.sci
|
8fedfa1ef128366c63995824683985941f807a02
|
[
"MIT"
] |
permissive
|
homeostasie/petits-pedestres
|
957695cdb8a7823ed2e3fe79f7b441410928cba9
|
557c810e26412bc34ebe063dcd904affe5a27855
|
refs/heads/master
| 2023-05-31T03:35:13.365160 | 2023-04-26T21:47:56 | 2023-04-26T21:47:56 | 163,504,589 | 2 | 0 | null | null | null | null |
ISO-8859-1
|
Scilab
| false | false | 986 |
sci
|
tcheby.sci
|
funcprot(0)
function [Coef_poly,Erreur]=F_Coef_Tcheby(fon_uti)
//Soit Coef_poly la matrice des coéfficients du polynôme
//Soit Vender la matrice de Vandermonde
for i=1:1:n+1
for j=0:1:n
Vander(i,j+1)=X_n(i)**j,
end
Vander(i,n+1)=(-1)**(i+1)
end
//Soit ColFunc1 le vecteur colonne de la fonction fon_uti aux points de X_n
for i=1:1:n+1
ColFunc1(i)=fon_uti(X_n(i))
end
Coef_poly=lsq(Vander,ColFunc1)
Erreur=abs(Coef_poly(n+1))
endfunction
funcprot(0)
function [Poly_tcheby]=F_Poly_Tcheby(x)
//On construit le polynome à partir des coefficients obtenu par Tcheby
//On appelle la fonction qui calcul les coeffs
A=0
for i=1:1:n
A=A+Coef_poly(i)*(x)^(i-1)
end
Poly_tcheby=A
endfunction
[Coef_poly,Erreur]=F_Coef_Tcheby(fon_uti);
[Poly_tcheby]=F_Poly_Tcheby;
funcprot(0)
function [fmoinsp]=F_fmoinsp(x)
fmoinsp=fon_uti(x)-Poly_tcheby(x)
endfunction
funcprot(0)
[fmoinsp]=F_fmoinsp;
|
0b411795cf0abfe4b7a2b6d09755caddb0de9cdc
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/32/CH2/EX2.01/2_01.sce
|
26aee15eee3005d4e77f5bf238994daf4baec372
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 335 |
sce
|
2_01.sce
|
//pathname=get_absolute_file_path('2.01.sce')
//filename=pathname+filesep()+'2.01-data.sci'
//exec(filename)
//Temperature of human body in degree Fahrenheit:
Tf=98.6;
//Temperature of the body in degree Celcius:
Tc=(Tf-32)/1.8
printf("\n\nRESULTS\n\n")
printf("\n\nTemperature of the human body in degree Celcius= %f \n\n",Tc)
|
b37c45c681546f8693d1c61bcfeae755b7aa2b1a
|
346b29127e59e672f20ebc2738580a91c78a2cb6
|
/Scilab/report3/markovchain.sce
|
9916bb46b7b77768b43ad7c91579bdf227be52da
|
[] |
no_license
|
cygnusbeta/tokuron
|
b19cce6ffd61e4aee20190fd6bc28c737a7a59ae
|
386957509f91508601c2981601fd39fd85c8e0e5
|
refs/heads/master
| 2020-11-24T13:49:38.292405 | 2020-01-12T19:15:52 | 2020-01-12T19:15:52 | 228,177,489 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 3,130 |
sce
|
markovchain.sce
|
// Markov 連鎖の定常状態を遷移確率行列 P の固有値・固有ベクトルから求める。
// また、連鎖の差分方程式（漸化式）を反復して、定常状態に収束するか調べる。
clear
xdel(winsid()); // すべてのグラフィックウィンドウを閉じる
// 状態の数と行列 P を与える。
p = [ 0.3 0 0.7; ...
0 0.6 0.4; ...
0.1 0.7 0.2]; // テキスト p.43 の例
n = size(p,1); // 正方行列 p を与えたと仮定している。
disp('n')
disp(n)
// p の左固有ベクトルが欲しい。spec 関数は右固有ベクトルを与えるので、
// p の転置行列の左固有ベクトルを求める。それを転置して、目的である
// p の右固有ベクトルが求まる。
[evec,eval]=spec(p.');
// 対角行列 eval の対角成分が固有値なので取り出す。
lambda = diag(eval);
disp('固有値は');
disp('lambda')
disp(lambda);
// 対応する固有ベクトルが各列に入った行列 evec を転置する。
evec = evec.';
disp('evec')
disp(evec)
// 定常状態の固有ベクトルは、すべての成分が同符号であり、厳密に 1 の
// 固有値に対応していなければならない。それを探す。
for i=1:n
if abs(sum(evec(i,:)))==sum(abs(evec(i,:))) then // 同符号の成分のとき等号が成立
if (abs(lambda(i)-1) < 1e-15) then
disp('定常状態の固有ベクトルが見つかりました。');
disp([i,lambda(i)]);
// *** 見つけた evec(i,:) は 2-norm で正規化されています。つまり成分の2乗の和が
// *** 1 となっています。各成分を定常状態の確率と見るには、1-norm で正規化する
// *** 必要があります。次の行でそうしてください。
steadystate = evec(i,:) / sum(evec(i,:));
disp(steadystate);
break;
end
end
end
if sum(abs(steadystate))==0 then
halt('定常状態の固有ベクトルが見つかりませんでした。');
end
// 初期条件（時刻 0 での各状態の確率）を適当に与え、行列 p による写像を
// 反復したときの変化を求め、3成分（各状態の確率）がどう変わるか、反復
// 回数を横軸にとって図示してください。
x = [ 1 0 0 ]; // 初期条件（別のも試してみてください。）
m = 20; // 反復回数
scf(0); clf;
p1 = zeros(1, m + 1)
p2 = zeros(1, m + 1)
p3 = zeros(1, m + 1)
p1(1, 1) = x(1, 1)
p2(1, 1) = x(1, 2)
p3(1, 1) = x(1, 3)
for i=2:m+1
x = x * p
steadystate = steadystate / sum(steadystate)
p1(1, i) = x(1, 1)
p2(1, i) = x(1, 2)
p3(1, i) = x(1, 3)
end
disp('p1')
disp(p1)
disp('p2')
disp(p2)
disp('p3')
disp(p3)
plot(p1, 'r')
plot(p2, 'g')
plot(p3, 'b')
title('x[1]:赤, x[2]:緑, x[3]:青 とsteadystate（横線）の比較');
p1theory = ones(1, m + 1).' * steadystate(1, 1)
p2theory = ones(1, m + 1).' * steadystate(1, 2)
p3theory = ones(1, m + 1).' * steadystate(1, 3)
plot(p1theory, 'r')
plot(p2theory, 'g')
plot(p3theory, 'b')
|
4f4939a74615793041d361c17baef23f4a9f7bd3
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1628/CH15/EX15.2/Ex15_2.sce
|
43ddc5fdbad57ad6ba4f2a0c15802859e11d4c9c
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 447 |
sce
|
Ex15_2.sce
|
// Examle 15.2
p=12; // No.Of poles
f=50; // Frequency
Ns=(120*f)/p; // Synchronous speed
disp(' The Synchronous Speed (Ns) = '+string(Ns)+' rpm');
N=485; // Speed of Motor
s=(Ns-N)/Ns; // Slip
fr=s*f; // The Frequence of Rotor (fr)
disp(' The Frequence of Rotor (fr) = '+string(fr)+' Hz');
// p 593 15.2
|
f0a3cbb644782e11ac3ca1af5743aaf8de2babc5
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1475/CH3/EX3.15/Example_3_15.sce
|
f9e2e2c48b7ff96e9af81175c7e1d8c44a875100
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 512 |
sce
|
Example_3_15.sce
|
//Example 3.15 The safety limit of a crane is known to be 32 tons
clc;
clear;
m=0.3;
s_d=0.2;
n=100;
disp(n,"Sample size =",s_d,"Standard Deviation",m,"Mean");
disp(s_d/sqrt(n),"and Standard Deviation =",0.3,"Since the sample size n=100 is large, the sample mean follows normal distribution approx. with Mean=");
disp(0.1587,"Probab. that mean is greater than 0.32=Area under the standard normal curve to the right of the ordinate at z=1",(0.32-m)/0.02,"The standarised value of sample mean 0.32 is ");
|
0321e1ba5ebd7f02bbaa7b25d4173d736adbe1da
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2672/CH5/EX5.28/Ex5_28.sce
|
c7e1b958373729664f006ca07b38d66e93bad423
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 307 |
sce
|
Ex5_28.sce
|
//Example 5_28
clc;
clear;
close;
format('v',5);
//given data :
Pmax=2.5;//W
Vf=900;//mV
If_max=Pmax/(Vf/1000);//A
disp(If_max,"(a) Maximum allowable forward current(A) : ");
Rf=Pmax/If_max^2;//ohm
format('v',7);
disp(Rf,"(b) Forward Diode Resistance(ohm)")
//Answer in the textbok is wrong.
|
e24869de8fc91d71e5b9f0258cda89d5afce198a
|
1d7cb1dbfad2558a4145c06cbe3f5fa3fc6d2c08
|
/Scilab/SparamToolBox/SparamToolbox/v1.1/x86_64/src/c/loader.sce
|
c9236fe8ed9896be28957ccea5cf6ef183194ea8
|
[] |
no_license
|
lrayzman/SI-Scripts
|
5b5f6a8e4ae19ccff53b8dab7b5773e0acde710d
|
9ab161c6deff2a27c9da906e37aa68964fabb036
|
refs/heads/master
| 2020-09-25T16:23:23.389526 | 2020-02-09T02:13:46 | 2020-02-09T02:13:46 | 66,975,754 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 805 |
sce
|
loader.sce
|
// This file is released under the 3-clause BSD license. See COPYING-BSD.
// Generated by builder.sce : Please, do not edit this file
// ----------------------------------------------------------------------------
//
if ~win64() then
warning(_("This module requires a Windows x64 platform."));
return
end
//
write_tchstn_path = get_absolute_file_path('loader.sce');
//
// ulink previous function with same name
[bOK, ilib] = c_link('write_tchstn');
if bOK then
ulink(ilib);
end
//
link(write_tchstn_path + filesep() + 'liberr_codes' + getdynlibext());
link(write_tchstn_path + 'libwrite_tchstn' + getdynlibext(), ['write_tchstn'],'c');
// remove temp. variables on stack
clear write_tchstn_path;
clear bOK;
clear ilib;
// ----------------------------------------------------------------------------
|
0988729a998cf73bdf57717507de8566bd46e802
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/50/DEPENDENCIES/F28.sce
|
e79b88348bf7771fd4f2441759e7720ddc7ab5fb
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 189 |
sce
|
F28.sce
|
function [F] = f28(x)
//f2(x) = 0, with x = [x(1);x(2)]
//represents a system of 2 non-linear equations
F(1) = x(1)^2+x(1)*x(2) + x(2)^2 - 7;
F(2) = x(1)^3+x(2)^3 -9;
endfunction
|
5c0d5fbf151f19e61e9aa9fdb41ac7c6840c902f
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1118/CH13/EX13.1/eg13_1.sce
|
275f91c3c33da6f0a1694e1f80cc060747e1dd85
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 788 |
sce
|
eg13_1.sce
|
clear;
clear;
//clc();
function [mag,theta]=c(r,i)
mag=sqrt(r*r + i*i)
theta=atand(i/r)
endfunction
previousprot = funcprot(0)
funcprot(0)
r=10;
x=30;
i=x;
vs=132;
vr=vs;
z=r + (%i)*x;
B=z;
A=1;
b=atand(x/r);
a=0;
[mag,theta]=c(r,i);
pm=(vs*vr/mag) - ((A*vr^(2)/mag)*cosd(theta));
printf("\n the maximum power is: %.2f MW\n",pm);
//maximum power is at an angle
del=theta;
printf("\n the maximum power angle is: %.2f degrees\n",del);
//determining the rating of the syncronous phase modifier
pl=100;
pr0=-(vr^2)*r/mag^(2);
qr0=-(vr^(2)*x)/mag^(2);
pr=vs*vr/mag;
q=sqrt(pr^(2) - (pr0 - pl)^(2)) + qr0;
qpm=pl*tand(acosd(0.9)) - q;
printf("\n the rating of the phase modifier is: %.2f (leading)",qpm);
|
10d6855b64471b4624e777e84a7b525e0efcb7ca
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/213/CH15/EX15.17/15_17.sce
|
266a0f083c6abb53cada4cb6c967f92ea26f3270
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,117 |
sce
|
15_17.sce
|
//To find radius and MI
clc
//Given:
m=55 //kg
l=850/1000, d1=75/1000, d2=100/1000 //m
tp1=1.83, tp2=1.68 //seconds
//Solution:
//Refer Fig. 15.20
//Calculating the length of equivalent simple pendulum when suspended from the top of small end bearing
L1=9.81*(tp1/(2*%pi))^2 //m
//Calculating the length of equivalent simple pendulum when suspended from the top of big end bearing
L2=9.81*(tp2/(2*%pi))^2 //m
//Radius of gyration of the rod about an axis passing through the centre of gravity and perpendicular to the plane of oscillation:
//Calculating the distances of centre of gravity from the top of small end and big end bearings
//We have, h1*(L1-h1) = h2*(L2-h2), or h1^2-h2^2+h2*L2-h1*L1 = 0 .....(i)
//Also, h1+h2 = d1/2+l+d2/2, or h1+h2-d1/2-l-d2/2 = 0 .....(ii)
function y=f(x)
h1=x(1)
h2=x(2)
y(1)=h1^2-h2^2+h2*L2-h1*L1
y(2)=h1+h2-d1/2-l-d2/2
endfunction
z=fsolve([1,1],f)
h1=z(1), h2=z(2) //m
//Calculating the required radius of gyration of the rod
kG=sqrt(h1*(L1-h1)) //m
//Calculating the moment of inertia of the rod
I=m*(kG)^2 //kg-m^2
//Dynamically equivalent system for the rod:
//Calculating the distance of the mass situated at the centre of small end bearing from the centre of gravity
l1=h1-d1/2 //m
//Calculating the distance of the second mass from the centre of gravity towards big end bearing
l2=(kG)^2/l1 //m
//Calculating the magnitude of the mass situated at the centre of small end bearing
m1=(l2*m)/(l1+l2) //kg
//Calculating the magnitude of the second mass
m2=(l1*m)/(l1+l2) //kg
//Results:
printf("\n\n Radius of gyration of the rod about an axis passing through the centre of gravity and perpendicular to the plane of oscillation, kG = %.3f m.\n\n",kG)
printf(" Moment of inertia of the rod, I = %.2f kg-m^2.\n\n",I)
printf(" Magnitude of the mass situated at the centre of small end bearing, m1 = %.2f kg.\n\n",m1)
printf(" Magnitude of the second mass, m2 = %.2f kg.\n\n",m2)
|
c47fe913a39949301cb9c7c2e5a6cd2efb9d0a40
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/491/CH1/EX1.7/1_7.sce
|
f68a744891e87a95ecfad75e1cd2cf9c94873ad0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 839 |
sce
|
1_7.sce
|
b1 = 1.5 ; // width of rectangular crosssection in inch
t = 0.5 ; // thickness of rectangular crosssection in inch
b2 = 3 ; // width of enlarged rectangular crosssection in inch
d = 1 ; // diameter in inch
// Part (a)
s_1 = 16000; // maximum allowable tensile stress in Psi
P_1 = s_1*t*b1 ;
disp("lb",P_1,"The allowable load P1 is")
// Part (b)
s_2 = 11000; // maximum allowable tensile stress in Psi
P_2 = s_2*t*(b2-d) ;
disp("lb",P_2,"allowable load P2 at this section is")
//Part (c)
s_3 = 26000; // maximum allowable tensile stress in Psi
P_3 = s_3*t*d
disp("lb",P_3,"The allowable load based upon bearing between the hanger and the bolt is")
// Part (d)
s_4 = 6500; // maximum allowable tensile stress in Psi
P_4 = (%pi/4)*(d^2)*2*s_4 ;
disp("lb",P_4,"the allowable load P4 based upon shear in the bolt is")
|
c7db1498b4979ce4cf5bc8d400a93066c90a1060
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449d555969bfd7befe906877abab098c6e63a0e8
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/3446/CH10/EX10.5/Ex10_5.sce
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0f6e2552a14803bb9eb07503c36718118ce1bb9d
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 757 |
sce
|
Ex10_5.sce
|
// Exa 10.5
// To calculate the optimum diameter (DH), spacing (S) for the antenna and total length of the antenna,
// To calculate the antenna gain,
// To calculate the beam width of the antenna.
clc;
clear all;
N=12; //number of turns
fr=1.8; //frequency in GHz
//solution
lamda=3*10^8/(fr*10^9);
DH=lamda/%pi;// diameter of helix in milli-meters
S=lamda/4;//turn spacing in millimetres
L=N*S;
G=15*N*S*(DH*%pi)^2/lamda^3;
Theta=52*lamda/(%pi*DH)*sqrt(lamda/(N*S));
printf('The optimim diameter is %d mm\n ',DH*1000);
printf('Spacing is %.1f mm\n ',S*1000);
printf('Total Length of antenna is %d mm\n ',L*1000);
printf('The antenna gain is %.1f dBi\n ',10*log10(G));
printf('The BeamWidth of antenna is %d degrees \n ',Theta);
|
0a78af83997715d911ed9b10b99124e9dbae4ffd
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449d555969bfd7befe906877abab098c6e63a0e8
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/569/CH6/EX6.28/6_28.sci
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25bc2b9a48f7ab2a0086a7bcb25afef09a0911af
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 152 |
sci
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6_28.sci
|
// Calculating the weight of MSB and LSB
clc;
Ra=10;
b=5;
Wmsb=Ra/2;
disp(Wmsb,'weight of MSB (V)=')
Wlsb=Ra/2^b;
disp(Wlsb,'weight of LSB (V)=')
|
15bffc1c0347ade88292cc1282a8f2d6a7c5272b
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449d555969bfd7befe906877abab098c6e63a0e8
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/2243/CH8/EX8.11/Ex8_11.sce
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de1dd6847bb3158a4876ece4f24ff134e8274d60
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 855 |
sce
|
Ex8_11.sce
|
clc();
clear;
//Given :
T_half = 5730; // carbon 14 half life in years
Na = 6.023*10^23; // Avogadro constant in nuclei/mole
M = 25;// charcoal mass in gm
mm = 12;// molar mass of carbon 12 in gm/mole
a = 250 ; // disinitegrations per minute (Carbon 14 activity)
// 1 year = 525949 minutes
lambda = 0.693/(T_half*525949);// disinitegrations per minute per nucleus
N0_1 = (Na/mm)*M ; // Number of nuclei (Carbon 12)
// Carbon 14 to Carbon 12 ratio = 1.3*10^-12
N0_2 = 1.3*10^-12*N0_1 ; // Number of nuclei (Carbon 14)
R0 = N0_2*lambda ; // disinitegrations per minute per nucleus
a0 = R0 ; // initial activity
t = log(a0/a)/lambda ;
// 1 year = 525949 minutes
printf("The tree died %d years ago",t/525949 );
// Result obtained differs from the textbook, because R0 value obtained here is 375.1025, where as in textbook it is 374.
|
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449d555969bfd7befe906877abab098c6e63a0e8
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/1748/CH2/EX2.4/Exa2_4.sce
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8499ff3fa81b308e64c5f18905dc54c7aa4878c3
|
[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 289 |
sce
|
Exa2_4.sce
|
//Exa 2.4
clc;
clear;
close;
//Given data :
P=8;//no. of poles
f=50;//in Hz
fr=1.5;//in Hz
//Formula : fr=S*f
S=fr/f;//slip(unitless)
Ns=120*f/P;//in rpm
//Formula : S=(Ns-Nr)/Ns
Nr=Ns-S*Ns;//in rpm
disp(round(Nr),"Motor running speed in rpm : ");
disp(S*100,"Slip(in %):");
|
69bb88ee6ddfcb5af4ed7600e59f5668b84ab3a4
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449d555969bfd7befe906877abab098c6e63a0e8
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/479/CH4/EX4.2/Example_4_2.sce
|
013071aa17d399a9771ada2e9a9016137e4d5d1b
|
[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 925 |
sce
|
Example_4_2.sce
|
//Chemical Engineering Thermodynamics
//Chapter 4
//Second Law of Thermodynamics
//Example 4.2
clear;
clc;
//Given
T1 = 373;//Temperature of the saturated steam in K
T2 = 298;//Temperature of the saturated water in K
//To calculate the total change in entropy and hence determine the reversibility of the process
//del_H = del_Q+(V*del_P)
//del_H =del_Q; since it is a constant pressure process
//From steam table,
//enthalpy of saturated steam at 373K is
H1 = 6348.5;// in Kcal/Kg
//enthalpy of saturated liquid water at 373K is
H2 = 99.15;//in Kcal/Kg
Q = H2-H1;//heat rejected in Kcal/Kg
del_S1 = Q/T1;//change in entropy of the system in Kcal/Kg K
del_S2 = Q/T2;//change in entropy of the surronding in Kcal/Kg K
del_St = del_S1+del_S2;//total change in the entropy in Kcal/Kg K
if(del_St == 0)
mprintf('Process is reversible');
else
mprintf('Process is irreversible');
end
//end
|
859225eab8aeb474f6f22be862f15ecefd120f88
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449d555969bfd7befe906877abab098c6e63a0e8
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/1952/CH1/EX1.12/Ex1_12.sce
|
9e511433a877a3afa80dbff576feb57051438615
|
[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 258 |
sce
|
Ex1_12.sce
|
// chapter 1 , Example1 12 , pg 25
V=13500//volume(in m^3)
T=1.2//reverberation time(in sec)
a=0.65//average absorption coefficient(in Sabine/m^2)
S=(0.165*V)/(a*T)//area of interior surface
printf("Area of interior surface\n")
printf("S=%.1f m^2",S)
|
9da325a5d3bd190b31fb702b0afe060e8d2bd626
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449d555969bfd7befe906877abab098c6e63a0e8
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/704/CH2/EX2.19/2_19.txt
|
62041e4898a25773d290a5ccc51a4d63544fa40b
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[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 466 |
txt
|
2_19.txt
|
//Capyion:find the change in back emf from no load to load
//Exam:2.19
clc;
clear;
close;
V=220;//given voltage to machine(in V)
R_a=0.5;//armature circuit resistance(in ohm)
I_1=25;//full load armature current(in Amp)
I_2=5;//no load armature current(in Amp)
E_1=V-I_1*R_a;//back emf at full load(in V)
E_2=V-I_2*R_a;//back emf at no load(in V)
E=E_2-E_1;//change in back emf no load to load
disp(E,'change in back emf from no load to load(in Volts)=');
|
24aa1eb8fca55df5f23a58aa589b8dccefca738f
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449d555969bfd7befe906877abab098c6e63a0e8
|
/991/CH10/EX10.1/Example10_1.sce
|
0cb977309f62ac3e1fd4a7a0864e1721316bd737
|
[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 3,590 |
sce
|
Example10_1.sce
|
//Example 10.1. refer fig.10.8.
clc
format(6)
hie=1600
hfe=60
hre=5*10^-4
hoe=25*10^-6
hic=1600
hfc=-61
hrc=1
hoc=25*10^-6
disp("The AC equivalent circuit of the CE-CC amplifier is shown in fig.10.9(a)")
disp("The Second Stage :")
disp("Current gain :")
disp("The current gain of a particular stage is given by")
disp(" AI = -hf / (1 + ho*ZL)")
disp("For the second stage ZL = RE2 and the current gain of the second stage is")
RE2=4000
AI2=-hfc/(1+(hoc*RE2))
disp(AI2," AI2 = -Ie2 / Ib2 = -hfc / (hoc*RE2) =")
disp("The input impedance Ri of a particular stage is given by")
disp(" Ri = hi + hf*AI*ZL")
disp("For the second stage,")
Ri2 = hic + (hrc*AI2*RE2)
Ri22=Ri2*10^-3
disp(Ri22," Ri2(k-ohm) = hic + (hrc*AI2*RE2) =")
disp("Thus, the CC stage has a high input impedance.")
disp("The voltage gain of a particular stage is")
disp(" AV = (AI*ZL) / Zi")
disp("For the second stage,")
Re2=4000
AV2=(AI2*Re2)/Ri2
disp(AV2," AV2 = Vo/V2 = (AI2*Re2) / Ri2")
disp("The First Stage :")
RC1=4000
format(5)
RL1=(RC1*Ri2)/(RC1+Ri2)
RL11=RL1*10^-3
disp(RL11," RL1(k-ohm) = RC1 || Ri2 =")
disp("Current gain,")
AI1= -hfe/(1+(hoe*RL1))
disp(AI1," AI1 = -IC1/Ib1 = -hfe/(1+(hoe*RL1)) =")
disp("The input impedance of the first stage, which is also the input impedance of the cascaded amplifier is")
Ri1=hie +(hre*AI1*RL1) // answer in textbook is wrong
Ri11=Ri1*10^-3
disp(Ri11," Ri1(k-ohm) = hie + hre*AI1*RL1 =")
disp("The voltage gain of the first stage is")
format(7)
AV1=(AI1*RL1)/Ri1 // answer in textbook is wrong
disp(AV1," AV1 = V2/V1 = (AI1*RL1) / Ri1 =")
disp("The output admittance of the first transistor Q1")
RS=600
format(5)
Yo1=hoe-((hfe*hre)/(hie+RS))
Yo0=Yo1*10^6
disp(Yo0," Yo1(uA/V) = hoe - ((hfe*hre) / (hie+RS)) =")
disp("The output impedance of the first stage")
format(6)
Ro1=1/Yo1
Ro0=Ro1*10^-3
disp(Ro0," Ro1(k-ohm) = 1 / Yo1 =")
disp("The output impedance taking RC1 into account is")
format(5)
Rot1=(Ro1*RC1)/(Ro1+RC1)
Rott=Rot1*10^-3
disp(Rott," Rot1(k-ohm) = Ro1 || RC1 =")
disp("This is the effective source resistance RS2 of the second stage")
disp("The output admittance of the second stage")
format(7)
Yo2=hoc-((hfc*hrc)/(hic+Rot1))
disp(Yo2," Yo2(A/V) = hoc-((hfc*hrc) / (hic+Rot1)) =")
disp("Output impedance,")
format(4)
RO2=1/(11.525*10^-3)
disp(RO2," RO2(ohm) = 1 / Yo2 =")
disp("The amplifier output impedance taking RE2 into account is RO2 || RE2")
format(6)
Ro2=(87*4000)/(87+4000)
disp(Ro2,"Hence, Ro2(ohm) = (RO2*RE2) / (RO2+RE2) =")
disp("Overall current gain :")
disp("The output or total current gain of both the stages is")
disp(" AI = -Ie2 / Ib1 = (-Ie2/Ib2)(Ib2/IC1)(IC1/Ib1)")
disp(" = -AI2*(Ib2/Ic1)*AI1")
disp("From fig.10.9(b),")
disp(" Ib2 = (-IC1)(Rc1 / Rc1+Ri2)")
Rc1=4000
format(7)
x=(-Rc1)/ (Rc1+Ri2)
disp(x," Ib2/Ic1 = -Rc1/ Rc1+Ri2 =")
format(6)
AI=-AI2*x*AI1
disp(AI," AI = -AI2*AI1*(Rc1 / Ri2+Rc1) =")
disp("The overall voltage gain of the amplifier,")
disp(" AV = Vo / V1 = (Vo/V2)(V2/V1)")
AV=AV2*AV1
disp(AV," AV = AV2*AV1 =") // answer in textbook is wrong
disp("The overall voltage gain taking the source impedance into account,")
format(4)
AVs=AV*(Ri1/(Ri1+RS))
disp(AVs," AVs = Vo/Vs = Av(Ri1 / Ri1+Rs) =") // answer in textbook is wrong
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5a6acad448276b653c709f88083e8d8a448fa360
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449d555969bfd7befe906877abab098c6e63a0e8
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/1733/CH2/EX2.18/2_18.sce
|
fcb43bd20872f2b79b17f55a3d2afb34b9640edd
|
[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 382 |
sce
|
2_18.sce
|
//2.18
clc;
Vdc=100;
Vm=(Vdc+2*1.7)*%pi/(2*cosd(30));
Vrms_sec=Vm/2^0.5;
Vrms_pri=230;
Turn_ratio=Vrms_pri/Vrms_sec;
printf("\nTurn Ratio = %.2f ", Turn_ratio)
Irms_sec=15/2^0.5;
Ip=15;
Trans_rating=Vrms_sec*Ip;
printf("\nTransformer rating = %.2f VA", Trans_rating)
PIV=Vm;
printf("\nPIV = %.2f V", PIV)
printf("\nRMS value of thyristor current = %.2f A", Irms_sec)
|
0f813278577cfd60818b056b0b30367940a99a14
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449d555969bfd7befe906877abab098c6e63a0e8
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/2126/CH5/EX5.25/25.sce
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4425d3e6058cf477b35cb8f2a60a3180639af138
|
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no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,083 |
sce
|
25.sce
|
clc
clear
//Input data
M1=2.8 //Inlet mach number
sig=42 //Shock wave angle in degree
Px=1 //Pressure upstream of shock in bar(Assuming)
k=1.4 //Adiabatic constant
//Calculations
Mx=M1*sind(sig) //Mach number before the shock
My=0.601 //Mach number after the shock from gas tables @Mx
p1=3.98 //Static pressure ratio after and before the shock from gas tables @Mx
Py=Px*p1 //Pressure after shock in bar
p2=4.994 //Stagnation pressure after shock to Static pressure before shock from gas tables @Mx
Poy=Px*p2 //Stagnation pressure after shock in bar
p3=0.788 //Stagnation pressure ratio after and before the shock from gas tables @Mx
Pox=Poy/p3 //Stagnation pressure before shock in kPa
dPl=Pox-Poy //Total pressure loss in bar
def=atand(((M1^2*sind(2*sig))-(2/tand(sig)))/(2+(M1^2*(k+cosd(2*sig))))) //Deflection angle in degree
M2=My/(sind(sig-def)) //Downstream mach number
//Output
printf('(A)Deflection angle is %3i degree\n (B)Downstream mach number is %3.3f\n (C)Static pressure is %3.3f bar\n (D)Total pressure loss is %3.3f bar',def,M2,Py,dPl)
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c263eceddca14820a0d79158055e337cf4d0c95a
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449d555969bfd7befe906877abab098c6e63a0e8
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/3760/CH8/EX8.8/ExA_8.sce
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3820eeb0393683d0e79c0e1cc414e818564a05ca
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no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 725 |
sce
|
ExA_8.sce
|
clc;
l=0.8; // length of conductor
B=1.2; // flux density of uniform magnetic field
v=30; // speed of conductor
disp('case a');
// conductor motion is normal to field flux
theta=90; // angle between direction of motion and field flux
e=B*l*v*sin(theta*(%pi/180));
printf('EMF induced is %f V\n',e);
disp('case b');
// conductor motion is at an angle of 30 degrees from direction of field
theta=30; // angle between direction of motion and field flux
e=B*l*v*sin(theta*(%pi/180));
printf('EMF induced is %f V\n',e);
disp('case c');
// conductor motion is parllel to field flux
theta=0; // angle between direction of motion and field flux
e=B*l*v*sin(theta*(%pi/180));
printf('EMF induced is %f V\n',e);
|
1d30c8b051364fa051896c268291cce67d2645ce
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449d555969bfd7befe906877abab098c6e63a0e8
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/689/CH8/EX8.4/4.sce
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fd1f4d42acb358e46dfeed4595580201ff402154
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 337 |
sce
|
4.sce
|
clc; funcprot(0);
//Example 8.4 Power Required by Wing
// Initialisation of variables
S = 350;
V = 80;
alpha = 6;
Cd = 0.0452; // Value of Cd from fig 8.8
rho = 0.002378;
// Calculations
D = Cd*rho/2*S*V^2;
HP = D*V/550;
//Results
disp(HP,"Horse power required to move the wing forward(hp) :",D,"Drag (lb):");
|
0e529e3f5dc612ae1060493f67efad50230b7ff3
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449d555969bfd7befe906877abab098c6e63a0e8
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/1553/CH10/EX10.28/10Ex28.sce
|
995cd1bf6490a8d22e81417a8bb876018f4a97bf
|
[] |
no_license
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FOSSEE/Scilab-TBC-Uploads
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948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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7bc77cb1ed33745c720952c92b3b2747c5cbf2df
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refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
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Scilab
| false | false | 150 |
sce
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10Ex28.sce
|
//chapter 10 Ex 28
clc;
clear;
close;
AmoreB=100/(3*100);
BlessA=(AmoreB/(1+AmoreB))*100;
mprintf("B earns %d percent less than A",BlessA);
|
7aef7a6c696ed1ae6ad2152110b85257ce63b470
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/965/CH13/EX13.16/16.sci
|
ca8e3587f02e8137b3a8208b14c550d32cfeecce
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 403 |
sci
|
16.sci
|
clc;
clear all;
disp("Nitrogen diffusion rate ")
A=1;
T=25+273;
L=12/1000;//m
G=8314;// gas constant
xB=0.2;
Dab=16*10^(-6);
xC=0.1;
Dac=14*10^(-6);
xD=0.7;
Dad=9*10^(-6);
D=1/(xB/Dab+xC/Dac+xD/Dad);//m^2/s
p=1.013;
pN1=0.15;//bar
pN2=0.08;//bar
pM1=p-pN1;
pM2=p-pN2;
Mn=28;
mn=(D*A*Mn*p*10^5/(G*T*L))*log(pM2/pM1)
disp("kg/m^2",mn,"diffusion rate of gaseous mixture =")
|
54c31f8f4c345bd5cf9fdf7410bae636ffba33a2
|
b2efed85f1632d9ed4b7d9f4eebc7126d3074940
|
/ted_mini/artandsci_positive/221.ted.sci
|
5f11ff5ba20d04276d9a42cfe8558fc3e2b05c15
|
[] |
no_license
|
joytafty-work/unsupervised_nlp
|
837d8ed75eb084b630d75a1deba7bdd53bbcf261
|
7812c7d24bb677c90cf6397ed0e274caba1b884c
|
refs/heads/master
| 2021-01-10T09:24:33.254190 | 2015-11-11T20:40:32 | 2015-11-11T20:40:32 | 45,651,958 | 2 | 7 | null | 2018-01-28T18:54:18 | 2015-11-06T01:42:42 |
Scilab
|
UTF-8
|
Scilab
| false | false | 7,990 |
sci
|
221.ted.sci
|
i m a historian steve told us about the future of little technology i m going to show you some of the past of big technology this was a project to build a 4 000 ton nuclear bomb propelled spaceship and go to saturn and jupiter this took place in my childhood 1957 to 65 it was deeply classified i m going to show you some stuff that not only has not been declassified but has now been reclassified if all goes well next year i ll be back and i ll have a lot more to show you and if all does n t go well i ll be in jail like wen ho lee so this ship was basically the size of the marriott hotel a little taller and a little bigger and one of the people who worked on it in the beginning was my father freeman there in the middle that s me and my sister esther who s a frequent tedster i did n t like nuclear bomb propelled spaceships i mean i thought it was a great idea but i started building kayaks so we had a few kayaks just so you know i am not dr strangelove but all the time i was out there doing these strange kayak voyages in odd beautiful parts of this planet i always thought in the back of my mind about project orion and how my father and his friends were going to build these big ships they were really going to go they were actually going to go ted taylor who led the project was going to take his children my father was not going to take his children that was one of the reasons we sort of had a falling out for a few years the project began in 57 at general atomics there that s right on the coast at la jolla look at that central building right in the middle of the picture that s the 130 foot diameter library that is exactly the size of the base of the spaceship so put that library at the bottom of that ship that s how big the thing was going to be it would take 2 000 or 3 000 bombs the people who worked on it were a lot of the los alamos people who had done the hydrogen bomb work it was the first project funded by arpa that s the contract where arpa gave the first million dollars to get this thing started spaceship project officially begun job waiting for you dyson that s july 58 two days later the space traveler s manifesto explaining why just like we heard yesterday why we need to go into space trips to satellites of the outer planets august 20 1958 these are the statistics of what would be the good places to go and stop some of the sizes of the ships ranging all the way up to ship mass of 8 million tons so that was the outer extreme here was version two 2 000 bombs these are five kiloton yield bombs about the size of small volkswagens it would take 800 to get into orbit here we see a 10 000 ton ship will deliver 1 300 tons to saturn and back essentially a five year trip possible departure dates october 1960 to february 1967 this is trajectories going to mars all this was done by hand with slide rules the little orion ship and what it would take to do what orion does with chemicals you have a ship the size of the empire state building nasa had no interest they tried to kill the project the people who supported it were the air force which meant that it was all secret and that s why when you get something declassified that s what it looks like military weapon versions that were versions that carried hydrogen bombs that could destroy half the planet there s another version there that sends retaliatory strikes at the soviet union this is the real secret stuff how to get directed energy explosions so you re sending the energy of a nuclear explosion not like just a stick of dynamite but you re directing it at the ship and this is still a very active subject it s quite dangerous but i believe it s better to have dangerous things in the open than think you re going to keep them secret this is what s happened at 600 microseconds the air force started to build smaller models and actually started doing this the guys in la jolla said we ve got to get started now they built a high explosive propelled model these are stills from film footage that was saved by someone who was supposed to destroy it but did n t and kept it in their basement for the last 40 years so these are three pound charges of c 4 that s about 10 times what the guy had in his shoes this is ed day putting so each of these coffee cans has three pounds of c 4 in it they re building a system that ejects these at quarter second intervals that s my dad in the sport coat there holding the briefcase so they had a lot of fun doing this but no children were allowed my dad could tell me he was building a spaceship and going to go to saturn but he could not say anything more about it so all my life i have wanted to find this stuff out and spent the last four years tracking these old guys down these are stills from the video jeff bezos kindly yesterday said he ll put this video up on the amazon site some little clip of it so thanks to him they got quite serious about the engineering of this the size of that mass for us is really large technology in a way we re never going to go back to if you saw the 1959 this is what it would feel like in the passenger compartment that s acceleration profile and pulse system yield we re looking at 20 kiloton yield for an effect for us of 10 million newtons well here we have a little problem the radiation doses at the crew station 700 rads per shot fission yields during development they were hoping to get clean bombs they did n t eyeburn this is what happens to the people in miami who are looking up personnel compartment noise that s not too bad it s very low frequencies it s basically like these subwoofers and now we have ground hazard assessments when you have a blow up on the pad finally at the very end in 1964 nasa steps in and says ok we ll support a feasibility study for a small version that could be launched with saturn vs in sections and pieced together so this is what nasa did getting an eight man version that would go to mars they liked it because the guys who kind of live there would be like it s just like living in a submarine this is crew compartment it switches so what s upside down is right side up when you go to artificial gravity mode the scientists were still going to go along they would take seven astronauts and seven scientists this is a 20 man version for going to jupiter bunks storm cellars exercise room you know it was going to be a nice long trip the air force version here we have a military version this is the kind of stuff that s not been declassified just that people managed to sneak home and after you know on their deathbed basically gave me the sort of artist conceptions these are basically powerpoint presentations given to the air force 40 years ago look at the little guys there outside the vehicle and one part of nasa was interested in it but the headquarters in nasa they killed the project so finally at the end we can see the thing followed its sort of design path right up to 1965 and then all those paths came to a halt results none this project is hereby terminated so that s the end all i can say in closing is we heard yesterday that one of the 10 bad things that could happen to us is an asteroid with our name on it and one of the bad things that could happen to nasa is if that asteroid shows up with our name on it nine months out and everybody says well what are we going to do and orion is really one of the only if not the only off the shelf technologies that could do something so i m going to tell you the good news and the bad news the good news is that nasa has a small secret contingency plan division that is looking at this trying to keep knowledge of orion preserved in the event of such a misfortune maybe keep a few little bombs of plutonium on the side that s the good news the bad news is when i got in contact with these people to try and get some documents from them they went crazy because i had all this stuff that they do n t have and nasa purchased 1 759 pages of this stuff from me so that s the state we re at it s not very good
|
63c7a528018bb34f042d87a7b2ba42236dad8461
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1073/CH2/EX2.38/2_38.sce
|
513f4198fcfde140a885ed2e0889524c8d33f667
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 498 |
sce
|
2_38.sce
|
clc;
clear;
//Example 2.38
//Given
dia=50 //mm
dia=dia/1000 //m
r=dia/2 //radius in m
h=115 //W/sq m.K
rho=8000 //kg/cubic m
Cp=0.42 //kJ/kg.K
Cp=Cp*1000 //J/(kg*K)
A=4*%pi*r^2 //Area in sq m
V=A*r/3 //Volume in cubic m
T=423 //K
T_inf=363 //K
T0=723 //K
//(T-T_inf)/(T0-T_inf)=e^(-3ht/(rho*Cp*r))
t=-rho*Cp*r*log((T-T_inf)/(T0-T_inf))/(3*h); //Time in seconds
printf("Time taken by centre of ball to reach a temperature of 423 K is %f s (=%f minutes",t,t/60);
|
0856b7ed6ce001db1bdc21e8ecd2e06487e4c91a
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3731/CH6/EX6.6/Ex6_6.sce
|
9e1487acd6d5436771a479dbc9ad361b0a9aeccf
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,464 |
sce
|
Ex6_6.sce
|
//Chapter 6:Induction Motor Drives
//Example 6
clc;
//Variable Initialization
//Ratings of the star connected Induction motor which operates under dynamic braking
f=50 // frequency in HZ
P=6 // number of poles
//Parameters referred to the stator
Xr_=3.01 // rotor winding reactance in ohm
Xs=Xr_ // stator winding reactance in ohm
Rr_=4.575 // resistance of the rotor windings in ohm
Rs=1.9 // resistance of the stator windings in ohm
J=0.1 // moment of inertia of the motor load system in kg-m2
Id=12 // given DC current
N=1500 //given asynchronous speed
//magnetization chacrateristic at the given asynchronous speed
Im=[0.13,0.37,0.6,0.9,1.2,1.7,2.24,2.9,3.9,4.9,6,8,9,9.5] //magnetization current
E=[12.8,32,53.8,80,106,142,173,200,227,246,260,280,288,292] //back emf
//Solution
Ns=120*f/P //synchronous speed in rpm
torque=[]
speed=[]
temp=[]
Is=sqrt(2/3)*Id //value of stator current for two lead connection
Wms=2*%pi*N/60
for i=2:14
x=(Is**2-Im(i)**2)/(1+2*Xr_*Im(i)/E(i)) //x=Ir_**2
Ir_=sqrt(x) //required rotor current
y=(E(i)/Ir_)**2-Xr_**2
S=Rr_/sqrt(y) //required slip
N=S*Ns //required speed
T=(3/Wms)*(Ir_)**2*Rr_/S //required torque
speed($+1)=N
torque($+1)=T
temp($+1)=T
end
mprintf("Hence the magnetization curve is")
disp(speed,"Speed:in rpm")
for i=1:13
torque(i)=-1*torque(i)
end
disp(torque,"Braking torque :in N-m")
//Results
//Plot of of torque vs speed
subplot(2,1,1)
plot(torque,speed)
xlabel('Torque, N-m')
ylabel('Speed, rpm')
title('Torque vs Speed')
xgrid(2)
//Plot of Wm vs J/T
inertia_over_torque=[]
for i=3:13
J_T=1000*J/temp(i)
inertia_over_torque($+1)=J_T
end
disp(inertia_over_torque,"J/t :")
Wm=[1,4,8,12,16,20,25,55,95,125,160]
//the values of Wm are taken for the angular frequency with maximum value of Wms=50*pi rad/s
subplot(2,1,2)
plot(Wm,inertia_over_torque)
xlabel('$Angular speed \omega_m$')
ylabel(' J/T,1*10e-2')
title('$J/T vs \omega_m$')
xgrid(2)
x=[6.5,6.5]
y=[2,4.5]
plot(x,y,'blue')
str=["${A}$"]
str1=["${B}$"]
str2=["${C}$"]
str3=["${D}$"]
str4=["${E}$"]
xstring(6,2,str)
xstring(6,4.5,str1)
xstring(80,3.4,str2)
xstring(156,8.3,str3)
xstring(156,2,str4)
mprintf("Hence from the plot the area ABCDEA between the curve and the speed axis for speed change ")
mprintf("for synchronous to 0.02 times synchrnous speed is the stopping time which is equal to: 9.36 sec")
|
ca7575a9cf5afe589b1e6df109e4871bd4013dbf
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/506/CH18/EX18.1.d/Example18_1d.sce
|
b7821f4985c40a80c670f60f9bcc5f4699f282ca
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,233 |
sce
|
Example18_1d.sce
|
clear;
clc;
//Caption:Calculation of change in output voltage due to change in input voltage and load current
//Given Data
Vo=25;//in V
ro=10;//in ohm
Rz = 12;//in ohm
Vo=25;//output voltage in V
Vr = 7.5 + 7.5;//because two diodes are used
Iz = 20;//in mA
Ie2=10;//in mA
Ic2 = Ie2;
Icmax=30;//in mA
Vcemax=45;//in V
hFE2=220;
hfe2=200;
hie2=800;//in ohm
Id=10;//in mA
Il = 1000;//in mA
Vi = 50;//in V
dVi = 10; //change in input voltage
dIl = 1;//change in load current
//For D1 and D2 operate
Iz = Id + Id;
Rd = (Vo-Vr)/Id;
Ib2 = (1000*Ic2)/hFE2;
//Since we require I1>Ib2 , we select
I1=10*(10^-3);//in A
Vbe = 0.7;//in V
V2 = Vbe + Vr;
R1 = (Vo-V2)/I1;
R2 = V2/I1;
//We are selecting Texas Instruments 2N1722 silicon power transistor, so following parameters are required
Ic1 = 1;//in A
hFE1=125;
hfe1=100;
hie1=20;
Ib1 =(1000*I1 + Il + Id)/hFE1;
//The current through resistor R3 is
I=Ib1 + Ic2;
R3 = (Vi - (Vbe + Vo))/I;
Gm = hfe2*(R2/(R2+R1))*(1/((R1*R2/(R1+R2))+hie2+(1+hfe2)*Rz)) ;
Sv = (10^-3)/(Gm*R3);
Ro = (ro + (((1000*R3) + hie1)/(1+hfe1)))/(1 + (Gm*((1000*R3) + ro)));
dVo = (Sv*dVi)+(Ro*dIl);
disp('V',dVo,'Change in output voltage = ');
//End
|
20138ab286d0bf0e81cc82e71b81bf52c22c85c9
|
6813325b126713766d9778d7665c10b5ba67227b
|
/Chapter6/Ch_6_Eg_6.30.sci
|
d230189f25a4e87dbb1f9b2955659ec2f0fd7de1
|
[] |
no_license
|
arvindrachna/Introduction_to_Scilab
|
955b2063b3faa33a855d18ac41ed7e0e3ab6bd1f
|
9ca5d6be99e0536ba1c08a7a1bf4ba64620ec140
|
refs/heads/master
| 2020-03-15T19:26:52.964755 | 2018-05-31T04:49:57 | 2018-05-31T04:49:57 | 132,308,878 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 300 |
sci
|
Ch_6_Eg_6.30.sci
|
// A program to find factorial of a number using recursion.
function [y]=fact(x)
disp(sprintf('Calling fact(%d)', x));
if x == 1 then
y=1
else
y=x*fact(x-1)
end
endfunction
// Main program
y=fact(5); // calling the function
disp(sprintf("Result: fact(5)=%d", y));
|
86f5b22cb685ed7da6bc76b05b7b396f96f0dfc4
|
417f69e36190edf7e19a030d2bb6aa4f15bb390c
|
/SMTTests/tests/ok_getRequiredOptions.tst
|
6536109c085822878cfcaebe5748793dee5b61b8
|
[] |
no_license
|
IETS3/jSMTLIB
|
aeaa7ad19be88117c7454d807a944e8581184a66
|
c724ac63056101bfeeb39cc3f366c8719aa23f7b
|
refs/heads/master
| 2020-12-24T12:41:17.664907 | 2019-01-04T10:47:43 | 2019-01-04T10:47:43 | 76,446,229 | 1 | 0 | null | 2016-12-14T09:46:41 | 2016-12-14T09:46:41 | null |
UTF-8
|
Scilab
| false | false | 196 |
tst
|
ok_getRequiredOptions.tst
|
; Tests whether the required options are implemented and give the correct
; default values
(get-option :print-success)
(get-option :regular-output-channel)
(get-option :diagnostic-output-channel)
|
35d5706392b8c934348146407ea4b3dc5f712917
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2216/CH14/EX14.3/ex_14_3.sce
|
383debcbb714f1eb0952e19c485f347b3c6c81b9
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 697 |
sce
|
ex_14_3.sce
|
//Example 14.3: output power
clc;
clear;
close;
h=0.6943*10^-6;//
lm=10;//in cm
r1=1.0;//
r2=0.8;//
t1=0.98;//
as=1;//cm^2;//
Ls=2;//cm
gth=((1/(2*lm))*log((1/(r1*r2*(t1)^8))))+(as*Ls)/lm;//
sg=1.5*10^-20;//
ndth=gth/sg;//cm^-3;//
nth=ndth*as*lm;//atoms
ni=5*nth;//atoms
ng=1.78;//
ns=2.7;//
lair=2;//
c=3*10^10;//
trt=((2*ng*lm)/c)+((2*ns*Ls)/c)+((2*lair)/c);//seconds
npmax=((ni-nth)/2)-(nth/2)*log(ni/nth);//photons
L=14;//cm
at=((as*Ls)/L)+((1/(2*L))*log(1/(r1*t1^8)));//
aext=((1/(2*L))*log(1/r2));//
tp=((trt)/(1-(r1*r2*t1^8*exp(-2*as*Ls))));//seconds
hc=6.6*10^-34;//
pmax=((aext/at)*hc*c*npmax)/(h*tp);//in watts
disp(pmax*10^-6,"maximum power in MW is")
//answer is wrong in the textbook
|
31b7be167d65e5eac2f24a1fa6f7565999bea979
|
67310b5d7500649b9d53cf62226ec2d23468413c
|
/tags/archive/TestCaseGenerator-Plugin-OpeningSequenceCoverage/trunk/tests/large-system-tests/inputs/jEdit/ground_truth/OpeningSequenceCoverage/length-1/max-150/t52.tst
|
9f8895f2ddd650723ee508f57f4b092ee677d5f3
|
[] |
no_license
|
csnowleopard/guitar
|
e09cb77b2fe8b7e38d471be99b79eb7a66a5eb02
|
1fa5243fcf4de80286d26057db142b5b2357f614
|
refs/heads/master
| 2021-01-19T07:53:57.863136 | 2013-06-06T15:26:25 | 2013-06-06T15:26:25 | 10,353,457 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 661 |
tst
|
t52.tst
|
<?xml version="1.0" encoding="UTF-8" standalone="yes"?>
<TestCase>
<Step>
<EventId>e49</EventId>
<ReachingStep>false</ReachingStep>
</Step>
<Step>
<EventId>e76</EventId>
<ReachingStep>false</ReachingStep>
</Step>
<Step>
<EventId>e34</EventId>
<ReachingStep>false</ReachingStep>
</Step>
<Step>
<EventId>e79</EventId>
<ReachingStep>false</ReachingStep>
</Step>
<Step>
<EventId>e60</EventId>
<ReachingStep>false</ReachingStep>
</Step>
<Step>
<EventId>e66</EventId>
<ReachingStep>false</ReachingStep>
</Step>
</TestCase>
|
431670916f2b39f6c2c94b20ecd9775d69e5dfc2
|
51a62cf6043094e32b4c75da5fe20ac31f53d711
|
/Computação Gráfica/GeometricTransformation-Translation.sce
|
2bbe41b414c2ddba123af7df6a3eadf7af379a4c
|
[
"MIT"
] |
permissive
|
AnneLivia/CollegeProjects
|
9e32c4da216caaa973ebd4e4fe472f57557a3436
|
96d33d0ed79b5efa8da4a1401acba60b0895e461
|
refs/heads/master
| 2022-12-23T10:13:03.503797 | 2022-12-12T16:35:29 | 2022-12-12T16:35:29 | 128,656,614 | 2 | 0 |
MIT
| 2022-12-12T16:36:09 | 2018-04-08T15:44:18 |
PHP
|
UTF-8
|
Scilab
| false | false | 778 |
sce
|
GeometricTransformation-Translation.sce
|
Q = [0, 0; 0, 2; 2, 2; 2, 0; 0, 0];
plot(Q(:, 1), Q(:, 2));
// para visualizar melhor o quadrado
plot(-4, -4);
plot(8, 8);
/*
A translation moves an object to a different position on the screen. You can translate a point in 2D by adding translation coordinate (tx, ty) to the original coordinate X,Y to get the new coordinate X′,Y′. The pair (tx, ty) is called the translation vector or shift vector. P' = P + T
*/
// Move the square to the right. x = 4, y = 0
T = [4, 0; 4, 0; 4, 0; 4, 0; 4, 0];
QT = Q + T;
plot(QT(:, 1), QT(:, 2));
// move the square up. x = 4, y = 4
T = [4, 4; 4, 4; 4, 4; 4, 4; 4, 4];
QT = Q + T;
plot(QT(:, 1), QT(:, 2));
// move the square left. x = 0, y = 4
T = [0, 4; 0, 4; 0, 4; 0, 4; 0, 4];
QT = Q + T;
plot(QT(:, 1), QT(:, 2));
|
3d6085ab0e0fcf30e301b8b2a6c14c3f972de263
|
8217f7986187902617ad1bf89cb789618a90dd0a
|
/browsable_source/2.5/Unix-Windows/scilab-2.5/tests/examples/%asn.man.tst
|
baf3cd5d51e3e012055de6abc412887ee5b4f09d
|
[
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-warranty-disclaimer"
] |
permissive
|
clg55/Scilab-Workbench
|
4ebc01d2daea5026ad07fbfc53e16d4b29179502
|
9f8fd29c7f2a98100fa9aed8b58f6768d24a1875
|
refs/heads/master
| 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 348 |
tst
|
%asn.man.tst
|
clear;lines(0);
m=0.8;z=%asn(1/sqrt(m),m);K=real(z);Ktilde=imag(z);
x2max=1/sqrt(m);
x1=0:0.05:1;x2=1:((x2max-1)/20):x2max;x3=x2max:0.05:10;
x=[x1,x2,x3];
y=%asn(x,m);
rect=[0,-Ktilde,1.1*K,2*Ktilde];
plot2d(real(y)',imag(y)',1,'011',' ',rect)
//
deff('y=f(t)','y=1/sqrt((1-t^2)*(1-m*t^2))');
intg(0,0.9,f)-%asn(0.9,m) //Works for real case only!
|
c8abda7f0e4828389c46cf2b6c4c1fe3265be093
|
e41b69b268c20a65548c08829feabfdd3a404a12
|
/3DCosmos/BCK/Scripts/planetarium.SCI
|
f2269dfd0b4fb6454afd29125dd010bf07e64f0f
|
[
"LicenseRef-scancode-khronos",
"MIT"
] |
permissive
|
pvaut/Z-Flux
|
870e254bf340047ed2a52d888bc6f5e09357a8a0
|
096d53d45237fb22f58304b82b1a90659ae7f6af
|
refs/heads/master
| 2023-06-28T08:24:56.526409 | 2023-03-01T12:44:08 | 2023-03-01T12:44:08 | 7,296,248 | 1 | 1 | null | 2023-06-13T13:04:58 | 2012-12-23T15:40:26 |
C
|
UTF-8
|
Scilab
| false | false | 9,782 |
sci
|
planetarium.SCI
|
codeblock readtextfile(ScriptDir+"\TOOLS.sci");
codeblock readtextfile(ScriptDir+"\SSYS.sci");
longit=(3+43/60.0)/180*Pi;
lattit=(51+3/60.0)/180*Pi;
ei=+23.4457889/180*Pi;
scfac=100000;
ssysframe=ssys_create;
ssys_createearth(1);
ssys_createluna(2);
ssys_createmilkyway;
ssys_createconstellationnames;
ssys_createstarnames;
ssys_showconstellations(true);
root.framerate=30;
#Create moon halo object
frame_moonhalo=ssysframe.addviewdirframe(point(0,0,0),"MoonHalo");
ssysframe.moveobject(frame_moonhalo.name,-1000);
tx=frame_moonhalo.createtexture("halo",DataDir+"\textures\star1.bmp",DataDir+"\textures\star1.bmp");
moonhalo=frame_moonhalo.add("Rectangle","EnableLight":false,
"Color":color(0.7,0.7,0.7,0.3),"BlendType":BlendTransparent,"DepthMask":DepthMaskDisable);
fc=scfac*0.6;
moonhalo.Texture=tx.name;
moonhalo.position=point(-1*fc,-1*fc,0);
moonhalo.Axis1=vector(2*fc,0,0);
moonhalo.Axis2=vector(0,2*fc,0);
#Create sun halo object
#frame_sunhalo=ssysframe.addviewdirframe(point(0,0,0),"SunHalo");
frame_sunhalo=ssysframe.addsubframe("SunHalo");
ssysframe.moveobject(frame_sunhalo.name,-1000);
tx=frame_sunhalo.createtexture("halo",DataDir+"\textures\star1.bmp");
#large halo
rc=frame_sunhalo.add("Rectangle","EnableLight":false,
"Color":color(1,1,0.7,0.3),"BlendType":BlendTransparent,"DepthMask":DepthMaskDisable);
fc=scfac*1;
rc.Texture=tx.name;
rc.position=point(-1*fc,-1*fc,0);
rc.Axis1=vector(2*fc,0,0);
rc.Axis2=vector(0,2*fc,0);
#small halo
rc=frame_sunhalo.add("Rectangle","EnableLight":false,
"Color":color(1,1,0.5,1.0),"BlendType":BlendTransparent,"DepthMask":DepthMaskDisable);
fc=scfac*0.05;
rc.Texture=tx.name;
rc.position=point(-1*fc,-1*fc,0);
rc.Axis1=vector(2*fc,0,0);
rc.Axis2=vector(0,2*fc,0);
#sunset/sunrise halo
sunsethalo=frame_sunhalo.add("Rectangle","EnableLight":false,
"Color":color(1,0.5,0.0,0.3),"BlendType":BlendTransparent,"DepthMask":DepthMaskDisable);
fc=scfac*1;
sunsethalo.Texture=tx.name;
sunsethalo.position=point(-3*fc,-1*fc,0);
sunsethalo.Axis1=vector(6*fc,0,0);
sunsethalo.Axis2=vector(0,2*fc,0);
#hide Earth orbit
root.SC.Universe.SolarSystem.EarthOrbit.visible=false;
#create planet objects
frame_planets=ssysframe.addsubframe("PlanetsIndicators");
ssysframe.moveobject(frame_planets.name,-1000);
planlist=list("Mercurius","Venus","Mars","Jupiter","Saturnus","Neptunus");
for i=0 to planlist.size-1 do {
ssys_createplanet(planlist(i),1);
GetPlanetOrbit(planlist(i)).visible=false;
fr=GetPlanetFrame(planlist(i));
fr.clearobjects;
fr=frame_planets.addsubframe(planlist(i));
fr.add("LightPoint","Size":5000,"Color":color(1,1,0));
fr.add("TextFlat","Size":8000,"Color":color(1,1,0,0.5),"BlendType":BlendTransparent,"DepthMask":DepthMaskDisable,
"Content":(" "+planlist(i)));
}
#starback=root.SC.Universe.StarBackFrame.StarBack;
#starback.LineSize=autokm(1000);
#starback.LineColor=color(1,0,0);
#ssysframe.add("Sphere","Name":"Sun","Radius":autokm(0.01),"EnableLight":false);
earthframe=GetPlanetBodyFrame("Earth");
earthframe.GlobeRendering.visible=false;
myviewport=T_getviewport;
myviewport.EnableUserNavigation=false;
#create viewer frame, but at earth center
vframe=earthframe.addsubframe("ViewerFrame");
vframe.transf.rotate(vector(0,1,0),Pi/2-lattit);
vframe.transf.rotate(vecrotate(vector(0,0,1),vector(0,1,0),-1*(Pi/2-lattit)),longit);
#s=20000*1000;
#vframe.add("Bar","Position":point(0,0,0),"SizeX":s,"SizeY":s,"SizeZ":s);
#vframe.add("Curve").makeline(point(0,0,0),point(0,0,2*s));
#Build scene
#atmosphere horizon glow
#atm1=vframe.add("Sphere","Name":"AtmopshereGlow");
atm1=vframe.add("Cylinder","Name":"AtmopshereGlow");
vframe.createtexture("Atm1",DataDir+"\textures\gradient1.bmp",DataDir+"\textures\gradient1.bmp");
atm1.renderback=true;atm1.renderfront=true;
atm1.enablelight=false;
atm1.Texture="Atm1";
atm1.BlendType=BlendTransparent;atm1.DepthMask=DepthMaskDisable;
atm1.radius=1.0*scfac;
atm1.Axis=vector(0,0,1.5*scfac);
atm1.IsClosed=false;
atm1.position=point(0,0,-0.05*scfac);
#full atmosphere (equal light)
atm2=vframe.add("Sphere","Name":"AtmosphereEqual");
atm2.renderback=true;atm2.renderfront=false;
atm2.enablelight=false;
atm2.BlendType=BlendTransparent;atm2.DepthMask=DepthMaskDisable;
atm2.radius=2*scfac;
atm2.resolution=5;
#azimuth grid
#for i=0 to 15 do {
# ang=i/16*2*Pi;
# vframe.add("Curve","Color":color(0,0.6,0.5,0.5),"BlendType":BlendTransparent,
# "Size":2).makecircle(point(0,0,0),vector(cos(ang),sin(ang),0),1.3*scfac,200);
#}
#for i=0 to 6 do {
# ang=i/6*Pi/2;
# vframe.add("Curve","Color":color(0,0.6,0.5,0.5),"BlendType":BlendTransparent,
# "Size":2).makecircle(point(0,0,1.3*scfac*sin(ang)),vector(0,0,1),1.3*scfac*cos(ang),200);
#}
#backdrop
bdframe=vframe.addsubframe("BackDropFrame");
bdframe.transf.rotate(vector(0,0,1),-42/180*Pi-Pi);
vframe.createtexture("bd",DataDir+"\textures\panovsrug.jpg",DataDir+"\textures\panovsrug_mask.jpg");
vframe.createtexture("bd2",DataDir+"\textures\koepel.jpg",DataDir+"\textures\koepel_mask.jpg");
bd=bdframe.add("Cylinder","Name":"BackDrop",
"Position":point(0,0,(-0.55+0.04)*scfac),
"Axis":vector(0,0,2*0.55*scfac),
"Radius":scfac);
bd.renderback=true;
bd.resolution=70;
bd.IsClosed=false;
bd.enablelight=false;
bd.Texture="bd";
bd.BlendType=BlendTranslucent;
bd2frame=vframe.addsubframe("BackDropFrame");
bd2frame.transf.rotate(vector(0,0,1),-42/180*Pi+Pi/2);
bd2=bd2frame.add("Surface","Name":"BackDropKoepel");
bd2.enablelight=false;
bd2.renderback=true;
bd2.dim(2,2);
bd2.points(0,0)=@point(scfac*vecnorm(vector(+0.8,-1,0))+scfac*vector(0,0,-0.44));
bd2.points(1,0)=@point(scfac*vecnorm(vector(-0.15,-1,0))+scfac*vector(0,0,-0.44));
bd2.points(1,1)=@point(scfac*vecnorm(vector(-0.22,-1,0))+scfac*vector(0,0,+0.7));
bd2.points(0,1)=@point(scfac*vecnorm(vector(+0.9,-1,0))+scfac*vector(0,0,+0.7));
bd2.Texture="bd2";
bd2.BlendType=BlendTranslucent;
myviewport.CameraPos=point(0,0,0);
myviewport.Cameradir=vecnorm(vector(1,0,0.5));
myviewport.FocalDistance=0.1*scfac*10;
myviewport.EyeSeparation=myviewport.FocalDistance/30;
myviewport.NearClipPlane=0.1*scfac;
myviewport.Aperture=70/180*Pi;
#clock overlay
clockframe=root.SC.Universe.addscreenframe("ClockFrame");
#time
clock=clockframe.add("Clock");
clock.enablelight=false;
clock.Position=point(0.085,0.085,0);
clock.Size=0.075;
clock.DepthTest=DepthTestDisable;
clock.DepthMask=DepthMaskDisable;
clock.BlendType=BlendTranslucent;
clock.color=color(0.7,0.7,0.7);
#date
clock=clockframe.add("Clock");
clock.enablelight=false;
clock.Position=point(0.15,0.01,0);
clock.Type=ClockTypeDateTime;
clock.Size=0.02;
clock.DepthTest=DepthTestDisable;
clock.DepthMask=DepthMaskDisable;
clock.BlendType=BlendTranslucent;
clock.color=color(0.7,0.7,0.7);
#root.time=time(2008,3,21,0,0,0);
root.time=CurrentTimeUT;
fr=0;
root.TimeSpeed=10;
while true do {
incrtime;
#root.time=CurrentTimeUT;
# root.time=CurrentTimeUT+0*60*60;
earthpos=GetPlanetPosition("Earth");
moonpos=GetLunaPosition;
#update positions of planet indicator
for i=0 to planlist.size-1 do
frame_planets.get(planlist(i)).transf.origin=earthpos+2*scfac*vecnorm(GetPlanetPosition(planlist(i))-earthpos);
#update position of moon halo & calculate intensity
frame_moonhalo.transf.origin=earthpos+1.5*scfac*vecnorm(@vector(moonpos));
fr=vecnorm(@vector(moonpos))^vecnorm(@vector(earthpos));
fr=1+fr;if (fr>1) then fr=1;
fr=fr*fr;
moonhalo.color=color(0.7,0.7,0.7,0.3*fr);
#update position of sun halo
ez=vecnorm(-1*@vector(earthpos));
ex=vecnorm(ez*(vframe.totaltransformation*vector(0,0,1)));
ey=ex*ez;
frame_sunhalo.transf.origin=earthpos+2*scfac*ez;
frame_sunhalo.transf.Xaxis=ex;
frame_sunhalo.transf.Yaxis=ey;
frame_sunhalo.transf.Zaxis=ez;
#calculate sun presence
vertdir=vframe.totaltransformation*vector(0,0,1);
sunang=vecnorm(point(0,0,0)-earthpos)^vertdir;
sunfr=(sunang+0.1)/0.2;
if sunfr<0 then sunfr=0;
if sunfr>1 then sunfr=1;
#adjust atmosphere color to sun presence
atm1.color=color(0.3,0.5,0.7,0.3+0.58*sunfr);
atm2.color=color(0.3,0.5,0.7,0.15+0.73*sunfr);
#adjust sunset/sunrise halo brightness
fr=6*(sunang+0.1);fr=1-fr*fr;
if fr<0 then fr=0;
sunsethalo.color=color(1,0.5,0.0,0.6*fr);
#backdrop illumunation
fr2=0.15+0.8*sunfr;
bd.color=color(fr2,fr2,fr2,1);
bd2.color=color(fr2,fr2,fr2,1);
#mechanism to co-move camera with earth
if true then {
root.SC.Universe.transf.reset;
ttf=vframe.totaltransformation;
# myviewport.CameraUpDir=ttf*vector(0,0,1);
ttf.invert;
# root.SC.Universe.transf=ttf;
# root.sc.light0pos=ttf*point(0,0,0);
root.viewports.main.transf=ttf;
}
render;
if UIGetAxisActive(UIAxisX,UIAxisLevel0) then {
vl=UIGetAxisPos(UIAxisX,UIAxisLevel0);
myviewport.CameraDir=vecrotate(myviewport.CameraDir,vector(0,0,1),0.03*vl);
}
if UIGetAxisActive(UIAxisY,UIAxisLevel0) then {
ok=false;
ang0=vecangle(myviewport.CameraDir,vector(0,0,1));
vl=UIGetAxisPos(UIAxisY,UIAxisLevel0);
if vl>2 then vl=2;
if vl<-2 then vl=-2;
if (vl>0) and (ang0>5/180*Pi) then ok=true;
if (vl<0) and (ang0<75/180*Pi) then ok=true;
if ok then {
dr1=vecnorm(myviewport.CameraDir*vector(0,0,1));
myviewport.CameraDir=vecrotate(myviewport.CameraDir,dr1,0.03*vl);
}
}
if UIGetAxisActive(UIAxisZ,UIAxisLevel0) then {
vl=UIGetAxisPos(UIAxisZ,UIAxisLevel0);
myviewport.Aperture=myviewport.Aperture*(1-vl/20);
if myviewport.Aperture<30/180*Pi then myviewport.Aperture=30/180*Pi;
if myviewport.Aperture>80/180*Pi then myviewport.Aperture=80/180*Pi;
}
# if IsKeyDown("F4") then stop;
}
|
4610ada32b90410f21b65ebecc402190c3fdc838
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/213/CH9/EX9.1/9_1.sce
|
6d4a6b32e3295d2dc496495cac2e771a98141b53
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 306 |
sce
|
9_1.sce
|
//To find inclination of track arm
clc
//Given:
c=1.2,b=2.7 //m
//Solution:
//Calculating the inclination of the track arm to the longitudinal axis
alpha=atan(c/(2*b))*180/%pi //degrees
//Results:
printf("\n\n Inclination of the track arm to the longitudinal axis, alpha = %.1f degrees.\n\n",alpha)
|
4503c17341de4eddc6adb23b636c7c7063102d8b
|
cfac21260a4737c49982a78160361703914dac1f
|
/sem1/old_src/Программы и so on/lab_5/Inv_pendulum/First_way.sce
|
8d6fe5da8968165206e91fb687b341722282ee00
|
[] |
no_license
|
Zenkin/courses
|
680442fa57bc3b1c872e15e9bc7e98b579bfd39e
|
b0b0aafe0c358a611868fd764a2ad1cb71078d8d
|
refs/heads/master
| 2020-03-23T22:19:20.542398 | 2018-07-24T13:55:20 | 2018-07-24T13:55:20 | 139,969,727 | 0 | 0 | null | 2018-07-06T10:19:48 | 2018-07-06T10:19:47 | null |
UTF-8
|
Scilab
| false | false | 5,121 |
sce
|
First_way.sce
|
mw = 0.017; //масса колес
Umax = 7.4 //управляющее напряжение (нужно только для моделирования)
mc = 0.595 - 4*mw; //масса тележки
mp = 0.051; //масса маятника
g = 9.82; //ускорение свободного падения
L = 0.68; //длина маятника
l = L/2; //расстояние до центра масс маятника
R = 7.54; //сопротивление цепи якоря двигателя
r = 0.058/2; //радиус колеса
km = 0.5; //конструктивные постоянные
ke = 0.5;
J = 0.0023; //приведенный момент инерции вала сервопривода
Jp = mp*L*L/12; //момент инерции маятника (=J одн стержня отн. его центра масс)
Jw = mw*r*r/2; //момент инерции колес
tper = 1.0; //Время перерегулирования
p=poly(0,"p"); //просто символ
//коэффициенты нужного характеристиского полинома (полином Ньютона)
p0 = 6.3/tper;
a_1 = p0^3;
a_2 = 3*p0^2;
a_3 = 3*p0;
//необходимые матрицы
E = {2*mp*L*r, mp*L*L + 4*Jp;
mp*r*r + mc*r*r + 4*mw*r*r + 4*Jw + 2*J, 0.5*mp*L*r};
F = {0, 0;
2*km*ke/R, 0};
G = {0, -2*mp*g*L;
0, 0};
H = {0;
2*km/R};
EG = (E^-1)*G;
EF = (E^-1)*F;
EH = (E^-1)*H;
EG = (-1)*EG;
EF = (-1)*EF;
A = { 0, 0, 1; //матрица, определяющая динамические свойства ОУ
EG(1,2), EF(1,1), EF(1,2);
EG(2,2), EF(2,1), EF(2,2)};
B = { 0; //матрица входа управляющих воздействий
EH(1,1);
EH(2,1)};
W = [B, A*B, A^2*B]; //матрица управляемости
//проверка на управляемость
if det(W) <> 0 then
printf("\nIt can be controlled\n\n");
end
if det(W) == 0 then
printf("\nIt can not be controlled\n\n");
end
C={1,0,0}; //матрица выхода
Q={ C; //матрица наблюдаемости
C*A;
C*A^2};
//проверка на наблюдаемость
if det(Q) <> 0 then
printf("It is observable\n");
end
if det(Q) == 0 then
printf("It is not observable\n");
end
a = coeff(det(p*eye(3,3) - A)); //коэффициенты характеристического полинома объекта управления
Ak = {0, 1, 0; //матрица, определяющая динамические свойства ОУ
0, 0, 1; //в канонической форме
-a(1),-a(2),-a(3)};
Bk = {0; //матрица управляющих воздействий
0; //в канонической форме
1};
Wk = {Bk, Ak*Bk, Ak^2*Bk]; //матрица управляемости в канонической форме
P = Wk*(W^-1); //матрица перехода
Kk = {a_1-a(1), a_2-a(2), a_3-a(3)}; //матрица коэффициентов обратной связи для Bk и Ak
K = Kk*P; //матрица коэффициентов обратной связи
printf("\nYou need: ");
disp(a_1+a_2*p+a_3*p^2+p^3);
printf("\nYou will have: ");
disp(det(p*eye(3,3)-(A-B*K)));
printf("\nWhere Koefs =:\n k1 = %g k2 = %g k3 = %g\n\n", K(1), K(2), K(3));
//Для структурной схемы
//начальные условия
psi0 = 0; //начальный угол маятника
dpsi0 = 0.2; //начальная скорость падения маятника
dtheta0 = 0; //начальная скорость колес
//Остальное
k1 = K(1);
k2 = K(2);
k3 = K(3);
i1 = A(2,2);
i2 = A(2,1);
i3 = B(2);
o1 = A(3,2);
o2 = A(3,1);
o3 = B(3);
////моделирование при рассчитанных коэффициентах:
//importXcosDiagram("C:\for_scilab\cart_on_3.zcos"); //полное имя файла со структурной схемой
//xcos_simulate(scs_m, 4);
////построение графиков с результатами
//subplot(2,2,1);
//xtitle("Угол (рад --- с)");
//plot2d(psi.time, psi.values,2);
//subplot(2,2,2);
//xtitle("Напряжение (В --- с)");
//plot2d(napr.time, napr.values,2);
//subplot(2,2,3);
//xtitle("Скорость падения (рад/с --- с)");
//plot2d(dpsi.time, dpsi.values,2);
//subplot(2,2,4);
//xtitle("Скорость колес (рад/с --- с)");
//plot2d(dtheta.time, dtheta.values,2);
//
//вывод найденных коэффициентов
printf("but in program you must put: \n");
disp(K*%pi/180)
|
f850927336886da1b7aa69ab913530098376f087
|
089894a36ef33cb3d0f697541716c9b6cd8dcc43
|
/NLP_Project/test/tweet/bow/bow.11_16.tst
|
556d60882aa870ce7a06595d3f48d1d4a5e17696
|
[] |
no_license
|
mandar15/NLP_Project
|
3142cda82d49ba0ea30b580c46bdd0e0348fe3ec
|
1dcb70a199a0f7ab8c72825bfd5b8146e75b7ec2
|
refs/heads/master
| 2020-05-20T13:36:05.842840 | 2013-07-31T06:53:59 | 2013-07-31T06:53:59 | 6,534,406 | 0 | 1 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 35,052 |
tst
|
bow.11_16.tst
|
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11 7:0.5 16:0.3333333333333333 237:0.1 277:0.5 362:0.5 616:0.1111111111111111 782:1.0 868:1.0 936:0.3333333333333333 1212:1.0 1469:1.0 2086:1.0 2590:1.0 3148:1.0 4511:1.0
11 31:0.2 50:0.5 55:0.5 66:0.4 103:0.5 105:0.16666666666666666 215:0.1111111111111111 1392:1.0 1773:1.0 2783:1.0 3439:1.0 8422:1.0
11 7:1.0 9:0.25 12:0.14285714285714285 22:1.0 23:1.0 33:1.0 41:1.0 46:0.2857142857142857 47:0.3333333333333333 52:0.09302325581395349 71:1.0 75:2.0 99:0.16666666666666666 105:0.16666666666666666 110:0.06666666666666667 112:0.5 127:0.3333333333333333 132:1.0 150:0.3333333333333333 260:0.1 286:1.0 293:1.0 330:0.5 336:1.0 343:1.0 348:0.25 362:0.5 536:0.5 755:0.125 811:1.0 1668:1.0 1946:1.0 2452:0.3333333333333333 2721:1.0 3156:1.0 3162:1.0 3230:1.0 3709:1.0 3882:1.0 5066:1.0 6053:1.0 6337:1.0 6832:1.0
11 9:0.25 12:0.07142857142857142 18:0.5 22:1.0 31:0.2 50:0.5 52:0.023255813953488372 59:0.16666666666666666 88:0.3333333333333333 105:0.16666666666666666 236:0.1111111111111111 275:0.1111111111111111 582:1.0 664:0.3333333333333333 936:0.3333333333333333 1506:1.0 1531:0.5 2508:1.0
11 12:0.14285714285714285 31:0.4 47:0.3333333333333333 50:0.5 52:0.023255813953488372 59:0.3333333333333333 60:2.0 66:0.4 75:1.0 128:0.3333333333333333 150:0.3333333333333333 260:0.1 275:0.1111111111111111 278:1.0 330:0.5 342:0.4 368:1.0 772:1.0 783:0.5 1020:1.0 1025:0.6666666666666666 1834:1.0 2770:1.0 3438:1.0 4891:1.0 5066:1.0 7906:1.0 7987:1.0 8380:1.0
11 7:1.0 16:0.3333333333333333 50:0.5 55:0.5 66:0.2 99:0.16666666666666666 127:0.3333333333333333 128:0.3333333333333333 221:1.0 240:0.25 275:0.1111111111111111 390:0.5 507:1.0 516:0.3333333333333333 804:1.0 1025:0.3333333333333333 1674:1.0 1746:0.5 1884:1.0 2159:0.5 2266:1.0 2401:1.0 2541:1.0 5921:1.0 7500:1.0 7629:1.0 7887:1.0
11 9:0.25 12:0.07142857142857142 31:0.2 33:1.0 41:1.0 46:0.7142857142857143 48:0.3333333333333333 50:1.0 52:0.046511627906976744 55:0.5 58:0.5 105:0.16666666666666666 106:0.5 126:1.0 150:0.3333333333333333 242:1.0 256:1.0 336:1.0 355:1.0 362:0.5 411:1.0 525:1.0 533:1.0 687:0.5 700:1.0 755:0.125 777:1.0 811:1.0 812:0.3333333333333333 3011:1.0 3142:1.0 6537:1.0
11 9:0.25 12:0.14285714285714285 15:2.0 50:0.5 52:0.046511627906976744 59:0.3333333333333333 66:0.2 165:0.3333333333333333 183:0.5 198:1.0 215:0.1111111111111111 491:1.0 536:0.5 943:1.0 1059:1.0 1116:1.0 1407:1.0 1813:1.0 2180:1.0 2599:1.0 5843:1.0 8442:1.0
11 7:0.5 11:0.25 14:1.0 66:0.2 110:0.06666666666666667 126:1.0 135:0.5 240:0.25 260:0.1 286:1.0 342:0.2 755:0.125 1332:1.0 1355:1.0 1399:1.0 1847:1.0 5646:1.0 7512:1.0
11 5:0.5 7:0.5 11:0.25 12:0.07142857142857142 41:1.0 46:0.14285714285714285 50:0.5 52:0.06976744186046512 66:0.4 105:0.16666666666666666 110:0.06666666666666667 128:0.6666666666666666 150:0.3333333333333333 153:1.0 222:0.3333333333333333 342:0.2 388:1.0 450:0.5 544:1.0 1297:1.0 2065:1.0 2150:1.0 2377:1.0 3271:1.0 3350:1.0 4343:1.0 4596:0.5 7471:1.0
11 7:0.5 9:0.25 12:0.07142857142857142 15:2.0 16:0.3333333333333333 22:1.0 26:0.3333333333333333 43:1.0 45:0.5 46:0.14285714285714285 48:0.3333333333333333 50:0.5 52:0.023255813953488372 66:0.4 70:0.1111111111111111 75:1.0 81:0.5 99:0.5 102:0.25 105:0.16666666666666666 110:0.06666666666666667 113:0.5 127:0.3333333333333333 128:0.3333333333333333 133:0.5 134:0.25 153:1.0 183:0.5 236:0.1111111111111111 258:1.0 320:1.0 355:1.0 432:1.0 616:0.1111111111111111 688:0.5 823:1.0 1118:1.0 1170:1.0 1182:1.0 1251:0.5 1393:1.0 1405:0.2 1464:1.0 1980:1.0 2105:1.0 2537:1.0 2978:1.0 4474:1.0 6212:1.0 6809:1.0
11 3:1.0 7:0.5 9:0.25 11:0.25 12:0.07142857142857142 15:2.0 31:0.2 47:0.3333333333333333 50:1.0 52:0.046511627906976744 55:0.5 59:0.16666666666666666 66:0.4 99:0.16666666666666666 102:0.25 106:0.75 110:0.06666666666666667 126:1.0 203:1.0 215:0.1111111111111111 257:1.0 275:0.1111111111111111 282:0.5 328:0.25 330:1.0 361:0.5 556:0.3333333333333333 619:1.0 777:1.0 999:1.0 1117:1.0 1581:1.0 1609:1.0 1757:0.5 1896:1.0 1908:0.2 2225:1.0 2657:1.0 2830:1.0 4714:1.0 4739:1.0 7761:1.0
11 9:0.25 55:0.5 59:0.16666666666666666 89:1.0 92:1.0 93:1.0 99:0.16666666666666666 102:0.25 103:0.5 106:0.25 110:0.06666666666666667 153:1.0 165:0.3333333333333333 183:0.5 236:0.1111111111111111 260:0.1 287:1.0 450:0.5 616:0.2222222222222222 1469:1.0 2336:1.0 2837:1.0 3437:1.0 5172:1.0 5400:1.0 6480:1.0
11 7:0.5 14:1.0 22:2.0 23:1.0 52:0.023255813953488372 66:0.4 99:0.16666666666666666 103:0.5 150:0.3333333333333333 216:1.0 229:1.0 233:1.0 236:0.1111111111111111 237:0.1 328:0.25 342:0.2 388:1.0 390:0.5 465:1.0 616:0.1111111111111111 653:1.0 729:1.0 746:1.0 1032:0.25 1114:1.0 1586:1.0 1851:1.0 2379:1.0 3313:1.0 3457:1.0 5843:1.0
11 11:0.25 19:1.0 32:1.0 41:1.0 46:0.14285714285714285 52:0.023255813953488372 66:0.4 99:0.16666666666666666 106:0.25 224:1.0 243:1.0 317:1.0 330:1.0 408:1.0 432:1.0 548:1.0 550:0.3333333333333333 554:1.0 960:0.5 1066:1.0 1148:0.5 1153:1.0 1558:1.0 1597:1.0 1767:1.0 2496:1.0 2981:1.0 3211:1.0 3922:1.0 5127:1.0
11 7:0.5 9:0.25 12:0.07142857142857142 14:1.0 15:1.0 24:0.3333333333333333 33:1.0 48:0.3333333333333333 50:0.5 55:1.0 60:1.0 66:0.4 75:1.0 99:0.3333333333333333 105:0.16666666666666666 135:0.5 178:1.0 269:1.0 286:1.0 371:1.0 388:1.0 542:1.0 795:0.25 982:1.0 1554:0.25 2093:1.0 2231:1.0 2270:1.0 3283:1.0 3301:1.0 4487:1.0 5971:1.0
11 9:0.5 12:0.07142857142857142 22:1.0 52:0.023255813953488372 55:0.5 58:0.5 103:0.5 110:0.06666666666666667 126:1.0 236:0.1111111111111111 275:0.1111111111111111 336:1.0 342:0.2 345:0.25 548:1.0 550:0.3333333333333333 580:1.0 616:0.1111111111111111 964:0.09090909090909091 1403:1.0 1461:1.0 1486:1.0 2054:1.0 2140:0.3333333333333333 2533:1.0 2951:1.0 3040:1.0 3838:1.0 4325:1.0 6639:1.0 7544:1.0 8033:1.0
11 5:0.5 7:0.5 36:0.09090909090909091 50:1.0 52:0.023255813953488372 59:0.3333333333333333 78:1.0 110:0.06666666666666667 113:0.5 135:0.5 165:0.6666666666666666 216:1.0 336:1.0 348:0.25 367:1.0 610:0.5 780:1.0 788:0.25 936:0.3333333333333333 1276:0.3333333333333333 1411:1.0 1780:1.0 2723:0.16666666666666666 4784:1.0 5402:1.0
11 7:1.0 9:0.25 12:0.07142857142857142 14:1.0 15:2.0 16:0.3333333333333333 41:1.0 45:0.5 46:0.14285714285714285 47:0.3333333333333333 50:2.0 53:0.6666666666666666 59:0.5 66:0.4 75:1.0 89:1.0 91:1.0 103:0.5 106:0.25 165:0.3333333333333333 236:0.1111111111111111 279:0.25 409:1.0 617:1.0 688:0.5 755:0.125 777:1.0 788:0.25 1025:0.3333333333333333 1260:1.0 1399:1.0 1518:1.0 1536:1.0 1538:1.0 2201:1.0 2590:1.0 3048:1.0 3060:1.0 3648:1.0 6095:1.0 6776:1.0 7194:1.0
11 7:1.0 12:0.14285714285714285 14:2.0 15:1.0 33:1.0 47:0.3333333333333333 50:0.5 66:0.2 102:0.25 128:0.3333333333333333 155:0.5 237:0.1 309:1.0 388:1.0 450:0.5 617:1.0 687:0.5 777:1.0 1025:0.3333333333333333 1212:1.0 2926:1.0 2973:1.0 3246:1.0 3747:1.0 5172:1.0
11 7:0.5 12:0.07142857142857142 15:2.0 22:1.0 31:0.4 46:0.42857142857142855 48:0.3333333333333333 50:1.5 52:0.023255813953488372 59:0.3333333333333333 66:0.2 105:0.16666666666666666 110:0.13333333333333333 126:1.0 165:0.3333333333333333 185:0.25 224:1.0 292:1.0 313:1.0 328:0.25 377:1.0 392:1.0 432:1.0 437:1.0 445:1.0 514:1.0 556:0.3333333333333333 617:1.0 687:0.5 825:1.0 1141:1.0 1301:1.0 1558:1.0 2263:1.0 2402:1.0 2624:1.0 3244:1.0 3579:1.0 4461:1.0 5074:1.0 5173:1.0 6971:1.0
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|
453e872f033fcdf0af762274ac33f3981505db61
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1370/CH2/EX2.13/example2_13.sce
|
863c25666c0d957ca67f7e9190f71dcbd64edf88
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,113 |
sce
|
example2_13.sce
|
//example2.13
clc
disp("Let no load,speed be N_0=1000 rpm")
disp("I_L0=Line current on no load=6 A")
disp("I_L0=(I_a0)+(I_sh)")
s=220/110
disp(s,"(I_sh)[in A]=V/(R_sh)=")
a=6-2
disp(a,"Therefore, (I_a0)[in A]=(I_L0)-(I_sh)=")
disp("Therefore, Back emf on no load E_b0 can be determined from the voltage equation.")
disp("V=(E_b0)+[(I_a0)+(R_a)]")
disp("Therefore, 220=(E_b0)+(4*0.3)")
b=220-1.2
disp(b,"E_b0(in V)=")
disp("On full load condition,supply voltage is constant and hence,")
s=220/110
disp(s,"(I_sh)[in A]=V/(R_sh)=")
disp("Now,(I_L)=(I_aFL)+(I_sh)")
disp("Therefore, 50=(I_aFL)+2")
f=50-2
disp(f,"Therefore, (I_aFL)[in A]=")
disp("And, V=(E_bFL)+[(I_aFL)*(R_a)]")
disp("Therefore, 220=(E_bFL+(48*0.3))")
b=220-(48*0.3)
disp(b,"Therefore, (E_bFL)[in V]=")
disp("From the speed equation,")
disp("N directly proportional to (E_b)/psi")
disp("But psi is constant as I_sh is constant for both the load conditions")
disp("Therefore, (N_0)/(N_FL)=(E_b0)/(E_bFL)")
n=(1000*205.6)/218.8
format(7)
disp(n,"Therefore, (N_FL)[in rpm]=[(N_0)*(E_bFL)]/(E_b0)=")
|
8993dec2705366c5b105c881cc74dc2ed2fee025
|
b0aff14da16e18ea29381d0bd02eede1aafc8df1
|
/mtlbSci/macros/moc_flipud.sci
|
b031501bfcb6453528bbfb0867dd03b01e7b1539
|
[] |
no_license
|
josuemoraisgh/mtlbSci
|
5d762671876bced45960a774f7192b41124a13ed
|
5c813ed940cccf774ccd52c9a69f88ba39f22deb
|
refs/heads/main
| 2023-07-15T23:47:11.843101 | 2021-08-26T17:52:57 | 2021-08-26T17:52:57 | 385,216,432 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 689 |
sci
|
moc_flipud.sci
|
function y = moc_flipud(x)
//Return a copy of X with the order of the rows reversed.
//Calling Sequence
//y = moc_fliplr(x)
//Description
// Return a copy of X with the order of the rows reversed. In
// other words, X is flipped upside-down about a horizontal axis. For
// Note that 'fliplr' only works with 2-D arrays.
// Examples
// moc_flipud ([1, 2; 3, 4])
if ndims(x)~=2,
disp('X must be a 2-D matrix!')
end
y = x($:-1:1,:);
endfunction
// %!assert((flipud ([1, 2; 3, 4]) == [3, 4; 1, 2]
// %! && flipud ([1, 2; 3, 4; 5, 6]) == [5, 6; 3, 4; 1, 2]
// %! && flipud ([1, 2, 3; 4, 5, 6]) == [4, 5, 6; 1, 2, 3]));
//
// %!error flipud ();
//
// %!error flipud (1, 2);
|
562e2dba752c39bcb2108ebebd212ee7139b5db2
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1919/CH1/EX1.4/Ex1_4.sce
|
40ddc0109a815e0b189d92f870078c90dfe3d576
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 626 |
sce
|
Ex1_4.sce
|
// Theory and Problems of Thermodynamics
// Chapter 1
// Basic Concepts
// Example 4
clear ;clc;
//Given data
Pf = 0.4 //Pf = pressure of the gas in MPa
Pa = 0.1 //Pa = atmospheric pressure in MPa
A = 10^-2 // A = cross-sectional area of piston in m^2
Vi = 0.1 // initial volume in m^3
Vf = 0.2 // final volume in m^3
//Calculate spring force constant
Pf = Pf * 10^6; // units conversion MPa to Pa
Pa = Pa * 10^6; // units conversion MPa to Pa
K = (Pf-Pa)*A^2/(Vf-Vi); //spring force constant
// Results
mprintf('Spring force constant = %3.0f N/m', K)
|
7df22832f4a2475dd8510c9744c8561a2f32dc42
|
8ad9380384d2751d79937ba5d6d581565596b891
|
/macros/generate.sci
|
b614cd685b42ee4b201ee76508dd86c280236deb
|
[
"BSD-3-Clause"
] |
permissive
|
iamAkshayrao/scilab_point_cloud_toolbox
|
1d8845f0830ddb623383c8dbfeadc8a3a35e8801
|
5d592a695b7976f4e63f0ae24d0a14937e474642
|
refs/heads/master
| 2022-12-17T23:14:11.513116 | 2020-09-25T18:57:02 | 2020-09-25T18:57:02 | 290,829,006 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,171 |
sci
|
generate.sci
|
function generate()
// Generates a random point cloud.
//
// Syntax
// PointCloud(OutputPCDFilename,options,"generate")
//
// Parameters
// outputPCDFilename : PCD file where the output pointcloud had to be saved
// options are
// -distribution = the distribution to be used (options: uniform / normal)(default: "uniform")
// -size = number of points in cloud (default: 10000);
// Options for uniform distribution:
// -(x,y,z)min = minimum for the (x,y,z) dimension (defaults: (0.0,0.0,0.0))
// -(x,y,z)max = maximum for the (x,y,z) dimension (defaults: (1.0,1.0,1.0))
// Options for normal distribution:
// -(x,y,z)mean = mean for the (x,y,z) dimension (defaults: (0.0,0.0,0.0))
// -(x,y,z)stddev = standard deviation for the (x,y,z) dimension (defaults: (1.0,1.0,1.0))
//
// Description
// This function generate a random point cloud of the specified name.
//
// Examples
// PointCloud("Output_generate1.pcd","-distribution","normal","-size","1000","-xmean","34","generate")
//
// Examples
// PointCloud("Output_generate2.pcd","generate")
//
//Authors
//Ankit Kumar
//Akshay S Rao
//Mohammed Rehab Sait
//Aliasgar AV
endfunction
|
30018c1940bd1b9061212241475f35bfe0b77fae
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2240/CH12/EX11.1/EX11_1.sce
|
e6de0cb1c36277ce0cad4a1f984af6e2fb1134aa
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 392 |
sce
|
EX11_1.sce
|
// Grob's Basic Electronics 11e
// Chapter No. 11
// Example No. 11_1
clc; clear;
// What is the area in circular mils of a wire with a diameter of 0.005 in.?
// Given data
Din = 0.005; // Diameter in Inches=0.005 in.
Dmil = 5; // Diameter in Mils=5 mil.
// 0.005 in. = 5 mil
// Therefore: Din == Dmil
A = Dmil*Dmil;
disp (A,'The Circular Area in cmils')
|
c30dfccadd23015708cc83484a37dfa6e4b2757d
|
3cbdc2f272df05cfe8c6636d4504e9e3d2e4fe3f
|
/SciLab/gauge-oscilator.sce
|
c604759ed91266ab52bee20b26b3f143a3418da4
|
[] |
no_license
|
bozhink/Code-Chunks
|
74355eb4c0d423c2f6484226e564030dff798678
|
860b7b8f53089ed96fd0ebead2e3eec16fa377cb
|
refs/heads/master
| 2020-12-24T06:19:04.343239 | 2019-11-13T14:09:15 | 2019-11-13T14:09:15 | 42,819,484 | 0 | 1 | null | 2019-11-13T14:09:16 | 2015-09-20T16:09:09 |
HTML
|
UTF-8
|
Scilab
| false | false | 345 |
sce
|
gauge-oscilator.sce
|
function z=GaugeOscilator(t,x)
n=32;
z(1) = x(n+1);
z(n+1) = x(n+2)-x(1);
for i=2:n-1
z(i) = x(n+i);
z(n+i) = x(n+i+1) - x(n+i-1) - x(i);
end
z(n) = x(n+n);
z(n+n) = -x(n+n-1) - x(n);
endfunction
xx=linspace(0,3*%pi,64);
y0=sin(xx);
t0=0;
t=t0:1:1000;
Z=ode(y0,t0,t,GaugeOscilator);
nz=max(size(Z));
|
927744615e77d6ca4967b87b4aa157521b380ab2
|
ece5c630921508b439ed25c5f7ab3db5a66f7a1a
|
/Assignment1_Team8/Decoder2to4bit.tst
|
0c8a93aa65daf245fa9d9ac24db56f985979f176
|
[] |
no_license
|
VedantS01/HDLProjectsCS2310
|
f8d17d1c9c28034a21026a4fbe2ae5d38cf39330
|
d2a39a4c062173475bd06ff0b3396f1ac6303103
|
refs/heads/main
| 2023-06-19T20:42:48.411561 | 2021-07-14T19:37:51 | 2021-07-14T19:37:51 | 386,054,022 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 340 |
tst
|
Decoder2to4bit.tst
|
load Decoder2to4bit.hdl ,
output-file Decoder2to4bit.out ,
output-list s1%B3.1.3 s0%B3.1.3 en%B3.1.3 y0%B3.1.3 y1%B3.1.3 y2%B3.1.3 y3%B3.1.3 ;
set en 1 ;
set s0 0 , set s1 0 ,
eval ,
output ;
set s0 1 , set s1 0,
eval ,
output ;
set s0 0 , set s1 1 ,
eval ,
output ;
set s0 1 , set s1 1 ,
eval ,
output ;
|
b54da9f2e950223e16a3c3f4ff031c132f37523d
|
8217f7986187902617ad1bf89cb789618a90dd0a
|
/browsable_source/1.1/Unix/scilab-1.1/macros/auto/des2tf.sci
|
ad165e5199c3ba9d797ad01e7b16a452fa0bd547
|
[
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-warranty-disclaimer",
"LicenseRef-scancode-unknown-license-reference"
] |
permissive
|
clg55/Scilab-Workbench
|
4ebc01d2daea5026ad07fbfc53e16d4b29179502
|
9f8fd29c7f2a98100fa9aed8b58f6768d24a1875
|
refs/heads/master
| 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 407 |
sci
|
des2tf.sci
|
function [Bfs,Bis,tf]=des2tf(des)
[LHS,RHS]=argn(0);
if LHS<>1 & LHS<> 3 then error('des2tf: 1 or 3 output args needed');end
A=des(2);B=des(3);C=des(4);E=des(6);
if norm(des(5),1) > 100*%eps then
warning('des2tf: D matrix is assumed to be 0!');end
s=poly(0,'s')
[Bfs,Bis,chis]=glever(E,A);
if LHS==3 then Bfs=C*Bfs*B; Bis=C*Bis*B;tf=chis;return;end
if LHS==1 then ww=C*Bfs*B;Bfs=ww/chis-c*Bis*b;return;end
|
f72008aa5fd1994998f5f81011bf5844dd26fdc3
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2789/CH5/EX5.5/Ex5_5.sce
|
30391c197827bb9f9397524efa262a4aa629e23a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 636 |
sce
|
Ex5_5.sce
|
clear;
clc;
//page no. 163
d = 1;// in
p_r = 100;//psi
T_r = 100;// degreeF
p_b = 14.7;// psi
p3 = 14.7;//psi
G = 2.03;// lb/sec
gam1 = 0.553;
gam = 1.4;
V3 = sqrt(2*32.2*(gam/(gam-1))*(p_r+p_b)*144/gam1 *(1-(p3/(p_r+p_b))^((gam-1)/gam)));
T3 = (T_r+460) - V3^2 /(2*32.2*186.5);
a3 = sqrt(gam*32.2*53.3*T3);
M3 = V3/a3;
A3 = G/(gam1*V3);
d3 = (A3/(0.25*%pi))^(1/2);
p3_dash = 103.3;// psia
p_B = p3*(1+ (2*gam/(gam+1))*(M3^2 -1));
printf('V3 = %d fps, a3 = %d fps, M3 = %.2f ',V3,a3,M3);
printf('\n p3_dash = %.1f psia, p_B = %.1f psia',p3_dash,p_B);
//there are minute errors in the answer given in textbook
|
c5009a8f1e3778261a8d10c0942cebe43d7adebe
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1238/CH8/EX8.6/8_6.sce
|
18c697601c9cc58311430d95a7db0ba31868d298
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 451 |
sce
|
8_6.sce
|
//calculating required data//
//example 6//
clc
//clears the command window//;
clear
//clears//
N=(2^8)-1;//no. of steps//
M=1000/N;//no. of steps in which motor speed can varied;motor speed varies from 0 to 1000rpm//
N1=450/M;//no. of steps required to reach 450rpm//
N2=round(N1);//rounding the no. of steps//
disp('For 115th step,speed of motor will be approximately 451rpm which gives an accuracy of .22%')
//displaying the answer//
|
26efe5c62c3461b9a53cfa7692b8a274e6efe8ac
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3401/CH3/EX3.4/Ex3_4.sce
|
7029cd47215dcb2847c01deb8bd6d20770eaf38e
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 111 |
sce
|
Ex3_4.sce
|
clc
y=10
Ni=10
gi=10
//(gi-Ni)!=1
z=(factorial(gi)/factorial(Ni)*factorial(gi-Ni))
printf('z=%f\n',z)
|
e8c3a13bdb53d7e8a3132e4de54c88c6eb2a4cda
|
32191356107e7ecaa8d06ca11fa40c4d6b3ba749
|
/code/fft-scilab/bp-1000-44100.sce
|
72f85a06bfba1b8712e066ee59dfcfe26b0c443f
|
[] |
no_license
|
mfkiwl/FIR-filter
|
9bfd6f96d52807ae744879668ddb922cc7db8149
|
bd08fa7d9f0162d7afab70a3e92ce140c7a422cb
|
refs/heads/master
| 2021-07-08T00:02:17.849458 | 2017-10-01T18:00:28 | 2017-10-01T18:00:28 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,611 |
sce
|
bp-1000-44100.sce
|
/**
* Script to generate filter coefficients for a linear phase, FIR bandpass filter
* centered at 5000 Hz.
*
* author: Rishi K Shukla
* website: www.technogeek310.wordpress.com
*
*/
/* n: determines the number of filter coefficients to be generated. */
n = 63;
/**
* bnd_edge: determines filter's frequency window. In Scilab, the frequency
* window can vary from 0 to 0.5 only. Here,
* f1 = 4420/44100 = 0.1 (lower cut-off frequency)
* f2 = 5580/44100 = 0.13 (higher cut-off frequency)
* f0 = (f1 + f2) / 2 = (0.1 + 0.13) / 2
* f0 = 0.115
* Central frequency = fo * sampling frequency = 0.115 * 44100
* Central frequency = 5071.5 Hz(approx. 5000 Hz)
*/
bnd_edge = [0, 4410/44100; 4420/44100, 5580/44100; 5590/44100, 22050/44100];
/* This is the desired magnitude for the central frequencies of the spectrum. */
des_magnit = [0 1 0];
/* This defines magnitude of weighted error across the frequency spectrum. */
rel_wght_err = [1 1 1];
/* generate band-pass filter coefficients as floating point values. */
[hn] = eqfir(n, bnd_edge, des_magnit, rel_wght_err);
/* save the coefficients in a text file */
print('coeff-44100.txt', hn);
/* convert floating point coefficients to signed int16_t format. */
hn = hn * 32768;
hn = round(hn);
/**
* hm - amplitude of the output
* fr - frequency
* 256 indicates the length of the array that will be returned
*/
[hm, fr] = frmag(hn, 256);
/* plot relationship between frequency and amplitude. */
plot(fr, hm);
xlabel('Normalized Digital Frequency');
ylabel('Magnitude');
title('Frequency Response of FIR BPF using REMEZ algorithm');
|
c5f9ff5d701e22e7725c4274dc33bb21b508c3f4
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3755/CH10/EX10.1/Ex10_1.sce
|
200faa2de40ad41a3729762ffd8e02249bde6a36
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 336 |
sce
|
Ex10_1.sce
|
clear
//
//
//
//Variable declaration
P=4.3*10^-8; //polarisation(per cm^2)
epsilon0=8.85*10^-12; //relative permeability(F/m)
E=1000; //electric field(V/m)
//Calculations
epsilonr=1+(P/(epsilon0*E)); //relative permittivity
//Result
printf("\n relative permittivity is %0.2f ",epsilonr)
|
18fd1017d7e918e6dcb7a7042d16ebbbb4809c37
|
717ddeb7e700373742c617a95e25a2376565112c
|
/72/CH12/EX12.4.3/12_4_3.sce
|
5b9bd9c4d829877840069d66d821dbd5a449e510
|
[] |
no_license
|
appucrossroads/Scilab-TBC-Uploads
|
b7ce9a8665d6253926fa8cc0989cda3c0db8e63d
|
1d1c6f68fe7afb15ea12fd38492ec171491f8ce7
|
refs/heads/master
| 2021-01-22T04:15:15.512674 | 2017-09-19T11:51:56 | 2017-09-19T11:51:56 | 92,444,732 | 0 | 0 | null | 2017-05-25T21:09:20 | 2017-05-25T21:09:19 | null |
UTF-8
|
Scilab
| false | false | 436 |
sce
|
12_4_3.sce
|
//CAPTION: Planar_Capacitor
//chapter_no.-12, page_no.-537
//Example_no.12-4-3
clc;
N=8;//number_of_fingers
er=13.1;//relative_dielectric_constant
h=.254;//substarte_height
l=.00254;//finger_length
w=.051;//finger_base_width
A1=.089;//contribution_of_interior_finger_for_h>w
A2=.1;//contribution_of_two_exterior_fingers_for_h>w
C=((er+1)*l*((A1*(N-3))+A2))/w;
disp(C,'the_Capacitance(in (pF/cm)is =');
|
48af7a981a684fea82e58bf92bb21ef92fb42448
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3751/CH11/EX11.8/Ex11_8.sce
|
0cae0067a577aa22dd32b509b6c1e5b2e53fa386
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,100 |
sce
|
Ex11_8.sce
|
//Fluid Systems - By - Shiv Kumar
//Chapter 11- Centrifugal Pumps
//Example 11.8
//To Determine the Power Required to drive the centrifugal Pump.
clc
clear
//Given Data:-
Q=40; //Discharge, litres/s
Hst=20; //Static Head, m
D=150; //Diameter of Pipe, mm
L=100; //length of pipe, m
eta_o=70/100; //Overall Efficiency
f=0.015; //Coefficient of friction
//Data Used:-
rho=1000; //Density of water, kg/m^3
g=9.81; //Acceleration due to gravity, m/s^2
//Computations:-
Q=Q/1000; //m^3/s
D=D/1000; //m
A=(%pi/4)*D^2; //m^2
V=Q/A; //m/s
Vd=V;
h_f=4*f*L*V^2/(2*g*D); //Frictional Head Loss in Pipe, m
Hm=Hst+h_f+Vd^2/(2*g); //Manometric Head, m
P=rho*Q*g*Hm/(eta_o*1000); //kW
//Result:-
printf("Power Required to drive the Centrifugal Pump=%.3f kW\n",P) //The answer vary due to round off error
|
c7cbdc6b848844851b082c1a253d2b79ce4ab7cb
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2015/CH7/EX7.8/7_8.sce
|
24e6b5bdde9c22c1353f3e51baffa5b6febbbaa5
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 529 |
sce
|
7_8.sce
|
clc
//initialisation of variables
ps1=0.056216 //bar pressure
phi1=0.2 //relative humidity
td1=35 //temp in degrees
p=1.01325 //pressure in bar
td2=25 //temp in degrees
ps2=0.03166 //bar
//CALCULATIONS
pv1=phi1*ps1
w1=0.622*(pv1/(p-pv1))
ha=(1.005*td1+w1*(2500+1.86*td1))
w2=(ha-(1.005*td2))/(2500+1.86*td2)
pv2=(w2*p)/(w2+0.622)
phi2=pv2/ps2
//RESULTS
printf('relative humidity rate is %2fkg/kg of da',ha)
printf('\nrelative humidity is %2f',phi2)
printf('\namount of water to be added is %2fkg/kg of da',w2)
|
5b181f4b323bf82c4d663e9ac854fd2825465c02
|
351fe6e47b1edc4fa8b9333340ba914299fa1b64
|
/rd7/as/pedm/backup.tst
|
53eef1028ba843a2f32ecca6da368d50d500321e
|
[
"MIT"
] |
permissive
|
ssavitzky/Silvermine-Resources
|
80ebba26f94a746da700e99320d06f7c629f7611
|
703375ba302929ad94ebe8326e0afecd6c06d633
|
refs/heads/master
| 2020-03-19T13:08:45.067855 | 2018-06-08T04:17:05 | 2018-06-08T04:17:05 | 136,563,434 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 25 |
tst
|
backup.tst
|
Sun Sep 11 21:47:40 1988
|
f6af747b22ba7f0e28959346b1029243ef3c3efa
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2444/CH6/EX6.18/ex6_18.sce
|
97b2b39066913b6d2bfe151dd52191ec5e9a0578
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 433 |
sce
|
ex6_18.sce
|
// Exa 6.18
clc;
clear;
close;
format('v',7)
// Given data
D = 10/100;// distortion without feedback
Df = 1/100;// distortion with feedback
A = 200;// unit less
// Df = D/(1+(Beta*A));
Beta = ((D/Df)-1)/A;// unit less
Af = A/(1+(Beta*A));// unit less
disp(Af,"The gain voltage with feed back is");
Vs = 10;// in mV
Vs = Vs * 10^-3;// in V
Vout = Af*Vs;// in V
disp(Vout,"The output voltage with feed back in V is");
|
dd7ed6b31d0746545809d2253f1537690654c752
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/926/CH3/EX3.1/Chapter3_Example1.sce
|
95e4356efbda940d66a391f588c00d66a96ac0eb
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,093 |
sce
|
Chapter3_Example1.sce
|
//Hougen O.A., Watson K.M., Ragatz R.A., 2004. Chemical process principles Part-1: Material and Energy Balances(II Edition). CBS Publishers & Distributors, New Delhi, pp 504
//Chapter-3, Illustration 1, Page 54
//Title: Calculation of volume
//=============================================================================
clear
clc
//INPUT
W1 = 30; //Weight of chlorine in lb
MW = 71; //Molecular weight of chlorine in lb/lb mole
P1 = 760; //Pressure at standard conditions in mm Hg
T1 = 492; //Temperature at standard conditions in degree R
P2 = 743; //Given pressure in mm Hg
T = 70; //Given temperature in degree F
//CALCULATIONS
n = W1/MW; //No of moles of chlorine in lb mole
V1= n*359; //Volume of chlorine at standard conditions in cu ft
T2 = 530; //Given temperature in degree R
V2 = V1*(P1/P2)*(T2/T1); //Volume of chlorine at given conditions in cu ft
//OUTPUT
mprintf(' \n Volume occupied by %2.0f lb of chlorine at given temperature and pressure is %3.0f cu ft',W1,V2);
//=================================END OF PROGRAM==============================
|
f560de8eb24c4e04c1d3c0097ce01c7377965e29
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3821/CH7/EX7.13/Example7_13.sce
|
bcc5efe7454c1959ae92568a31412b3fb09de7fa
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 592 |
sce
|
Example7_13.sce
|
///Chapter No 7 Fluid Mechanics
///Example 7.13 Page No:124
///Find Discharge through pipe
///Input data
clc;
clear;
D1=0.2; //Diameter of pipe section 1 in m
D2=0.3; //Diameter of pipe section 2 in m
V1=15; //Velocity of water in m/s
pi=3.14;
///calculation
Q=((3.14/4)*(0.2)^2)*15; //Discharge through pipe in m**3/s
V2=(((3.14/4)*(0.2)^2)*15)/((3.14/4)*(0.3)^2); //velocity of section2 in m/s
///Output
printf('Discharge through pipe= %f m^3/s \n ',Q);
printf('velocity of section2= %f m/s \n ',V2);
|
706490d90d09a39229ac90803f50c6ba6e46accd
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1538/CH21/EX21.15/Ex21_15.sce
|
47c5f2d0eddfc0cea39109a025eccf9c057eed36
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 374 |
sce
|
Ex21_15.sce
|
//example-21.15
//page no-651
//given
//length of wire
l=250*10^-3 //m
//no of turns
N=400
//current
I=15 //A
//permeability in vaccum
mu0=1.2457*10^-6 //H/m
//relative permeability
mur=1
//magnetic field strength
H=N*I/l //AT/m
//flux density is
B=mu0*mur*H //Wb/m^2
printf ("the magnetic field strength is %f AT/m and flux density is %f Wb/m",H,B)
|
f04df1e83cb8221eaee830f68620e48afe0b7d50
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1301/CH4/EX4.9/ex4_9.sce
|
33ff823e83beff60ebba216a691e3dfaaeb8ae44
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 711 |
sce
|
ex4_9.sce
|
clc;
G=6.67*10^-11 //universal gravitational constant in Nm square/kg square.
m1=5.98*10^24; //mass of earth in kg
m2=7.36*10^22; //mass of moon in kg
r=3.84*10^8; //radius of moon's orbit
F=(G*m1*m2)/(r*r); //calculating gravitationalforce in Newton
v=sqrt((G*m1)/r); //calculating velocity of moon in m/sec
s=2*%pi*r; //calculating circumference of moon's orbit in metre
t=s/v; //calculating time in sec
disp(F,"Gravitational Force in Newton = "); //displaying gravitational force in Newton
disp(v,"Velocity in metre/sec = "); //displaying velocity in metre
disp(t,"Time in sec = "); //displaying time in sec.
disp(t/86400,"Time in days = "); //displaying time in days
|
6692472b9416513b43e262fb2214e12e5057fbb9
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1904/CH7/EX7.2/7_2.sce
|
fef83fce338eb6a07183f7b56447474c1ad431d2
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,463 |
sce
|
7_2.sce
|
//To determine the voltage drop or voltage regulation of a 3phase system
//Page 327
clc;
clear;
Vll=416; //Voltage Line to Line
Vph=Vll/(sqrt(3)); //Phase Voltage and Base Voltage
//Load Currents
Ia=30;
Ib=20;
Ic=50;
//Power Factors of the load
pfa=1;
pfb=0.5;
pfc=0.9;
//Impedances of the Sections
ZA=0.05+(%i*0.01);
ZAB=0.1+(%i*0.02);
ZBC=0.05+(%i*0.05);
//Impedance upto the point of load
ZB=ZA+ZAB;
ZC=ZB+ZBC;
//Function to Calculate Voltage Drop
deff('x=VD(a,b,c)','x=a*((real(b)*c)+(imag(b)*sind(acosd(c))))')
//Voltage Drops at A,B and C
VDA=VD(Ia,ZA,pfa);
VDB=VD(Ib,ZB,pfb);
VDC=VD(Ic,ZC,pfc);
TVD=VDA+VDB+VDC; //Total Voltage Drop
TVDpu=TVD/Vph; // In Per Unit
deff('x=Real(y,z)','x=Vph*y*z') //Function to Calculate Real Power
deff('x=Reactive(y,z)','x=Vph*y*sind(acosd(z))') //Funtion to Calculate the Reactive power
//Real Powers
Pa=Real(Ia,pfa);
Pb=Real(Ib,pfb);
Pc=Real(Ic,pfc);
P=Pa+Pb+Pc; //Total Real Power
//Reactive Powers
Qa=Reactive(Ia,pfa);
Qb=Reactive(Ib,pfb);
Qc=Reactive(Ic,pfc);
Q=Qa+Qb+Qc; //Total Reactive Power
S=sqrt((P^2)+(Q^2)); //Total output from the Transformer
PF=P/S; //Load Power Factor
printf('\na) The Total Voltage drop is %g pu\n',TVDpu)
printf('b) The Real Power per Phase is %g kW\n',P/1000)
printf('c) The Reactive Power per Phase is %g kVAr\n',Q/1000)
printf('d) The Kilovoltampere output and load factor is %g kVA and %g lagging\n',S/1000,PF)
|
d66950703c02641e49e77d1476fb1bb5c66c1f1c
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/409/CH7/EX7.4/Example7_4.sce
|
d4ac12bf44488bab2a6422e50110a1677b7582a6
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 540 |
sce
|
Example7_4.sce
|
clear ;
clc;
// Example 7.4
printf('Example 7.4\n\n');
//Page no. 180
// Solution
n_un= 7 ;// Number of unknowns in the given problem- 3 values of xi and 4 values Fi
n_ie = 5 ;// Number of independent equations
// Summary of independent equations
// Three material balances:CH4,C2H6 and N2
// One specified ratio: moles of CH4 to C2H6 equal 1.5
// One summation of mole fraction in mixture equals 1
d_o_f = n_un-n_ie ;// No. of degree of freedom
printf('Number of degree of freedom for the given system is %i .\n',d_o_f);
|
87f8168abc14b18cc76a95010ba0074fe9874d63
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1382/CH5/EX5.4/EX_5_4.sce
|
c0d1ab1e17e3a139c842db03729f9a4803f74c4d
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 267 |
sce
|
EX_5_4.sce
|
// Example 5.4:amplifier gain
clc;
clear;
close;
f=50;//frequency in hertz
Avm=150/0.707;//mid voltage gain
fh=20;//lower cut off frequency in hertz
Avh= (Avm/(sqrt(1+(f/fh)^2)));//gain at upper cut off frequency
disp(Avh,"gain at upper cut off frequency")
|
5284772029a5fca641f08754e2db095c784356c2
|
389bd4af3bf5a0f54f51e8aafea5035f568ba445
|
/13kasım_fonkfx.sce
|
ca85d5573c2cc02c39c254f591db5ca9fded0ed4
|
[] |
no_license
|
esraatlici/Bilgisayar-Destekli-Matematik
|
d47f057d9cb7ee987e367c67f8923cfcf02342d8
|
dae1079f60fc7e0d3b54802b4cbed9182b52fcd7
|
refs/heads/main
| 2022-12-25T11:14:25.575530 | 2020-10-05T15:09:58 | 2020-10-05T15:09:58 | 301,447,895 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 240 |
sce
|
13kasım_fonkfx.sce
|
//Çok tanımlı bir matematikse ifadenin fonksiyonu
function out=f(x)
if 0<x & x<=10 then
out=5*x;end
if 10<x & x<=100 then
out=5*(x^2);end
if x>100 then
out=0.5*(x^2);
end
endfunction
|
b414cf51a5daaeba23ed7bf236c0c79d622e0505
|
2391eec552dac38c05f9c53bae1ec612f2871f51
|
/Lab 5/fucmeup.sce
|
78a7fd19959b12c227b2bf440141d3899d8d8be4
|
[] |
no_license
|
Zebz13/EEE-S7-Power-Systems
|
fe9e00e27242fa51650bf87e46c504a716a22edf
|
1fc9ab29e96a5d5f8a23d629364cadf2c70c4a40
|
refs/heads/main
| 2023-01-10T03:53:34.295752 | 2020-11-08T17:03:45 | 2020-11-08T17:03:45 | 309,158,346 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 3,296 |
sce
|
fucmeup.sce
|
//please run or read and edit out unnecessary stuff
//start
clc ;
clear ;
//line inputs
disp("Enter the line data in the order-> From,To,Res,Reat,Half Admit,Tap")
linedata =input("Enter line data:")
Yshunt=input("Enter shunt admittance:")
// line data extraction
from= linedata(:,1)
to= linedata(:,2)
imp= linedata(:,3)+ linedata(:,4)*%i
half_adm= linedata(:,5)*%i
bus_no= max(max(from,to));
Ybus= zeros(bus_no,bus_no);
line_number=length(from)
//Ybus building
for i=1:line_number
m=from(i);
n=to(i);
Ybus(m,m)=Ybus(m,m) +1/imp(i)+ (half_adm(i)) ;
Ybus(n,n)=Ybus(n,n) +1/imp(i)+ (half_adm(i)) ;
Ybus(m,n)= -1/ imp(i);
Ybus(n,m)=Ybus(m,n);
end
//Adding shunt to diagonal elements
for i=1:bus_no
Ybus(i,i)=Ybus(i,i)+Yshunt(i)
end
//display Ybus
disp("Ybus Admittance is:")
disp(Ybus)
//Input and extract bus data. Taps are avoided
disp("Enter data in the order-> Bus, type, Vsp, theta, Pgi, Qgi, Pli, Qli, Qmin, Qmax")
busdata = input("Enter bus data:")
bus=busdata(:,1)
typ = busdata(:,2)
qmin = busdata(:,9)
qmax = busdata(:,10)
//net p and q
p= busdata (:,5)- busdata(:,7)
q= busdata(:,6)- busdata(:,8)
v= busdata(:,3).*(cosd(busdata(:,4))+ %i*sind(busdata(:,4)));
//parameter setting
//default. Can take alpha as input() if needed
count =0;
err =1;
vold =v;
//gauss seidel method
while abs(err)>5*10^(-5)
//while count<23 //testing
for i=2:bus_no
sumyv=0;
for j=1:bus_no
if i~=j
sumyv=sumyv+Ybus(i,j)*v(j);
end
end
if typ(i)==2
q(i)=-imag(conj(v(i))*(sumyv+(Ybus(i,i)*v(i))));
if q(i)<qmin (i) | q(n)>qmax (i)
if q(i)<qmin (i)
q(i)= qmin (i);
else
q(i)= qmax (i);
end
end
end
v(i) =(1/Ybus(i,i)) *(((p(i)-%i*q(i))/(conj(v(i)))) -sumyv);
end
count=count+1;
err=max(abs(abs(v)-abs(vold)));
vold=v;
end
//Load flow and slack power
Amp=zeros(bus_no,bus_no)
Powerflow=zeros(bus_no,bus_no)
Lineloss=zeros(line_number)
slackpower=0
for start=1:bus_no
for fin=1:bus_no
if(start~=fin)
//-Ybus since off diagonal elements are negative
Amp(start,fin)=-Ybus(start,fin)*(v(start)-v(fin))
Amp(fin,start)=-Amp(start,fin)
Powerflow(start,fin)=v(start)*(conj(Amp(start,fin)))
Powerflow(fin,start)=v(fin)*(conj(Amp(fin,start)))
Lineloss(start,fin)=Powerflow(start,fin)+Powerflow(fin,start)
if(start==1)
slackpower=slackpower+(conj(v(1))*Amp(1,fin))
end
end
end
end
//making sparse and removing duplicates (1,2) and (2,1)
Lineloss_mod=zeros(bus_no,bus_no)
for temp=1:line_number
m=from(temp)
n=to(temp)
Lineloss_mod(m,n)=Lineloss(m,n)
end
Lineloss_mod=sparse(Lineloss_mod)
//disp output
disp("Voltage rectangular:",v)
volt=abs(v)
angle=atan(imag(v),real(v))*(180/%pi);
disp("Voltage:",volt)
disp("Angle:",angle)
printf("Gauss Seidel Load Flow converged after %i iteration.", count)
disp("Line flow",Powerflow)
disp("Line losses",Lineloss_mod)
disp("Slack bus power",slackpower)
|
74bd7bb1fb8d3845e5c95f1d35de4f9b1aaa5b88
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3843/CH4/EX4.6/Ex4_6.sce
|
bd9bf8e6d44c07b8d6b27d709b87593da78a1479
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 754 |
sce
|
Ex4_6.sce
|
// Example 4_6
clc;funcprot(0);
// Given data
T_1=300;// °C
T_2=700;// °C
m=3;// kg
// Calculation
// (a)
delH=m*integrate('(2.07+((T-400)/1480))','T',T_1,T_2);
printf("\n(a)The enthalpy change,delH=%4.0f kJ",delH);
// From steam tables
h_1=3073;// kJ/kg
h_2=3928;// kJ/kg
delH=m*(h_2-h_1);// kJ/kg
printf("\n Using the values from steam tables,the enthalpy change,delH=%4.0f kJ",delH);
// (b)
delT=T_2-T_1;// °C
c_pav=(m*integrate('(2.07+((T-400)/1480))','T',T_1,T_2))/(m*delT);// kJ/kg.°C
printf("\n(b)The average value of c_p=%1.2f kJ/kg.°C",c_pav);
// Using the values from steam tables
c_pav=(h_2-h_1)/delT;// kJ/kg.°C
printf("\n Using the values from steam tables,the average value of c_p=%1.2f kJ/kg.°C",c_pav);
|
f18ed72a2a44993953715118762860c6369a6182
|
7b5fc14eb97ac069fb310c30488cf43459cd667b
|
/LA_Assignment_1.sce
|
4a03c6ad945b4789f0090a58df419669b9e06829
|
[] |
no_license
|
Araz1103/Linear-Algebra-Assignments
|
97406f1e10ed80570c0bb6d404c8fbd59b769ac3
|
84644aec95bc7e430bcc01f6075d60b23e2e4a65
|
refs/heads/master
| 2020-12-31T10:07:47.386678 | 2020-04-10T12:01:32 | 2020-04-10T12:01:32 | 238,992,825 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 813 |
sce
|
LA_Assignment_1.sce
|
str = input("Enter a 3x4 augmented matrix which has spaces to seperate", "string")
v = evstr(strsplit(str, " "))
init11=v(1)
init12=v(2)
init13=v(3)
init21=v(5)
init22=v(6)
init23=v(7)
init31=v(9)
init32=v(10)
init33=v(11)
sec1=v(4)
sec2=v(8)
sec3=v(12)
A=[init11,init12,init13,sec1;init21,init22,init23,sec2;init31,init32,init33,sec3]
n=3;
for k=2:n
for j=2:n+1
A(k,j)=A(k,j)-A(1,j)*A(k,1)/A(1,1);
end
A(k,1)=0;
end
for i=3:n
for j=3:n+1
A(i,j)=A(i,j)-A(2,j)*A(i,2)/A(2,2);
end
A(i,2)=0;
end
x(n)=A(n,n+1)/A(n,n);for i=n-1:-1:1
sumk=0;
for k=i+1:n
sumk=sumk+A(i,k)*x(k);
end
x(i)=(A(i,n+1)-sumk)/A(i,i);
end
disp(x(3),x(2),x(1),'Tha values of x,y,z are');
disp(A(1,1),A(2,2),A(3,3),'The pivots are');
|
98c6f6d48d4bdf7526fd8549ce0f12b4ad831d5c
|
931df7de6dffa2b03ac9771d79e06d88c24ab4ff
|
/Shoot Down Target.sce
|
9f107f672f17cb2532fa7e2ffd0d6cb953de504b
|
[] |
no_license
|
MBHuman/Scenarios
|
be1a722825b3b960014b07cda2f12fa4f75c7fc8
|
1db6bfdec8cc42164ca9ff57dd9d3c82cfaf2137
|
refs/heads/master
| 2023-01-14T02:10:25.103083 | 2020-11-21T16:47:14 | 2020-11-21T16:47:14 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 41,456 |
sce
|
Shoot Down Target.sce
|
Name=Shoot Down Target
PlayerCharacters=player_char
BotCharacters=down_strafe.bot
IsChallenge=true
Timelimit=60.0
PlayerProfile=player_char
AddedBots=down_strafe.bot;down_strafe.bot;down_strafe.bot;down_strafe.bot;down_strafe.bot
PlayerMaxLives=0
BotMaxLives=0;0;0;0;0
PlayerTeam=1
BotTeams=2;2;2;2;2
MapName=shoot_down.map
MapScale=10.0
BlockProjectilePredictors=true
BlockCheats=true
InvinciblePlayer=false
InvincibleBots=false
Timescale=1.0
BlockHealthbars=false
TimeRefilledByKill=0.0
ScoreToWin=0.0
ScorePerDamage=1.0
ScorePerKill=10.0
ScorePerMidairDirect=0.0
ScorePerAnyDirect=0.0
ScorePerTime=0.0
ScoreLossPerDamageTaken=0.0
ScoreLossPerDeath=0.0
ScoreLossPerMidairDirected=0.0
ScoreLossPerAnyDirected=0.0
ScoreMultAccuracy=true
ScoreMultDamageEfficiency=false
ScoreMultKillEfficiency=false
GameTag=click-timing,tracking
WeaponHeroTag=LG
DifficultyTag=3
AuthorsTag=NFNT
BlockHitMarkers=false
BlockHitSounds=false
BlockMissSounds=false
BlockFCT=false
Description=Track and kill targets that drop when you shoot.
GameVersion=2.0.1.1
ScorePerDistance=0.0
MBSEnable=false
MBSTime1=0.25
MBSTime2=0.5
MBSTime3=0.75
MBSTime1Mult=1.0
MBSTime2Mult=2.0
MBSTime3Mult=3.0
MBSFBInstead=false
MBSRequireEnemyAlive=false
LockFOVRange=false
LockedFOVMin=60.0
LockedFOVMax=120.0
LockedFOVScale=Clamped Horizontal
[Aim Profile]
Name=Default
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
AimingStyle=Original
ScanSpeedMultiplier=1.0
MaxSeekPitch=30.0
MaxSeekYaw=30.0
AimingSpeed=5.0
MinShootDelay=0.3
MaxShootDelay=0.6
[Bot Profile]
Name=down_strafe
DodgeProfileNames=down_strafe
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=100.0
DodgeProfileMinChangeTime=100.0
WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0
AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default
WeaponSwitchTime=3.0
UseWeapons=false
CharacterProfile=down_strafe_char
SeeThroughWalls=false
NoDodging=false
NoAiming=true
AbilityUseTimer=0.0001
UseAbilityFrequency=1.0
UseAbilityFreqMinTime=0.3
UseAbilityFreqMaxTime=0.6
ShowLaser=false
LaserRGB=X=1.000 Y=0.300 Z=0.000
LaserAlpha=1.0
[Character Profile]
Name=player_char
MaxHealth=100.0
WeaponProfileNames=LG;;;;;;;
MinRespawnDelay=1.0
MaxRespawnDelay=5.0
StepUpHeight=75.0
CrouchHeightModifier=0.5
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=8.0
MovementType=Base
MaxSpeed=0.0
MaxCrouchSpeed=500.0
Acceleration=16000.0
AirAcceleration=16000.0
Friction=8.0
BrakingFrictionFactor=2.0
JumpVelocity=800.0
Gravity=0.0
AirControl=0.25
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=255.000 Y=0.000 Z=0.000
EnemyHeadColor=X=255.000 Y=255.000 Z=255.000
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cylindrical
MainBBHeight=230.0
MainBBRadius=55.0
MainBBHasHead=true
MainBBHeadRadius=45.0
MainBBHeadOffset=0.0
MainBBHide=true
ProjBBType=Cylindrical
ProjBBHeight=230.0
ProjBBRadius=55.0
ProjBBHasHead=true
ProjBBHeadRadius=45.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=true
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.5
AllowBufferedJumps=true
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=1.0
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=2048.0
VerticalSpawnOffset=265.0
TerminalVelocity=0.0
CharacterModel=None
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=false
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=false
FlightObeysPitch=false
FlightVelocityUp=800.0
FlightVelocityDown=800.0
[Character Profile]
Name=down_strafe_char
MaxHealth=70.0
WeaponProfileNames=;;;;;;;
MinRespawnDelay=0.0001
MaxRespawnDelay=0.0001
StepUpHeight=0.0
CrouchHeightModifier=1.0
CrouchAnimationSpeed=0.1
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=0.0
MovementType=Base
MaxSpeed=600.0
MaxCrouchSpeed=2400.0
Acceleration=50000.0
AirAcceleration=16000.0
Friction=0.0
BrakingFrictionFactor=0.0
JumpVelocity=2400.0
Gravity=0.0
AirControl=0.0
CanCrouch=false
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=255.000 Y=0.000 Z=0.000
EnemyHeadColor=X=255.000 Y=255.000 Z=255.000
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Spheroid
MainBBHeight=100.0
MainBBRadius=50.0
MainBBHasHead=false
MainBBHeadRadius=0.1
MainBBHeadOffset=0.0
MainBBHide=true
ProjBBType=Spheroid
ProjBBHeight=0.02
ProjBBRadius=0.01
ProjBBHasHead=false
ProjBBHeadRadius=0.1
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.0
JetpackFullFuelTime=100.0
JetpackFuelIncPerSec=100.0
JetpackFuelRegensInAir=false
JetpackThrust=1600.0
JetpackMaxZVelocity=800.0
JetpackAirControlWithThrust=1.0
AbilityProfileNames=down_strafe.abilmov;;;
HideWeapon=true
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=0.001
RespawnInvulnTime=0.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=500.0
RespawnAnimationDuration=0.0
AllowBufferedJumps=false
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=0.001
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=0.0
VerticalSpawnOffset=0.0
TerminalVelocity=1.0
CharacterModel=None
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=false
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=true
FlightObeysPitch=true
FlightVelocityUp=0.0
FlightVelocityDown=0.0
[Dodge Profile]
Name=down_strafe
MaxTargetDistance=4000.0
MinTargetDistance=0.0
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=4.0
MaxLRTimeChange=4.0
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=false
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=0.0
DamageReactionResetTimer=0.1
JumpFrequency=0.0
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Ignore
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.3
MaxJumpTime=0.6
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.0
BlockedMovementPercent=0.0
BlockedMovementReactionMin=0.0
BlockedMovementReactionMax=0.0
WaypointLogic=Ignore
WaypointTurnRate=200.0
MinTimeBeforeShot=0.15
MaxTimeBeforeShot=0.25
IgnoreShotChance=0.0
ForwardTimeMult=1.0
BackTimeMult=1.0
DamageReactionChangesFB=false
[Weapon Profile]
Name=LG
Type=Hitscan
ShotsPerClick=1
DamagePerShot=10.0
KnockbackFactor=0.0
TimeBetweenShots=0.05
Pierces=false
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=true
HeadshotMultiplier=2.0
MagazineMax=0
AmmoPerShot=1
ReloadTimeFromEmpty=0.1
ReloadTimeFromPartial=0.1
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
ProjectileGraphic=Ball
VisualLifetime=0.1
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=false
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.001
HitSoundCooldown=0.001
HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=0.0
RecoilNegatable=false
DecalType=0
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=true
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=0.0
AimPunchResetTime=0.2
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=false
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=No Scope
ADSFOVOverride=104.0
ADSFOVScale=Apex Legends
ADSAllowUserOverrideFOV=false
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
WeaponModel=Heavy Surge Rifle
WeaponAnimation=Primary
UseIncReload=false
IncReloadStartupTime=0.1
IncReloadLoopTime=0.1
IncReloadAmmoPerLoop=1
IncReloadEndTime=0.1
IncReloadCancelWithShoot=true
WeaponSkin=Default
ProjectileVisualOffset=X=0.000 Y=0.000 Z=-50.000
SpreadDecayDelay=0.0
ReloadBeforeRecovery=true
3rdPersonWeaponModel=Pistol
3rdPersonWeaponSkin=Default
ParticleMuzzleFlash=None
ParticleWallImpact=Gunshot
ParticleBodyImpact=Gunshot
ParticleProjectileTrail=
ParticleHitscanTrace=Tracer
ParticleMuzzleFlashScale=1.0
ParticleWallImpactScale=1.0
ParticleBodyImpactScale=1.0
ParticleProjectileTrailScale=1.0
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=0.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,0.0
SpreadSCA=1.0,1.0,-1.0,0.0
SpreadMSA=1.0,1.0,-1.0,0.0
SpreadMCA=1.0,1.0,-1.0,0.0
SpreadSSH=1.0,1.0,-1.0,0.0
SpreadSCH=1.0,1.0,-1.0,0.0
SpreadMSH=1.0,1.0,-1.0,0.0
SpreadMCH=1.0,1.0,-1.0,0.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=0
AAPreferClosestPlayer=false
AAAlpha=0.05
AAMaxSpeed=1.0
AADeadZone=0.0
AAFOV=30.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Movement Ability Profile]
Name=down_strafe
MaxCharges=10.0
ChargeTimer=0.01
ChargesRefundedOnKill=0.0
DelayAfterUse=0.0
FullyAuto=false
AbilityDuration=0.0
LockDirectionForDuration=true
NegateGravityForDuration=false
MainVelocity=200.0
MainVelocityCanGoVertical=false
MainVelocitySetToMovementKeys=false
UpVelocity=-200.0
EndVelocityFactor=0.0
Hurtbox=false
HurtboxRadius=50.0
HurtboxDamage=50.0
HurtboxGroundKnockbackFactor=1.0
HurtboxAirKnockbackFactor=1.0
AbilityBlocksTurning=true
AbilityBlocksMovement=true
AbilityBlocksAttack=false
AttackCancelsAbility=false
AbilityReloadsWeapon=false
HealthRestore=0.0
AIUseInCombat=false
AIUseOutOfCombat=false
AIUseOnGround=false
AIUseInAir=false
AIReuseTimer=0.01
AIMinSelfHealth=0.0
AIMaxSelfHealth=100.0
AIMinTargHealth=0.0
AIMaxTargHealth=100.0
AIMinTargDist=0.0
AIMaxTargDist=1000000.0
AIMaxTargFOV=360.0
AIDamageReaction=true
AIDamageReactionIgnoreChance=0.0
AIDamageReactionMinDelay=0.01
AIDamageReactionMaxDelay=0.01
AIDamageReactionCooldown=0.01
AIDamageReactionThreshold=0.01
AIDamageReactionResetTimer=0.01
[Map Data]
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entity
type PlayerSpawn
Vector3 position 0.000000 65.000000 0.000000
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Bool8 modeCTF 0
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Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type CameraPath
UInt8 posLerp 2
UInt8 angleLerp 2
entity
type PlayerSpawn
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Bool8 teamA 0
Bool8 initialSpawn 0
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Bool8 modeFFA 0
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Bool8 mode2v2 0
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type PlayerSpawn
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Bool8 modeCTF 0
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Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
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Bool8 teamA 0
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Bool8 mode1v1 0
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Bool8 mode2v2 0
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Bool8 modeCTF 0
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Bool8 mode1v1 0
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Bool8 mode2v2 0
entity
type PlayerSpawn
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Bool8 modeCTF 0
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Bool8 modeTDM 0
Bool8 mode1v1 0
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Bool8 mode2v2 0
entity
type PlayerSpawn
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Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -100.000000 7.000000 430.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -200.000000 7.000000 420.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -300.000000 7.000000 390.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -100.000000 107.000000 430.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -100.000000 207.000000 430.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -200.000000 107.000000 420.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -200.000000 207.000000 420.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
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Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position -300.000000 207.000000 390.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
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Bool8 mode2v2 0
entity
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Bool8 mode1v1 0
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Bool8 mode2v2 0
entity
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Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
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Bool8 mode2v2 0
entity
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Bool8 initialSpawn 0
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Bool8 modeTDM 0
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Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
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Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
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Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Bool8 initialSpawn 0
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Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Bool8 initialSpawn 0
Bool8 modeCTF 0
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Bool8 mode1v1 0
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Bool8 mode2v2 0
entity
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Bool8 mode2v2 0
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Bool8 initialSpawn 0
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Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
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Bool8 initialSpawn 0
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Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
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Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Vector3 angles 180.000000 0.000000 0.000000
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Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Vector3 angles 180.000000 0.000000 0.000000
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Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
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Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
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Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position 250.000000 57.000000 405.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
Bool8 initialSpawn 0
Bool8 modeCTF 0
Bool8 modeFFA 0
Bool8 modeTDM 0
Bool8 mode1v1 0
Bool8 modeRace 0
Bool8 mode2v2 0
entity
type PlayerSpawn
Vector3 position 250.000000 157.000000 405.000000
Vector3 angles 180.000000 0.000000 0.000000
Bool8 teamA 0
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|
59b72afabadf8a549c1175ad6561c13dccdc9a38
|
8217f7986187902617ad1bf89cb789618a90dd0a
|
/source/2.4/examples/intersci-examples/ex7.sce
|
eb2620379d33e7c7d9b813c4580cb7e7e743f105
|
[
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-warranty-disclaimer"
] |
permissive
|
clg55/Scilab-Workbench
|
4ebc01d2daea5026ad07fbfc53e16d4b29179502
|
9f8fd29c7f2a98100fa9aed8b58f6768d24a1875
|
refs/heads/master
| 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 462 |
sce
|
ex7.sce
|
//ex7 example
//1-Creating interface source file
// from ex7fi.desc file by call to intersci
// Making object files
// Interface file '/tmp/ex7fi.o'
// User's files '/tmp/ex7f.o';
files=G_make(['/tmp/ex7fi.o','/tmp/ex7f.o'],'ex7.dll');
//2-Link object files .o with addinter
//addinter(files,'intex7',intex1_funs);
exec('ex7fi.sce');
//Run Scilab functions:
if calc('one')<>1 then pause,end
if calc('two')<>2 then pause,end
if calc('other')<>-1 then pause,end
|
4e2add9da4b521252aae0ccab35981628921f9d3
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1682/CH11/EX11.3/Exa11_3.sce
|
396bf6ee028ba10d7133523b4de8ffca0e999e3a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,585 |
sce
|
Exa11_3.sce
|
//Exa 11.3
clc;
clear;
close;
IR=5;//in % per year
i=15;//in % per year
//Machine X :
disp("Machine X : ");
Ppx=1500000;//in Rs.
n=7;//in years
S=200000;//in Rs.
AMC=300000;//in Rs.
disp("End of year AMC InflationFactor InflatedAmount P/F PW");
format('v',9)
Pw=0;//For initialising
for n=1:7
FP=(1+IR/100)^n
IA=AMC*FP;//in Rs.
PF=1/((1+i/100)^n);
PW=IA*PF;//in Rs.
Pw=Pw+PW;//in Rs.
disp(" "+string(n)+" "+string(AMC)+" "+string(FP)+" "+string(IA)+" "+string(PF)+" "+string(PW));
end
disp(Pw,"Present worth of inflated annual operating and maintenance cost in Rs. : ");
PWX=Ppx+Pw-S*1/((1+i/100)^n);
disp(PWX,"Present worth of machine X in Rs. : ");
//Machine Y
disp("Machine Y : ");
Ppy=2000000;//in Rs.
n=7;//in years
S=300000;//in Rs.
AMC=250000;//in Rs.
disp("End of year AMC InflationFactor InflatedAmount P/F PW");
format('v',9)
Pw=0;//For initialising
for n=1:7
FP=(1+IR/100)^n
IA=AMC*FP;//in Rs.
PF=1/((1+i/100)^n);
PW=IA*PF;//in Rs.
Pw=Pw+PW;//in Rs.
disp(" "+string(n)+" "+string(AMC)+" "+string(FP)+" "+string(IA)+" "+string(PF)+" "+string(PW));
end
disp(Pw,"Present worth of inflated annual operating and maintenance cost in Rs. : ");
PWY=Ppy+Pw-S*1/((1+i/100)^n);
disp(PWY,"Present worth of machine Y in Rs. : ");
disp("Since the present worth of Machine X is less than Machine Y, select Machine X")
//Note : Calculations are not accurate in the book
|
b54e8db8872d3225da4f0977493b19099c97f51b
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1991/CH6/EX6.12/12.sce
|
9f1b9d35b8d35db2b12d11dd1df21fb86afaf7f8
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 225 |
sce
|
12.sce
|
clc
clear
//input
r100=6.9//resistence of steam
r0=5.8 //resistece of ice
t=550 //temperature
//calculation
r=(t*(r100-r0))/100 +5.8//platinum resistance thermometre
//output
printf("the resistence is %3.3f ohm",r)
|
6edab78428736214f3b2601f8dd48671eb17cc54
|
8781912fe931b72e88f06cb03f2a6e1e617f37fe
|
/scilab/gr_harm/condor/test1/out/fluxes.sce
|
23dda5965fd3784ad96d7d5d9311697b0195fd0f
|
[] |
no_license
|
mikeg2105/matlab-old
|
fe216267968984e9fb0a0bdc4b9ab5a7dd6e306e
|
eac168097f9060b4787ee17e3a97f2099f8182c1
|
refs/heads/master
| 2021-05-01T07:58:19.274277 | 2018-02-11T22:09:18 | 2018-02-11T22:09:18 | 121,167,118 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 3,289 |
sce
|
fluxes.sce
|
function [fxxx,fxxy,fxxz,fxyy,fxyz,fxzz,...
fyxx,fyxy,fyxz,fyyy,fyyz,fyzz,...
fzxx,fzxy,fzxz,fzyy,fzyz,fzzz...
]=fluxes(...
nx,ny,nz,...
x,y,z,r,psi,...
alp,cux,cuy,cuz,rg,...
uxx,uxy,uxz,uyy,uyz,uzz,...
gxx,gxy,gxz,gyy,gyz,gzz,...
qxx,qxy,qxz,qyy,qyz,qzz,...
dxuxx,dxuxy,dxuxz,dxuyy,dxuyz,dxuzz,...
dyuxx,dyuxy,dyuxz,dyuyy,dyuyz,dyuzz,...
dzuxx,dzuxy,dzuxz,dzuyy,dzuyz,dzuzz...
)
//[fxxx,fxxy,fxxz,fxyy,fxyz,fxzz,...
// fyxx,fyxy,fyxz,fyyy,fyyz,fyzz,...
// fzxx,fzxy,fzxz,fzyy,fzyz,fzzz...
// ]=fluxes(...
// nx,ny,nz,...
// x,y,z,r,psi,...
// alp,cux,cuy,cuz,rg,...
// uxx,uxy,uxz,uyy,uyz,uzz,...
// gxx,gxy,gxz,gyy,gyz,gzz,...
// qxx,qxy,qxz,qyy,qyz,qzz,...
// dxuxx,dxuxy,dxuxz,dxuyy,dxuyz,dxuzz,...
// dyuxx,dyuxy,dyuxz,dyuyy,dyuyz,dyuzz,...
// dzuxx,dzuxy,dzuxz,dzuyy,dzuyz,dzuzz,...
// )
//==============================================================================
//
// [ROUTINE NAME] Fluxes
// [AUTHOR] Joan Masso, NCSA & UIB
//
// [PURPOSE] Compute the fluxes of the equations
//
// [ARGUMENTS]
// [INPUT]
// nx,ny,nz : grid sizes of the 3d cube.
// Full list of grid and metric arrays
// [OUTPUT]
// fxxx,fxxy,... : fluxes of the qxx,..., as they are the only
// variables with "complicated" fluxes.
// That is, F^k_{ij} of the $q^{ij}$
//
// [INCLUDES] metric.h declares all the passed grid and metric arrays.
//
// [CALLED BY] Method
//
//<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<
//c ******* q fluxes *******
fxxx = alp.*rg.*(2.*cux.*uxx + dxuxx.*uxx + dyuxx.*uxy + dzuxx.*uxz);
fxxy = alp.*rg.*(cuy.*uxx + dxuxy.*uxx + cux.*uxy + dyuxy.*uxy + dzuxy.*uxz);
fxyy = alp.*rg.*(dxuyy.*uxx + 2.*cuy.*uxy + dyuyy.*uxy + dzuyy.*uxz);
fxxz = alp.*rg.*(cuz.*uxx + dxuxz.*uxx + dyuxz.*uxy + cux.*uxz + dzuxz.*uxz);
fxyz = alp.*rg.*(dxuyz.*uxx + cuz.*uxy + dyuyz.*uxy + cuy.*uxz + dzuyz.*uxz);
fxzz = alp.*rg.*(dxuzz.*uxx + dyuzz.*uxy + 2.*cuz.*uxz + dzuzz.*uxz);
fyxx = alp.*rg.*(2.*cux.*uxy + dxuxx.*uxy + dyuxx.*uyy + dzuxx.*uyz);
fyxy = alp.*rg.*(cuy.*uxy + dxuxy.*uxy + cux.*uyy + dyuxy.*uyy + dzuxy.*uyz);
fyyy = alp.*rg.*(dxuyy.*uxy + 2.*cuy.*uyy + dyuyy.*uyy + dzuyy.*uyz);
fyxz = alp.*rg.*(cuz.*uxy + dxuxz.*uxy + dyuxz.*uyy + cux.*uyz + dzuxz.*uyz);
fyyz = alp.*rg.*(dxuyz.*uxy + cuz.*uyy + dyuyz.*uyy + cuy.*uyz + dzuyz.*uyz);
fyzz = alp.*rg.*(dxuzz.*uxy + dyuzz.*uyy + 2.*cuz.*uyz + dzuzz.*uyz);
fzxx = alp.*rg.*(2.*cux.*uxz + dxuxx.*uxz + dyuxx.*uyz + dzuxx.*uzz);
fzxy = alp.*rg.*(cuy.*uxz + dxuxy.*uxz + cux.*uyz + dyuxy.*uyz + dzuxy.*uzz);
fzyy = alp.*rg.*(dxuyy.*uxz + 2.*cuy.*uyz + dyuyy.*uyz + dzuyy.*uzz);
fzxz = alp.*rg.*(cuz.*uxz + dxuxz.*uxz + dyuxz.*uyz + cux.*uzz + dzuxz.*uzz);
fzyz = alp.*rg.*(dxuyz.*uxz + cuz.*uyz + dyuyz.*uyz + cuy.*uzz + dzuyz.*uzz);
fzzz = alp.*rg.*(dxuzz.*uxz + dyuzz.*uyz + 2.*cuz.*uzz + dzuzz.*uzz);
endfunction
|
e3c59a419aae525791404386893264ddfa686746
|
777ac7fa75f240739af167655f7fab95cba80ef6
|
/docs/Basics.New/Goto.tst
|
8c0af2f1461af18f27651c554267fa2402664f31
|
[] |
no_license
|
Karabur/TML-project
|
8d498d8133f4b1ea8e8c3fe6f6f47f7ab5de4b5c
|
0bfe006b0e66628427b769bc1be903875e77d5b7
|
refs/heads/master
| 2021-01-02T09:20:39.055827 | 2013-12-28T22:02:15 | 2013-12-28T22:02:15 | null | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,538 |
tst
|
Goto.tst
|
Title:
TestName: Проверка примитива Goto;
Difficulty: A1;
FullTime: 0;
Questions: 3;
EndTitle.
StartTest:
Question: 1;
Weight: 1.0;
BeginText:
Тест намеренно зациклен следующим образом первый вопрос, второй вопрос.
Чтобы остановиться выберите пункт меню Файл/закрыть тест.
EndText;
Choice:
AtX: 8;
AtY: 8;
Width: 100;
Height: 100;
1: правильно endcase;
2: ошибка endcase;
Right: 1;
Ask;
goto 2;
Question: 2;
Weight: 1.0;
BeginText:
Вопрос 2
Тест намеренно зациклен следующим образом первый вопрос, второй вопрос.
Чтобы остановиться выберите пункт меню Файл/закрыть тест.
EndText;
Choice:
AtX: 8;
AtY: 8;
Width: 100;
Height: 100;
1: правильно endcase;
2: ошибка endcase;
Right: 1;
Ask;
goto 1;
Question: 3;
Weight: 1.0;
BeginText:
Вопрос 3.
При правильной работе системы Вы этот вопрос никогда не увидите
Тест намеренно зациклен следующим образом первый вопрос, второй вопрос.
Чтобы остановиться выберите пункт меню Файл/закрыть тест.
EndText;
Choice:
AtX: 8;
AtY: 8;
Width: 100;
Height: 100;
1: правильно endcase;
2: ошибка endcase;
Right: 1;
Ask;
EndTest.
|
f897698f98de7c5be96b0c8473a41bb707ed0990
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2102/CH1/EX1.8/exa_1_8.sce
|
4aa61befabf12924bf50e71e5fb573e532f18145
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 621 |
sce
|
exa_1_8.sce
|
// Exa 1.8
clc;
clear;
close;
// Given data
format('v',13)
d= 2;// in mm
d=d*10^-3;//in m
sigma= 5.8*10^7;// in s/m
miu_c= 0.0032;// in m^2/v-sec
E= 20;//in mV/m
E=E*10^-3;//in V/m
e= 1.6*10^-19;// in C
// Part (a)
n= sigma/(e*miu_c);//in /m^3
disp(n,"Charge density per meter cube is : ")
// Part (b)
J= sigma*E;//in A/m^2
disp(J,"Current density in A/m^2 is : ")
// Part (c)
Area= %pi*d^2/4;// in area of cross-section of wire in m^2
I= J*Area;// in A
disp(I,"Current flowing in the wire in amp is : ")
// Part (d)
v= miu_c*E;// in m/sec
disp(v,"Electron drift velocity in m/sec is : ")
|
d8a668fb6fac456f1c22fa1364621ef5c3d50227
|
244971ae8af51184d278cdc2be1c80775413adae
|
/SSSoEDFAgain.sci
|
2abd831f52a40ba522c9f9014c006de6df8f2dcb
|
[] |
no_license
|
MSCA-SIMFREE/748767
|
5879f1f139b608c7cd2f1bd62325b281c9c1e7d1
|
4726206e514f1e47e939e73b9339c056057866db
|
refs/heads/master
| 2020-12-27T15:21:13.646362 | 2020-02-03T11:40:00 | 2020-02-03T11:40:00 | 237,951,088 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 802 |
sci
|
SSSoEDFAgain.sci
|
// The code was developed under Horizon2020 Framework Programme
// Project: 748767 — SIMFREE
function [Out,P_dBm]=SSSoEDFAgain(In,G_dB)
// A simple optical amplifier
//
// Calling Sequence
// [Out,P_dBm]=SSSoEDFAgain(In,G_dB)
//
// Parameters
// In : Optical Input
// Out : Optical Output
// G_dB : small signal gain [dB]
// P_dBm : output power [dBm]
//
// Description
// A simple optical amplifier model with constant gain
// The amplifier gain is flat with wavelength.
//
[lhs,rhs]=argn(0);
select rhs
case 0 then
error("Expect at least one argument");
case 1 then
G_dB=0;
end
Pin=sum(real(In.*conj(In)));
G=sqrt(10^(G_dB/10));
Out=G*In;
P_dBm=10*log10(G*Pin);
endfunction
|
7667d72bc135c0677cc6a4109139ca9635944614
|
397456b742a46d88c251aa168bfe794903987f93
|
/Butterfly Optimization Algorithm/standard/scilab/butterfly-oa.sce
|
7d7bde2de322ce94e9db0164429fbfe6a2e0e448
|
[] |
no_license
|
JonesCG/PROJECT-NIOA
|
b5dcc7820d818369a4115fbb34b0f7ba02d7a129
|
7e6a3aa9a5deda6aa4eec9f4d523556844593c8b
|
refs/heads/master
| 2022-08-16T14:06:54.967718 | 2020-05-18T08:17:47 | 2020-05-18T08:17:47 | 264,872,793 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,929 |
sce
|
butterfly-oa.sce
|
clc
clear
exec('objective.sce');
disp('RUNNING...')
rand('seed',getdate('s'))
POPSIZE = 50
DIM = 2
UPPER = 100
LOWER = -100
MAXITER = 50
a = 0.1 // power exponent
c = 0.01 // sensory modality
prob = 0.5 // or 0.8 // switch probability
BUTTERFLY = rand(POPSIZE,DIM).*(UPPER-LOWER)+LOWER
FIT = F1(BUTTERFLY)
[BESTFIT IND] = min(FIT, 'r')
GBESTPOS = BUTTERFLY(IND,:)
GBESTFIT = BESTFIT
xtitle("INITIALIZATION")
square(LOWER,LOWER,UPPER,UPPER)
plot(BUTTERFLY(:,1),BUTTERFLY(:,2),'b.')
plot(GBESTPOS(:,1),GBESTPOS(:,2),'g.')
xs2png(gcf(),'gif/boa/ITER0.png')
clf()
for ITER=1:MAXITER
//CALCULATE FRAGRANCE
FRAG = (FIT.^a).*c
RANDOM = rand(POPSIZE,1)
IND1 = find(RANDOM<prob)
IND2 = find(RANDOM>=prob)
if length(IND1)>0
R1 = rand(length(IND1),DIM)
DIST1 = (R1.^2).*repmat(GBESTPOS,[length(IND1) 1]) - BUTTERFLY(IND1,:)
STEP1 = DIST1.*repmat(FRAG(IND1),[1 DIM])
BUTTERFLY(IND1,:) = BUTTERFLY(IND1,:) + STEP1
end
if length(IND2)>0
INDRAND = grand(1,'prm',(1:POPSIZE)')
R2 = rand(length(IND2),DIM)
DIST2 = (R2.^2).*BUTTERFLY(INDRAND(1:length(IND2)),:) - BUTTERFLY(INDRAND(1:length(IND2)),:)
STEP2 = DIST2.*repmat(FRAG(IND2),[1 DIM])
BUTTERFLY(IND2,:) = BUTTERFLY(IND2,:) + STEP2
end
BUTTERFLY = ammend(BUTTERFLY,UPPER,LOWER)
FIT = F1(BUTTERFLY)
[BESTFIT IND] = min(FIT,'r')
if BESTFIT < GBESTFIT
GBESTFIT = BESTFIT
GBESTPOS = BUTTERFLY(IND,:)
end
a = 0.1 - (0.1-0.3)*(ITER/MAXITER) // UPDATE POWER EXPONENT
c = c + 0.025/(c*MAXITER)
FITRUN(ITER) = GBESTFIT
//gcf().axes_size = [500 500]
xtitle("ITER "+string(ITER))
square(LOWER,LOWER,UPPER,UPPER)
plot(BUTTERFLY(:,1),BUTTERFLY(:,2),'b.')
plot(GBESTPOS(:,1),GBESTPOS(:,2),'g.')
xs2png(gcf(),'gif/boa/ITER'+string(ITER)+'.png')
clf()
end
//plot((1:MAXITER)',FITRUN,'g-')
|
d5c9a5f277e0c3638fafb50756b10d4c65ff5078
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1919/CH6/EX6.16/Ex6_16.sce
|
104649b86d7eb7dbebd172dcfc987bd0d53e96e2
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,359 |
sce
|
Ex6_16.sce
|
// Theory and Problems of Thermodynamics
// Chapter 6
// Thermodynamic Potentials and Availability
// Example 16
clear ;clc;
//Given data
Ng = 10 // moles of a gas in kmol
T1_g = 700 // initial temperature of gas in K
T2_g = 320 // final temperature of gas in K
T1_a = 300 // air inlet temperature in K
T2_a = 330 // air outlet temperature in K
T0 = 298 // ambient temperature in K
Pa = 0.1 // ambient pressure in MPa
R = 8.314 // gas constant
Cp = 3.5*R // specific heat ratio of gas and air
// Calculations
E_g_a = Ng*Cp*(T1_g-T2_g) // Energy transfered from gas to air
Na = E_g_a/(Cp*(T2_a-T1_a)) // number moles of air
// change in availability of air
C_a = Na*(Cp*(T2_a-T1_a)-T0*Cp*log(T2_a/T1_a))
C_a = C_a * 1e-3 // units conversion from kJ/s to MJ/s
// change in availability of gas
C_g = Ng*(Cp*(T2_g-T1_g)-T0*Cp*log(T2_g/T1_g))
C_g = C_g * 1e-3 // units conversion from kJ/s to MJ/s
// loss in available energy
L_E = -C_g - C_a
// Output Results
mprintf('(a) Change in availability of air = %4.3f MJ/s' ,C_a);
mprintf('\n (b) Change in availability of gas = %4.3f MJ/s' ,C_g);
mprintf('\n (c) loss in availability of energy = %4.2f MJ/s' ,L_E);
|
1521b156fb3a204a4d63c17f11102126bb9cb4a7
|
08bfc8a1f8e44adc624d1f1c6250a3d9635f99de
|
/SDKs/swig/Examples/test-suite/scilab/struct_rename_runme.sci
|
482f49c61eb44eba9dfb50eae134b21175d638f1
|
[] |
no_license
|
Personwithhat/CE_SDKs
|
cd998a2181fcbc9e3de8c58c7cc7b2156ca21d02
|
7afbd2f7767c9c5e95912a1af42b37c24d57f0d4
|
refs/heads/master
| 2020-04-09T22:14:56.917176 | 2019-07-04T00:19:11 | 2019-07-04T00:19:11 | 160,623,495 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 128 |
sci
|
struct_rename_runme.sci
|
version https://git-lfs.github.com/spec/v1
oid sha256:a02063d3b77def630ab140dba81444aa27034665a13b810a5111f1df520d4790
size 182
|
093555e3513e1d4400bb12acf315de19986fb454
|
da5b40d917ec2982828bd9bdf06b18b7bf189f26
|
/sim/cmd/test/langs.tst
|
813ec645ab5318bd38180e97318e15f4263e207d
|
[] |
no_license
|
psy007/NNPC-CHEMICAL-SIM-
|
4bddfc1012e0bc60c5ec6307149174bcd04398f9
|
8fb4c90180dc96be66f7ca05a30e59a8735fc072
|
refs/heads/master
| 2020-04-12T15:37:04.174834 | 2019-02-06T10:10:20 | 2019-02-06T10:10:20 | 162,587,144 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 647 |
tst
|
langs.tst
|
language Spanish
$thermo = VirtualMaterials.Advanced_Peng-Robinson
. -> $thermo
cd thermo
/thermo + PROPANE ISOBUTANE n-BUTANE
language Portuguese
/thermo - ISOBUTANE n-BUTANE
/thermo + ETHANE ISOBUTANE
language French
/thermo + n-BUTANE ISOPENTANE
cd $
cd $
thermo2 = VirtualMaterials.RK
cd thermo2
$thermo2 + PROPANE ISOBUTANE n-BUTANE
language Malay
$thermo2 - ISOBUTANE
cd /
language Spanish
stream = Stream.Stream_Material()
cd stream
language Malay
/stream.In.T = 20
/stream.In.P = 101
cd /stream.In.Fraction
/stream.In.Fraction = 0.0 2 3 0.0 0.0
cd /
language Portuguese
mix = Mixer.Mixer()
cd mix
/mix.In0 -> /stream.Out
language English
|
5c1c7f6a6a7ce5f3e4b1b33d323cf218e827dcea
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3809/CH8/EX8.4/EX8_4.sce
|
76dcbc22a48dbe2560324ddc95a9a1bd3966f27b
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 849 |
sce
|
EX8_4.sce
|
//Chapter 8, Example 8.4
funcprot()
clc
//Initialisation
p1=20 //gain
p2=30 //gain
p3=40 //gain
//initialising a function for gain
function [x]=pgain(a) //function for power gain
x=10**(a/10)
endfunction
function [x]=vgain(a) //function for voltage gain
x=10**(a/20)
endfunction
//calling a functions
[pd1]=pgain(p1)
[pd2]=pgain(p2)
[pd3]=pgain(p3)
[vd1]=vgain(p1)
[vd2]=vgain(p2)
[vd3]=vgain(p3)
//Result
printf("Power Gain (dB) of 20 = %.1f dB\n",pd1)
printf("Voltage Gain (dB) of 30 = %.1f dB\n\n",vd1)
printf("Power Gain (dB) of 40 = %.1f dB\n",pd2)
printf("Voltage Gain (dB) of 20 = %.1f dB\n\n",vd2)
printf("Power Gain (dB) of 30 = %.1f dB\n",pd3)
printf("Voltage Gain (dB) of 40 = %.1f dB\n",vd3)
|
b9dbbbb1a22b882ef7d4e6e0959f352b62ef9762
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3860/CH3/EX3.7/Ex3_7.sce
|
18f53b0be60e674339892002843cae796223fe2a
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 358 |
sce
|
Ex3_7.sce
|
//Example 3.7 Reduction using K-Map
clc; //clears the console window
clear; //clears the variable browser
disp('f = a''b''c + a''bc'' + a''bc + ab''c''')
disp('The mapping is shown below')
disp(' A''B'' A''B AB AB''')
disp('C'' 1 1 - 1')
disp('C - 1 - -') //The kmap for f is displayed//
disp('f = a''b + b''c''')
|
f056eac2a73f9dc1f9b0229fc5834ca287f7e04d
|
23314c7f41e73d972d0c32ef5e7a202967e3e7fb
|
/Code/sacred_new_prg.sce
|
98e5d1e0dce25c54adbb40a0f20d4eb060b88933
|
[
"MIT"
] |
permissive
|
eyantra/CS684_Re--Plantation-bot_2013
|
aaa5742fc39d2b690816bfe75405dee0e13facc3
|
4ed104aae46ec6efd3c27ccb88783e26e49f217c
|
refs/heads/master
| 2020-04-29T02:15:31.538554 | 2019-10-16T10:06:23 | 2019-10-16T10:06:23 | 20,951,259 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 3,401 |
sce
|
sacred_new_prg.sce
|
clc;
getd('./functions') //adding the functions directly. location of all my function files
h = openserial(4,"9600,n,8,1"); // open serial port
//avicloseall(); //closing all open camera ports
//n = camopen(0); //opening the camera
//for i=1:20 //looping to provide enough time for camera to initialize before capturing image
//image0 = avireadframe(n); //reading image from camera
//image0 = imread('real.jpg');
//imshow(image0);
//end
//imshow(image0);
//closing the open camera port
//h=openserial(4,"9600,n,8,1");
detected=0;
while(detected==0)
avicloseall();
//disp(detected);
//detected = 0;
n=camopen(0);
for i=1:10
im = avireadframe(n);
imshow(im);
end;
//imread('real.jpg');
imshow(im);
//avilistopened();
avicloseall();
il=imwrite(im,"catch.jpg")
image0=im;
imshow(image0);
orig_image = image0
imagegray = rgb2gray(image0); //converting color image to grayscale
//imshow(imagegray);
i2 = uint8(255*ones(size(imagegray,1),size(imagegray,2)));
inverted_image = i2-uint8(imagegray); //complementing the grayscale image
//imshow(inverted_image);
//imshow(i2);
i1 = inverted_image;
threshold = CalculateOtsuThreshold(i1); //calculating threshold for the given image
//imshow(threshold);
disp(threshold,'threshold');
seg_image = SegmentByThreshold(i1,threshold+20); //segmenting the image based on the threshold calculated above
imshow(seg_image);
blobimage = SearchBlobs(seg_image); //searching segments for blobs
//imshow(blobimage);
//[CumulatedSizeHistogram Listofsizes] = CumulatedSizeHistogram(blobimage);
//figure();plot(Listofsizes,CumulatedSizeHistogram);
filteredimage = FilterBySize(blobimage,40); //filtering out blobs that are too small.
figure();ShowImage(filteredimage,'image is filtered',jetcolormap(4))
//Iscalculated = CreateFeatureStruct();
Iscalculated = CreateFeatureStruct(%f);
//Iscalculated.BoundingBox = %t;
Iscalculated.Centroid = %t;
Blobstatistics = AnalyzeBlobs(filteredimage,Iscalculated);
Figurewindow = ShowColorImage(image0,'image with boxes');
plot(Blobstatistics(1).Centroid(1),Blobstatistics(1).Centroid(2),'r*');
//disp("color",getcolor(image0);
//DrawBoundingBoxes(Blobstatistics,[0 0.5 0],Figurewindow);
disp("centroid",Blobstatistics(1).Centroid(1),Blobstatistics(1).Centroid(2));
if Blobstatistics(1).Centroid(1) > 121 then
detected =1;
end
//h=openserial(4,"9600,n,8,1");
if detected == 0 then
writeserial(h,"8"); // sending command to move bot 2 cm
else
writeserial(h,"1"); //sending command that bot is detected now collect the plant
end
//xpause(200000);
//buf = readserial(h);
//xpause(200000);
//disp(buf);
//mprintf("buffer %d",buf);
disp(detected);
end
closeserial(h);
|
cb1e6d9728adf6873c86079b17ec8a62d9b388eb
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/24/CH8/EX8.2/Example8_2.sce
|
efe8e106c2aecbf9c071c8cbac37987b48a5e094
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 634 |
sce
|
Example8_2.sce
|
//Given that
mass = 2 //in kg
y1 = 5 //in meter
g = 9.8 //in m/s^2
ref = [0, 3, 5, 6]
//Sample Problem 8-2a
printf("**Sample Problem 8-2a**\n")
for x = ref
U = mass* g* (y1 - x)
printf("The potential energy at y1 is %dJ if reference is assumed to be at y=%d\n", U, x)
end
//sample Probelm 8-2b
printf("\n**Sample Problem 8-2b**\n")
y2 = 0
//The change in potential energy doesn't depend on choice of reference
deltaY = y2 - y1
//because the deltaY doesn't depend upon the choice of references
deltaU = mass* g* deltaY
printf("The change in potential energy is %dJ same for all the references", deltaU)
|
375506afe13fa99ea1304c45be096b8d09cfaf9c
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2354/CH4/EX4.3/4_3.sce
|
12d9fd69ac80d8540cc768c4a9708b4e83616ebd
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 202 |
sce
|
4_3.sce
|
//example 4.3
clc; funcprot(0);
// Initialization of Variable
V=10.0;//ft^3
v1=26.8;//ft^3/lb
u1=1077.6;//btu/lb
u2=1161.6;//Btu/lb;
m=V/v1;
W=-m*(u2-u1);
disp(W,"Work done in Btu");
clear()
|
1eef73b8ff170d4996dcfbe6cc9d6bed3b69fe8c
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1301/CH1/EX1.4/ex1_4.sce
|
d2a6fec3a12ae579d1a4cbdaa32459490be8448b
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 47 |
sce
|
ex1_4.sce
|
clc;
disp((460*0.00003*100000)/(9000*0.0062));
|
77c1ebbc226e8ede82db2fad1c5e0c8c91797c96
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1529/CH15/EX15.13/15_13.sce
|
5c3ecdc55d1627ddd1c59d0ec2dcac058d87b443
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 562 |
sce
|
15_13.sce
|
//Chapter 15, Problem 13
clc;
R=25; //resistance in ohm
C=45e-6; //capacitance in farad
V=240; //supply voltage
f=50; //supply frequency
Xc=1/(2*%pi*f*C); //capacitive reactance
Z=sqrt(R^2+Xc^2); //impedance
I=V/Z; //current
a=atan(Xc/R);
printf("(a) Impedance, Z = %.2f ohm\n\n",Z);
printf("(b) Current, I = %.2f A\n\n",I);
printf("Phase angle between the supply voltage and current, = %.2f deg (leading)\n\n",a*(180/%pi));
|
e371b493418dc87d0bee25a6047240f7e5bcc528
|
5c4a19e674d3d4c9f8714cc056d7597a0f9cab51
|
/Experiment_2.sce
|
d0d1503c7fff069df1caaaf866435f185820cd26
|
[] |
no_license
|
idyczko/Graduate_Project
|
f1fa672fd22b894d16f4ec82d101e13b624b1e56
|
aced90cd634af106df651dd8761744a38cd1f7a1
|
refs/heads/master
| 2021-01-10T10:19:25.994422 | 2016-03-01T21:42:17 | 2016-03-01T21:42:17 | 44,832,960 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 2,206 |
sce
|
Experiment_2.sce
|
xdel(winsid());
clear;
File = mgetl("frequency_double_measurement.txt");
Vector = evstr(File);
len= size(Vector);
frequency = len(2)/20;
time_stamp = 10000/frequency;
File = mgetl("Experiment_2_top.txt");
Vector = evstr(File);
Vector=Vector(131:length(Vector));
time_axis = 0:time_stamp/10000:length(Vector)*time_stamp/10000/2;
f = linspace(0,frequency,length(time_axis));
n = length(time_axis);
top=Vector(1:2:length(Vector));
bottom=Vector(2:2:length(Vector));
plot(time_axis(1:length(top)),top, 'b');
a=gca();
a.font_size=3;
xgrid(1, 1, 7);
mtlb_axis([0,5,-80,80]);
title("Wykres sygnału górnego akcelerometru", "fontsize",5);
xlabel("Czas [s]", "fontsize",5);
ylabel("Przyśpieszenie [m/s^2]", "fontsize",5);
figure;
plot(time_axis(1:length(bottom)),bottom, 'r');
title("Wykres sygnału dolnego akcelerometru", "fontsize",5);
a=gca();
a.font_size=3;
xgrid(1, 1, 7);
mtlb_axis([0,5,-80,90]);
xlabel("Czas [s]", "fontsize",5);
ylabel("Przyśpieszenie [m/s^2]", "fontsize",5);
figure;
X=fft(top)./(length(top)/2);
plot(f(1:n/2),abs(X(1:n/2)), 'b');
a=gca();
a.font_size=3;
xgrid(1, 1, 7);
title("Charakterystyka częstotliwościowa sygnału", "fontsize",5);
xlabel("Częstotliwość [Hz]", "fontsize",5);
ylabel("Moduł widma", "fontsize",5);
figure;
hz = iir(8,'lp','butt',6/frequency,[]);
[hzm,fr]=frmag(hz,256);
fr2 = fr.*frequency;
plot(f(1:n/2),abs(X(1:n/2)),fr2,hzm);
a=gca();
a.font_size=3;
xgrid(1, 1, 7);
title("Charakterystyka częstotliwościowa sygnału oraz filtra", "fontsize",5);
xlabel("Częstotliwość [Hz]", "fontsize",5);
ylabel("Moduł widma", "fontsize",5);
figure;
y = flts(top,hz);
Y = fft(y)./(length(top)/2);
plot(f(1:n/2),abs(Y(1:n/2)));
a=gca();
a.font_size=3;
xgrid(1, 1, 7);
xlabel("Częstotliwość [Hz]", "fontsize",5);
ylabel("Moduł widma", "fontsize",5);
title("Charakterystyka częstotliwościowa przefiltrowanego sygnału", "fontsize",5);
figure;
plot(time_axis(1:length(y)), y);
a=gca();
a.font_size=3;
xgrid(1, 1, 7);
mtlb_axis([0,5,-80,80]);
xlabel("Czas [s]", "fontsize",5);
ylabel("Przyśpieszenie [m/s^2]", "fontsize",5);
title("Wykres przefiltrowanego sygnału górnego akcelerometru", "fontsize",5);
figure;
plot(time_axis, sin(time_axis));
|
34ad91f13d6c827086036c2c572efa81c2cdf376
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/605/CH9/EX9.10/9_10.sce
|
2a5d341b83a98752dcfc2de8d99c72d47dcbf325
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 495 |
sce
|
9_10.sce
|
fl=10*10^6
fu=40*10^6
Wu=2*%pi*40*10^6
Wl=2*%pi*10*10^6
gc=0.9662
gL=0.62425
Wo=2*%pi*20*10^6
fo=sqrt(fl*fu)
printf("\nfo=%.2e Hz",fo)
CBP1=(Wu-Wl)/(Wo^2*gL)
LBP1=gL/(Wu-Wl)
printf("\nCBP1=%.3e F\nLBP1=%.4e H",CBP1,LBP1)
CBP2=(Wu-Wl)/(Wo^2*gc)
LBP2=gc/(Wu-Wl)
printf("\nCBP2=%.3e F\nLBP2=%.4e H",CBP2,LBP2)
printf("\nC1=C3=%.2f pF",19.122*1000/75)
printf("\nL1=L3=%.4f nH",75*3.3116)
printf("\nL2=%.4f uH",75*12.354/1000)
printf("\nC2=%.3f pF",5.1258/75*1000)
|
4b86d6665c09b363882732cb3cb1b8e821dac217
|
3a031f437fdd7426aec9731b31871506b540c723
|
/Pract8_1.sce
|
9c561e44ee6392e47270253733b2f6ee579b3f32
|
[] |
no_license
|
mohammedkesury/Digital-Image-Processing
|
006294df3c05100912ade8f75dcadc59f518cbba
|
6589dcf0f400a803862fcd2194ff4b008ceb795e
|
refs/heads/master
| 2020-04-20T05:20:20.161398 | 2019-04-09T16:04:04 | 2019-04-09T16:04:04 | 168,653,548 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 157 |
sce
|
Pract8_1.sce
|
a=imread('D:\TYCS 37\DIP\letter1.bmp')
figure
imshow(a)
b=[1 1 1;1 1 1;1 1 1]
c=imdilate(a,b)
figure
imshow(c)
d=imerode(a,b)
figure
imshow(d)
|
e945bfcce8e29f97415dd9e0f7c5c20c094c5dbf
|
62e6605ab494919b6833bf1a1b158bcb6f9b79df
|
/predict.sci
|
ec84de1c27af280baee953fddd37366dcf0badfb
|
[] |
no_license
|
mani1250/system-identification
|
c597c26d10bb5dd62b1b4db650b3945afc336e37
|
5db0536c792dfaa4a8f01561315263503ff34d3d
|
refs/heads/master
| 2021-01-12T06:56:00.703593 | 2017-03-07T12:18:15 | 2017-03-07T12:18:15 | 76,865,655 | 0 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,365 |
sci
|
predict.sci
|
function ypred = predict(x,data,nahead)
// x is an idpoly object
[lhs,rhs] = argn(0);
if(rhs<3)
nahead = 1;
end
y = data(:,1);
// make sure that data has output signal in its first coloumn
u = data(:,2);
// make sure that data has input signal in its second colou
k = x.ioDelay;
b = [zeros(1,k) x.B];
a = x.F1;
G = struct('b',b,'a',a)
[det_sys,zf] = filter(b,a,u);
if(x.Type=="oe" | nahead == %inf)
ypred = det_sys;
else
Hden = x.A*x.D;
Hinv = [Hden x.C]
[filtered,zf] = filter(Hden,x.C,(y-det_sys));
if(nahead~=1)
H = coeff(poly(x.C,'m')*polyinv(Hden,nahead));
h1 = H(1:nahead);
[filtered,zf] = filter(h1(1),h1(2),filtered);
end
ypred = y - filtered;
end
endfunction
function X = polyinv(x,k)
p1 = poly(x,'m','coeff');
p2 = roots(p1);
p3 = real(p2)
p4 = 1./p3;
z = inverse(p4,k);
z1 = [];
for(i = 1 : size(z,'r'))
z1 = [z1;poly(z(i,:),'x','coeff')];
end
temp = z1(1)
if(length(z1)>1) then
for(i = 2:length(z1))
temp = temp*z(i)
end
end
X = temp;
endfunction
function X = inverse(y,k)
X = [];
for(i=1:k-1)
X = [X y.^(i-1)]
end
endfunction
|
e0bd0696f4d3dbe24fa923ecabae801c6c0707fa
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/174/CH6/EX6.3/example6_3.sce
|
750ee3a64fe4e17ba629dfabd347e566237ea55b
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 998 |
sce
|
example6_3.sce
|
// To find the maximum time
// Modern Electronic Instrumentation And Measurement Techniques
// By Albert D. Helfrick, William D. Cooper
// First Edition Second Impression, 2009
// Dorling Kindersly Pvt. Ltd. India
// Example 6-3 in Page 144
clear; clc; close;
// Given data
R = 100*(10^3); // Value of resistance in ohm
C = 0.1*(10^-6); // The value of integrating capacitor in F
V_ref = 2; // The reference voltage in V
V_out = 10; // The maximum limit of the output in V
//Calculations
T = R*C;
printf("The integrator time constant = %0.3f s\n",T);
V_s = V_ref/T; //Unit is V/s
V = 1/V_s;
printf("Therefore the integrator output = %0.3f s/V",V)
disp('Therefore to integrate 10V');
T_max = V*V_out; //The max time the ref voltage can be integrated
printf("The time required = %0.4f s",T_max);
//Result
// The integrator time constant = 0.010 s
// Therefore the integrator output = 0.005 s/V
// Therefore to integrate 10V
// The time required = 0.0500 s
|
de0c894e40bc11fd14bf514163d21f51b19f985c
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/2223/CH13/EX13.2/Ex13_2.sce
|
980d10dae6e3823d889e4143c615794511d15ed0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,718 |
sce
|
Ex13_2.sce
|
// scilab Code Exa 13.2 Mach Number and loss coefficient
t=650; // in degree C
T01=t+273; // in Kelvin
p3=1; // Exit Pressure in bar
gamma=1.4;
sigma=0.66; // blade-to-isentropic speed ratio
N=16e3; // rotor Speed in RPM
b2=5/100; // blade height at entry in m
alpha_2=20; // air angle at nozzle exit
d_r=0.45; // rotor diameter ratio(d3/d2)
p01_3=3.5; // total-to-static Pressure Ratio(p01/p3)
n_N=0.95; // Nozzle Efficiency
cp=1005; // Specific Heat at Constant Pressure in J/(kgK)
R=287;
n=(gamma-1)/gamma;
c_0=sqrt(2*cp*T01*(1-(p01_3^(-n))))
u_2=sigma*c_0;
Mb0=u_2/sqrt(gamma*R*T01);
// part(a) Mach number at nozzle exit
M2=Mb0/(cosd(alpha_2)*sqrt(1-(0.5*(gamma-1)*(Mb0^2)*(secd(alpha_2)^2))));
disp(M2,"(a)the flow Mach number at nozzle exit M2=")
// part(b)rotor exit Relative Mach number
d2=60*u_2/(%pi*N);
d3=d2*d_r;
c_r2=u_2*tand(alpha_2);
u3=%pi*d3*N/60;
beta3=atand(c_r2/u3);
w3=u3/(cosd(beta3));
T03=T01-((u_2^2)/cp);
T3=T03-((c_r2^2)/(2*cp));
a3=sqrt(gamma*R*T3);
M3_rel=w3/a3;
disp(M3_rel,"(b)the Relative Mach number at rotor exit is")
// part(c) Nozzle enthalpy loss coefficient
T2=T3+((0.5*(u_2^2))/cp);
c2=u_2/(cosd(alpha_2));
T2s=T01-((0.5*(c2^2))/(cp*n_N));
c2=u_2/(cosd(alpha_2));
zeeta_N=cp*(T2-T2s)/(0.5*(c2^2));
disp(zeeta_N,"(c)the Nozzle enthalpy loss coefficient is")
// part(d)rotor enthalpy loss coefficient
p01_2=(1-(((0.5*(c2^2))/(cp*n_N))/T01))^(-1/n);
p01=p3*p01_3;
p2=p01/p01_2;
T3s=T2/((p2/p3)^n);
zeeta_R=cp*(T3-T3s)/(0.5*(w3^2));
disp(zeeta_R,"(d)the rotor enthalpy loss coefficient is")
disp("comment: Nozzle enthalpy loss coefficient value is not correctly calculated in the textbook. the above value is correct.")
|
6e7f7daa441b4c4c9dffe46036c07cc2e15d3353
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/446/CH8/EX8.2/8_2.sce
|
2c0e8fb7a62947efcdd2aabf88018b70ad79c1a6
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 365 |
sce
|
8_2.sce
|
clear
clc
disp('Exa-8.2(a)');
EKa=21.990;EKb=25.145;EK=25.514 //all the values are in KeV
ELo=EKb-EKa;printf('The enrgy of La of X-ray is %.3fKeV.\n',ELo); //Energy of La X-ray
disp('Exa-8.2(b)');
EL=-EK+EKa;printf('Hence the binding energy of the L electon is %.3fKeV.',EL); // for electron L electron
|
d36c4b23216fe39dfd773fbfe0163b52d0c410e7
|
b3c9357cd1290921e67444ae057761959fdf24f1
|
/Curso de programação com Scilab/códigos/bola.sce
|
2a9dc0ac99241fdbc360597aea37e39e55a068e6
|
[] |
no_license
|
joaolrneto/Scilab
|
91742520422426dc8a772997ef4a5d6376008b6e
|
f383f87e4585955cf19d0dae1b5c29f93c3f70b4
|
refs/heads/master
| 2023-02-05T20:13:03.677069 | 2020-12-30T14:53:09 | 2020-12-30T14:53:09 | 264,671,730 | 1 | 0 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 1,803 |
sce
|
bola.sce
|
clc
clear
close
conv=%pi/180; //conversão de radianos para graus
g=-9.81;//aceleração devido a gravidade
vo=20;//velocidade inicial
//cria um vetor para todas as distâncias
distancia=zeros(1,91);
//calcula as distâncias máximas
for ii=1:91
theta=ii-1;
vxo=vo*cos(theta*conv);
vyo=vo*sin(theta*conv);
max_tempo=-2*vyo/g;
distancia(ii)=vxo*max_tempo;
end
//escreve a tabela de saida das distâncias
printf('Distância versus ângulo theta :\n');
for ii=1:91
theta=ii-1;
printf('%2d %8.4f\n',theta, distancia(ii));
end
//calcula a distância máxima e ângulo
[maxdist,indice]=max(distancia);
maxangulo=indice - 1;
printf('\nDistância máxima = %8.4f a %2d graus. \n',maxdist, maxangulo);
//plota as trajetórias
for ii=5:10:85
//considera velocidade e tempo máximo para este ângulo
theta=ii;
vxo=vo*cos(theta*conv);
vyo=vo*sin(theta*conv);
max_tempo=-2*vyo/g;
//calcula as posições(x,y)
x=zeros(1,21);
y=zeros(1,21);
for jj=1:21
tempo=(jj-1)*max_tempo/20;
x(jj)=vxo*tempo;
y(jj)=vyo*tempo+0.5*g*tempo^2;
end
plot(x,y,'b');
//considera velocidade e tempo máximo para este ângulo
theta=ii;
vxo=vo*cos(theta*conv);
vyo=vo*sin(theta*conv);
max_tempo=-2*vyo/g;
//calcula as posições(x,y)
x=zeros(1,21);
y=zeros(1,21);
for jj=1:21
tempo=(jj-1)*max_tempo/20;
x(jj)=vxo*tempo;
y(jj)=vyo*tempo+0.5*g*tempo^2;
end
plot(x,y,'b');
end
//adiciona titulos e rótulos nos eixos
title('Trajetória da bola x ângulo theta');
xlabel('x(metros)');
ylabel('y(metros)');
mtlb_axis([0 45 0 25]);
mtlb_grid on
//plota a trajetoria para a distancia maxima
vxo=vo*cos(maxangulo*conv);
vyo=vo*sin(maxangulo*conv);
max_tempo=-2*vyo/g;
//calcula as posicoes (x,y)
x=zeros(1,21);
y=zeros(1,21);
for jj=1:21
tempo=(jj-1)*max_tempo/20;
x(jj)=vxo*tempo;
y(jj)=vyo*tempo+0.5*g*tempo^2;
end
plot(x,y, 'r','LineWidth',3.0);
|
d1a79a3096ee9893b31ca5e7262a68e76f2a764d
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1280/CH5/EX5.9/5_9.sce
|
c44d8a99f6f4cd8820dc53729e63b139e52df7a0
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 203 |
sce
|
5_9.sce
|
clc
//initialisation of variables
v= 27 //cp
s= 0.85
d= 1 //in
//CALCULATIONS
V= v/s
V1= V*0.001552
V2= 2000*V1/(12*d)
V3= 4000*V1/(12*d)
//RESULTS
printf ('Critical velocity = %.2f fps',V3)
|
27f02c0040b131f815914b8999c7bc0435d87dbd
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/1655/CH7/EX7.5.3/Example_7_5_3.sce
|
ff68835ff4f98c0083d0f16b721f48fab8472bed
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 516 |
sce
|
Example_7_5_3.sce
|
// Example 7.5.3 page 7.24
clc;
clear;
lamda1=1300d-9;
lamda2=1600d-9;
h=6.625d-34; //plank's constant
c=3d8; //speed of light
q=1.6d-19; //charge of electron
eta=90/100; //quantum efficiency
E=0.73; //energy gap in eV
R1=eta*q*lamda1/(h*c);
R2=eta*q*lamda2/(h*c);
lamdac=1.24/E;
printf("\nResponsivity at 1300nm is %.2f A/W.\nResponsivity at 1600nm is %.2f A/W.\nCut-off wavelength is %.1f micrometer.",R1,R2,lamdac);
//R1 is calculated as 0.92 in the book, deviation of 0.02.
|
f8c790837407aa62e3bfc201dd0665f3fdd7a510
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/3250/CH4/EX4.22/Ex4_22.sce
|
5de68f024cfd2b632fa2bf9eb43c3c0fd981261c
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 443 |
sce
|
Ex4_22.sce
|
clc
// Given that
d= 0.05 // Depth of cut in mm
f =200 // Feed rate in mm/min
theta = 850 // Surface temperature in °C
Theta = 700 // Maximum surface temperature of workpiece surface required to maintain in °C
// Sample Problem 22 on page no. 251
printf("\n # PROBLEM 4.22 # \n")
K = theta * (f^0.2)/(d^0.9)
r = Theta/K
C = d*f
Dm = (r*C^0.2)^(1/1.1)
fm = C/Dm
printf(" \n Required depth of cut = %f mm,\n Required feed = %d mm/min",Dm,fm)
|
8f360fcdae8ae4b1e8027582f4afdad3761e3385
|
eec3a6e2cd91307fd7a55b7fc83bb86b35f86a6c
|
/stlfiles/demos/ship_binary.sce
|
5bd52d759a2eae4885e07426afe679070101d4cf
|
[] |
no_license
|
Matthieu-71/PowerSubsystemSimulation
|
d1a5171ff763ca42db9d701f893d3ab257a1b882
|
cdcff61d4a11509f5d9023fb295af6b8092a3c66
|
refs/heads/master
| 2020-03-16T23:33:28.836945 | 2018-05-24T00:10:57 | 2018-05-24T00:10:57 | 133,082,402 | 2 | 2 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 213 |
sce
|
ship_binary.sce
|
stlpath = get_absolute_file_path("ship_binary.sce")
t = stlread(fullfile(stlpath, "ship.stl"), "binary");
figure
tcolor = 2*ones(1, size(t.x,"c"))
plot3d(t.x,t.y,list(t.z,tcolor));
a = gca()
a.isoview = "on"
|
c78c383f7c957211beadc25f4a4893367c0c5b77
|
449d555969bfd7befe906877abab098c6e63a0e8
|
/992/CH3/EX3.10/Ex3_10.sce
|
6caa12423164a9fbc304584403d140db390a39a9
|
[] |
no_license
|
FOSSEE/Scilab-TBC-Uploads
|
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
|
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
|
refs/heads/master
| 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null |
UTF-8
|
Scilab
| false | false | 275 |
sce
|
Ex3_10.sce
|
//Exa:3.10
clc;
clear;
close;
//Given:
mf=1.0;
Jo=0.77;
//According the bessels Function table
j1=0.44;
j2=0.11;
j3=0.02;
printf("\n Firstsideband pairs :J1 = %f",j1);
printf("\n Secondsideband pairs :J2 = %f",j2);
printf("\n Thirdsideband pairs :J3 = %f",j3);
|
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