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getd ../../common_files/ getd dc/scilab exec ../../common_files/loader.sce exec ser_init.sce exec prbs_pp.sci exec twodof_para.sce xcos prbs_pp.xcos
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//Find density of Copper //Ex:4.4 clc; clear; close; r=1.278;//radius of copper in angstorm //copper has FCC structure a=4*r/sqrt(2);//in angstorm disp(a,"a (in Angstorm) = "); a1=a*10^-8;//in cm aw=63.54;//atomic weight of copper ne=4;//fcc na=6.023*10^23;//Avagadro's no. p=aw*ne/(na*a1^3);//in g/cm^3 p1=10^3*p; disp(p1,"Density of Copper (in kg/cu m)");
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clear// //Variables VS = 24.0 //Source voltage (in volts) RS = 500.0 //Series resistance (in ohm) VZ = 12.0 //Zener Voltage (in volts) IZmin = 3.0 //Minimum Zener current (in milli-Ampere) IZmax = 90.0 //Maximum Zener current (in milli-Ampere) rZ = 0.0 //Zener resistance (in ohm) //Calculation IS = (VS - VZ) / RS //Current through RS (in Ampere) ILmax = IS - IZmin * 10**-3 //Maximum value of load Current (in Ampere) RLmin = VZ / ILmax //Minimum value of Load resistance (in ohm) //Result printf("\n Minimum value of load resistance is %0.0f ohm.",RLmin)
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clc(); clear; //To determine the signal attenuationnper kilometer pi=100; //mean optical power launched in micro meter po=5; //mean optical power at fibre output S=10*log10(pi/po); //signal attenuation un dB l=6; //length in km Sk=S/l //signal ayyenuation per kilometer printf("The signal attenuation per kilometer is %f dB/km",Sk);
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//Electric Power Generation, Transmission and Distribution by S.N.Singh //Publisher:PHI Learning Private Limited //Year: 2012 ; Edition - 2 //Example 4.3 //Scilab Version : 6.0.0 ; OS : Windows clc; clear; peak_dem_light=200; //Peak demand of the light load in kW max_dem_light=200; //Maximum demand of the light load in kW max_dem_rest=1800; //Maximum demand of the rest load in kW peak_dem_rest=1800; //Peak demand of the rest load in kW c_light=peak_dem_light/max_dem_light; //Contribution factor for street lighting load c_rest=peak_dem_rest/max_dem_rest; //Contribution factor for street rest load DF=(peak_dem_light+peak_dem_rest)/(c_light*max_dem_light+c_rest*max_dem_rest); //Diversity factor of the feeder CF=1/DF; //Coincidence factor of the load group printf("\nClass contribution factor for street lightning is %.1f and the remaining load is %.1f",c_light,c_rest); printf("\nDiversity factor of the feeder %.1f",DF); printf("\nCoincidence factor of the load group %.1f",CF);
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//[macr]=obs_cont(sysn) //[macr]=obs_cont(sysn) // //cette macro renvoit le systeme observe-commande //construit a partir du systeme sysn linearise autour de (xe,ue) // // sysn : chaine de caractere donnant le nom du systeme a commander // gaincom,gainobs : vecteurs colonnes des gains demandes // // Retour : une nouvelle macro donnant le syst\`eme observe-commande // [x1dot]=macr(t,x1,abruit,pas,n) // x1=[x;xchap], // pour l'appel il faudra creer un vecteur de bruit de nom br // d'autre part la macro cr\'ee va chercher dans l'environnement // global les valeurs de (xe,ue) le point d'equilibre // f,g,h les matrices du systeme linearise // l et k les deux matrices de gain // exemple : // pas=10;n=200; // br=rand(1,n) // ode([x0;xchap0],0,pas*(0:n),list(macr,1.0,pas,n)); //! deff('[zdot]=macr(t,z,abr,pas,n)',... ['u=ue-k(1)*(z(3)-xe(1))-k(2)*(z(4)-xe(2))'; 'ff_brui=abr*br(ent(mini(t/pas+1,n)))'; 'y=h(1)*z(1)+h(2)*z(2)+ff_brui'; 'xdot='+sysn+'(t,z(1:2),u)'; 'xdot1=f*(z(3:4)-xe) +g*(u-ue)-l*(h*z(3:4)-y)'; 'zdot=[xdot;xdot1]';]); //end
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clc p1=7*10^5; //N/m^2 T1=873; //K p2=1.05*10^5; //N/M62 n=1.25; m=1; //kg R=0.287; cp=1.005; T2=T1*(p2/p1)^((n-1)/n); // At constant temperature from 1 to A ds_1A=R*log(p1/p2); // At constant pressure from A to 2 ds_2A=cp*log(T1/T2); ds_12=ds_1A - ds_2A; disp("Increase in entropy = ") disp(ds_12) disp("kJ/kg.K")
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clc clear //Input data P1=10;//Pressure of steam in bar f=0.9;//Dryness fraction of steam At=350;//Throat area in mm^2 Pb=1.4;//Back pressure in bar h1=2574.8;//Enthalpy of steam at nozzle inlet from steam tables in kJ/kg ft=0.87;//Dryness fraction of steam at throat pressure fe=0.81;//Dryness fraction of steam at exit pressure ht=2481;//Enthalpy of steam at throat pressure at ft in kJ/kg vt=0.285;//Specific volume of steam at throat in m^3/kg he=2266.2;//Enthalpy of steam at exit conditions in kJ/kg ve=1.001;//Specific volume of steam at exit conditions in m^3/kg //Calculations Pt=0.582*P1;//Steam pressure at the throat in bar hd=h1-ht;//Enthalpy drop upto the throat in kJ/kg Vt=44.7*(hd)^(0.5);//Velocity of steam at the throat in m/s hde=h1-he;//Enthalpy drop from nozzle entrance to exit in kJ/kg Ve=44.7*(hde)^(0.5);//Velocity of steam at nozzle exit in m/s Ae=(At*Vt*ve)/(Ve*vt);//Exit area of nozzle from the mass rate of flow equation in mm^2 //Output printf('(a)Final exit velocity of steam is %3.1f m/s\n (b)Cross sectional area of the nozzle at exit for maximum discharge is %3.0f mm^2',Ve,Ae)
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s = poly(0, 's'); t = 0:0.01:10; Km = 10^-3; Kb = 5.5*10^-2; La = 10*10^-6; Ra = 0.2; Jm = 1*10^-3; Dm = 1*10^-2; //Gs = Km/((La*s + Ra)*(Jm*s^2 + Dm*s) + Km*Kb*s) Gs = Km/((Ra)*(Jm*s^2 + Dm*s) + Km*Kb*s) Gs1 = syslin('c', Gs); Ts = Gs1/(1+Gs1); den1 = denom(Ts); routh_t(den1); //plot(t,csim('step', t, Ts)) Wn = sqrt(5); Theta = 10.275/(2*Wn); Theta1 = -log(0.1)/sqrt(%pi^2 + log(0.1)^2) Theta2 = -log(0.2)/sqrt(%pi^2 + log(0.2)^2) evans(Gs1) sgrid([Theta1,Theta2],1) K = 2055 K1 = 15.1 K2 = 25.43 Ts = K*Gs1/(1+K*Gs1) Ts1 = K1*Gs1/(1+K1*Gs1) Ts2 = K2*Gs1/(1+K2*Gs1) //plot(t,csim('step', t, Ts),t,csim('step', t, Ts1),t,csim('step', t, Ts2)) xgrid()
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clc // initialization of variables V1=2 // initial volume in m^3 V2=0.2 // final volume in m^3 T1=20+273// temperature in kelvin P=200 // pressure in kPa R=0.287 // constant for air gama=1.4 // polytropic index for air Cv=0.717// specific heat at constant volume for air //solution //using the ideal gas equation m=(P*V1)/(R*T1) // mass in kg // process is adiabatic thus T2=T1*((V1/V2)**(gama-1))// final temperature W=-m*Cv*(T2-T1)// work from first law printf("The Work is "+string(W)+" kJ") // solution is approximated in textbook
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a=(8-4)-3 b=8-(4-3) disp('since a and b are not equal so subtraction is non-commutative on Z(set of integers)') a=[1 2;3 4] b=[5 6;0 -2] g= a*b k= b*a disp('since g and k are not equal matrix multiplication is non-commutative') h=(2^2)^3 j=2^(2^3) disp('since h and j are not equal so exponential operation is non associative on the set of positive integers N')
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clc clear //Initialization of variables gc=32.1739 //lbm ft/lbf s^2 m=10 //lbm a=10 //ft/s^2 //calculations F=m*a/gc //results printf("Force to accelerate = %.3f lbf",F)
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//Example No.2.2. // Page No.60. clc;clear; w = 632.8*10^(-9);//wavelength -[m]. h = 6.626*10^(-34);//Planck's constant. c = (3*10^(8));//Velocity of light. E = ((h*c)/(w));// Energy of one photon printf("\nThe energy of emitted photon in joules is %3.3e J",E); E = E/(1.6*10^(-19)); printf("\nThe energy of emitted photon in eV is %.2f eV",E);
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// 08.10.26 function Out=Viewfrom(varargin) global THETA PHI Nargs=length(varargin); Nvec=varargin(1); GL=varargin(2); Flg=1; if Nargs>=3 Flg=varargin(3); end; Theta=THETA; Phi=PHI; Tmp=Rotate3data(GL,Nvec,[-1,0,0]); THETA=%pi/2; PHI=0; Out=Projpara(Tmp); if Flg==1 Windisp(Out); end; THETA=Theta; PHI=Phi; endfunction;
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//Problem 23.01: In an electrical circuit the total impedance ZT is given by ZT = (Z1*Z2/(Z1 + Z2))+ Z3. Determine ZT in (a + jb) form, correct to two decimal places, when Z1 = 5 - j3, Z2 = 4 - i7 and Z3 = 3.9 - i6.7. //initializing the variables: Z1 = 5 - 3*%i; Z2 = 4 + 7*%i; Z3 = 3.9 - 6.7*%i; //calculation: ZT = (Z1*Z2/(Z1 + Z2))+ Z3 y = imag(ZT) x = real(ZT) printf("\n\n Result \n\n") printf("\n ZT is %.2f + (%.2f)i", x,y)
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//CHAPTER 7- SINGLE PHASE TRANSFORMER //Example 28 disp("CHAPTER 7"); disp("EXAMPLE 28"); //VARIABLE INITIALIZATION va=10000; //apparent power v1=2500; //primary voltage in Volts v2=250; //secondary voltage in Volts f=50; //open circuit parameters Voc=250; Io=0.8; Wi=50; // watts HT side //short circuit test Vsc=60; Isc=3; Wc=45; // watts HT side // //loads pf=0.8; //SOLUTION I1=va/v1; //full rated current on hv side Psc0=Wc*(I1/Isc)^2; //ohmic loss/ cu loss at full load rated current Pc=Wi; // core losses // 1/4 load Psc=(1/4)^2*Psc0; Pout=va*pf*(1/4); Pin=Pout+Pc+Psc; eff=Pout*100/Pin; disp("SOLUTION (a)"); disp(sprintf("The efficiency at 1/4 load is %f",eff)); // // 1/2 load Psc=(1/2)^2*Psc0; Pout=va*pf*(1/2); Pin=Pout+Pc+Psc; eff=Pout*100/Pin; disp(sprintf("The efficiency at 1/2 load is %f",eff)); // // full load Psc=(1/1)^2*Psc0; Pout=va*pf*(1/1); Pin=Pout+Pc+Psc; eff=Pout*100/Pin; disp(sprintf("The efficiency at full load is %f",eff)); // // 1 1/4 = 5/4 load Psc=(5/4)^2*Psc0; Pout=va*pf*(5/4); Pin=Pout+Pc+Psc; eff=Pout*100/Pin; disp(sprintf("The efficiency at 1 1/4 or 5/4 load is %f",eff)); // //maximum efficiency at x, but then ohmic loss=core loss x=sqrt(Pc/Psc0); Pout=va*x*pf; Pin=Pout+Pc+Pc; //Ohmic losses = core losses at max efficiency eff=Pout*100/Pin; disp("SOLUTION (b)"); disp(sprintf("The maximum efficiency is %f",eff)); // //short circuit phisc=acos(Wc/(Vsc*Isc)); pf1=cos(phisc); R_e1=Vsc*pf1/Isc; Z_e1=Vsc/Isc; X_e1=sqrt(Z_e1^2-R_e1^2); disp("SOLUTION (c)"); disp(sprintf("The value of Re1 is %f Ohm",R_e1)); disp(sprintf("The value of Ze1 is %f Ohm",Z_e1)); disp(sprintf("The value of Xe1 is %fΩ",X_e1)); // //ee, ex; er=I1*R_e1/v1; ex=I1*X_e1/v1; disp(sprintf("The value of Er is %f pu",er)); disp(sprintf("The value of Ex is %f",ex)); // phi=acos(pf); //R=ercosphi2+vx.sinphi2 //E2=V2+I2.R %reg=(I1*R_e1*pf+I1*X_e1*sin(phi))*100/v1; //same as using er and ex disp(sprintf("The percent regulation at full load lagging is %f",%reg)); %reg1=(I1*R_e1*pf-I1*X_e1*sin(phi))*100/v1; //same as using er and ex disp(sprintf("The percent regulation at full load leading is %f",%reg1)); V21=(1-%reg/100)*v2; V22=(1-%reg1/100)*v2; disp(sprintf("The secondary terminal voltage at full load lagging is %f",V21)); disp(sprintf("The secondary terminal voltage at full load leading is %f",V22)); disp(" "); // //END
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errcatch(-1,"stop");mode(2);//ques13 disp('The complex form of series is summation of f(n,x) where n varies from -%inf to %inf and f(n,x) is given by :'); syms n x cn=1/2*integ(exp(-x)*exp(-%i*%pi*n*x),x,-1,1); fnx=float(cn)*exp(%i*n*%pi*x); disp(float(fnx)); exit();
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//Chapter-1,Example1_5_1,pg 1-29 //refer diagram from textbook //on joining centre of 3 anions,an equilateral triangle is formed and on joining centres of any anion and cation a right angle triangle ABC os formed //where AC=rc+ra //and BC=ra //m(angle (ACB))=30 degree //therefore cos (30)=ra/(rc+ra) //assume rc/ra=r r=(1-cosd(30))/cosd(30) //by arrangimg terms we get value of r printf("critical radius ratio of ligancy 3=") disp(r)
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-- CD4041A.TST -- Grant of Unlimited Rights -- -- Under contracts F33600-87-D-0337, F33600-84-D-0280, MDA903-79-C-0687, -- F08630-91-C-0015, and DCA100-97-D-0025, the U.S. Government obtained -- unlimited rights in the software and documentation contained herein. -- Unlimited rights are defined in DFAR 252.227-7013(a)(19). By making -- this public release, the Government intends to confer upon all -- recipients unlimited rights equal to those held by the Government. -- These rights include rights to use, duplicate, release or disclose the -- released technical data and computer software in whole or in part, in -- any manner and for any purpose whatsoever, and to have or permit others -- to do so. -- -- DISCLAIMER -- -- ALL MATERIALS OR INFORMATION HEREIN RELEASED, MADE AVAILABLE OR -- DISCLOSED ARE AS IS. THE GOVERNMENT MAKES NO EXPRESS OR IMPLIED -- WARRANTY AS TO ANY MATTER WHATSOEVER, INCLUDING THE CONDITIONS OF THE -- SOFTWARE, DOCUMENTATION OR OTHER INFORMATION RELEASED, MADE AVAILABLE -- OR DISCLOSED, OR THE OWNERSHIP, MERCHANTABILITY, OR FITNESS FOR A -- PARTICULAR PURPOSE OF SAID MATERIAL. --* -- OBJECTIVE: -- CHECK THAT AN ALIGNMENT CLAUSE CAN BE GIVEN FOR A RECORD -- REPRESENTATION CLAUSE. -- HISTORY: -- RJW 08/25/87 CREATED ORIGINAL TEST. -- DHH 03/30/89 CHANGED MOD 4 TO A MACRO VALUE AND CHANGED -- EXTENSION FROM '.DEP' TO '.TST'. -- MACRO SUBSTITUTION: -- $ALIGNMENT IS THE VALUE USED TO ALIGN A RECORD ON A BOUNDARY -- DEFINED BY THE IMPLEMENTATION. WITH REPORT; USE REPORT; WITH SYSTEM; PROCEDURE CD4041A IS UNITS_PER_INTEGER : CONSTANT := (INTEGER'SIZE + SYSTEM.STORAGE_UNIT - 1) / SYSTEM.STORAGE_UNIT; TYPE CHECK_CLAUSE IS RECORD INT_COMP : INTEGER; CHAR_COMP : CHARACTER; END RECORD; FOR CHECK_CLAUSE USE RECORD AT MOD $ALIGNMENT; INT_COMP AT 0 RANGE 0..INTEGER'SIZE - 1; CHAR_COMP AT 1*UNITS_PER_INTEGER RANGE 0..CHARACTER'SIZE - 1; END RECORD; CHECK_RECORD : CHECK_CLAUSE := (1, 'A'); BEGIN TEST ("CD4041A", "CHECK THAT AN ALIGNMENT CLAUSE CAN BE " & "GIVEN FOR A RECORD REPRESENTATION CLAUSE"); IF CHECK_RECORD.INT_COMP'FIRST_BIT /= 0 THEN FAILED ("INCORRECT VALUE FOR FIRST_BIT OF INT_COMP"); END IF; IF CHECK_RECORD.INT_COMP'LAST_BIT /= INTEGER'SIZE - 1 THEN FAILED ("INCORRECT VALUE FOR LAST_BIT OF INT_COMP"); END IF; IF CHECK_RECORD.INT_COMP'POSITION /= 0 THEN FAILED ("INCORRECT VALUE FOR POSITION OF INT_COMP"); END IF; IF CHECK_RECORD.CHAR_COMP'FIRST_BIT /= IDENT_INT (0) THEN FAILED ("INCORRECT VALUE FOR FIRST_BIT OF CHAR_COMP"); END IF; IF CHECK_RECORD.CHAR_COMP'LAST_BIT /= IDENT_INT (CHARACTER'SIZE - 1) THEN FAILED ("INCORRECT VALUE FOR LAST_BIT OF CHAR_COMP"); END IF; IF CHECK_RECORD.CHAR_COMP'POSITION /= IDENT_INT (UNITS_PER_INTEGER) THEN FAILED ("INCORRECT VALUE FOR POSITION OF CHAR_COMP"); END IF; RESULT; END CD4041A;
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//Ex 5.14 clc; clear; close; format('v',4); R1=1;//kohm R2=1;//kohm R3=1;//kohm Rf=R2+R3;//kohm Vin=1;//V //Capacitor remains open circuited for steady state in both cases. Vout=-Rf/R1*Vin;//V disp(Vout,"Output Voltage(V)");
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function data = mdaq_exec_profile() data = []; if isfile(TMPDIR + filesep() + "profiling_data") then load(TMPDIR + filesep() + "profiling_data"); data = dsp_exec_profile; clear dsp_exec_profile; else disp("WARNING: Unable to get profiling data - make sure it is enabled in SETUP block!") return; end endfunction
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clear // Variable declaration Q=500// The amount of heat required for the building in kW T=19// The temperature at which air enters the heater coil in °C m_a=68// // The mass flow rate of air in kg/s C_pa=1.02// The specific heat capacity of air in kJ/kg.K // Calculation t=T+(Q/(m_a*C_pa))// The air supply temperature in °C printf("\n The air-supply temperature,t=%2.1f°C",t)
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clear; clc; disp("--------------Example 6.8---------------") n=4; // number of channels channel_byte=1; // each frame carries 1 byte from each channel frame_size=n*channel_byte; //bytes frame_size_bits=frame_size*8; // 1 byte = 8 bits byte_rate=100; // each channel sends 100 bytes/s frame_rate=channel_byte*byte_rate; // frames per second frame_duration=1/frame_rate; // seconds bit_rate=frame_rate*frame_size_bits; // bps // display the result printf("Each frame carries %d byte from each channel; the size of each frame, therefore, is %d bytes, or %d bits.\nThe frame rate is %d frames per second. The duration of a frame is %3.2f s.\nThe bit rate is %d bps.",channel_byte,frame_size,frame_size_bits,frame_rate,frame_duration,bit_rate); // display the figure clf(); xname("--------------Example 6.8----------------"); xpoly([.3 .3],[.3 .7]); xset("color",4.2); xfrect(0,.7,.28,.05); xfrect(.58,.58,.035,.045); xfrect(.88,.58,.035,.045); xset("color",2.9); xfrect(0,.6,.28,.05); xfrect(.545,.58,.035,.045); xfrect(.845,.58,.035,.045); xset("color",3.8); xfrect(0,.5,.28,.05); xfrect(.51,.58,.035,.045); xfrect(.81,.58,.035,.045); xset("color",0); xfrect(0,.4,.28,.05); xfrect(.475,.58,.035,.045); xfrect(.775,.58,.035,.045); xpoly([-.05 .3],[.625 .625]); xpoly([-.05 .3],[.525 .525]); xpoly([-.05 .3],[.425 .425]); xpoly([-.05 .3],[.325 .325]); xset("font size",4) xstring(.33,.5,"MUX"); xpoly([.3 .45],[.7 .5]); xpoly([.3 .45],[.3 .5]); xstring(.1,.27,"100 bytes/s"); xset("font size",3) xstring(.65,.45,"100 frames/s"); xstring(.67,.41,"3200 bps"); xstring(.6,.33,"Frame duration = 1/100 s"); xstring(.5,.7,"Frame 4 bytes"); xstring(.8,.7,"Frame 4 bytes"); xstring(.54,.65,"32 bits"); xstring(.84,.65,"32 bits"); xrect(.47,.59,.15,.07); xrect(.77,.59,.15,.07); xset("thickness",2); xarrows([.45 1],[.5 .5],.2); xset("font size",7); xstring(.66,.53,". . .");
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function y=f1(x,t) y=x(1)*exp(x(2)*t); endfunction
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function combine() // Perform column-wise combine with another DataFrame. // // Syntax // dfr.combine(obj,input_string) // // Parameters // obj : DataFrame object // input_string : String containing the function to be passed. Scilab functions are not supported as of now. Additional parameters supported can be passed // // For additional information on parameters, see https://pandas.pydata.org/docs/reference/api/pandas.DataFrame.combine.html?#pandas.DataFrame.combine // Returns : DataFrame // // Examples // // Combine another DataFrame with this DataFrame by using np.sqrt function // dfr.combine(df1.age,"np.sqrt") // // // Lambda functions are also supported. // // Authors // Aditya Dhinavahi // Sundeep Akella endfunction
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//pathname=get_absolute_file_path('12.05.sce') //filename=pathname+filesep()+'12.05-data.sci' //exec(filename) //Steam consumption rate(in kg/a): m=18/60 //Indicated power(in kW): IP=100 //Rpm of engine: n=240 //Bore diameter(in m): d=0.3 //Stroke length(in m): L=0.4 //Pressure at which steam is admitted(in bar): p1=10 //Exhaust pressure(in bar): p3=0.75 //Occurance of cut-off: r1=0.25 //Enthalpy of steam(in kJ/kg): h1=2875.3 //kJ/kg hf=384.39 //kJ/kg //Heat added per kg of steam(in kJ/kg): Q=h1-hf //Expansion ratio: r=1/r1 //Hypothetical mean effective pressure(in bar): mep=p1/r*(1+log(r))-p3 //Theoretical indicated power(in kW): IPt=mep*L*%pi*d^2*n*10^2/(60) //Diagarm factor: d1=IP/IPt //Indicated thermal efficiency: n=IPt/(m*Q)*100 printf("\n RESULT \n") printf("\nDiagram factor = %f",d1) printf("\nIndicated thermal efficiency = %f percent",n)
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@relation vowel @attribute TT integer[0,1] @attribute SpeakerNumber integer[0,14] @attribute Sex integer[0,1] @attribute F0 real[-5.211,-0.941] @attribute F1 real[-1.274,5.074] @attribute F2 real[-2.487,1.431] @attribute F3 real[-1.409,2.377] @attribute F4 real[-2.127,1.831] @attribute F5 real[-0.836,2.327] @attribute F6 real[-1.537,1.403] @attribute F7 real[-1.293,2.039] @attribute F8 real[-1.613,1.309] @attribute F9 real[-1.68,1.396] @attribute Class{0,1,2,3,4,5,6,7,8,9,10} @inputs TT,SpeakerNumber,Sex,F0,F1,F2,F3,F4,F5,F6,F7,F8,F9 @outputs Class @data 0 0 4 4 6 8 1 1 7 8 8 8 0 0 1 1 2 1 1 1 6 9 5 5 1 1 4 4 6 10 6 10 10 10 3 3 8 8 10 10 1 1 2 2 3 3 5 5 10 10 6 6 7 7 10 10 3 3 6 6 0 0 1 0 9 9 7 7 1 1 5 5 2 2 0 0 1 1 6 6 3 10 0 0 2 2 7 9 9 9 10 10 3 3 5 4 3 3 4 4 7 7 2 2 7 7 8 6 0 0 7 7 9 9 8 9 8 9 9 9 4 4 8 9 10 10 9 9 2 2 5 10 3 3 0 1 8 8 3 3 5 4 8 8 0 1 2 1 6 6 7 7 4 4 5 5 9 9 1 1 2 10 10 10 9 9 4 4 4 4 9 9 10 10 8 8 4 4 4 4 9 9 0 0 7 7 5 10 10 10 2 10 3 3 5 5 6 6
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//Caption:calculate_Wn,zeta,Wd,tp,Mp //example 6.10.5 //page 174 //given G(s)=20/(s+1)*(s+2) clc; s=%s; G=syslin('c',[20/((s+1)*(s+5))])//G(s):transfer function in forward path H=1;//backward path transfer function a=G/.H //closed loop transfer function b=denom(a) c=coeff(b) //Wn^2=c(1,1) Wn=sqrt(c(1,1))//natural frequency disp(Wn,"natural frequency,Wn=") //2*zeta*Wn=c(1,2) zeta=c(1,2)/(2*Wn)//damping ratio disp(zeta,"damping ratio,zeta=") Wd=Wn*sqrt(1-zeta^2)//damped frequency disp(Wd,"damping ratio,Wd=") Tp=%pi/Wd//peak time disp(Tp,"peak time,Tp=") Mp=(exp(-(zeta*%pi)/sqrt(1-zeta^2)))*100//max. overshoot disp(Mp,"max overshoot,Mp=") t=(2*%pi)/(Wn*sqrt(1-zeta^2))//period of oscillation disp(t,'time at which first overshoot occurs=') disp(t,"period of oscillation,t=") ts=4/(zeta*Wn)//settling time disp(ts,"settling time,ts=") N=Wd/(2*%pi)*ts//no. of oscillations completed before reaching steady state disp(N,"no. of oscillations completed before reaching steady state,N=")
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/991/CH14/EX14.7/Example14_7.sce
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Example14_7.sce
//Example 14.7. refer fig.14.6 clc format(6) RL=((40*2)/42)*10^3 //in ohm disp(RL," R''L(ohm) = RB || RL =") Av=(-80*1905)/5000 disp(Av," Av = -hfe*R''L / hie =") format(9) x1=(40000)/(1+30.48) Rif=(x1*5000)/(x1+5000) //in ohm disp(Rif," Rif(ohm) = hie || (RB / 1-Av) =") format(6) Avf=(-30.48*1013.172)/(600+1013.172) disp(Avf," Avf = Vo/Vs = Av*Rif / RS+Rif =") Rof=(40000/600)*(5600/80) //in ohm x2=Rof*10^-3 //in k-ohm disp(x2," Rof(k-ohm) = (RB / RS) * (RS+hie / hfe) =") Roff=(4.666*2)/(6.666) //in k-ohm disp(Roff," R''of(k-ohm) = Rof || RL =")
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MetodoNewtonComErroRelativo.sce
function [resultado] = erro_relativo(x, xl) resultado = abs((x-xl)/x) endfunction //Método de Newton para f(x) = x - cos(x) x = 0.7 xl = x primeira = %T while primeira | erro_relativo(x,xl) < 10^(-5) if primeira then primeira = %F end xl = x x = x - (x - cos(x))/(1 + sin(x)) end disp(x)
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/964/CH6/EX6.8/6_8.sce
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6_8.sce
//clc() del = 0.01; z = 0.56714329 x1 = 1; //f(x) = exp(-x) - x disp(x1,"x1 = ") for i = 1:4 if i == 1 then x(i) = 1 else w = x(i-1); m = exp(-x(i-1)) - x(i-1); x(i-1) = x(i-1)*(1+del); n = exp(-x(i-1)) - x(i-1); x(i) = w - (x(i-1)- w) * m/(n-m); em = (z - x(i))*100/z; disp(x(i),"x = ") disp("%",em,"error = ") end end
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//Example 1.17<i> //Determine the power and the rms value of the signal clc; t=0:0.001:10; y=5*cos(50*t+%pi/3); P=(integrate('5^2*(cos(50*t))^2','t',0,2*%pi))/(2*%pi); rmsvalue=sqrt(P); disp(P,'The power of the given signal is:'); disp(rmsvalue,'the rms value is:'); //Example 1.17<ii> //Determine the power amd rms value of the signal clc; t=0:0.001:10; x1=10*sin(50*t+%pi/4); x2=16*cos(100*t+%pi/3); P1=(integrate('10^2*(sin(50*t))^2','t',0,2*%pi))/(2*%pi); P2=(integrate('16^2*(cos(100*t))^2','t',0,2*%pi))/(2*%pi); P=P1+P2; rmsvalue=sqrt(P); disp(P,'The power of the given signal is:'); disp(rmsvalue,'the rms value is:'); //Example 1.17 <iii> //Determine the power and rms value of the signal clc; t=0:0.001:10; x1=5*cos(15*t); x2=5*cos(5*t); P1=(integrate('5^2*(cos(15*t))^2','t',0,2*%pi))/(2*%pi); P2=(integrate('5^2*(cos(5*t))^2','t',0,2*%pi))/(2*%pi); P=P1+P2; rmsvalue=sqrt(P); disp(P,'The power of the given signal is:'); disp(rmsvalue,'the rms value is:');
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mode(-1); function[]= ANN_train(layers,epochs,batchsize) dataset = uigetfile(["*.csv"],"~", "Choose a dataset file", %t); label = input("Enter label column:","string"); disp('Training...'); unix("python3.8 KerasANN.py "+dataset+" "+label+" "+layers+" "+string(epochs)+" "+string(batchsize)) endfunction function[output]= ANN_test_sample(test_sample) model_d= unix_g("pwd")+"/models"; model_file = uigetfile(["neural*.ml"],model_d,"Choose a model file", %t); output= ANN_test(test_sample,int32(length(test_sample)),model_file) endfunction function[output]= image_model(epochs) image_dir = uigetdir("~","Choose an image directory"); disp("Training..."); output = image_train_tl(image_dir,epochs); printf("Training accuracy: %0.2f",(output*100)); endfunction function[output]= image_model_test() model_d= unix_g("pwd")+"/models"; model_file = uigetfile(["image*.ml"],model_d, "Choose a model file", %t); image_file = uigetfile(["*.jpeg";"*.jpg";"*.png"],"~", "Choose an image file", %t); output = image_test_tl(image_file,model_file); disp('The selected image is of:') disp(output) endfunction function[]=plotTrainingAccuracy() unix_w("python3.8 GetSessionInfo.py accuracy") unix_w("xdg-open plots/AccuracyPlot.png"); endfunction function[]=plotTrainingLoss() unix_w("python3.8 GetSessionInfo.py loss") unix("xdg-open plots/LossPlot.png"); endfunction function[]=plotConfusionMatrix() unix_w("python3.8 GetSessionInfo.py cmat") unix_w("xdg-open plots/ConfusionMatrixPlot.png"); endfunction
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/[Pressure] Longbow Highground.sce
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[Pressure] Longbow Highground.sce
Name=[Pressure] Longbow Highground PlayerCharacters=Counter-Striker BotCharacters=Counter-Striker Bot PEEKER.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Counter-Striker AddedBots=Counter-Striker Bot PEEKER.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=1 BotTeams=2 MapName=longbow.map MapScale=3.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1.0 ScorePerDamage=10.0 ScorePerKill=100.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=1.0 ScoreLossPerDeath=200.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=true ScoreMultKillEfficiency=true GameTag=Apex Legends WeaponHeroTag=Longbow 1x no stock, Longbow 4x with stock DifficultyTag=3 AuthorsTag=dock :) BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=false Description=Longbow 1v1 highground scenario, accuracy is accounted for and so is dmg + death. Feel free to leave feedback :) GameVersion=1.0.8.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=0.9 MBSTime2Mult=0.8 MBSTime3Mult=0.8 MBSFBInstead=false MBSRequireEnemyAlive=true [Aim Profile] Name=High Skill MinReactionTime=0.25 MaxReactionTime=0.35 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=10.0 TrackSpeed=5.0 TrackError=2.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=35.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=cs MinReactionTime=0.18 MaxReactionTime=0.3 MinSelfMovementCorrectionTime=0.007 MaxSelfMovementCorrectionTime=0.035 FlickFOV=10.0 FlickSpeed=1.0 FlickError=3.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=90.0 MinRecenterTime=0.25 MaxRecenterTime=0.4 OptimalAimFOV=35.0 OuterAimPenalty=1.1 MaxError=35.0 ShootFOV=1.0 VerticalAimOffset=-5.0 MaxTolerableSpread=2.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [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 [Bot Profile] Name=Counter-Striker Bot PEEKER DodgeProfileNames=MidStrafes DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=10.0 DodgeProfileMinChangeTime=0.1 WeaponProfileWeights=1.5;1.5;1.5;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=High Skill;High Skill;cs;cs;cs;Default;Default;Default WeaponSwitchTime=5.0 UseWeapons=true CharacterProfile=Counting-Striker SeeThroughWalls=false NoDodging=false NoAiming=false [Character Profile] Name=Counter-Striker MaxHealth=100.0 WeaponProfileNames=Longbow 1x no stock;Longbow 4x with stock;;;;;; MinRespawnDelay=0.0001 MaxRespawnDelay=0.0001 StepUpHeight=75.0 CrouchHeightModifier=0.75 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=1100.0 MaxCrouchSpeed=250.0 Acceleration=6000.0 AirAcceleration=16000.0 Friction=7.5 BrakingFrictionFactor=1.25 JumpVelocity=800.0 Gravity=2.5 AirControl=1.0 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=true EnemyBodyColor=X=0.546 Y=0.776 Z=0.546 EnemyHeadColor=X=0.608 Y=0.463 Z=0.314 TeamBodyColor=X=0.000 Y=0.000 Z=0.771 TeamHeadColor=X=0.149 Y=0.542 Z=1.000 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=210.0 MainBBRadius=35.0 MainBBHasHead=true MainBBHeadRadius=25.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=250.0 ProjBBRadius=35.0 ProjBBHasHead=true ProjBBHeadRadius=25.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=256.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=100.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=5000.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Character Profile] Name=Counting-Striker MaxHealth=100.0 WeaponProfileNames=R-99 Projectile - H80;Wingman - Projectile - H80;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=10.0 StepUpHeight=75.0 CrouchHeightModifier=0.75 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=200.0 MaxCrouchSpeed=50.0 Acceleration=6000.0 AirAcceleration=16000.0 Friction=7.5 BrakingFrictionFactor=1.25 JumpVelocity=800.0 Gravity=2.5 AirControl=1.0 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=true EnemyBodyColor=X=0.546 Y=0.776 Z=0.546 EnemyHeadColor=X=0.608 Y=0.463 Z=0.314 TeamBodyColor=X=0.000 Y=0.000 Z=0.771 TeamHeadColor=X=0.149 Y=0.542 Z=1.000 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=100.0 MainBBRadius=10.0 MainBBHasHead=true MainBBHeadRadius=7.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=100.0 ProjBBRadius=10.0 ProjBBHasHead=true ProjBBHeadRadius=7.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=Run.abilsprint;Slide.abilsprint;; HideWeapon=false 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=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Dodge Profile] Name=MidStrafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.32 MaxLRTimeChange=0.35 MinFBTimeChange=0.25 MaxFBTimeChange=0.6 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.2 DamageReactionMinimumDelay=0.13 DamageReactionMaximumDelay=0.16 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.2 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.5 TargetStrafeOverride=Oppose TargetStrafeMinDelay=0.13 TargetStrafeMaxDelay=0.18 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.5 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=0.9 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Longbow 1x no stock Type=Projectile ShotsPerClick=1 DamagePerShot=55.0 KnockbackFactor=4.0 TimeBetweenShots=0.555 Pierces=false Category=SemiAuto 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=22720.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=22720.000 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=1.9 MagazineMax=12 AmmoPerShot=1 ReloadTimeFromEmpty=3.1 ReloadTimeFromPartial=2.3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Rocket VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Flare BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=true ADSZoomDelay=0.22 ADSZoomSensFactor=0.82 ADSMoveFactor=0.33 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=10.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 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 ProjectileTrail=Sparks 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=12 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=100 ADSFOVOverride=71.0 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.6 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=3.0,3.0,5.0,10.0 SpreadSCH=3.0,3.0,-1.0,8.0 SpreadMSH=3.0,3.0,-1.0,8.0 SpreadMCH=3.0,3.0,-1.0,8.0 MaxRecoilUp=5.0 MinRecoilUp=5.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.15 TimeToRecoilReset=0.15 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 [Weapon Profile] Name=Longbow 4x with stock Type=Projectile ShotsPerClick=1 DamagePerShot=55.0 KnockbackFactor=4.0 TimeBetweenShots=0.555 Pierces=false Category=SemiAuto 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=25520.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=25520.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=10.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=1.9 MagazineMax=12 AmmoPerShot=1 ReloadTimeFromEmpty=3.1 ReloadTimeFromPartial=2.3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Rocket VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Gunshot BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.2 CanAimDownSight=true ADSZoomDelay=0.22 ADSZoomSensFactor=0.282 ADSMoveFactor=0.33 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 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 ProjectileTrail=Sparks 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=12 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=100 ADSFOVOverride=22.5 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=3.0,3.0,5.0,10.0 SpreadSCH=3.0,3.0,-1.0,8.0 SpreadMSH=3.0,3.0,-1.0,8.0 SpreadMCH=3.0,3.0,-1.0,8.0 MaxRecoilUp=0.7 MinRecoilUp=0.7 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.12 TimeToRecoilReset=0.12 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 [Weapon Profile] Name=R-99 Projectile - H80 Type=Projectile ShotsPerClick=1 DamagePerShot=12.0 KnockbackFactor=4.0 TimeBetweenShots=0.0555 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=21000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=21000.000 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=1.12 MagazineMax=30 AmmoPerShot=1 ReloadTimeFromEmpty=2.25 ReloadTimeFromPartial=1.66 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=12.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.2 CanAimDownSight=true ADSZoomDelay=0.15 ADSZoomSensFactor=0.87 ADSMoveFactor=0.9 ADSStartDelay=0.0 ShootSoundCooldown=0.03 HitSoundCooldown=0.03 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=10.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300000.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.2 TaggingMaxFactor=0.75 TaggingHitFactor=0.75 ProjectileTrail=Smoke 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=true PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=30 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=77.0 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,1.0,-1.0,0.0 SpreadSCA=0.0,1.0,-1.0,0.0 SpreadMSA=0.0,1.0,-1.0,0.0 SpreadMCA=0.0,1.0,-1.0,0.0 SpreadSSH=0.4,1.0,1.0,2.0 SpreadSCH=0.4,1.0,0.8,2.0 SpreadMSH=0.4,0.1,1.0,2.0 SpreadMCH=0.4,0.1,1.0,2.0 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=true PSRLoopStartIndex=0 PSRViewRecoilTracking=1.0 PSRCapUp=34.0 PSRCapRight=34.0 PSRCapLeft=34.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=30.0 PSR0=0.547,0.094 PSR1=0.141,0.0 PSR2=0.609,-0.016 PSR3=0.64,-0.141 PSR4=0.593,0.203 PSR5=0.656,0.234 PSR6=0.578,0.39 PSR7=0.375,0.031 PSR8=0.672,0.141 PSR9=0.547,-0.172 PSR10=0.484,-0.422 PSR11=0.344,-0.047 PSR12=0.718,-0.187 PSR13=0.25,0.203 PSR14=0.141,0.156 PSR15=0.094,0.062 PSR16=-0.094,0.437 PSR17=0.328,-0.328 PSR18=0.031,-0.39 PSR19=0.203,-0.25 PSR20=0.125,-0.359 PSR21=0.141,-0.344 PSR22=-0.078,0.187 PSR23=0.062,0.562 PSR24=-0.141,0.344 PSR25=0.086,0.257 PSR26=0.086,0.257 PSR27=0.086,-0.257 PSR28=0.086,-0.257 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=Wingman - Projectile - H80 Type=Projectile ShotsPerClick=1 DamagePerShot=45.0 KnockbackFactor=4.0 TimeBetweenShots=0.384 Pierces=false Category=SemiAuto 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=18000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=18000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=100.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=1.68 MagazineMax=10 AmmoPerShot=1 ReloadTimeFromEmpty=1.83 ReloadTimeFromPartial=1.83 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=45.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.5 CanAimDownSight=true ADSZoomDelay=0.15 ADSZoomSensFactor=0.87 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=10.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300000.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.25 TaggingMaxFactor=0.5 TaggingHitFactor=0.5 ProjectileTrail=Smoke 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=10 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=77.0 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=0.6,1.0,1.0,3.0 SpreadSCH=0.6,1.0,1.0,2.5 SpreadMSH=0.5,0.1,0.3,3.0 SpreadMCH=0.0,0.1,0.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.1 TimeToRecoilReset=0.05 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=true PSRLoopStartIndex=2 PSRViewRecoilTracking=1.0 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.5 PSRResetDegreesPerSec=30.0 PSR0=1.4,0.3 PSR1=0.61,0.23 PSR2=0.2,-0.094 PSR3=0.115,0.146 PSR4=0.0,0.124 PSR5=-0.2,0.2 PSR6=-0.21,-0.05 PSR7=-0.178,-0.084 PSR8=-0.104,-0.115 UsePerBulletSpread=false PBS0=0.0,0.0 [Sprint Ability Profile] Name=Run MaxCharges=1.0 ChargeTimer=0.001 ChargesRefundedOnKill=0.0 DelayAfterUse=0.1 FullyAuto=false AbilityDuration=0.0 BlockAttackWhileSprinting=false AbilityBlockedWhenAttacking=false SpeedModifier=1.6 45DegreeSprint=true 90DegreeSprint=false 135DegreeSprint=false 180DegreeSprint=false TapToSprint=true Block45DegreesWhenSprinting=false AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Sprint Ability Profile] Name=Slide MaxCharges=1.0 ChargeTimer=2.0 ChargesRefundedOnKill=0.0 DelayAfterUse=3.0 FullyAuto=true AbilityDuration=0.4 BlockAttackWhileSprinting=false AbilityBlockedWhenAttacking=false SpeedModifier=2.25 45DegreeSprint=true 90DegreeSprint=false 135DegreeSprint=true 180DegreeSprint=true TapToSprint=true Block45DegreesWhenSprinting=false AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn brush vertices -64.000000 -16.000000 -320.000000 -64.000000 -16.000000 320.000000 -64.000000 16.000000 320.000000 -64.000000 16.000000 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// Program to fin short Time Autocorrelation Function // Using Rectangular and Hamming window clear,close,clear, [y,Fs]=wavread('C:\Test_Project\a-team_my_way.wav'); beg= 5200; // Sample at which window is to be applied N= 500; // Length of window in Sample x=y(beg:beg+N-1); // Obtainin the required segment whm= window('hm',N); // Hamming window Ham_seg=x.*whm; // Multiplying window with the signal wr=window('re',N);// Rectangular Window Rect_seg=x.*wr; t=(beg:beg+N-1)/Fs; // Adjusting the x axis to time subplot(311) plot(t,Rect_seg) xlabel('Time in seconds') title('Selected segment in the signal') c1= xcorr(Rect_seg); // Autocorrelation lag=(1:length(c1))-ceil(length(c1)/2); // Adjusting x axis to get peak at lag=0 subplot(312) plot(lag,c1) title('Short Time Autocorrelation using Rectangular window') xlabel(' Lag k') ylabel('STACF') ////////////////// c2=xcorr(Ham_seg); lag=(1:length(c1))-ceil(length(c2)/2); // Adjusting x axis // to get peak at lag=0 subplot(313) plot(lag,c2) title('Short Time Autocorrelation using Hamming window') xlabel('Lag k') ylabel('STACF')
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errcatch(-1,"stop");mode(2);//Exa 4.2 ; ; //given data : delVDS=1.5;//in Volt delID=120;//in uAmpere delID=delID*10^-6;//in Ampere rd=delVDS/delID;//in Ohm disp(rd*10^-3,"AC drain Resistance of JFET in Kohm : "); exit();
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// Find depletion layer capacitance // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 2-5 in page 86 clear; clc; close; // Given data epsln=12/(36*%pi*10^11); // Constant for Si in F/cm A=8.11058*10^-1; // Cross sectional area in m^2 mu_p=500; // Mobility of holes e=1.6*10^-19; // Charge on an electron in C V_j=4.9; // Junction potential in V // Calculation printf("(a)We have C_t/A = sqrt((e*epsnl)/2)*sqrt(Na/Vj)\n"); K=sqrt((e*epsln)/2); printf("sqrt((e*epsln)/2) = %0.2e\n",K); printf("Hence C_t = %0.2e * sqrt(Na/Vj) F/cm^2\n",K); K1=K*10^12; printf("Or C_t = %0.2e * sqrt(Na/Vj) pF/cm^2\n",K1); N_A=1/(3*mu_p*e); C_T=(2.9*10^-4)*sqrt(N_A/V_j)*(8.14*10^-3); printf("(b)The depletion layer capacitance = %0.2f pF",C_T); // Result // (a) The expression for depletion layer capacitance is proved // (b) The depletion layer capacitance in silicon is 68.84 pF
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clc // Given that m = 2.5 // Mass flow rate in kg/s p1 = 1 // Inlet pressure in bar T1 = 300 // Inlet temperature in bar n_s = 0.88 // Stage efficiency Wc = 600 // Power input in kW delta_t = 21 // Temperature rise in first stage in degree centigrade gama = 1.4 // Ratio of heat capacities cp = 1.005 // Heat capacity in kJ/kgK printf("\n Example 19.21\n") x = n_s*gama/(gama-1)// Where x = (n/(n-1)) T = Wc/(m*cp)+T1 p = p1*((T/T1)^(x)) T2 = T1 + n_s*delta_t r = ((T2/T1)^(gama/(gama-1)))// Where r = p2/p1 N = log(p/p1)/log(r) N_ = ceil(N) Ts = T1*(p/p1)^((gama-1)/gama) n_inter = (Ts-T1)/(T-T1) printf("\n The delivery pressure = %f bar,\n The no of stages = %d,\n The internal efficiency = %f ",p,N_,n_inter)
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Expanding for base=2, level=7, reasons+features=base,similiar invall,norm Refined variables=x,y [0+1x,0+1y]: unknown -> [1] [0,0] x²-y³+2 ---------------- level 0 expanding queue[0]^-1,meter=[2,2]: x²-y³+2 [1+2x,1+2y]: unknown -> [1] [1,1] 2x+2x²-3y-6y²-4y³+1 endexp[0] ---------------- level 1 expanding queue[1]^0,meter=[2,2]: 2x+2x²-3y-6y²-4y³+1 [1+4x,3+4y]: unknown -> [2] [0,1] 2x+4x²-27y-36y²-16y³-6 -> solution [5,3],NONTRIVIAL [3+4x,3+4y]: unknown -> [3] [1,1] 6x+4x²-27y-36y²-16y³-4 endexp[1] ---------------- level 2 expanding queue[2]^1,meter=[2,2]: 2x+4x²-27y-36y²-16y³-6 [1+8x,3+8y]: unknown -> [4] [0,0] 2x+8x²-27y-72y²-64y³-3 [5+8x,3+8y]: unknown -> [5] [1,0] 10x+8x²-27y-72y²-64y³ -> solution [5,3],NONTRIVIAL endexp[2] expanding queue[3]^1,meter=[2,2]: 6x+4x²-27y-36y²-16y³-4 [3+8x,3+8y]: unknown -> [6] [0,0] 6x+8x²-27y-72y²-64y³-2 [7+8x,3+8y]: unknown -> [7] [1,0] 14x+8x²-27y-72y²-64y³+3 endexp[3] ---------------- level 3 expanding queue[4]^2,meter=[2,2]: 2x+8x²-27y-72y²-64y³-3 [1+16x,11+16y]: unknown -> [8] [0,1] 2x+16x²-363y-528y²-256y³-83 [9+16x,11+16y]: unknown -> [9] [1,1] 18x+16x²-363y-528y²-256y³-78 endexp[4] expanding queue[5]^2,meter=[2,2]: 10x+8x²-27y-72y²-64y³ [5+16x,3+16y]: unknown -> [10] [0,0] 10x+16x²-27y-144y²-256y³ -> solution [5,3],NONTRIVIAL [13+16x,3+16y]: unknown -> [11] [1,0] 26x+16x²-27y-144y²-256y³+9 endexp[5] expanding queue[6]^3,meter=[2,2]: 6x+8x²-27y-72y²-64y³-2 [3+16x,3+16y]: unknown -> [12] [0,0] 6x+16x²-27y-144y²-256y³-1 [11+16x,3+16y]: unknown -> [13] [1,0] 22x+16x²-27y-144y²-256y³+6 endexp[6] expanding queue[7]^3,meter=[2,2]: 14x+8x²-27y-72y²-64y³+3 [7+16x,11+16y]: unknown -> [14] [0,1] 14x+16x²-363y-528y²-256y³-80 [15+16x,11+16y]: unknown -> [15] [1,1] 30x+16x²-363y-528y²-256y³-69 endexp[7] ---------------- level 4 expanding queue[8]^4,meter=[2,2]: 2x+16x²-363y-528y²-256y³-83 [1+32x,27+32y]: unknown -> [16] [0,1] 2x+32x²-2187y-2592y²-1024y³-615 [17+32x,27+32y]: unknown -> [17] [1,1] 34x+32x²-2187y-2592y²-1024y³-606 endexp[8] expanding queue[9]^4,meter=[2,2]: 18x+16x²-363y-528y²-256y³-78 [9+32x,11+32y]: unknown -> [18] [0,0] 18x+32x²-363y-1056y²-1024y³-39 [25+32x,11+32y]: unknown -> [19] [1,0] 50x+32x²-363y-1056y²-1024y³-22 endexp[9] expanding queue[10]^5,meter=[2,2]: 10x+16x²-27y-144y²-256y³ [5+32x,3+32y]: unknown -> [20] [0,0] 10x+32x²-27y-288y²-1024y³ -> solution [5,3],NONTRIVIAL [21+32x,3+32y]: unknown -> [21] [1,0] 42x+32x²-27y-288y²-1024y³+13 endexp[10] expanding queue[11]^5,meter=[2,2]: 26x+16x²-27y-144y²-256y³+9 [13+32x,19+32y]: unknown -> [22] [0,1] 26x+32x²-1083y-1824y²-1024y³-209 [29+32x,19+32y]: unknown -> [23] [1,1] 58x+32x²-1083y-1824y²-1024y³-188 endexp[11] expanding queue[12]^6,meter=[2,2]: 6x+16x²-27y-144y²-256y³-1 [3+32x,19+32y]: unknown -> [24] [0,1] 6x+32x²-1083y-1824y²-1024y³-214 [19+32x,19+32y]: unknown -> [25] [1,1] 38x+32x²-1083y-1824y²-1024y³-203 endexp[12] expanding queue[13]^6,meter=[2,2]: 22x+16x²-27y-144y²-256y³+6 [11+32x,3+32y]: unknown -> [26] [0,0] 22x+32x²-27y-288y²-1024y³+3 [27+32x,3+32y]: unknown -> [27] [1,0] 54x+32x²-27y-288y²-1024y³+22 endexp[13] expanding queue[14]^7,meter=[2,2]: 14x+16x²-363y-528y²-256y³-80 [7+32x,11+32y]: unknown -> [28] [0,0] 14x+32x²-363y-1056y²-1024y³-40 [23+32x,11+32y]: unknown -> [29] [1,0] 46x+32x²-363y-1056y²-1024y³-25 endexp[14] expanding queue[15]^7,meter=[2,2]: 30x+16x²-363y-528y²-256y³-69 [15+32x,27+32y]: unknown -> [30] [0,1] 30x+32x²-2187y-2592y²-1024y³-608 [31+32x,27+32y]: unknown -> [31] [1,1] 62x+32x²-2187y-2592y²-1024y³-585 endexp[15] ---------------- level 5 expanding queue[16]^8,meter=[2,2]: 2x+32x²-2187y-2592y²-1024y³-615 [1+64x,59+64y]: unknown -> [32] [0,1] 2x+64x²-10443y-11328y²-4096y³-3209 [33+64x,59+64y]: unknown -> [33] [1,1] 66x+64x²-10443y-11328y²-4096y³-3192 endexp[16] expanding queue[17]^8,meter=[2,2]: 34x+32x²-2187y-2592y²-1024y³-606 [17+64x,27+64y]: unknown -> [34] [0,0] 34x+64x²-2187y-5184y²-4096y³-303 [49+64x,27+64y]: unknown -> [35] [1,0] 98x+64x²-2187y-5184y²-4096y³-270 endexp[17] expanding queue[18]^9,meter=[2,2]: 18x+32x²-363y-1056y²-1024y³-39 [9+64x,43+64y]: unknown -> [36] [0,1] 18x+64x²-5547y-8256y²-4096y³-1241 [41+64x,43+64y]: unknown -> [37] [1,1] 82x+64x²-5547y-8256y²-4096y³-1216 endexp[18] expanding queue[19]^9,meter=[2,2]: 50x+32x²-363y-1056y²-1024y³-22 [25+64x,11+64y]: unknown -> [38] [0,0] 50x+64x²-363y-2112y²-4096y³-11 [57+64x,11+64y]: unknown -> [39] [1,0] 114x+64x²-363y-2112y²-4096y³+30 endexp[19] expanding queue[20]^10,meter=[2,2]: 10x+32x²-27y-288y²-1024y³ [5+64x,3+64y]: unknown -> [40] [0,0] 10x+64x²-27y-576y²-4096y³ -> solution [5,3],NONTRIVIAL [37+64x,3+64y]: unknown -> [41] [1,0] 74x+64x²-27y-576y²-4096y³+21 endexp[20] expanding queue[21]^10,meter=[2,2]: 42x+32x²-27y-288y²-1024y³+13 [21+64x,35+64y]: unknown -> [42] [0,1] 42x+64x²-3675y-6720y²-4096y³-663 [53+64x,35+64y]: unknown -> [43] [1,1] 106x+64x²-3675y-6720y²-4096y³-626 endexp[21] expanding queue[22]^11,meter=[2,2]: 26x+32x²-1083y-1824y²-1024y³-209 [13+64x,51+64y]: unknown -> [44] [0,1] 26x+64x²-7803y-9792y²-4096y³-2070 [45+64x,51+64y]: unknown -> [45] [1,1] 90x+64x²-7803y-9792y²-4096y³-2041 endexp[22] expanding queue[23]^11,meter=[2,2]: 58x+32x²-1083y-1824y²-1024y³-188 [29+64x,19+64y]: unknown -> [46] [0,0] 58x+64x²-1083y-3648y²-4096y³-94 [61+64x,19+64y]: unknown -> [47] [1,0] 122x+64x²-1083y-3648y²-4096y³-49 endexp[23] expanding queue[24]^12,meter=[2,2]: 6x+32x²-1083y-1824y²-1024y³-214 [3+64x,19+64y]: unknown -> [48] [0,0] 6x+64x²-1083y-3648y²-4096y³-107 [35+64x,19+64y]: unknown -> [49] [1,0] 70x+64x²-1083y-3648y²-4096y³-88 endexp[24] expanding queue[25]^12,meter=[2,2]: 38x+32x²-1083y-1824y²-1024y³-203 [19+64x,51+64y]: unknown -> [50] [0,1] 38x+64x²-7803y-9792y²-4096y³-2067 [51+64x,51+64y]: unknown -> [51] [1,1] 102x+64x²-7803y-9792y²-4096y³-2032 endexp[25] expanding queue[26]^13,meter=[2,2]: 22x+32x²-27y-288y²-1024y³+3 [11+64x,35+64y]: unknown -> [52] [0,1] 22x+64x²-3675y-6720y²-4096y³-668 [43+64x,35+64y]: unknown -> [53] [1,1] 86x+64x²-3675y-6720y²-4096y³-641 endexp[26] expanding queue[27]^13,meter=[2,2]: 54x+32x²-27y-288y²-1024y³+22 [27+64x,3+64y]: unknown -> [54] [0,0] 54x+64x²-27y-576y²-4096y³+11 [59+64x,3+64y]: unknown -> [55] [1,0] 118x+64x²-27y-576y²-4096y³+54 endexp[27] expanding queue[28]^14,meter=[2,2]: 14x+32x²-363y-1056y²-1024y³-40 [7+64x,11+64y]: unknown -> [56] [0,0] 14x+64x²-363y-2112y²-4096y³-20 [39+64x,11+64y]: unknown -> [57] [1,0] 78x+64x²-363y-2112y²-4096y³+3 endexp[28] expanding queue[29]^14,meter=[2,2]: 46x+32x²-363y-1056y²-1024y³-25 [23+64x,43+64y]: unknown -> [58] [0,1] 46x+64x²-5547y-8256y²-4096y³-1234 [55+64x,43+64y]: unknown -> [59] [1,1] 110x+64x²-5547y-8256y²-4096y³-1195 endexp[29] expanding queue[30]^15,meter=[2,2]: 30x+32x²-2187y-2592y²-1024y³-608 [15+64x,27+64y]: unknown -> [60] [0,0] 30x+64x²-2187y-5184y²-4096y³-304 [47+64x,27+64y]: unknown -> [61] [1,0] 94x+64x²-2187y-5184y²-4096y³-273 endexp[30] expanding queue[31]^15,meter=[2,2]: 62x+32x²-2187y-2592y²-1024y³-585 [31+64x,59+64y]: unknown -> [62] [0,1] 62x+64x²-10443y-11328y²-4096y³-3194 [63+64x,59+64y]: unknown -> [63] [1,1] 126x+64x²-10443y-11328y²-4096y³-3147 endexp[31] ---------------- level 6 expanding queue[32]^16,meter=[2,2]: 2x+64x²-10443y-11328y²-4096y³-3209 [1+128x,123+128y]: unknown -> [64] [0,1] 2x+128x²-45387y-47232y²-16384y³-14538 [65+128x,123+128y]: unknown -> [65] [1,1] 130x+128x²-45387y-47232y²-16384y³-14505 endexp[32] expanding queue[33]^16,meter=[2,2]: 66x+64x²-10443y-11328y²-4096y³-3192 [33+128x,59+128y]: unknown -> [66] [0,0] 66x+128x²-10443y-22656y²-16384y³-1596 [97+128x,59+128y]: unknown -> [67] [1,0] 194x+128x²-10443y-22656y²-16384y³-1531 endexp[33] expanding queue[34]^17,meter=[2,2]: 34x+64x²-2187y-5184y²-4096y³-303 [17+128x,91+128y]: unknown -> [68] [0,1] 34x+128x²-24843y-34944y²-16384y³-5885 [81+128x,91+128y]: unknown -> [69] [1,1] 162x+128x²-24843y-34944y²-16384y³-5836 endexp[34] expanding queue[35]^17,meter=[2,2]: 98x+64x²-2187y-5184y²-4096y³-270 [49+128x,27+128y]: unknown -> [70] [0,0] 98x+128x²-2187y-10368y²-16384y³-135 [113+128x,27+128y]: unknown -> [71] [1,0] 226x+128x²-2187y-10368y²-16384y³-54 endexp[35] expanding queue[36]^18,meter=[2,2]: 18x+64x²-5547y-8256y²-4096y³-1241 [9+128x,107+128y]: unknown -> [72] [0,1] 18x+128x²-34347y-41088y²-16384y³-9570 [73+128x,107+128y]: unknown -> [73] [1,1] 146x+128x²-34347y-41088y²-16384y³-9529 endexp[36] expanding queue[37]^18,meter=[2,2]: 82x+64x²-5547y-8256y²-4096y³-1216 [41+128x,43+128y]: unknown -> [74] [0,0] 82x+128x²-5547y-16512y²-16384y³-608 [105+128x,43+128y]: unknown -> [75] [1,0] 210x+128x²-5547y-16512y²-16384y³-535 endexp[37] expanding queue[38]^19,meter=[2,2]: 50x+64x²-363y-2112y²-4096y³-11 [25+128x,75+128y]: unknown -> [76] [0,1] 50x+128x²-16875y-28800y²-16384y³-3291 [89+128x,75+128y]: unknown -> [77] [1,1] 178x+128x²-16875y-28800y²-16384y³-3234 endexp[38] expanding queue[39]^19,meter=[2,2]: 114x+64x²-363y-2112y²-4096y³+30 [57+128x,11+128y]: unknown -> [78] [0,0] 114x+128x²-363y-4224y²-16384y³+15 [121+128x,11+128y]: unknown -> [79] [1,0] 242x+128x²-363y-4224y²-16384y³+104 endexp[39] expanding queue[40]^20,meter=[2,2]: 10x+64x²-27y-576y²-4096y³ [5+128x,3+128y]: unknown -> [80] [0,0] 10x+128x²-27y-1152y²-16384y³ -> solution [5,3],NONTRIVIAL [69+128x,3+128y]: unknown -> [81] [1,0] 138x+128x²-27y-1152y²-16384y³+37 endexp[40] expanding queue[41]^20,meter=[2,2]: 74x+64x²-27y-576y²-4096y³+21 [37+128x,67+128y]: unknown -> [82] [0,1] 74x+128x²-13467y-25728y²-16384y³-2339 [101+128x,67+128y]: unknown -> [83] [1,1] 202x+128x²-13467y-25728y²-16384y³-2270 endexp[41] expanding queue[42]^21,meter=[2,2]: 42x+64x²-3675y-6720y²-4096y³-663 [21+128x,99+128y]: unknown -> [84] [0,1] 42x+128x²-29403y-38016y²-16384y³-7577 [85+128x,99+128y]: unknown -> [85] [1,1] 170x+128x²-29403y-38016y²-16384y³-7524 endexp[42] expanding queue[43]^21,meter=[2,2]: 106x+64x²-3675y-6720y²-4096y³-626 [53+128x,35+128y]: unknown -> [86] [0,0] 106x+128x²-3675y-13440y²-16384y³-313 [117+128x,35+128y]: unknown -> [87] [1,0] 234x+128x²-3675y-13440y²-16384y³-228 endexp[43] expanding queue[44]^22,meter=[2,2]: 26x+64x²-7803y-9792y²-4096y³-2070 [13+128x,51+128y]: unknown -> [88] [0,0] 26x+128x²-7803y-19584y²-16384y³-1035 [77+128x,51+128y]: unknown -> [89] [1,0] 154x+128x²-7803y-19584y²-16384y³-990 endexp[44] expanding queue[45]^22,meter=[2,2]: 90x+64x²-7803y-9792y²-4096y³-2041 [45+128x,115+128y]: unknown -> [90] [0,1] 90x+128x²-39675y-44160y²-16384y³-11866 [109+128x,115+128y]: unknown -> [91] [1,1] 218x+128x²-39675y-44160y²-16384y³-11789 endexp[45] expanding queue[46]^23,meter=[2,2]: 58x+64x²-1083y-3648y²-4096y³-94 [29+128x,19+128y]: unknown -> [92] [0,0] 58x+128x²-1083y-7296y²-16384y³-47 [93+128x,19+128y]: unknown -> [93] [1,0] 186x+128x²-1083y-7296y²-16384y³+14 endexp[46] expanding queue[47]^23,meter=[2,2]: 122x+64x²-1083y-3648y²-4096y³-49 [61+128x,83+128y]: unknown -> [94] [0,1] 122x+128x²-20667y-31872y²-16384y³-4438 [125+128x,83+128y]: unknown -> [95] [1,1] 250x+128x²-20667y-31872y²-16384y³-4345 endexp[47] expanding queue[48]^24,meter=[2,2]: 6x+64x²-1083y-3648y²-4096y³-107 [3+128x,83+128y]: unknown -> [96] [0,1] 6x+128x²-20667y-31872y²-16384y³-4467 [67+128x,83+128y]: unknown -> [97] [1,1] 134x+128x²-20667y-31872y²-16384y³-4432 endexp[48] expanding queue[49]^24,meter=[2,2]: 70x+64x²-1083y-3648y²-4096y³-88 [35+128x,19+128y]: unknown -> [98] [0,0] 70x+128x²-1083y-7296y²-16384y³-44 [99+128x,19+128y]: unknown -> [99] [1,0] 198x+128x²-1083y-7296y²-16384y³+23 endexp[49] expanding queue[50]^25,meter=[2,2]: 38x+64x²-7803y-9792y²-4096y³-2067 [19+128x,115+128y]: unknown -> [100] [0,1] 38x+128x²-39675y-44160y²-16384y³-11879 [83+128x,115+128y]: unknown -> [101] [1,1] 166x+128x²-39675y-44160y²-16384y³-11828 endexp[50] expanding queue[51]^25,meter=[2,2]: 102x+64x²-7803y-9792y²-4096y³-2032 [51+128x,51+128y]: unknown -> [102] [0,0] 102x+128x²-7803y-19584y²-16384y³-1016 [115+128x,51+128y]: unknown -> [103] [1,0] 230x+128x²-7803y-19584y²-16384y³-933 endexp[51] expanding queue[52]^26,meter=[2,2]: 22x+64x²-3675y-6720y²-4096y³-668 [11+128x,35+128y]: unknown -> [104] [0,0] 22x+128x²-3675y-13440y²-16384y³-334 [75+128x,35+128y]: unknown -> [105] [1,0] 150x+128x²-3675y-13440y²-16384y³-291 endexp[52] expanding queue[53]^26,meter=[2,2]: 86x+64x²-3675y-6720y²-4096y³-641 [43+128x,99+128y]: unknown -> [106] [0,1] 86x+128x²-29403y-38016y²-16384y³-7566 [107+128x,99+128y]: unknown -> [107] [1,1] 214x+128x²-29403y-38016y²-16384y³-7491 endexp[53] expanding queue[54]^27,meter=[2,2]: 54x+64x²-27y-576y²-4096y³+11 [27+128x,67+128y]: unknown -> [108] [0,1] 54x+128x²-13467y-25728y²-16384y³-2344 [91+128x,67+128y]: unknown -> [109] [1,1] 182x+128x²-13467y-25728y²-16384y³-2285 endexp[54] expanding queue[55]^27,meter=[2,2]: 118x+64x²-27y-576y²-4096y³+54 [59+128x,3+128y]: unknown -> [110] [0,0] 118x+128x²-27y-1152y²-16384y³+27 [123+128x,3+128y]: unknown -> [111] [1,0] 246x+128x²-27y-1152y²-16384y³+118 endexp[55] expanding queue[56]^28,meter=[2,2]: 14x+64x²-363y-2112y²-4096y³-20 [7+128x,11+128y]: unknown -> [112] [0,0] 14x+128x²-363y-4224y²-16384y³-10 [71+128x,11+128y]: unknown -> [113] [1,0] 142x+128x²-363y-4224y²-16384y³+29 endexp[56] expanding queue[57]^28,meter=[2,2]: 78x+64x²-363y-2112y²-4096y³+3 [39+128x,75+128y]: unknown -> [114] [0,1] 78x+128x²-16875y-28800y²-16384y³-3284 [103+128x,75+128y]: unknown -> [115] [1,1] 206x+128x²-16875y-28800y²-16384y³-3213 endexp[57] expanding queue[58]^29,meter=[2,2]: 46x+64x²-5547y-8256y²-4096y³-1234 [23+128x,43+128y]: unknown -> [116] [0,0] 46x+128x²-5547y-16512y²-16384y³-617 [87+128x,43+128y]: unknown -> [117] [1,0] 174x+128x²-5547y-16512y²-16384y³-562 endexp[58] expanding queue[59]^29,meter=[2,2]: 110x+64x²-5547y-8256y²-4096y³-1195 [55+128x,107+128y]: unknown -> [118] [0,1] 110x+128x²-34347y-41088y²-16384y³-9547 [119+128x,107+128y]: unknown -> [119] [1,1] 238x+128x²-34347y-41088y²-16384y³-9460 endexp[59] expanding queue[60]^30,meter=[2,2]: 30x+64x²-2187y-5184y²-4096y³-304 [15+128x,27+128y]: unknown -> [120] [0,0] 30x+128x²-2187y-10368y²-16384y³-152 [79+128x,27+128y]: unknown -> [121] [1,0] 158x+128x²-2187y-10368y²-16384y³-105 endexp[60] expanding queue[61]^30,meter=[2,2]: 94x+64x²-2187y-5184y²-4096y³-273 [47+128x,91+128y]: unknown -> [122] [0,1] 94x+128x²-24843y-34944y²-16384y³-5870 [111+128x,91+128y]: unknown -> [123] [1,1] 222x+128x²-24843y-34944y²-16384y³-5791 endexp[61] expanding queue[62]^31,meter=[2,2]: 62x+64x²-10443y-11328y²-4096y³-3194 [31+128x,59+128y]: unknown -> [124] [0,0] 62x+128x²-10443y-22656y²-16384y³-1597 [95+128x,59+128y]: unknown -> [125] [1,0] 190x+128x²-10443y-22656y²-16384y³-1534 endexp[62] expanding queue[63]^31,meter=[2,2]: 126x+64x²-10443y-11328y²-4096y³-3147 [63+128x,123+128y]: unknown -> [126] [0,1] 126x+128x²-45387y-47232y²-16384y³-14507 [127+128x,123+128y]: unknown -> [127] [1,1] 254x+128x²-45387y-47232y²-16384y³-14412 endexp[63] ---------------- level 7 Maximum level 7 [128] mod 2: x²-y³+2
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
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clc; funcprot(0); //Example 11.3 Lift at subsonic speed // Initialisation of variables alp_z = -4; //Angle of attack at zero lift M16 = 0.16; Cl = 0.3; alp = 1.5; M0 = 0; M65 = 0.65; alp25 = 2.5; // Calculations //At M = 1.6 DCl_by_Dalp16 = Cl/(alp-alp_z); //At M = 0 DCl_by_Dalp0 = DCl_by_Dalp16*sqrt(1-M16^2); ////At M = 0.65 DCl_by_Dalp65 = DCl_by_Dalp0/sqrt(1-M65^2); Cl25 = (alp25 - alp_z)*DCl_by_Dalp65; //Results disp(Cl25,"Lift Coefficient at alpha = 2.5 degree: ") ;
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// Example no 8.1 // To compute the mean square error distortion and output signal-to-distortion ratio. // Page no. 420 clc; clear all; //Given data l1=1; // 1st Quantization level l2=3; // 2nd Quantization level l3=5; // 3rd Quantization level l4=7; // 4th Quantization level U1=(l1+l2)/2; // upper boundary of 1st level U2=(l2+l3)/2; // upper boundary of 2nd level U3=(l3+l4)/2; // upper boundary of 3rd level U4=l4+(U1-l1); // upper boundary of 4th level L1=l1-(U1-l1); // Lower boundary of 1st level D1=integrate('(x^3-2*x^2+x)/32','x',L1,U1); // Mean square error distortion of 1st level D2=integrate('(x^3-6*x^2+9*x)/32','x',U1,U2); // Mean square error distortion of 2nd level D3=integrate('(x^3-10*x^2+25*x)/32','x',U2,U3); // Mean square error distortion of 3rd level D4=integrate('(x^3-14*x^2+49*x)/32','x',U3,U4); // Mean square error distortion of 4th level D=D1+D2+D3+D4; // Total square error distortion P=integrate('x^3/32','x',L1,U4); // Signal power SDR=10*log10(P/D); // Output signal-to-distortion ratio. // Displaying the result in command window printf('\n The mean square error distortion = %0.3f',D); printf('\n The output signal-to-distortion ratio = %0.2f dB',SDR); printf('\n To minimize the distortion, we need to place the quantization levels closer at amplitudes close to 8 and farther at amplitudes close to zero.'); printf('\n This quantizer would be optimal for an input with a uniform pdf.');
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// C-Exercise 17 // Jurian Kahl // Nattawut Phanrattinon // download distfun package atomsInstall("distfun"); // Part a) // Hill estimator function function alpha = Hill_Estimator(x, k) y = gsort(x); alpha = k/sum( log(y(1:(k-1))) - log(y(k))); endfunction // Part b) // Hill plot function function Hill_Plot(x) y = x(x>0); n = length(y); for k = 2:n a(k-1) = Hill_Estimator(y, k); end plot(2:n, a'); endfunction // part(c) scf(0); clf(); m = 3; N = 500; lambda = 1; subplot(3,1,1); title ("t-distribution with df = 3"); xlabel("k"); ylabel("Hill estimator"); for k=1:m Hill_Plot(distfun_trnd(3, N, 1)); end subplot(3,1,2); title ("t-distribution with df = 8"); xlabel("k"); ylabel("Hill estimator"); for k=1:m Hill_Plot(distfun_trnd(8, N, 1)); end subplot(3,1,3); title ("Exponential distribution with lambda = 1"); xlabel("k"); ylabel("Hill estimator"); for k=1:m Hill_Plot(grand(N,1,'exp',lambda)); end // Part d) // VaR and ES function [VaR,ES]=VaR_ES_Hill(x,p,k) N = length(x); alpha = Hill_Estimator (x,k); y=gsort(x); // From section 3.2.3 Equation (3.5) VaR=(N/k*(1-p))^(-1/alpha)*y(k); // From section 3.2.4 ES=(1-1/alpha)^(-1)*VaR; endfunction // Part e) data = csvRead('risk1920_Exercise_17_data.dat') scf(1); clf(); Hill_Plot(data); title("Hill plot"); //choose k = 40 for reasonable choice since it seems to be constant after some initial oscilations from Hill plot above p = 0.98; k = 40; [VaR,ES]=VaR_ES_Hill(data,p,k) disp ("for k=40 VaR="+string(VaR)+" ES="+string(ES));
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// ============================================================================= // gfx4scilab - drawing // dgerod@xyz-lab.org.es // ============================================================================= function lg_enable(isOn) global logCfg; if isOn == %t then logCfg.enabled = %t; else logCfg.enabled = %f; end endfunction // ----------------------------------------------------------------------------- function lg_setFileMode(isFileMode) global logCfg; if isFileMode == %t then logCfg.logFile.fileType = %t; else logCfg.logFile.fileType = %f; end endfunction // =============================================================================
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clc; clear; format('e',11); v=4*10^4; e=-1.6*10^-19; Me=9.1*10^-31; //Me=mass of electron. B=0.4*10^-4; Wc=-e*B/Me; //Wc=angular frequency. f=Wc/(2*3.14); R=v/Wc; disp(f,"The frequency of the electron(in Hz)="); disp(R,"The redius of the circle,R(in meter)=");
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errcatch(-1,"stop");mode(2);//Exa1 ; ; //given data is : P=10000;//in rupees n=3;//in years r=10;//% per annum A=P*(1+r/100)^n; CI=A-P;//in rupees disp("Compound interest is : "+string(CI)+" Rupees.") exit();
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<?xml version="1.0" encoding="utf-8"?> <test> <description>55 Artery Network, P=5</description> <executable>PulseWaveSolver</executable> <parameters>55_Artery_Network.xml</parameters> <files> <file description="Session File">55_Artery_Network.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="A" tolerance="1e-12">35.2833</value> <value variable="u" tolerance="1e-12">66.3241</value> </metric> <metric type="Linf" id="2"> <value variable="A" tolerance="1e-12">6.35242</value> <value variable="u" tolerance="1e-12">22.2798</value> </metric> </metrics> </test>
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//Exa:2.7 clc; clear; close; //Given: m1=0.55;//modulation percent 1 m2=0.65;//modulation percent 2 Pc=360;// in watts mt=sqrt(m1*m1+m2*m2); printf("\n\n\t total modulation = %f ",mt); Pb=(mt*mt)*Pc/2; printf("\n\n\t total sideband power radiated = %f W",Pb);
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clc // Given that m1 = 4.00260 // mass of He(4) in a.m.u. m2 = 0.00055 // mass of electron in a.m.u. m3 = 12 // mass of C(12) in a.m.u. // Sample Problem 27 on page no. 12.40 printf("\n # PROBLEM 27 # \n") printf(" Standard formula used \n") printf(" del_E = del_m * c^2 \n") delta_m = 3 * m1 - m3 E = delta_m * 931 printf("\n Energy produce by each reaction is %f MeV.",E)
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clc //initialisation of variables logh= 0.1761 logk= -0.415 logv= 0.3010 //CALCULATIONS n= (logh-logk)/logv //RESULTS printf ('n = %.2f ',n)
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clc //solution //given //ref fig 10.32 and 33 s=6//mm P=20*10^3//N l=40//mm b=90//mm //let t throat thickness //let x is distance of Cg from left edge x=l^2/(2*l+b)//mm //J=t*[(b+2*l)^3/12-(l^2*(b+l)^2/(b*2*l))] J=0.707*s*[{(b+2*l)^3/12}-{(l^2*(b+l)^2)/(b+2*l)}]//mm^4 printf("the value of J is,%f mm^4\n",J) Bg=40 e=200-x//mm r1=Bg-x//mm Ab=(90/2)//mm r2=sqrt(Ab^2+Bg^2)//mm //cos(q)=r2/r1=0.5625 a=0.5625 A=2*0.707*s*l+(0.707*s*b)//mm^2 t1=P/A//N/mm^2' t2=P*e*r2/J//N/mm^2 T=sqrt(t1^2 + t2^2 + 2*t1*t2*a)//N/mm^2' printf( "the value of x is,%f mm\n",x) printf("the value of direct shear stress is,%f N/mm^2\n",t1) printf("the value of secondary shear stress is,%f N/mm^2\n",t2) printf("the max shera stress is,%f N/mm^2",T)
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function [tree] = sci_studyfile(tree) // Copyright INRIA (Generated by M2SCI) // Conversion function for Matlab studyfile() // Input: tree = Matlab funcall tree // Ouput: tree = Scilab equivalent for tree // dims(i,:) is the ith output argument dimensions vector dims=list(list(1,-1),list(1,-1),list(1,-1),list(1,1)) // dims(i,:) is the ith output argument dimensions vector vtype=[1;1;1;1] // prop(i) is the ith output argument property prop=[0;0;0;0] for k=1:lhs tree.lhs(k).dims=dims(k) tree.lhs(k).vtype=vtype(k) tree.lhs(k).property=prop(k) end endfunction
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//To find the pu voltages and tolerable and favourable voltages //Page 310 clc; clear; N=19; //Number Transformers St=500; //Load on each transformer in kVA L=5096+(%i*3158); //Load Vlf=114; //Favourable Voltage Vlt=111; //Tolerable Volatage Vb=125; //Base Voltage //Per Unit Tolerable and favourable voltages puVlf=Vlf/Vb; puVlt=Vlt/Vb; ZM=0.181+(%i*0.115); //The Positive Sequence Impedance ZTi=0.0086+(%i*0.0492); //Transformer Impedance for 500kVA ZT=2*ZTi; //Transformer Impedance for 1000kVA AAF=N*St/abs(L); //Actual Application Factor printf('\na) The Lowest favourable Voltage is %g pu and The Lowest tolerable voltage is %g pu\n',puVlf,puVlt) printf('b) There Are No buses in Table 6-5, for the first contingency outage which satisfy the necessary condition\n') printf('c) For Second Contingency Outage\n') printf('1) Less than Favourable Voltage are B,C,J,K,R and S\n') printf('2) Less than Tolerable Voltage are B,C,J,K.\n') printf('d) ZM/ZT = %g and (1/2)*ZM/ZT = %g respectively.\n',(abs(ZM)/abs(ZT)),(1/2)*(abs(ZM)/abs(ZT))) printf('The Actual Application Factor is %g\n',AAF) printf('Therefore the Design of this network is sufficient\n')
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//Example 4.14. clc disp("R = 6 k-ohm, C = 1500 pF, R_C = 18 k-ohm") k=18/6 disp(k,"Now K = R_C / R =") disp("Therefore, f = 1 / 2*pi*R*C*sqrt(6+4K)") f=(1/(2*%pi*(6*10^3)*(1500*10^-12)*sqrt(6+12)))*10^-3 // in kHZ format(6) disp(f," f(in kHz) =") hfe=(4*3)+23+(29/3) disp(hfe," (h_fe)min = 4K + 23 + 29/K =")
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//Rodríguez Montiel Moisés Ulises //2NM51 function y = interpolLagrange(funcTab, grado, x) y = 0 [n, m] = size(funcTab) if(n <> 2) error("No es una función tabular") end if ~(isreal(funcTab)) error('Elementos no numericos o complejos en el arreglo.'); end grado = round(grado); if (or([~isreal(grado), grado <= 0])) error('El grado tiene que ser un valor entero positivo (mayor a 0).'); end if grado > m error('El grado del polinomio es mayor al permitido por el metodo.'); end for i=1:1:grado numerador = 1; denominador = 1; for j=1:1:grado if j ~= i numerador = numerador * (x - funcTab(1, j)); denominador = denominador * (funcTab(1, i) - funcTab(1, j)); end end y = y + (numerador/denominador) * funcTab(2, i); end endfunction
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//Example 2.7.3.a: Arithmetic mean clc; clear; close; //given data : X1=147.2;// in nF X2=147.4;// in nF X3=147.9;// in nF X4=148.1;// in nF X5=148.1;// in nF X6=147.5;// in nF X7=147.6;// in nF X8=147.4;// in nF X9=147.6;// in nF X10=147.5;// in nF AM=(X1+X2+X3+X4+X5+X6+X7+X8+X9+X10)/10; disp(AM,"Arithmetic mean,AM(nF) = ")
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//Ex 5.12 clc;clear;close; format('v',4); tau=1;//ms //R1/R2=1.8:9;given range //Let R1/R2=1.8 R1BYR2=1.8;//ratio Beta1=1/(R1BYR2+1); R1BYR2=9;//ratio Beta2=1/(R1BYR2+1);//unitless Beta=Beta1:Beta2;//Range of Beta //For fmin Tmax=2*log((1+Beta1)/(1-Beta1));//ms fmin=1000/Tmax;//Hz //For fmax Tmin=2*log((1+Beta2)/(1-Beta2));//ms fmax=1/Tmin;//kHz disp("Frequency range is "+string(fmin)+" Hz to "+string(fmax)+" kHz");
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// Example 3.4 // Determine (a) Circulating current in the paralleled secondaries // (b) Circulating current as a percent of the rated current of transformer A // (c) Percent difference in secondary voltage that caused the circulating current // Page No. 104 clc; clear; close; // Given data S=100000; // Transformer A and B rating VLSA=460; // Voltage at the low side of transformer A VLSB=450; // Voltage at the low side of transformer A RPUA=0.0136; // Percent resistance of transformer A XPUA=0.0350; // Percent reactance of transformer A RPUB=0.0140; // Percent resistance of transformer B XPUB=0.0332; // Percent reactance of transformer B // (a) Circulating current in the paralleled secondaries IA= S/VLSA; // Rated low side current for transformer A IB= S/VLSB; // Rated low side current for transformer B ReqA=RPUA*VLSA/IA; // Equivalent resistance of transfomer A ReqB=RPUB*VLSB/IB; // Equivalent resistance of transfomer B XeqA=XPUA*VLSA/IA; // Equivalent reactance of transfomer A XeqB=XPUB*VLSB/IB; // Equivalent reactance of transfomer B // Impedance of the closed loop formed by two secondaries is Zloop=ReqA+%i*XeqA+ReqB+%i*XeqB; // Complex to Polar form... Zloop_Mag=sqrt(real(Zloop)^2+imag(Zloop)^2); // Magnitude part Zloop_Ang=atan(imag(Zloop),real(Zloop))*180/%pi; // Angle part
 Icirc_Mag=(VLSA-VLSB)/Zloop_Mag; // Circulating current magnitude Icirc_Ang=0- Zloop_Ang; // Circulating current angle // (b) Circulating current as a percent of the rated current of transformer A IcircA=Icirc_Mag*100/IA; // (c) Percent difference in secondary voltage that caused the circulating current PD=(VLSA-VLSB)*100/VLSB; // Display result on command window printf("\n Circulating current magnitude = %0.1f A ",Icirc_Mag); printf("\n Circulating current angle = %0.1f deg ",Icirc_Ang); printf("\n Circulating current as a percent of the rated current = %0.1f Percent ",IcircA); printf("\n Percent difference in secondary voltage = %0.1f Percent ",PD);
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// Given:- y1 = 0.8 // mole fraction of CO2 y2 = 0.2 // mole fraction of O2 T1 = 700.0 // in kelvin p1 = 5.0 // in bars V1 = 3.0 // in m/s p2 = 1.0 // in bars // Part(a) // From table A-23 sO2barT1 = 231.358 sCO2barT1 = 250.663 // Calculations RHS = y2*sO2barT1 + y1*sCO2barT1 + 8.314*log(p2/p1) // Using table A-23 LHSat510K = y2*221.206 + y1*235.7 LHSat520K = y2*221.812 + y1*236.575 // Using linear interpolation, T2 = 510 +((520-510)/(LHSat520K-LHSat510K))*(RHS-LHSat510K) // Result printf( 'The temperature at the nozzle exit in K is: %f',T2); // Part(b) // From table A-23 sbarO2T2 = 221.667 // in kj/kmol.K sbarO2T1 = 231.358 // in kj/kmol.K sbarCO2T2 = 236.365 // in kj/kmol.K sbarCO2T1 = 250.663 // in kj/kmol.K // Calculations deltasbarO2 = sbarO2T2-sbarO2T1-8.314*log(p2/p1) // in kj/kmol.K deltasbarCO2 = sbarCO2T2-sbarCO2T1-8.314*log(p2/p1) // in kj/kmol.K // Results printf( 'The entropy changes of the CO2 from inlet to exit, in KJ/Kmol.K is: %f',deltasbarCO2) printf( 'The entropy change of the O2 from inlet to the exit in kj/kmol.k is: %f',deltasbarO2) // Part(c) // From table A-23, the molar specific enthalpies of O2 and CO2 are h1barO2 = 21184.0 h2barO2 = 15320.0 h1barCO2 = 27125.0 h2barCO2 = 18468.0 // Calculations M = y1*44.0 + y2*32.0 // apparent molecular weight of the mixture in kg/kmol deltah = (1.0/M)*(y2*(h1barO2-h2barO2) + y1*(h1barCO2-h2barCO2)) V2 = sqrt(V1**2+ 2*deltah*10**3) // Result printf( 'The exit velocity in m/s is: %f',V2)
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hi this is tst file i want to create and push
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// Example 4.3 // Determine (a) Synchronous speed (b) Slip (c) Rotor impedance (d) Rotor current // (e) Rotor current if changing the shaft load resulted in 1.24 percenr slip // (f) Speed for the condition in (e) // Page No. 146 clc; clear; close; // Given data fs=60; // Frequency p=6; // Number of poles nr=1164; // Rotor speed Rr=0.10; // Equivalent resistance Xbr=0.54; // Equivalent reactance Ebr=150; // Blocked rotor voltage per phase s1=0.0124; // Percent slip // (a) Synchronous speed ns=120*fs/p; // Speed // (b) Slip s=(ns-nr)/ns; // (c) Rotor impedance Zr=(Rr/s)+%i*Xbr; // Complex to Polar form... Zr_Mag=sqrt(real(Zr)^2+imag(Zr)^2); // Magnitude part Zr_Ang=atan(imag(Zr),real(Zr))*180/%pi; // Angle part
 // (d) Rotor current Ir_Mag=Ebr/Zr_Mag; // Magnitude Ir_Ang=0-Zr_Ang; // Angle // (e) Rotor current if changing the shaft load resulted in 1.24 percent slip Zrnew=Rr/s1+%i*Xbr; // Complex to Polar form... Zrnew_Mag=sqrt(real(Zrnew)^2+imag(Zrnew)^2); // Magnitude part Zrnew_Ang=atan(imag(Zrnew),real(Zrnew))*180/%pi; // Angle part
 Irnew_Mag=Ebr/Zrnew_Mag; // Magnitude Irnew_Ang=0-Zrnew_Ang; // Angle // (f) Speed for the condition in (e) nr=ns*(1-s1); // Display result on command window printf("\n Synchronous speed = %0.0f r/min ",ns); printf("\n Slip = %0.3f ",s); printf("\n Rotor impedance magnitude = %0.2f Ohm ",Zr_Mag); printf("\n Rotor impedance angle = %0.2f deg ",Zr_Ang); printf("\n Rotor current magnitude = %0.1f Ohm ",Ir_Mag); printf("\n Rotor current angle = %0.1f deg ",Ir_Ang); printf("\n Rotor current magnitude by changing the shaft load = %0.1f Ohm ",Irnew_Mag); printf("\n Rotor current angle by changing the shaft load = %0.2f deg ",Irnew_Ang); printf("\n New rotor speed = %0.0f r/min ",nr);
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//Solutions to Problems In applied mechanics //A N Gobby clear all; clc //initialisation of variables w=4//lbf h=40//lbf/ft d=2//in g=32.2//ft/s //CALCULATIONS P=(d*%pi)*sqrt(w/(h*g))//sec V=(d*%pi*d)/(P*12)//ft/s M=(d*%pi/P)^2*(d/12)//ft/s //RESULTS printf('the period of vibration=% f sec',P) printf('Maximum veloity=% f ft/s',V) printf('Maximum acceleration=% f ft/s',M)
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function plot_stencil(d) scf(); a = gca(); // [xmin,ymin; xmax,ymax] a.data_bounds = [ min(d(1,:))-2, min(d(2,:))-2; max(d(1,:))+2, max(d(2,:))+2 ]; plot(d(1,:), d(2,:), 'O'); yy = unique(d(2,:)); yy = yy(:)'; // now, yy is a row vector X = repmat([min(d(1,:))-2; max(d(1,:))+2], 1, length(yy)); Y = repmat(yy, 2, 1); plot(X, Y, 'blue'); endfunction function out = unfold(d, n, min_gap) batches = []; y_group = gsort(unique(d(2,:)), 'g', 'i'); y_weight = []; for i = 1 : length(y_group) y_weight = [y_weight, length(find(d(2,:) == y_group(i)))]; end out = []; endfunction function out = sort_by_y_coord(d) d_swapped = [d(2,:); d(1,:)]; d_swap_and_sorted = gsort(d_swapped, 'lc', 'i'); d_sorted = [d_swap_and_sorted(2,:); d_swap_and_sorted(1,:)]; out = d_sorted; endfunction function out = find_y_interval_of_adjacent_y_groups(d) d_sorted_by_y_coord = sort_by_y_coord(d); y1 = d_sorted_by_y_coord(2,:); if length(y1) < 2 then out = []; return; end y1 = unique(y1); y2 = [y1(2:$), 0]; y_diff = [y2; (y2 - y1)]; y_diff(:, find(y_diff(2,:) <= 0)) = []; out = y_diff; endfunction function out = penalty(s, y, w_total, w_avg, w, a, b, c) out = a * abs(y - s) + b * (w_total + w - w_avg) + c; endfunction function out = pp(d, m, min_gap, l) y = gsort(unique(d(2,:)), 'g', 'i'); // number of distinct y values n = length(y); // weight vector w = []; for i = 1 : n w = [w, length(find(d(2,:) == y(i)))]; end // range of movement of tip number i under the situation that all other // tips been moved to both ends of the rack. limits = []; for i = 1 : m limits = [limits; (i - 1) * min_gap, l - ((m - i) * min_gap)]; end mprintf("limits: \n %e \n\n", limits); dp = list(); wtotal = list(); for i = 1 : n dp_i = list(); wtotal_i = list(); for j = 1 : m A_j = zeros(n, n); next = find(y > limits(j,1) && y < limits(j,2)); mprintf("available next(j=%d): \n %d \n\n", j, next); for r = 1 : n p = [next; %nan * ones(next)]; for s = next if () end end dp_i(j) = A_j; end dp(i) = dp_i; wtotal(i) = wtotal_i; end out = []; endfunction
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global Ut_sim Kappa_sim; function block=Hyst_diff_c(block,flag) //disp(flag) if flag==1 in_out_num = block.ipar(1); //Vectorized row_vec_io = 1:in_out_num; // Row vector for input & output block.outptr(1)(row_vec_io)=block.x(2*row_vec_io); //Output elseif flag==0 in_out_num = block.ipar(1); //Vectorized row_vec_io = 1:in_out_num; // Row vector for input & output Cout=1e-12; C=100e-15; Ibias=block.rpar(row_vec_io) block.xd(2*row_vec_io)=(Ibias./Cout).*tanh((Kappa_sim*(block.inptr(1)(row_vec_io)- block.x(2*row_vec_io-1)))/(2*Ut_sim)); //OTA computation Ioffp=0; Ioffn=0; Voffp=0; Voffn=0; V1=block.inptr(1)(row_vec_io); V2=block.x(2*row_vec_io-1) m_tanh=tanh((Kappa_sim/(2*Ut_sim))*(V1-V2)) I1=Ibias*(0.5+0.5*m_tanh+Voffp)+Ioffp; I2=Ibias*(0.5-0.5*m_tanh+Voffn)+Ioffn; sig=1e-4; Vdd=2.5 Iout=(-I1*(exp(-sig*block.x(2*row_vec_io) /Ut_sim))*(1-exp(-(Vdd-block.x(2*row_vec_io) )/Ut_sim)))+(I2*(exp(-sig*(Vdd-block.x(2*row_vec_io))/Ut_sim))*(1-exp(-block.x(2*row_vec_io)/Ut_sim))); // //disp(Iout) block.xd(2*row_vec_io) =- Iout/Cout; // Isatn=53.58e-9; Isatp=110e-9; sigma=5e-2 Vtp=0.866; Vtn= 0.313; Inmos=Isatn * log(1 + exp((Kappa_sim*(block.x(2*row_vec_io)-Vtn) - block.x(2*row_vec_io-1) + sigma*2.5)/Ut_sim ))^2 - Isatn * log(1 + exp((Kappa_sim*(block.x(2*row_vec_io)-Vtn) + sigma*block.x(2*row_vec_io-1) - 2.5)/Ut_sim ))^2 Ipmos=Isatp * log(1 + exp((Kappa_sim*(2.5 - block.x(2*row_vec_io)-Vtp) - (2.5 - block.x(2*row_vec_io-1)) + sigma*2.5)/Ut_sim ))^2 -Isatp * log(1 + exp((Kappa_sim*(2.5 - block.x(2*row_vec_io)-Vtp) +sigma* (2.5 - block.x(2*row_vec_io-1)) - 2.5)/Ut_sim ))^2 Iout1=Inmos - Ipmos; block.xd(2*row_vec_io-1)=Iout1./C;//Vc of the hyst diff end endfunction
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// PARCIAL // (1) /* function f = fx(x) f = 4*x(1) + 4*x(2) - 2*x(3) disp(-7*x(1)+10*x(2)+2*x(3)) disp(-7*x(1)+10*x(2)+2*x(3) >= 59) disp(-4*x(1)+7*x(2)+2*x(3)) disp(-4*x(1)+7*x(2)+2*x(3) >= 47) disp(2*x(1)-3*x(2)-1*x(3)) disp(2*x(1)-3*x(2)-1*x(3) >= -21) disp(16*x(1)-25*x(2)-5*x(3)) disp(16*x(1)-25*x(2)-5*x(3) >= -155) endfunction function f = fy(x) f = 59*x(1) + 47*x(2) - 21*x(3)- 155*x(4) disp(-7*x(1) - 4*x(2) + 2*x(3) + 16*x(4)) disp(-7*x(1) - 4*x(2) + 2*x(3) + 16*x(4) <= 4) disp(10*x(1) + 7*x(2) - 3*x(3) - 25*x(4)) disp(10*x(1) + 7*x(2) - 3*x(3) - 25*x(4) <= 4) disp(2*x(1) + 2*x(2) - 1*x(3) -5*x(4)) disp(2*x(1) + 2*x(2) - 1*x(3) -5*x(4) <= -2) endfunction x = [0 ; 5 ; 6] y = [0 ; 10 ; 22 ; 0] fx = fx(x) disp('----------------') fy = fy(y) disp(fy,'f(y)',fx,'f(x)') */ // (2) function y = f3x(x) y = x(1)**2 + x(2)**2 + x(3)**2 + 6*x(1)*x(2) +4*x(1)*x(3)+8*x(2)*x(3) -12*x(1)-4*x(2) - 2*x(3) //disp(x,'Este x') //disp(x(1)<=1.5) //disp(x(2)<=1.5) //disp(x(3)<=1.5) //disp(x(2) + x(3) ==2) endfunction x3 = [1.5 ; 1 ; 1] q = f3x(x3) disp(q,'f(x)') gr = numderivative (f3x,x3)' disp(gr,'gr') o = [0 1 0] z = -o'\gr disp(z,'u') disp(z*o'+gr,'sol total') // (3) /* function y = fx(x) disp(x,'Para x = ') y = (x(1)-6)**4 + 2*(x(1)+x(2)-13)**2 disp(x(1)+x(2) == 10) disp(x(1) >= 4) disp(x(2) >= 0) endfunction x1 = [4 ; 6] x2 = [5 ; 5] f1 = fx(x1) f2 = fx(x2) disp(f2,'f(x2)',f1,'f(x1)') x = [6 ; 7] //grx = numderivative(fx,x) //disp(grx,'grx') grx1 = numderivative(fx,x1)' grx2 = numderivative(fx,x2)' disp(grx2,'grx2',grx1,'grx1') a = [1 0 1; 0 1 1] sol1 = -a\grx1 u11 = sol1(1) u21 = sol1(2) v11 = sol1(3) disp(v11,'v11',u21,'u2',u11,'u1') sol2 = -a\grx2 u12 = sol2(1) u22 = sol2(2) v12 = sol2(3) disp(v12,'v12',u22,'u2',u12,'u1') disp(sol2,'kkt x2',sol1,'kkt x1') disp('---------------------------------------------') kktx1 = grx1 + u11*[1;0] + u21 * [0;1] + v11*[1;1] kktx2 = grx2 + u12*[1;0] + u22 * [0;1] + v12*[1;1] disp(kktx2,'kktx2',kktx1,'kktx1') */
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//pathname=get_absolute_file_path('5.10.sce') //filename=pathname+filesep()+'5.10-data.sci' //exec(filename) //Initial pressure(in kPa): p1=3000 //Initial volume(in m^3): v1=0.05 //Final volume(in m^3): v2=0.3 //Value of n: n=1.4 //Final pressure(in MPa): p2=p1*((v1/v2)^n) //Entropy change: dS=0 //Change in enthalpy(in kJ): dH=((p1*(v1^n))^(1/n))*(p1^((n-1)/n)-p2^((n-1)/n))/((n-1)/n) printf("\nRESULT\n") printf("\nEnthalpy change = %f kJ",dH) printf("\nEntropy change = %d",dS)
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clc(); clear; // To calculate the de Broglie wavelength c=3*10^8; //velocity of light in m/s v=c/10; //velocity of proton in m/s m=1.67*10^(-27); //mass of proton in kg h=6.626*10^(-34); lamda=h/(m*v); //de Broglie wavelength printf("The de Broglie wavelength in metres is"); disp(lamda);
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example14_sce.sce
//chapter 3 //example 3.14 //page 101 printf("\n") printf("given") Edc=20;vo=.24;Vo=20;Il=40*10^-3;fr=120; Eomax=(3.14*Edc)/2 Epeak=(4*Eomax)/(3*3.14) vi=Epeak; Rl=Vo/Il Xlc=(2*Rl)/3 Lc=Xlc/(2*3.14*fr) L=1.25*Lc; Xl=2*3.14*fr*L Xc=Xl/((vi/vo)+1) C1=1/(2*3.14*fr*Xc)
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augstate.sci
function[]=augstate(sys) // //Calling Sequence //function[]=augstate(sys) //Parameters //sys- SISO or MIMO state space models //Description //augstate function appends states to the outputs of a state-space model //this command is useful to close the loop on a full-state feedback gain u = Kx. After preparing the plant with augstate,you can use the FEEDBACK command to derive the closed-loop model. // augstate function is not defined for array of SISO. //Examples: // 1.aa=syslin('c',[1,3;4,5],[6;8],[2,3],[1]); // a1=augstate(aa) // 2.ab=syslin('c',[1,2;3,4],[4,5;6,7],[8,9;0,1],[1,0;0,5]) // a2=augstate(ab) //See also // siso ,mimo //Authors //Rutuja Moharil //Bibliography //http://www-rohan.sdsu.edu/doc/matlab/toolbox/control/ref/augstate.html //http://octave.sourceforge.net/control/function/augstate.html select typeof(sys) case "state-space" then // check if the entered system is state space model [A B C D]=abcd(sys); // extracting A,B,C,D matrices t=mtlb_size(A); [row,col]=size(B); if (isempty(C)==%t) then C=zeros(size(A,1),size(A,2)); end if(isempty(D)==%t) then D=zeros(size(C,1),size(B,2)); end C=cat(1,C,eye(t,t)) // cocatenation of matrix C and identity matrix of size of A D=cat(1,D,zeros(t,col)) // cocatenation of matrix A and null matrix of row of A and column of D if sys.dt=='c' then sysa=syslin('c',A,B,C,D); disp(sysa) else if sys.dt=='d' then dt=1 else dt=sys.dt end sysa=syslin('d',A,B,C,D); disp(sysa) disp (dt,"Sample time :") end else // for any other system display the error error(msprintf(_("\n %s: Wrong type of input argument #%d: State space model expected.\n"),"augstate",1)) end; endfunction
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ex2_22.sce
//ex2.22 Design the transmission line section as areactive element f=6e9; w=2*%pi*f; L=0.01e-6; X=w*L; Z0=150; lamda=4.0; b=2*%pi/lamda; loc=(1/b)*acot(-X/Z0); //length of the line disp('The reactance to be realized is '+string(X)+' ohm'); disp('The length of the line therefore is = '+string(loc)+' cm');
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ex3_5.sce
//Solutions to Problems In applied mechanics //A N Gobby clear all; clc //initialisation of variables w=3//lbf v=5//ft a=60//degree g=32.2//ft u=28.4//ft/s t=25.4//ft/s q=12//ft p=1.5//ft //CALCULATIONS U=sqrt(g*v)//ft/s T=w*(t)^2/(2*g)+w*cosd(a)//lbf W=q+p//lbf //RESULTS printf('the tension in the string at position C=% f lbf',W)
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Ex9_2.sce
//Ex:9.2 clc; clear; close; r1=1000; r2=1000; c=100*10^-9; f=(1/(2*%pi*c*r1)); printf("The freq of oscillation at 1 kohm= %f Hz",f); R1=6000; R2=6000; F=(1/(2*%pi*c*R1)); printf("\nThe freq of oscillation at 6 kohm= %f Hz",F);
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Ex14_1.sce
clc; //page 738 //problem 14.1 //Boltzman constant k = 1.3806488 × 10-23 m2 kg s-2 K-1 k = 1.3806488 * 10^-23; //Let room temperature be 27 C T = 27 + 273; //Bandwidth BW = 10 MHz BW = 10 * 10 ^6; //For (a) //Let the equivalent resistance be Ra Ra = 10 + 10; //RMS Noise Voltage be Va Va = (4*k*T*Ra*BW)^0.5; disp('The rms voltage at output a is '+string(Va)+' Volt'); //For (b) //Let the equivalent resistance be Rb Rb = (10 * 10)/(10+10); //RMS Noise Voltage be Vb Vb = (4*k*T*Rb*BW)^0.5; disp('The rms voltage at output b is '+string(Vb)+' Volt'); //For (c) Rc = 10; C = 1*10^-9; //In the textbook, the author has forgotten to multiply the result with T, hence has obtained an erroneous result. //The given answer is 28.01uV but the correct answer is found out to be 1.2uV Vc_square = 2*k*integrate('Rc/(1 + (2*%pi*Rc*C*f)^2)','f',-10^7,10^7); Vc = Vc_square^0.5; disp('The rms voltage at output c is '+string(Vc)+' Volt');
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Ex6_27.sce
//=========================================================================== //chapter 6 example 27 clc; clear all; //variable declaration KT = 198; //turn ratio e =0; //ratio error Is = 5; // secondary current in A P = 5; //load in VA Rs = 0.02; //resistance in Ω KN = 200; //KN=KC since e=0 KC = 200; //calculations V2 = P/Is; //secondary voltage in V Es = V2+(Is*Rs); //secondary induced emf in V Ep = Es/KT; //primary induced emf Ie = (KC-KT)*Is; //eddy current loss in A IL = Ep*Ie; //iron loss in W //result mprintf("iron loss = %3.3f mW",(IL*10^3));
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cell2sos1.sce
//i/p is a 1X4 cell c=cell(1,4); c(1,1).entries=[0.3209,0.5183,0.3209]; c(1,2).entries=[1,0.1677,0.2575]; c(1,3).entries=[1,0.8927,1]; c(1,4).entries=[1,0.6196,0.8747]; sos=cell2sos(c); disp(sos); //output //column 1 to 4 // // 0.3209 0.5183 0.3209 1. // 1. 0.8927 1. 1. // // column 5 to 6 // // 0.1677 0.2575 // 0.6196 0.8747 //
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Ex8_4.sce
clear //Given a=60 //degree u=4*3.14*10**-7 //T/A m Bc=2 //Calculation // a=(Bc/2.0)/(tan(60)*180/3.14) B1=(10**-7*tan(60)*(sin(60*180/3.14)+sin(60*180/3.14)))*10 B=3*B1 //Result printf("\n Magnetic fieldat the centroid of the triangle is %0.0f *10**-7 T",B*10**7)
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3211.tst
#---------------------------------------------------------- # In addition to the below 3211.core file this test # also uses an associated "3211.rexx" script as well. #---------------------------------------------------------- *If \$rexx_supported *Message SKIPPING: Testcase 3211 printer *Message REASON: No Hercules Rexx support. *Else *If $rexx_VERSION = '' *Message SKIPPING: Testcase 3211 printer *Message REASON: Rexx is not installed. *Else *If $rexx_package = 'Regina' *Testcase 3211 printer (Regina) # Prepare test environment mainsize 1 numcpu 1 sysclear archlvl 390 loadcore "$(testpath)/3211.core" detach 00f attach 00f 3211 "3211.txt" diag8cmd enable noecho # need diag8 to exec rexx script shcmdopt enable diag8 # rexx script needs shell access # Set needed Hercules Rexx processing options rexx mode subroutine msglevel off msgprefix off errprefix off resolver on syspath on extensions .rexx start auto #--------------------------------------------------- # Define the tests we want to be run # Skip tests 3, 4 and 9 because Regina Rexx sucks. #--------------------------------------------------- r ff0=00000000000000000000000000000000 # (start with none) r ff0=00f1f20000f5f6f7f800000000000000 # (skip 3, 4 and 9) # Run the tests... runtest 0.1 # (plenty of time) # Clean up afterwards detach 000f # (no longer needed) diag8cmd disable noecho # (no longer needed) shcmdopt disable nodiag8 # (no longer needed) *Compare r 1000.10 *Want "Return Code flags" 00000000 00000000 00000000 00000000 *Done *Else *If $rexx_SOURCE = 'DARWIN' *Testcase 3211 printer (Apple) # Prepare test environment mainsize 1 numcpu 1 sysclear archlvl 390 loadcore "$(testpath)/3211.core" detach 00f attach 00f 3211 "3211.txt" diag8cmd enable noecho # need diag8 to exec rexx script shcmdopt enable diag8 # rexx script needs shell access # Set needed Hercules Rexx processing options rexx mode subroutine msglevel off msgprefix off errprefix off resolver on syspath on extensions .rexx start auto #---------------------------------------------------------- # Define the tests we want to be run # Skip tests 3, 4 and 9 because the only OORexx available # for Apple Mac is OORexx 5.0, and it apparently has the # same or similar Rexx bug as Regina! (i.e. for reasons # that are unknown tests 3, 4 and 9 seem to always fail) #---------------------------------------------------------- r ff0=00000000000000000000000000000000 # (start with none) r ff0=00f1f20000f5f6f7f800000000000000 # (skip 3, 4 and 9) # Run the tests... runtest 0.1 # (plenty of time) # Clean up afterwards detach 000f # (no longer needed) diag8cmd disable noecho # (no longer needed) shcmdopt disable nodiag8 # (no longer needed) *Compare r 1000.10 *Want "Return Code flags" 00000000 00000000 00000000 00000000 *Done *Else *Testcase 3211 printer (OORexx) # Prepare test environment mainsize 1 numcpu 1 sysclear archlvl 390 loadcore "$(testpath)/3211.core" detach 00f attach 00f 3211 "3211.txt" diag8cmd enable noecho # need diag8 to exec rexx script shcmdopt enable diag8 # rexx script needs shell access # Set needed Hercules Rexx processing options rexx mode subroutine msglevel off msgprefix off errprefix off resolver on syspath on extensions .rexx start auto # Define the tests we want to be run r ff0=00000000000000000000000000000000 # (start with none) r ff0=00f1f2f3f4f5f6f7f8f9000000000000 # (default = all) # Run the tests... runtest 0.1 # (plenty of time) # Clean up afterwards detach 000f # (no longer needed) diag8cmd disable noecho # (no longer needed) shcmdopt disable nodiag8 # (no longer needed) *Explain *Explain If the above is an "unexpected wait state" of 000100D8 *Explain it means that the DIAG8 instruction completed with a non- *Explain zero condition code. The likely reason for this is the *Explain results buffer wasn't large enough because the Hercules *Explain command the test issued resulted in an unexpected error *Explain message (which couldn't fit into DIAG8's response buffer). *Explain *Explain If any of the below test completion flags are non-zero *Explain it means that particular test has failed. For example, *Explain if the completion flags are 000000F3 F4F5F6F7 F8F90000... *Explain it means that tests 3 thru 9 have failed (F3 = '3' etc). *Explain *Compare r 1000.10 *Want "Return Code flags" 00000000 00000000 00000000 00000000 * ************************************************* * The following should all have valid file sizes. * (i.e. they should all be numbers, e.g. 38, etc) * If they are not numbers (e.g. still "aa"), then * it means the Rexx being used is SEVERLY BROKEN! * ************************************************* * * Test 03 sizes should be the same * Test 04 " " " DIFFERENT * Test 09 " " " the same * * ************************************************* r 2100.100 # SIZ03A (before) r 2200.100 # SIZ03B (after) should be SAME * ************************************************* r 2300.100 # SIZ04A (before) r 2400.100 # SIZ04B (after) should be DIFFERENT * ************************************************* r 2500.100 # SIZ09A (before) r 2600.100 # SIZ09B (after) should be SAME * ************************************************* *Done *Fi *Fi *Fi *Fi
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example19_7.sce
clc // Given that w = 26.91 // isotopic mass of superconducting sample Tc = 1.19 // first critical temperature in K w_ = 32.13 // increased isotope mass of superconducting sample // Sample Problem 7 on page no. 19.16 printf("\n # PROBLEM 7 # \n") printf("Standard formula used \n ") printf(" T_c*M^(1/2) = constant \n") Tc_ = Tc * (w / w_)^(1/2) printf("\n Critical temperature is %f K.",Tc_)
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ko:ji ko:ji N;SG ko:ji kokji N;PL cihil cihil N;SG cihil cihil N;PL si:l si:l N;PL si:l si:l N;SG baʼa baʼad V;IPFV;SG;FUT baʼa ba: V;PRF;SG;PRS baʼa baʼad V;IPFV;PL;FUT baʼa ba'iñ V;IMP;PL;PRS baʼa baʼa V;IPFV;SG;PRS baʼa baʼa V;IPFV;PL;PRS baʼa ba: V;PRF;PL;PRS baʼa ba'iñ V;IMP;SG;PRS ha:hag ha:hag N;SG ha:hag ha:hag N;PL kotoñ kotoñ N;SG kotoñ koktoñ N;PL naw naw N;PL naw naw N;SG s-da:pk s-dadpkad V;IPFV;PL;FUT s-da:pk s-dadpkiñ V;IMP;PL;PRS s-da:pk s-dadpk V;IPFV;PL;PRS s-da:pk s-da:pkiñ V;IMP;SG;PRS s-da:pk s-da:pkad V;IPFV;SG;FUT s-da:pk s-da:pk V;IPFV;SG;PRS wu:s̥ad wu:s̥adad V;IPFV;SG;FUT wu:s̥ad wu:s̥a V;PRF;SG;PRS wu:s̥ad wu:s̥a V;PRF;PL;PRS wu:s̥ad wu:s̥ad V;IPFV;SG;PRS wu:s̥ad wu:s̥ad V;IPFV;PL;PRS wu:s̥ad wu:s̥adiñ V;IMP;PL;PRS wu:s̥ad wu:s̥adiñ V;IMP;SG;PRS wu:s̥ad wu:s̥adad V;IPFV;PL;FUT siswuimad siswuimad V;IPFV;SG;PRS siswuimad siswuimadiñ V;IMP;PL;PRS siswuimad siswuimadiñ V;IMP;SG;PRS siswuimad siswuimad V;PRF;SG;PRS siswuimad siswuimadad V;IPFV;PL;FUT siswuimad siswuimad V;PRF;PL;PRS siswuimad siswuimad V;IPFV;PL;PRS siswuimad siswuimadad V;IPFV;SG;FUT ʼu:gk ʼu:gkiñ V;IMP;SG;PRS ʼu:gk ʼuʼugkiñ V;IMP;PL;PRS ʼu:gk ʼu:gk V;IPFV;SG;PRS ʼu:gk ʼuʼugk V;IPFV;PL;PRS ʼu:gk ʼu:gkad V;IPFV;SG;FUT ʼu:gk ʼuʼugkad V;IPFV;PL;FUT wosonakud̥ wosonakud̥ N;SG wosonakud̥ wopsonakud̥ N;PL ceposid cecposid V;IPFV;PL;PRS ceposid cepos V;PRF;SG;PRS ceposid ceposidad V;IPFV;SG;FUT ceposid cecposidad V;IPFV;PL;FUT ceposid ceposid V;IPFV;SG;PRS ceposid ceposidiñ V;IMP;SG;PRS ceposid cecposidiñ V;IMP;PL;PRS ceposid cecpos V;PRF;PL;PRS s-muʼuk s-muʼuk V;IPFV;SG;PRS s-muʼuk s-muʼukad V;IPFV;SG;FUT s-muʼuk s-muʼumkiñ V;IMP;PL;PRS s-muʼuk s-muʼukiñ V;IMP;SG;PRS s-muʼuk s-muʼumkad V;IPFV;PL;FUT s-muʼuk s-muʼumk V;IPFV;PL;PRS tas̥ga tas̥ga N;SG tas̥ga tas̥ga N;PL ʼi:bhĕ ʼi:bhĕ V;PRF;SG;PRS ʼi:bhĕ ʼi:bhed V;IPFV;SG;FUT ʼi:bhĕ ʼi:bhĕ V;PRF;PL;PRS ʼi:bhĕ ʼi:bhed V;IPFV;PL;FUT ʼi:bhĕ ʼi:bheñ V;IMP;PL;PRS ʼi:bhĕ ʼi:bheñ V;IMP;SG;PRS ʼi:bhĕ ʼi:bhĕ V;IPFV;PL;PRS ʼi:bhĕ ʼi:bhĕ V;IPFV;SG;PRS hewek hewekiñ V;IMP;SG;PRS hewek hewek V;PRF;SG;PRS hewek hewek V;IPFV;SG;PRS hewek hewek V;IPFV;PL;PRS hewek hewekiñ V;IMP;PL;PRS hewek hewek V;PRF;PL;PRS hewek hewekad V;IPFV;PL;FUT hewek hewekad V;IPFV;SG;FUT kahon kahon N;SG kahon kakhon N;PL ceoj ceoj N;SG ceoj cecoj N;PL s-wohocid s-wohocidiñ V;IMP;SG;PRS s-wohocid s-wohoc V;PRF;PL;PRS s-wohocid s-wohocidiñ V;IMP;PL;PRS s-wohocid s-wohocid V;IPFV;PL;PRS s-wohocid s-wohocidad V;IPFV;SG;FUT s-wohocid s-wohocid V;IPFV;SG;PRS s-wohocid s-wohoc V;PRF;SG;PRS s-wohocid s-wohocidad V;IPFV;PL;FUT s-ape s-apeñ V;IMP;PL;PRS s-ape s-aped V;IPFV;SG;FUT s-ape s-apeñ V;IMP;SG;PRS s-ape s-aped V;IPFV;PL;FUT s-ape s-ape V;IPFV;PL;PRS s-ape s-ape V;IPFV;SG;PRS cicwi cicwi V;PRF;SG;PRS cicwi cicwiñ V;IMP;SG;PRS cicwi cicwi V;PRF;PL;PRS cicwi cicwid V;IPFV;PL;FUT cicwi cicwi V;IPFV;SG;PRS cicwi cicwid V;IPFV;SG;FUT cicwi cicwi V;IPFV;PL;PRS cicwi cicwiñ V;IMP;PL;PRS si:s̥p si:s̥p V;IPFV;SG;PRS si:s̥p si:s̥piñ V;IMP;SG;PRS si:s̥p sisis̥p V;IPFV;PL;PRS si:s̥p si:s̥pad V;IPFV;SG;FUT si:s̥p si:s̥ V;PRF;SG;PRS si:s̥p sisis̥piñ V;IMP;PL;PRS si:s̥p sisis̥pad V;IPFV;PL;FUT si:s̥p sisis̥ V;PRF;PL;PRS ʼod̥pig ʼod̥pĭ V;PRF;SG;PRS ʼod̥pig ʼod̥pig V;IPFV;SG;PRS ʼod̥pig ʼoʼod̥pigiñ V;IMP;PL;PRS ʼod̥pig ʼod̥pigiñ V;IMP;SG;PRS ʼod̥pig ʼod̥pigad V;IPFV;SG;FUT ʼod̥pig ʼoʼod̥pigad V;IPFV;PL;FUT ʼod̥pig ʼoʼod̥pig V;IPFV;PL;PRS ʼod̥pig ʼoʼod̥pĭ V;PRF;PL;PRS ʼoʼohana ʼoʼohana N;SG ʼoʼohana ʼoʼohana N;PL kud̥ut kud̥utiñ V;IMP;PL;PRS kud̥ut kud̥utad V;IPFV;PL;FUT kud̥ut kud̥utad V;IPFV;SG;FUT kud̥ut kud̥ut V;IPFV;PL;PRS kud̥ut kud̥utiñ V;IMP;SG;PRS kud̥ut kud̥ut V;IPFV;SG;PRS pa:nt papant V;PRF;PL;PRS pa:nt pa:ntiñ V;IMP;SG;PRS pa:nt papantiñ V;IMP;PL;PRS pa:nt papant V;IPFV;PL;PRS pa:nt pa:ntad V;IPFV;SG;FUT pa:nt papantad V;IPFV;PL;FUT pa:nt pa:nt V;IPFV;SG;PRS pa:nt pa:nt V;PRF;SG;PRS kawhi kawhi N;PL kawhi kawhi N;SG s-iʼowĭ s-iʼowĭ N;PL s-iʼowĭ s-iʼowĭ N;SG pisaltakud̥ pipsaltakud̥ N;PL pisaltakud̥ pisaltakud̥ N;SG memd̥a memd̥ad V;IPFV;SG;FUT memd̥a wopoʼod V;IPFV;PL;FUT memd̥a wopo'iñ V;IMP;PL;PRS memd̥a memd̥a V;IPFV;SG;PRS memd̥a wopoʼo V;IPFV;PL;PRS memd̥a memd̥añ V;IMP;SG;PRS hu:ñ hu:ñ N;SG hu:ñ huhuñ N;PL s-onk s-onkad V;IPFV;SG;FUT s-onk s-oʼonkiñ V;IMP;PL;PRS s-onk s-oʼonk V;IPFV;PL;PRS s-onk s-oʼonkad V;IPFV;PL;FUT s-onk s-onk V;IPFV;SG;PRS s-onk s-onkiñ V;IMP;SG;PRS ʼelid ʼelidad V;IPFV;PL;FUT ʼelid ʼelĭ V;PRF;PL;PRS ʼelid ʼelidiñ V;IMP;SG;PRS ʼelid ʼelidad V;IPFV;SG;FUT ʼelid ʼelidiñ V;IMP;PL;PRS ʼelid ʼelid V;IPFV;SG;PRS ʼelid ʼelĭ V;PRF;SG;PRS ʼelid ʼelid V;IPFV;PL;PRS ʼoʼohan ʼoʼohaniñ V;IMP;SG;PRS ʼoʼohan ʼoʼohanad V;IPFV;SG;FUT ʼoʼohan ʼoʼoha V;PRF;PL;PRS ʼoʼohan ʼoʼohaniñ V;IMP;PL;PRS ʼoʼohan ʼoʼoha V;PRF;SG;PRS ʼoʼohan ʼoʼohan V;IPFV;SG;PRS ʼoʼohan ʼoʼohan V;IPFV;PL;PRS ʼoʼohan ʼoʼohanad V;IPFV;PL;FUT tapial tatpial N;PL tapial tapial N;SG ceʼewidakud̥ ceʼewidakud̥ N;PL ceʼewidakud̥ ceʼewidakud̥ N;SG ceʼewid ceʼewi V;PRF;SG;PRS ceʼewid ceʼewidiñ V;IMP;SG;PRS ceʼewid ceʼewidad V;IPFV;PL;FUT ceʼewid ceʼewid V;IPFV;SG;PRS ceʼewid ceʼewid V;IPFV;PL;PRS ceʼewid ceʼewidiñ V;IMP;PL;PRS ceʼewid ceʼewi V;PRF;PL;PRS ceʼewid ceʼewidad V;IPFV;SG;FUT hemajkam hemajkam N;SG hemajkam hehemajkam N;PL hi:wodag hihwodag N;PL hi:wodag hi:wodag N;SG huhuʼid huhuʼidiñ V;IMP;PL;PRS huhuʼid huhuʼi V;PRF;SG;PRS huhuʼid huhuʼid V;IPFV;PL;PRS huhuʼid huhuʼidiñ V;IMP;SG;PRS huhuʼid huhuʼid V;IPFV;SG;PRS huhuʼid huhuʼi V;PRF;PL;PRS huhuʼid huhuʼidad V;IPFV;PL;FUT huhuʼid huhuʼidad V;IPFV;SG;FUT koʼokolmad koʼokolmadad V;IPFV;SG;FUT koʼokolmad koʼokolmadad V;IPFV;PL;FUT koʼokolmad koʼokolmad V;IPFV;PL;PRS koʼokolmad koʼokolmad V;PRF;PL;PRS koʼokolmad koʼokolmadiñ V;IMP;SG;PRS koʼokolmad koʼokolmadiñ V;IMP;PL;PRS koʼokolmad koʼokolmad V;PRF;SG;PRS koʼokolmad koʼokolmad V;IPFV;SG;PRS tlo:gi tlo:gi N;SG tlo:gi tlolgi N;PL cendad cecendad V;IPFV;PL;PRS cendad cecendad V;PRF;PL;PRS cendad cecendadiñ V;IMP;PL;PRS cendad cendad V;IPFV;SG;PRS cendad cendadiñ V;IMP;SG;PRS cendad cendad V;PRF;SG;PRS cendad cecendadad V;IPFV;PL;FUT cendad cendadad V;IPFV;SG;FUT gaʼa gaʼañ V;IMP;SG;PRS gaʼa gaʼad V;IPFV;SG;FUT gaʼa gaʼad V;IPFV;PL;FUT gaʼa gai V;PRF;PL;PRS gaʼa gaʼa V;IPFV;SG;PRS gaʼa gaʼa V;IPFV;PL;PRS gaʼa gai V;PRF;SG;PRS gaʼa gaʼañ V;IMP;PL;PRS to:nk totonk N;PL to:nk to:nk N;SG giʼipig giʼipigad V;IPFV;SG;FUT giʼipig giʼipig V;IPFV;PL;PRS giʼipig giʼipig V;IPFV;SG;PRS giʼipig giʼipigiñ V;IMP;SG;PRS giʼipig giʼipĭ V;PRF;PL;PRS giʼipig giʼipĭ V;PRF;SG;PRS giʼipig giʼipigiñ V;IMP;PL;PRS giʼipig giʼipigad V;IPFV;PL;FUT s-wagima s-wapagimañ V;IMP;PL;PRS s-wagima s-wagima V;IPFV;SG;PRS s-wagima s-wapagimad V;IPFV;PL;FUT s-wagima s-wapagima V;IPFV;PL;PRS s-wagima s-wagimad V;IPFV;SG;FUT s-wagima s-wagimañ V;IMP;SG;PRS elpig ʼeʼelpigad V;IPFV;PL;FUT elpig ʼelpi V;PRF;SG;PRS elpig elpigad V;IPFV;SG;FUT elpig ʼeʼelpi V;PRF;PL;PRS elpig elpigiñ V;IMP;SG;PRS elpig elpig V;IPFV;SG;PRS elpig ʼeʼelpigiñ V;IMP;PL;PRS elpig ʼeʼelpig V;IPFV;PL;PRS cu:hug cu:hug N;PL cu:hug cu:hug N;SG wakonakud̥ wakonakud̥ N;SG wakonakud̥ wapkonakud̥ N;PL wopo wopo N;PL wopo wopo N;SG mehĭ mehĭ N;SG mehĭ mehĭ N;PL ki: ki: N;SG ki: ki: V;IPFV;PL;PRS ki: ki:d V;IPFV;PL;FUT ki: ki:d V;IPFV;SG;FUT ki: ki: V;IPFV;SG;PRS ki: ki:ñ V;IMP;SG;PRS ki: ki:kĭ N;PL ki: ki:ñ V;IMP;PL;PRS ki: ki:k N;PL siʼi si'id V;IPFV;PL;FUT siʼi si: V;PRF;PL;PRS siʼi si: V;PRF;SG;PRS siʼi siʼi V;IPFV;PL;PRS siʼi si'id V;IPFV;SG;FUT siʼi siʼi V;IPFV;SG;PRS siʼi siʼiñ V;IMP;PL;PRS siʼi siʼiñ V;IMP;SG;PRS wamigĭ wa:pam V;PRF;PL;PRS wamigĭ wa:pamgid V;IPFV;PL;FUT wamigĭ wamigiñ V;IMP;PL;PRS wamigĭ wamigĭ V;IPFV;SG;PRS wamigĭ wa:pamgĭ V;IPFV;PL;PRS wamigĭ wamigiñ V;IMP;SG;PRS wamigĭ wam V;PRF;SG;PRS wamigĭ wamigid V;IPFV;SG;FUT huc huc N;SG huc huhuc N;PL Tohono ʼOʼodham Tohono ʼOʼodham N;SG Tohono ʼOʼodham Tohono ʼOʼodham N;PL ʼoimed̥ ʼoimed̥ad V;IPFV;SG;FUT ʼoimed̥ ʼoyopo V;IPFV;PL;PRS ʼoimed̥ ʼoime V;PRF;SG;PRS ʼoimed̥ ʼoyopoad V;IPFV;PL;FUT ʼoimed̥ ʼoime V;PRF;PL;PRS ʼoimed̥ ʼoimed̥ V;IPFV;SG;PRS ʼoimed̥ ʼoimed̥añ V;IMP;SG;PRS ʼoimed̥ ʼoyopoiñ V;IMP;PL;PRS sitolmad sitolmadad V;IPFV;PL;FUT sitolmad sitolmadiñ V;IMP;SG;PRS sitolmad sitolmad V;PRF;SG;PRS sitolmad sitolmad V;IPFV;SG;PRS sitolmad sitolmad V;IPFV;PL;PRS sitolmad sitolmadad V;IPFV;SG;FUT sitolmad sitolmad V;PRF;PL;PRS sitolmad sitolmadiñ V;IMP;PL;PRS ñeid ñeidiñ V;IMP;SG;PRS ñeid ñeidad V;IPFV;SG;FUT ñeid ñeid V;IPFV;SG;PRS ñeid ñeidiñ V;IMP;PL;PRS ñeid ñei V;PRF;SG;PRS ñeid ñeidad V;IPFV;PL;FUT ñeid ñei V;PRF;PL;PRS ñeid ñeid V;IPFV;PL;PRS dahă dahiwa V;PRF;SG;PRS dahă dahiñ V;IMP;SG;PRS dahă dahă V;IPFV;SG;PRS dahă dad̥hă V;IPFV;PL;PRS dahă dad̥had V;IPFV;PL;FUT dahă dahad V;IPFV;SG;FUT dahă dadhiwua V;PRF;PL;PRS dahă dahiñ V;IMP;PL;PRS wopopig wopopigiñ V;IMP;PL;PRS wopopig wopopĭ V;PRF;PL;PRS wopopig wopopig V;IPFV;PL;PRS wopopig wopopigiñ V;IMP;SG;PRS wopopig wopopĭ V;PRF;SG;PRS wopopig wopopig V;IPFV;SG;PRS wopopig wopopigad V;IPFV;SG;FUT wopopig wopopigad V;IPFV;PL;FUT dai dads̥ V;PRF;PL;PRS dai dai V;PRF;SG;PRS mansa:na mansa:na N;PL mansa:na mansa:na N;SG gogs gogogs N;PL gogs gogs N;SG s̥u:s̥k s̥u:s̥k N;PL s̥u:s̥k s̥u:s̥k N;SG towa towa N;SG towa totwa N;PL to:lo to:lo N;SG to:lo totlo N;PL nawoj nanwoj N;PL nawoj nawoj N;SG ʼiʼihog ʼiʼihog V;IPFV;SG;PRS ʼiʼihog ʼiʼihogad V;IPFV;SG;FUT ʼiʼihog ʼiʼihogiñ V;IMP;SG;PRS ʼiʼihog ʼiʼihog V;IPFV;PL;PRS ʼiʼihog ʼiʼiho V;PRF;SG;PRS ʼiʼihog ʼiʼiho V;PRF;PL;PRS ʼiʼihog ʼiʼihogad V;IPFV;PL;FUT ʼiʼihog ʼiʼihogiñ V;IMP;PL;PRS s-wihonig s-wihonigiñ V;IMP;SG;PRS s-wihonig s-wiphionig V;IPFV;PL;PRS s-wihonig s-wiphionigad V;IPFV;PL;FUT s-wihonig s-wiphionigiñ V;IMP;PL;PRS s-wihonig s-wihonigad V;IPFV;SG;FUT s-wihonig s-wihonig V;IPFV;SG;PRS ʼo:gĭ ʼoʼo:gĭ N;PL ʼo:gĭ ʼo:gĭ N;SG s̥onwuikud̥ s̥os̥onwuikud̥ N;PL s̥onwuikud̥ s̥onwuikud̥ N;SG
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//scilab 5.4.1 //windows 7 operating system //chapter 5:Semiconductor Junction Diodes clc clear V=15//V=supply voltage Vz=12//Vz=Zener voltage P=0.36//P=power of Zener diode //P=Vz*I I=(P/Vz)//I=maximum allowable Zener current disp("A",I,"I=") Iz=2*10^(-3)//Iz=minimum value attained by the zener current Rl=1000//Rl=load resistance i=Vz/Rl//i=load current disp("A",i,"i=") Imin=Iz+i//Imin=minimum allowable value of current R=100//R=series resistance Vr=Imin*R//Vr=voltage drop across R disp("V",Vr,"Vr=") Vmin=Vz+Vr//Vmin=minimum value of V disp("V",Vmin,"Vmin=") I1=I+i disp("A",I1,"I1=") VR=I1*R disp("V",VR,"VR=") Vmax=Vz+VR//Vmax=maximum value of V disp("V",Vmax,"Vmax=") disp("V can vary between Vmin & Vmax")
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//Caption:Find the torque and efficiency of the motor //Exa:6.7 clc; clear; close; V_s=120;//in volts N_m=2400;//speed of motor (in rpm) I_in=7;//input current (in Amperes) L=0.5;//arm length (in meter) F_d=4.57;//deflection force (in Newton) W=0.03;//weight (in Newton) F=F_d-W; T_s=F*L; disp(T_s,'shaft torque of motor (in Newton-meter)='); w_m=(2*%pi*N_m)/60; P_o=T_s*w_m; P_in=V_s*I_in; Eff=P_o/P_in; disp(Eff*100,'Efficiency of motor (%)=');
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Ex10_9.sce
// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh Chapter 10 Example 9") h=10;//height of indicator diagram in mm k=25;//indicator constant in KN/m^2 per mm N=300;//engine rpm Vs=1.5*10^-2;//swept volume in m^3 M=60;//effective brake load upon dynamometer in kg r=50*10^-2;//effective brake drum radius in m m=0.12;//fuel consumption in kg/min C=42*10^3;//calorific value in KJ/kg mw=6;//circulating water rate in kg/min T1=35;//cooling water entering temperature in degree celcius T2=70;//cooling water leaving temperature in degree celcius Eg=30;//exhaust gases leaving energy in KJ/s Cw=4.18;//specific heat of water in KJ/kg K g=9.81;//accelaration due to gravity in m/s^2 disp("indicated mean effective pressure(P_imeb)=h*k in Kpa") P_imeb=h*k disp("indicated power(IP)=P_imeb*L*A*N/2 in KW") IP=P_imeb*Vs*N/(2*60) disp("brake power(BP)=2*%pi*N*T in KW") BP=2*%pi*N*(M*g*r*10^-3)/(2*60) disp("mechanical efficiency(n_mech)=BP/IP") n_mech=BP/IP disp("in percentage") n_mech=n_mech*100 disp("so indicated power=9.375 KW") disp("brake power=4.62 KW") disp("mechanical efficiency=49.28%") disp("energy liberated from fuel(Ef)=C*m/60 in KJ/s") Ef=C*m/60 disp("energy available as brake power(BP)=4.62 KW") disp("energy to coolant(Ec)=(mw/M)*Cw*(T2-T1) in KW") Ec=(mw/M)*Cw*(T2-T1) disp("energy carried by exhaust gases(Eg)=30 KJ/s") disp("unaccounted energy loss=Ef-BP-Ec-Eg in KW") Ef-BP-Ec-Eg disp("NOTE=>overall energy balance sheet is attached as jpg file with this code.")
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ex6_7.sci
//Ex6.7 clc; V=100 Il=200 Rs=0.03 Rf=60 Ra=0.04 Vsfw=Il*Rs printf("\n Voltage drop in series field winding =%.0f V \n",Vsfw) If=(V+(Il*Rs))/Rf printf("\n If=%.2f A \n",If) Ia=Il+If printf("\n Ia=%.2f A \n",Ia) Eg=V+(Il*Rs)+(Ia*Ra) printf("\n Generated EMF=%.2f V \n",Eg)
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Example12_16.sce
// Electric Machinery and Transformers // Irving L kosow // Prentice Hall of India // 2nd editiom // Chapter 12: POWER,ENERGY,AND EFFICIENCY RELATIONS OF DC AND AC DYNAMOS // Example 12-16 clear; clc; close; // Clear the work space and console. // Given data // code letter = J P = 6 ; // Number of poles S_r = 1176 ; // rotor speed in rpm V = 220 ; // Rated voltage of SCIM in volt f = 60 ; // Frequency in Hz hp_SCIM = 7.5 ; // Power rating of SCIM in hp R_ap = 0.3 ; // armature resistance in ohm/phase R_r = 0.144 ; // rotor resistance in ohm/phase jX_m = 13.5 ; // reactance in ohm/phase jX_s = 0.5 ; // synchronous reactance in ohm/phase jX_lr = 0.2 ; // Locked rotor reactance in ohm/phase P_r = 300 ; // Rotational losses in W disp("Example 12-16 : "); // Calculations S = (120*f/P); // Speed of synchronous magnetic field in rpm // case a s = (S-S_r)/S ; // Slip R_r_by_s = R_r / s ; // case b printf(" \n From fig.12-11 , using the format method of mesh analysis,we may write"); printf(" \n the array by inspection :\n "); printf(" \n_______________________________________________"); printf(" \n \t I_1 \t I_2 \t\t V "); printf(" \n_______________________________________________"); printf(" \n\t (0.3+j14) -(0+j13.5) \t(127+j0)"); printf(" \n\t-(0+j13.5) (7.2+j13.7) \t 0"); printf(" \n_______________________________________________\n"); A = [ (0.3 + %i*14) -%i*13.5 ; (-%i*13.5) (7.2 + %i*13.7) ]; // Matrix containing above mesh eqns array delta = det(A); // Determinant of A // case b : Stator armature current I_p in A I_p = det( [ (127+%i*0) (-%i*13.5) ; 0 (7.2 + %i*13.7) ] ) / delta ; I_p_m = abs(I_p);//I_p_m=magnitude of I_p in A I_p_a = atan(imag(I_p) /real(I_p))*180/%pi;//I_p_a=phase angle of I_p in degrees I_1 = I_p ; // Stator armature current in A // case c : Rotor current I_r per phase in A I_r = det( [ (0.3 + %i*14) (127+%i*0) ; (-%i*13.5) 0 ] ) / delta ; I_r_m = abs(I_r);//I_r_m=magnitude of I_r in A I_r_a = atan(imag(I_r) /real(I_r))*180/%pi;//I_r_a=phase angle of I_r in degrees // case d theta = I_p_a ; // Motor PF angle in degrees cos_theta = cosd(theta); // Motor PF // case e I_p = I_p_m ; // Stator armature current in A V_p = V / sqrt(3); // Phase voltage in volt SPI = V_p * I_p * cos_theta ; // Stator Power Input in W // case f SCL = (I_p)^2 * R_ap ; // Stator Copper Loss in W // case g // Subscripts 1 and 2 for RPI indicates two methods of calculating RPI RPI_1 = SPI - SCL ; // Rotor Power Input in W RPI_2 = (I_r_m)^2 * (R_r/s); // Rotor Power Input in W RPI =RPI_1 ; // case h RCL = s*(RPI); // Rotor copper losses in W // case i // Subscripts 1 , 2 and 3 for RPD indicates three methods of calculating RPD RPD_1 = RPI - RCL ; // Rotor Power Developed in W RPD_2 = RPI * ( 1 - s ); // Rotor Power Developed in W RPD = RPD_1 ; // case j RPO = 3*RPD - P_r ; // Rotor Power Developed in W // case k P_to = RPO ; // Total rotor power in W T_o = (7.04*P_to)/S_r ; // Total 3-phase torque in lb-ft // case l hp = P_to / 746 ; // Output horsepower // case m P_in = 3*SPI ; // Input power to stator in W P_o = RPO ; // Output power in W eta = P_o / P_in * 100 ; // Motor efficiency at rated load // Display the results disp("Solution : "); printf(" \n a: s = %.2f \n R_r/s = %.1f Ω \n",s,R_r_by_s ); printf(" \n Determinant Δ = ");disp(delta); printf(" \n b: Stator armature current :\n I_p in A = ");disp(I_1); printf(" \n I_p = I_1 = %.2f <%.2f A \n ",I_p_m , I_p_a ); printf(" \n c: Rotor current per phase :\n I_r in A = ");disp(I_r); printf(" \n I_r = I_2 = %.3f <%.2f A \n ",I_r_m , I_r_a ); printf(" \n d: Motor PF :\n cosӨ = %.4f \n",cos_theta); printf(" \n e: Stator Power Input :\n SPI = %d W \n",SPI); printf(" \n f: Stator Copper Loss :\n SCL = %.1f W \n",SCL); printf(" \n g: Rotor Power Input :\n RPI = %.1f W(method 1) ", RPI_1); printf(" \n RPI = %.1f W (method 2)\n",RPI_2); printf(" \n h: Rotor copper loss :\n RCL = %.1f W\n",RCL); printf(" \n i: Rotor Power Developed :\n RPD = %.1f W \n",RPD_1); printf(" \n RPD = %.1f W \n ",RPD_2); printf(" \n j: Total 3-phase rotor power:\n RPO = %f W \n",RPO); printf(" \n k: Total output torque developed :\n T_o = %.2f lb-ft\n",T_o); printf(" \n l: Output horsepower : \n hp = %.2f hp (rated 7.5 hp)\n",hp); printf(" \n m: Motor efficiency at rated load :\n η = %.2f percent \n",eta); printf(" \n n: See Fig.12-12");
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Exa1_2.sce
//Exa 1.2 clc; clear; close; //given data : H=5.2;//in mA/m Eta=120*%pi;//constant //Formula : E/H=Eta E=H*10^-3*Eta;//in V/m disp(round(E),"Strength of Electric field in free space in V/m : ");
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Ex9_04.sce
// Scilab Code Ex9.4: Page-310 (2014) clc; clear; m = 1; // For simplicity assume mass of gas molecule to be unity, kg k = 1.38e-023; // Boltzmann constant, J/K T = 293; // Room temperature, K bita = k*T; // Energy associated with three degrees of freedom, J v_mps = sqrt(2/(bita*m)); // For simplcity assume most probable speed to be unity, m/s C = (bita*m/(2*%pi))^(3/2); // Constant in the distribution function P = integrate('4*%pi*C*exp(-1/2*bita*m*v^2)*v^2', 'v', 0.99*v_mps, 1.01*v_mps); printf("\nThe fraction of molecules in an ideal gas in equilibrium which have speeds within 1 percent above and below the most probable speed = %5.3f", P); // Result // The fraction of molecules in an ideal gas in equilibrium which have speeds within 1 percent above and below the most probable speed = 0.017
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ex6_3.sce
//Ex 6.3 clc; syms s; i=5; R=2; L=1; C=1/2; Z=((R+L*s)*(1/(C*s)))/((R+L*s)+(1/(C*s))); V=Z*i; v=ilaplace(V); disp(v,'v(t)=');
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Ex5_5.sce
//Ex:5.5 clc; clear; close; Nm=1.24*10^6/10^6;// electron density in per m^3 fc=9*sqrt(Nm);// critical frequency in MHz printf("The critical frequency = %f MHz", fc);
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Ex4_17.sce
//Ex:4.17 clc; clear; close; r=0.45;// distance in m f=10*10^3;// frequenc in MHz y=300/f;// wavelength in m Wtr=8.9; wtr=10^(Wtr/10); wrt=1/wtr; D=(4*%pi*r/y)*(sqrt(wrt));// gain of the horn antenna d=10*log(D)/log(10);// gain of the horn antenna in dB printf("The gain of the horn antenna = %f dB", d);
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Solved_EX_6_5c.sce
//Determine even and odd parts of the signals x(n)={4,-4,2,-2} clc; clear; x1={0 0 0 4 -4 2 -2}; plot2d3(x1);//for discrete plot x2={-2 2 -4 4 0 0 0}; Xo=(x1/2-x2/2); Xe=(x1/2+x2/2); disp(Xo,'Odd part'); disp(Xe,'Even part'); xset('window',1); subplot(1,2,1); plot2d3(Xo); xlabel("time"); ylabel("odd part"); subplot(1,2,2); plot2d3(Xe); xlabel("time"); ylabel("even part"); xset('window',2); X=(Xo+Xe); plot2d3(X);
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Ex11_11.sce
clc A= 10^-2 disp("A= "+string(A)+"cm^2") //initializing value of diode area Na=5*10^16 disp("Na = "+string(Na)+"cm^-3") //initializing value of p side doping Nd=5*10^17 disp("Nd = "+string(Nd)+"cm^-3") //initializing value of n side doping Dn = 30 disp("Dn= "+string(Dn)+"cm^2/s")//initializing value of electron diffusion coefficient Dp = 15 disp("Dp= "+string(Dp)+"cm^2/s")//initializing value of hole diffusion coefficient Tn = 10^-8 disp("Tn= "+string(Tn)+"s")//inializing value of electron minority carrier lifetime Tp = 10^-7 disp("Tp= "+string(Tp)+"s")//inializing value of hole minority carrier lifetime e = 1.6*10^-19 disp("e= "+string(e)+"C")//initializing value of charge of electron ni = 1.84*10^6 disp("ni = "+string(ni)+"cm^-3") //initializing value of intrinsic carrier concentration in GaAs kbT = 0.026 disp("kbT = "+string(kbT)+"V/K") //initializing value of kbT at 300K V = 1 disp("V = "+string(V)+"V") //initializing value of forward bias potential nQr=.5 disp("nQr = "+string(nQr)) //initializing value of radiative recombination efficiency Eph = 1.41 disp("Eph= "+string(Eph)+"eV")//initializing value of Energy of each photon np = ni^2/Na disp(" np = ni^2/Na= "+string(np)+"cm^-3")//calculation pn = ni^2/Nd disp(" pn = ni^2/Nd= "+string(pn)+"cm^-3")//calculation Ln = sqrt(Dn*Tn) disp("The electron diffusion length is ,Ln = sqrt(Dn*Tn)= "+string(Ln)+"cm")//calculation Lp = sqrt(Dp*Tp) disp("The hole diffusion length is ,Lp = sqrt(Dp*Tp)= "+string(Lp)+"cm")//calculation In = ((A*e*Dn*np)/Ln)*(exp(V/kbT)-1) disp("The injected current is ,In = ((A*e*Dn*np)/Ln)*(exp(V/kbT)-1)= "+string(In)+"A")//calculation Iph = (In*nQr)/e disp("The photon generated per second is ,Iph = (In*nQr)/e= "+string(Iph)+"s^-1")//calculation P = Iph*e*Eph disp("The optical power is ,P = Iph*e*Eph= "+string(P)+"W")//calculation
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exa_1_13.sce
// Exa 1.13 clc; clear; close; // Given data Rf= 250;// in kohm // Output voltage expression, Vo= -5*Va+3*Vb // and we know that for a difference amplifier circuit, // Vo= -Rf/R1*Va + [R2/(R1+R2)]*[1+Rf/R1]*Vb // Comparing both the expression, we get // -Rf/R1*Va= -5*Va, or R1= Rf/5;// in kohm disp(R1,"The value of R1 in kohm") // and R2= 3*R1^2/(R1+Rf-3*R1) disp(R2,"The value of R2 in kohm") // Note : Answer in the book is wrong
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Ex9_6.sce
clc //initialisation of variables d=30//in w=50//lbf ft d1=10//in G=12*10^6//lbf/in^2 T1=50//lbf ft T2=16.7//lbf ft J=4810//lbf ft TA=w/3//lbf ft Tab=w-TA//lbf ft //CALCULATIONS Ta=Tab-TA//lbf ft Qmax=T3*G*(3/8)/(%pi/32)*(3/4)^4//lbf/in^2 M=(T3*12*d1)/(%pi/4*(3/4)^4*G)*(180/%pi)//degree //RESULTS printf('The couples required to hold the ends=% f lbf ft',Ta) printf('The magnitude of the greatest shear stress set up in the shaft=% f lbf/in^2',Qmax) printf('the angular rotation in degree of the section=% f degree',M)
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sadiku_11_2.sce
clear; clc; Zo=60,a=20*10^-3,u=.6*3*10^8, f=100*10^6; R=a*Zo,disp(R,'R='); L=Zo/u,disp(L*10^9,'L in nH='); G=a*a/R,disp(G*10^6,'G in micro S per meter ='); C=1/(u*Zo),disp(C*10^12,'C in pF ='); l=u/f;disp(l,'l=');
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cummulativeProduct.sce
// Function Name: cummulativeProduct // Calculate the cummulativeProduct for given array // Calculating the cummulativeProduct. inputvec1 = [1, 2, 3]; result = armaVec("cummulativeProduct",inputvec1)
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1_3.sce
errcatch(-1,"stop");mode(2);; all; format('v',11); mod_a=sqrt(3^2+2^2); mod_b=sqrt(15^2+3^2); angle_a=atand(2/3); angle_b=atand(3/15); mod_ans=mod_a*mod_b; angle_ans=angle_a+angle_b; disp(angle_ans,"phase angle of ans(in degree)=",mod_ans,"mod of ans="); exit();
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builder_help.sce
help_dir = get_absolute_file_path('builder_help.sce'); tbx_builder_help_lang("en_US", help_dir); helpdoc_path = help_dir+'en_US'; //xmltopdf(helpdoc_path, 'OpenPR Manual', 'en_US'); //xmltohtml(helpdoc_path, 'OpenPR Manual', 'en_US'); clear help_dir;
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Example2_4.sce
clear; clc; // Example: 2.4 // Page: 41 printf("Example: 2.4 - Page: 41\n\n"); // Solution //*****Data*****// // From Fig. 2.4 (Page: 41) // For process A-1-B: Q1 = 60;// [kJ] W1 = 35;// [kJ] // For process A-2-B: W2 = 50;// [kJ] // For process B-3-A: W3 = -70;// [kJ] //************// // For process A-1-B: // The internal energy of the process A-1-B can be estimated as: // Q = delta_U + W delta_U = Q1 - W1;// [kJ] // For process A-2-B: Q2 = delta_U + W2;// [kJ] // For process B-3-A: Q3 = -delta_U + W3;// [kJ] printf("The amount of heat transferred from the system to the surroundings during process B-3-A is %d kJ\n",-Q3);
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clc //Example 8.6 //Calculate the cross sectional area, pressure, temperature and mach number at a pt in duct where air velocity is 1400ft/s P1=30//psia T1=660//R (Rankine temperature scale) m=10//lbm/s mass flow rate v1=1400//ft/s R=4.98*10^4//(ft^2/s^2)*(lbm/lbmol.R)^0.5 k=1.4//dimentionless M=29//lbm/lbmol T2=T1-v1^2*((k-1)/k)*M/2/R//R (Rankine temperature scale) printf("The temperature at the pt in the duct where air velocity is 1400 ft/s is %f R\n",T2); c=223*(k*T2/M)^0.5//ft/s Ma=v1/c//dimentionless (Mach number) printf("The mach number at the pt in the duct where air velocity is 1400 ft/s is %f\n",Ma); P2=P1/(T1/T2)^(k/(k-1))//psia printf("The pressure at the pt in the duct where air velocity is 1400 ft/s is %f psia\n",P2); //1 lbf.s^2 = 32.2 lbm.ft A0=m/(P1*(M*k)^0.5*32.2/223/(T1)^0.5/((k-1)/2+1)^((k+1)/2/(k-1)))//in^2 ratio_A=((Ma^2*(k-1)/2+1)/((k-1)/2+1))^((k+1)/2/(k-1))/Ma//dimentionless A=ratio_A*A0//in^2 printf("The cross sectional at the pt in the duct where air velocity is 1400 ft/s is %f in^2",A);
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Ex10_17_3.sce
//Section-10,Example-2,Page no.-CT.29 //To find the largest mass which can be lifted through a height of 10 meters in the given expansion.. clc; P_2=1 P_1=5 R=8.314 T=298 n=1 W=-(n*R*T)*log(P_1/P_2) disp(W,'Maximum work done in(J)') m_bar=-W/98.1 disp(m_bar,'Required mass(kg)')
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EX14_11.sce
// Example14.11 // Design a video amplifier of IC 1550 circuit clc; clear; close; Vcc = 12 ; // V Av = -10 ; Vagc = 0 ; // at bandwidth of 20 MHz hfe = 50 ; // forward emitter parameter rbb = 25 ; // ohm // base resistor Cs = 1*10^-12 ; // F // source capacitor Cl = 1*10^-12 ; // F // load capacitor Ie1 = 1*10^-3 ; // A // emitter current of Q1 f = 1000*10^6 ; // Hz Vt = 52*10^-3 ; Vt1 = 0.026 ; // When Vagc =0 the transistor Q2 is cut-off and the collector current of transistor Q2 flow through the transistor Q3 // i.e Ic1=Ie1=Ie3 Ie3 = 1*10^-3 ; // A // emitter current of Q3 Ic1 = 1*10^-3 ; // A // collector current of the transistor Q1 // it indicates that the emitter current of Q2 is zero Ie2 = 0 then the emitter resistor of Q2 is infinite re2 = %inf ; // emitter resistor of Q3 re3 = (Vt/Ie1); disp('The emitter resistor of Q3 is = '+string(re3)+' ohm '); // the trans conductance of transistor is gm = (Ie1/Vt1); disp('The trans conductance of transistor is = '+string(gm)+' A/V '); // the base emitter resistor rbe rbe = (hfe/gm); disp('The base emitter resistor rbe is = '+string(rbe)+' ohm '); // the emitter capacitor Ce Ce = (gm/(2*%pi*f)); disp('The emitter capacitor is = '+string(Ce)+' F '); // the voltage gain of video amplifier is // Av = (Vo/Vin) ; // Av = -((alpha3*gm)/(rbb*re3)*((1/rbb)+(1/rbe)+sCe)*((1/re2)+(1/re3)+sC3)*((1/Rl)+(s(Cs+Cl)))) // At Avgc = 0 i.e s=0 in the above Av equation alpha3 = 1 ; s = 0 ; Av =-10 ; Rl = -((alpha3*gm)/((rbb*re3)*(((1/rbb)+(1/rbe))*((1/re2)+(1/re3))*(Av)))); Rl = (1/Rl); disp('The value of resistance RL is = '+string(Rl)+' ohm '); // there are three poles present in the transfer function of video amplifier each pole generate one 3-db frequency Rl = 265 fa = 1/(2*%pi*Rl*(Cs)); disp('The pole frequency fa is = '+string(fa)+' Hz '); fb = 1/(2*%pi*Ce*((rbb*rbe)/(rbb+rbe))); disp('The pole frequency fb is = '+string(fb)+' Hz '); fc = 1/(2*%pi*Cs*re3); disp('The pole frequency fc is = '+string(fc)+' Hz '); disp(' Hence fa is a dominant pole frequency ');