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// Exa 4.8 clc; clear; close; format('v',7) // Given data I_CBO = 10;// in µA I_CBO = I_CBO * 10^-6;// in A Beta = 50; h_FE = Beta; I_B = 0.25;// in mA I_B = I_B * 10^-3;// in A // The collector current I_C = (Beta*I_B) + ((1+Beta)*I_CBO);//in A I_C = I_C * 10^3;// in mA disp(I_C,"The collector current in mA is"); T2 = 50;// in degree C T1 = 25;// in degree C I_CBOat25 = 10;// in µA I_CBOat50 = I_CBOat25 * (2^((T2-T1)/10));// in µA I_CBOat50 = I_CBOat50 * 10^-6;// in A //The new collector current I_C = (Beta*I_B) + ((1+Beta)*I_CBOat50);// in A I_C = I_C * 10^3;// in mA disp(I_C,"The new collector current in mA is");
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clc T1 = 473 // Boiler temperature in K T2 = 293 // Home temperature in K T3 = 273 // Outside temperature in K printf("\n Example 6.5") MF = (T2*(T1-T3))/(T1*(T2-T3)) printf("\n The multiplication factor is %f ",MF) //The answers vary due to round off error
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global Z0; Z0=50; //define the S-parameters of the transistor s11=0.3*exp(%i*(+30)/180*%pi); s12=0.2*exp(%i*(-60)/180*%pi); s21=2.5*exp(%i*(-80)/180*%pi); s22=0.2*exp(%i*(-15)/180*%pi); s_param = [s11 s12;s21 s22] delta = abs(det(s_param)); k = (1 - abs(s11)^2 - abs(s22)^2 +delta^2)./(2*abs(s12*s21)); //noise parameters of the transistor Fmin_dB=1.5 Fmin=10^(Fmin_dB/10); Rn=4; Gopt=0.5*exp(%i*45/180*%pi); //compute a noise circle Fk_dB=1.6;//desired noise performance Fk=10^(Fk_dB/10); Qk=abs(1+Gopt)^2*(Fk-Fmin)/(4*Rn/Z0); //noise circle parameter dfk=Gopt/(1+Qk); //circle center location rfk=sqrt((1-abs(Gopt)^2)*Qk+Qk^2)/(1+Qk); //circle radius //plot a noise circle a=[0:360]/180*%pi; mtlb_hold on plot(real(dfk)+rfk*cos(a),imag(dfk)+rfk*sin(a),'b','linewidth',2); //specify the goal gain G_goal_dB=8; G_goal=10^(G_goal_dB/10); //find constant operating power gain circles go=G_goal/abs(s21)^2; //normalized gain dgo=go*conj(s22-delta*conj(s11))/(1+go*(abs(s22)^2)); //center rgo=sqrt(1-2*K*go*abs(s12*s21)+go^2*abs(s12*s21)^2); rgo=rgo/abs(1+go*(abs(s22)^2)); //radius //map a constant gain circle into the Gs plane rgs=rgo*abs(s12*s21/(abs(1-s22*dgo)^2-rgo^2*abs(s22)^2)); dgs=((1-s22*dgo)*conj(s11-delta*dgo)-rgo^2*s22)/(abs(1-s22*dgo)^2-rgo^2*abs(s22)^2); //plot constant gain circle in the Smith Chart mtlb_hold on plot(real(dgs)+rgs*cos(a),imag(dgs)+rgs*sin(a),'r','linewidth',2); //choose a source reflection coefficient Gs Gs=dgs+%i*rgs; //find the corresponding GL GL=(s11-conj(Gs))/(delta-s22*conj(Gs)); //find the actual noise figure F=Fmin+4*Rn/Z0*abs(Gs-Gopt)^2/(1-abs(Gs)^2)/abs(1+Gopt)^2; //% print out the actual noise figure Actual_F_dB=10*log10(F) //find the input and output reflection coefficients Gin=s11+s12*s21*GL/(1-s22*GL); Gout=s22+s12*s21*Gs/(1-s11*Gs); //find the VSWRin and VSWRout Gimn=abs((Gin-conj(Gs))/(1-Gin*Gs)); Gomn=abs((Gout-conj(GL))/(1-Gout*GL)); VSWRin=(1+Gimn)/(1-Gimn); //VSWRin should be unity since we used the constant operating gain approach VSWRout=(1+Gomn)/(1-Gomn); //specify the desired VSWRin VSWRin=1.5; //find parameters for constant VSWR circle Gimn=(1-VSWRin)/(1+VSWRin) dvimn=(1-Gimn^2)*conj(Gin)/(1-abs(Gimn*Gin)^2); //circle center rvimn=(1-abs(Gin)^2)*abs(Gimn)/(1-abs(Gimn*Gin)^2); //circle radius //plot VSWRin=1.5 circle in the Smith Chart plot(real(dvimn)+rvimn*cos(a),imag(dvimn)+rvimn*sin(a),'g','linewidth',2); //plot a graph of the output VSWR as a function of the Gs position on the constant VSWRin circle Gs=dvimn+rvimn*exp(%i*a); Gout=s22+s12*s21*Gs./(1-s11*Gs); //find the reflection coefficients at the input and output matching networks Gimn=abs((Gin-conj(Gs))./(1-Gin*Gs)); Gomn=abs((Gout-conj(GL))./(1-Gout*GL)); //and find the corresponding VSWRs VSWRin=(1+Gimn)./(1-Gimn); VSWRout=(1+Gomn)./(1-Gomn); figure; //open new figure for the VSWR plot plot(a/%pi*180,VSWRout,'r',a/%pi*180,VSWRin,'b','linewidth',2); legend('VSWR_{out}','VSWR_{in}'); title('Input and output VSWR as a function of \Gamma_S position'); xlabel('Angle \alpha, deg.'); ylabel('Input and output VSWRs'); mtlb_axis([0 360 1.3 2.3]) //choose a new source reflection coefficient Gs=dvimn+rvimn*exp(%i*85/180*%pi); //find the corresponding output reflection coefficient Gout=s22+s12*s21*Gs./(1-s11*Gs); //compute the transducer gain in this case GT=(1-abs(GL)^2)*abs(s21)^2.*(1-abs(Gs).^2)./abs(1-GL*Gout).^2./abs(1-Gs*s11).^2; GT_dB=10*log10(GT) //find the input and output matching network reflection coefficients Gimn=abs((Gin-conj(Gs))./(1-Gin*Gs)); Gomn=abs((Gout-conj(GL))./(1-Gout*GL)); //and find the corresponding VSWRs VSWRin=(1+Gimn)./(1-Gimn) VSWRout=(1+Gomn)./(1-Gomn) //also compute the obtained noise figure F=Fmin+4*Rn/Z0*abs(Gs-Gopt)^2/(1-abs(Gs)^2)/abs(1+Gopt)^2; F_dB=10*log10(F)
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clear clc //Example 3.1 LOAD LIFTED BY A HYDRAULIC JACK //Moment equilibrium at C, (F*l)-(F1*l1)=0 l=0.33; //[m] F=100; //[N] l1=0.03; //[m] F1=l*F/l1 //[N] //Force equilibrium (small piston), (p1*A1)-F1=0 d1=1.5*10^-2; //[m] A1=%pi*d1^2/4; //[m^2] p1=F1/A1 //[N/m^2] //Force equilibrium (lifter), F2-(p2*A2)=0 d2=5*10^-2; //[m] A2=%pi*d2^2/4 //[m^2] p2=p1 //[N/m^2](as both are at same elevation) F2=p2*A2/10^3 //[kN] printf("\nThe load that the jack can support = %.1f kN.\n",F2)
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//consider an airfoil mounted in a low speed subsonic wind tunnel. V=30.5;//flow velocity in test section(m/s) D=1.225;//standard sea level density,Kg/m^3 P=1.014*10^5;//standard sea level pressure,N/m^2 P1=1.01*10^5;//pressure at a point on airfoil,N/m^2 q=D*V^2/2 //dynamic pressure,N/m^2
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//data W=2*%pi*26*10^6 //rad/s Vp=200*10^6 //m/S B=W/Vp Zo=50 //ohm Zs=50 //ohm Vs=100 //volt ZL=100+%i*50 //ohm l=10 //m //formulas and result printf("\nresult:-") printf("\nB=%f rad/m",B) Zin=Zo*(ZL+%i*Zo*tan(B*l))/(Zo+%i*ZL*tan(B*l)) disp(Zin,"Zin=") VA=Vs/(Zs+Zin)*Zin disp(VA,"VA=") ZTh=Zo*complex(Zs,Zo*tan(B*l))/complex(Zo,Zs*tan(B*l)) disp(ZTh,"ZTh=") Vin=50*exp(%i*(-8.168)) VTh=2*Vin disp(VTh,"VTh=") VL=VTh/(ZTh+ZL)*ZL disp(VL,"VL=") F=(complex(19.21,3.52)-50)/(complex(19.21,3.52)+50) disp(F,"F=") Z=10 VL=Vin*(exp(-%i*B*Z)+F*exp(%i*B*Z)) disp(VL,"VL=")
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clear; clc; close; E = 10; //volts R = 500; //ohms Vdq = 0; //volts Idq = 20*10^(-3); //amperes diary('C:\Users\DELL\Desktop\intern\chapter_2\2_3.txt'); disp(Vdq,'Voltage at Q-point is :'); disp(Idq,'Current at Q-point is :');
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function[value] = func(x) //f(x) = 3x + sin(x) - exp(x) = 0 value = 3 * x + sin(x) - exp(x) endfunction function[root] = bisection(a, b) tolerence = 0.00001 while(%t) m = (a + b)/2 fa = func(a) fb = func(b) fm = func(m) if(fa == 0 | fb == 0 | fm == 0) then if(fa == 0) then root = a break end if(fb == 0) then root = b break end if(fm == 0) then root = m break end end if(fa < 0 & fm > 0) then b = m else a = m end if(abs(a-b) < tolerence) then if (abs(func(a)) < tolerence | abs(func(b)) < tolerence) then root = a break else disp("root doesnt exists") root = %nan end break end end endfunction
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clear //Given m=9*10**9 q=16*10**-10 //C r=0.1 r1=0.06 q1=12*10**-10 //Calculation Vb=m*q/r Vb1=m*q/r1 V=Vb1-Vb W=q1*V //Result printf("\n Workdone is %0.3f *10**-8 J", W*10**8)
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printf("\t example 15.6\n"); printf("\t approximate values are mentioned in the book \n"); //20000=WD+WB; //0.99*WD+(0.05*WB)=(20000*.5); // solving above two eq. we get WD and WB WD=9570; // lb/hr WB=10430; // lb/hr HBl=108; // fig 3 and 12 HDl=85.8; //fig 3 and 12 HDv=253.8; // fig 3 and 12 HFl=92; // fig 3 and 12 l=153; // fig 3 and 12 QR=((2.54+1)*WD*(HDv))-(2.54*WD*HDl)+(WB*HBl)-(20000*HFl); printf("\t total heat duty : %.1e Btu/hr \n",QR); Q=QR/153; printf("\t total heat duty : %.2e lb/hr \n",Q); // end
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<?xml version="1.0" encoding="utf-8"?> <test> <description>Channel Flow P=8 BodyForce</description> <executable>IncNavierStokesSolver</executable> <parameters>--use-scotch ChanFlow_m8_BodyForce.xml</parameters> <processes>3</processes> <files> <file description="Session File">ChanFlow_m8_BodyForce.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="u" tolerance="1e-8">9.90432e-06</value> <value variable="v" tolerance="1e-8">2.82461e-11</value> <value variable="p" tolerance="1e-8">3.91926e-09</value> </metric> <metric type="Linf" id="2"> <value variable="u" tolerance="1e-8">1.40069e-05</value> <value variable="v" tolerance="1e-8">6.84991e-11</value> <value variable="p" tolerance="1e-8">1.21984e-08</value> </metric> </metrics> </test>
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function [bp,a]= iirpowcomp(b,a,varargin) //Power complementary IIR filter //Calling Sequences // //[bp,ap] = iirpowcomp(b,a) returns the coefficients of the power complementary IIR filter g(z) = bp(z)/ap(z) in vectors bp and ap, given the coefficients of the IIR filter h(z) = b(z)/a(z) in vectors b and a. b must be symmetric (Hermitian) or antisymmetric (antihermitian) and of the same length as a. // //[bp,ap] = iirpowcomp(b,a,c) where c is a complex scalar of unity magnitude, forces bp to satisfy the generalized hermitian property: //conj(bp(end:-1:1)) = c*bp. //When c is omitted, the function chooses c as follows: //When b is real, the function chooses c as 1 or -1, whichever yields bp as real. //When b is complex, c defaults to 1. // //Input Parameters: // b: Coefficients of numerator of the IIR filter // a: Coefficients of denominator of the IIR filter // c: Complex scalar of unit magnitude // //Output Parameters // bp: Coefficients of the numerator of the power complementary IIR filter // ap: Coefficients of the denominator of the power complementary IIR filter // //Example: // [b,a]=cheby1(10,.5,.4); // [bp,ap]=iirpowcomp(b,a); // [xm,fr]=frmag(bp,ap,256); // plot(fr,xm); // //Author: Shrenik Nambiar // // Input validation statements // if argn(2)<2 | argn(2)>3 then error("2/3 input arguments allowed"); end if argn(1)~=2 then error("The number of output arguments should be 2"); end if ~(or(size(b)==1) | or(size(a)==1)) then error("size of either b or a must not be 1"); end if length(b)~=length(a) then error("Both the vectors must be of equal length"); end n= length(b)-1; //order of the numerator //Converting both the vectors to row vectors b=b(:).' ; a=a(:).' ; if n<1 then error("Order should be greater than 1 "); end // Reversed conjugated polynomial of b and a by replacing z with z^(-1) and conjugating the coefficients rb= conj(b($:-1:1)); ra= conj(a($:-1:1)); r= conv(rb,b)-conv(a,ra); // Computing the numerator of the power complementary filter if isreal(b) & argn(2)==2 then bp= recursion(r,n,1); if ~isreal(bp) then bp=recursion(r,n,-1); end if ~isreal(bp) then error("Filter type 4"); end else if argn(2)==3 then c=varargin(1); if max(size(c))>1 then error(warning("c must be scalar")); end if abs(c)-1 > %eps^(2/3) then error(warning("Filter error")); end end bp= recursion(r,n,c); end endfunction function [bp]= recursion(r,n,c) // Computes the numerator q of the power complementary transfer function needed to compute the allpass decomposition. bp(1)= sqrt(-r(1)./c); bp(n+1)= conj(c*bp(1)); bp(2)= -r(2)./(2*c*bp(1)); bp(n)= conj(c*bp(2)); for i= 3:ceil(n/2) bp(n)= (-r(i)./c - bp(2:i-1)*bp(i-1:-1:2).')./(2*bp(1)); bp(n+2-i)= conj(c*bp(i)); end // Compute middle coefficient separately when order is even if pmodulo(n,2) ==0 then bp((n+2)/2)= (-r((n+2)/2)./c - bp(2:(n+2)/2 -1)*bp((n+2)/ -1:-1:2).')./(2*bp(1)); end endfunction
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//((x^2)/(a^2))+((y^2)/(b^2))=(2*(z^2)/(c^2)) (PARABOLOIDE) a=1; b=2; c=3; x=-5:0.1:5; y=-3:0.1:3; deff('z=f1(x,y)','z=sqrt((c^2/2)*((x^2)/(a^2)+(y^2)/(b^2)))'); fplot3d(x,y,f1) deff('z=f2(x,y)','z=-sqrt((c^2/2)*((x^2)/(a^2)+(y^2)/(b^2)))'); fplot3d(x,y,f2)
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exercice1_matrice.sce
// Premier script // Définition de la matrice A A = [-3 2 4;6 3 7;-2 5 0] // Matrice identitée I = [1 0 0; 0 1 0; 0 0 1] // Matrice B B = 2*A - 3*I // A + B somme = A+B produit = A*B' detA = det(A) detB = det(B) invA = inv(A) invB = inv(B) // Affichage des résultats disp("A:", A, "A + B:", somme, "A x tB:", produit, "det(A):", detA, "det(B):", detB, "invA:", invA, "invB:", invB)
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function [blklst,cmat,ccmat,cor,corinv,ok]=c_pass1(x,ksup) //%Purpose // Determine one level blocks and connections matrix //%Parameters // x : scicos data structure // ksup : // blklst : a list containing the "model" information structure for each block // // cmat : nx4 matrix. Each row contains, in order, the block // number and the port number of an outgoing scicopath, // and the block number and the port number of the target // ingoing scicopath. // // ccmat : same as cmat but for clock scico-paths. //! [lhs,rhs]=argn(0); sup_tab=[] if rhs<=1 then ksup=0;end if ksup==0 then // main scheme MaxBlock=countblocks(x); nsblk=0; // numer of special blocks (clock split,clock sum,super_blocks) sup_tab=[] end //initialize outputs blklst=list(),nb=0,cor=list(),corinv=list(),cmat=[],ccmat=[];ok=%t n=size(x) for k=1:n, cor(k)=0;end clksplit=[] // clock split table for this level clksum=[] // clock sum table for this level sel=2:n for k=sel o=x(k) if o(1)=='Block' then model=o(3) sel(k-1)=0 if o(5)=='CLKSPLIT_f' then nsblk=nsblk+1 cor(k)=MaxBlock+nsblk clksplit=[clksplit,MaxBlock+nsblk] elseif o(5)=='CLKSOM_f' then nsblk=nsblk+1 cor(k)=MaxBlock+nsblk clksum=[clksum,MaxBlock+nsblk] elseif o(5)=='SOM_f' then [graphics,model]=o(2:3) sgn=model(7) if ~and(graphics(5)) then //all input ports are not connected,renumber connected ones //and modify signs connected=get_connected(x,k) count=0;cnct=[] for kk=1:prod(size(connected)) kc=connected(kk) lk=x(kc);to=lk(9) if to(1)==k then // an input link cnct=[cnct to(2)] count=count+1 to(2)=count;lk(9)=to;x(kc)=lk; end end model(2)=prod(size(cnct));model(7)=sgn(cnct);o(3)=model end if ~and(graphics(6)) then x_message('A summation block has unconnected output port'); ok=%f;return; end // nb=nb+1 corinv(nb)=k blklst(nb)=o(3) cor(k)=nb elseif model(1)=='super'|model(1)=='csuper' then nsblk=nsblk+1 sup_tab=[sup_tab MaxBlock+nsblk] [graphics,model]=o(2:3) // check connections if ~and(graphics(5))|~and(graphics(6))|.. ~and(graphics(7))|~and(graphics(8)) then x_message(['A block has unconnected ports';'Please check']) ok=%f return end connected=get_connected(x,k) for kk=1:prod(size(connected)) kc=connected(kk); lk=x(kc);from=lk(8);to=lk(9); if to(1)==k then // an input link to(1)=MaxBlock+nsblk; lk(9)=to;x(kc)=lk; end if from(1)==k then // an output link from(1)=MaxBlock+nsblk; lk(8)=from;x(kc)=lk; end end [blklsts,cmats,ccmats,cors,corinvs,ok]=c_pass1(model(8),MaxBlock+nsblk) if ~ok then return,end nbs=size(blklsts) for kk=1:nbs blklst(nb+kk)=blklsts(kk) corinv(nb+kk)=[k,corinvs(kk)] end cors=shiftcors(cors,nb) if cmats<>[] then f=find(cmats(:,2)>0) if f<>[] then cmats(f,1)=cmats(f,1)+nb,end f=find(cmats(:,4)>0) if f<>[] then cmats(f,3)=cmats(f,3)+nb,end cmat=[cmat;cmats] end if ccmats<>[] then f=find(ccmats(:,2)>0) if f<>[] then ccmats(f,1)=ccmats(f,1)+nb,end f=find(ccmats(:,4)>0) if f<>[] then ccmats(f,3)=ccmats(f,3)+nb,end ccmat=[ccmat;ccmats] end cor(k)=cors nb=nb+nbs elseif o(5)=='IN_f' then if ksup==0 then x_message('Input port must be only used in a Super Block') ok=%f return end connected=get_connected(x,k) if connected==[] then x_message(['A Super Block Input port is unconnected';'Please check']) ok=%f return end lk=x(connected) model=o(3) //ipar=model(9) contient le numero de port d'entree affecte //a ce bloc from=[-ksup -model(9)] lk(8)=from;x(connected)=lk elseif o(5)=='OUT_f' then if ksup==0 then x_message('Output port must be only used in a Super Block') ok=%f return end connected=get_connected(x,k) if connected==[] then x_message(['A Super Block Output port is unconnected';'Please check']) ok=%f return end lk=x(connected) model=o(3) //ipar=model(9) contient le numero de port de sortie affecte //a ce bloc to=[-ksup -model(9)] lk(9)=to;x(connected)=lk elseif o(5)=='CLKIN_f' then if ksup==0 then x_message('Clock Input port must be only used in a Super Block') ok=%f return end connected=get_connected(x,k) if connected==[] then x_message(['A Super Block Clock Input port is unconnected'; 'Please check']) ok=%f return end lk=x(connected) //ipar=model(9) contient le numero de port d'entree affecte //a ce bloc from=[-ksup -model(9)] lk(8)=from;x(connected)=lk elseif o(5)=='CLKOUT_f' then if ksup==0 then x_message('Clock Output port must be only used in a Super Block') ok=%f return end connected=get_connected(x,k) if connected==[] then x_message(['A Super Block Clock Output port is unconnected'; 'Please check']) ok=%f return end lk=x(connected) model=o(3) //ipar=model(9) contient le numero de port de sortie affecte //a ce bloc to=[-ksup -model(9)] lk(9)=to;x(connected)=lk else graphics=o(2) // check connections if ~and(graphics(5))|~and(graphics(6))|.. ~and(graphics(7))|~and(graphics(8)) then x_message(['A block has unconnected ports'; 'Please check']) ok=%f return end nb=nb+1 corinv(nb)=k model=o(3) if model(1)=='scifunc' then model(1)=genmac(model(9)) end blklst(nb)=model cor(k)=nb end elseif o(1)=='Deleted'|o(1)=='Text' then sel(k-1)=0 end end if ksup==0&nb==0 then x_message('Empty diagram') ok=%f return end //loop on links sel(find(sel==0))=[] for k=sel o=x(k); [ct,from,to]=o(7:9); if from(2)<0& from(1)<0then //fil issu d'un port d'entree d'un super block //on remet la valeur de from(1) au numero du superbloc dans x from(1)=-from(1) elseif or(from(1)==sup_tab) then //fil provenant d'un super block // from(2)=-from(2) else from(1)=cor(from(1)), end if to(2)<0&to(1)<0 then //fil connecte a un port de sortie d'un super block to(1)=-to(1) elseif or(to(1)==sup_tab) then //fil connecte a un super block // to(2)=-to(2) else to(1)=cor(to(1)), end if ct(2)==1 then cmat=[cmat;[from(1),from(2),to(1),to(2)]]; else ccmat=[ccmat;[from(1),from(2),to(1),to(2)]]; end end // strip super block input connection //========================================== to_kill=[] for k=sup_tab //loop on super blocks fn=find(cmat(:,1)==k); //super block inputs if fn<>[] then ni=max(abs(cmat(fn,2))) //number of super block input ports for kp=1:ni //loop on ports ip=find(cmat(fn,2)==-kp);fnp=fn(ip), to=[cmat(fnp(1),1), -cmat(fnp(1),2)] c=find(abs(cmat(:,3:4)-ones(cmat(:,1))*to)*[1;1]==0) //connected blocks if c<>[] then cmat(c,3:4)=ones(c')*cmat(fnp(1),3:4);to_kill=[to_kill;fnp(1)], end end end end cmat(to_kill,:)=[];to_kill=[] [nc,nw]=size(cmat) // strip super block output clock connection //=========================================== for k=sup_tab //loop on super blocks fn=find(cmat(:,3)==k); //super block outputs if fn<>[] then no=max(abs(cmat(fn,4))); //number of super block output ports for kp=1:no //loop on ports ip=find(cmat(fn,4)==-kp);fnp=fn(ip); to=[cmat(fnp(1),3), -cmat(fnp(1),4)] c=find(abs(cmat(:,1:2)-ones(cmat(:,1))*to)*[1;1]==0) ;//connected blocks if c<>[] then cmat(c,1:2)=ones(c')*cmat(fnp(1),1:2);to_kill=[to_kill;fnp(1)]; end end end end cmat(to_kill,:)=[] [nc,nw]=size(ccmat) if nc==0 then return,end //strip clksplit and clksum blocks and change corresponding links //=============================================================== // strip clksplit to_kill=[] for ksplit=clksplit kfrom=find(ccmat(:,1)==ksplit); //links coming from the clksplit kto=find(ccmat(:,3)==ksplit); // link going to the clksplit if ~or(to_kill==kto) then to_kill=[to_kill,kto];end ccmat(kfrom,1:2)=ccmat(kto*ones(kfrom'),1:2); end ccmat(to_kill,:)=[];to_kill=[] // strip clksum [nc,nw]=size(ccmat) if nc==0 then return,end for ksum=clksum //link(s) coming from the clksum. //Due to previous substitutions, many links may go out of the clksum kfrom=find(ccmat(:,1)==ksum); // links coming from the clksum kto=find(ccmat(:,3)==ksum); // links going to the clksum if ~or(to_kill==kfrom(1)) then to_kill=[to_kill,kfrom(1)];end ccmat(kto,3:4)=ccmat(kfrom(1)*ones(kto'),3:4); kfrom(1)=[]; nto=size(kto,'c'); //add new links for k=kfrom if ~or(to_kill==k(1)) then to_kill=[to_kill,k(1)];end nc=size(ccmat,'r'); ccmat=[ccmat;ccmat(kto,:)]; ccmat(nc+1:nc+nto,3:4)=ccmat(k*ones(kto'),3:4); end ccmat(to_kill,:)=[];to_kill=[] [nc,nw]=size(ccmat) end if nc==0 then return,end // strip super block input clock connection //========================================== to_kill=[] for k=sup_tab //loop on super blocks fn=find(ccmat(:,1)==k); //super block inputs if fn<>[] then ni=max(abs(ccmat(fn,2))) //number of super block input ports for kp=1:ni //loop on ports ip=find(ccmat(fn,2)==-kp);fnp=fn(ip), to=[ccmat(fnp(1),1), -ccmat(fnp(1),2)] c=find(abs(ccmat(:,3:4)-ones(ccmat(:,1))*to)*[1;1]==0) //connected blocks if c<>[] then ccmat(c,3:4)=ones(c')*ccmat(fnp(1),3:4);to_kill=[to_kill;fnp(1)], // handle clock sum outputs (many links issued from a single port) for ii=2:size(fnp,'*') ccmat=[ccmat;[ccmat(c,1:2),ones(c')*ccmat(fnp(ii),3:4)] ] to_kill=[to_kill;fnp(ii)], end end end end end ccmat(to_kill,:)=[];to_kill=[] [nc,nw]=size(ccmat) if nc==0 then return,end // strip super block output clock connection //=========================================== for k=sup_tab //loop on super blocks fn=find(ccmat(:,3)==k); //super block outputs if fn<>[] then no=max(abs(ccmat(fn,4))); //number of super block output ports for kp=1:no //loop on ports ip=find(ccmat(fn,4)==-kp);fnp=fn(ip); to=[ccmat(fnp(1),3), -ccmat(fnp(1),4)] c=find(abs(ccmat(:,1:2)-ones(ccmat(:,1))*to)*[1;1]==0) ;//connected blocks if c<>[] then ccmat(c,1:2)=ones(c')*ccmat(fnp(1),1:2);to_kill=[to_kill;fnp(1)]; // handle clock sum outputs (many links issued from a single port) for ii=2:size(fnp,'*') ccmat=[ccmat;[ones(c')*ccmat(fnp(ii),1:2),ccmat(c,3:4)] ]; to_kill=[to_kill;fnp(ii)]; end end end end end ccmat(to_kill,:)=[] if ksup==0 then if or(ccmat(:,1)>MaxBlock)|or(ccmat(:,3)>MaxBlock) then x_message(['Compilation problem: may be event loop'; 'if no event loop, please report']) ok=%f return end end function n=countblocks(x) // count number of blocks used in the scicos data structure x nx=size(x) n=0 for o=x if o(1)=='Block' then model=o(3) if model(1)=='super'|model(1)=='csuper' then n=n+countblocks(model(8)) else n=n+1 end else n=n+1 end end function cors=shiftcors(cors,ns) n=size(cors) for k=1:n if type(cors(k))==15 then cors(k)=shiftcors(cors(k),ns) else cors(k)=cors(k)+ns end end function mac=genmac(tt) [txt1,txt2,txt3]=tt(1:3) mac=null() deff('[%_1,%_2]=mac(t,x,z,u,n_evi,%_flag,rpar,%_ipar)',.. ['%_1=[];%_2=[];'; 'select %_flag'; 'case 1 then'; txt1 '%_1=y'; 'case 2 then'; txt2 '%_1=xd'; '%_2=zp'; 'case 3 then'; txt3 '%_1=t_evo '; 'case 4 then'; '%_1=x' '%_2=z' 'end']) comp(mac)
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clc; clear all; disp("rate of diffusion") T=273;// K D=0.17;// cm^2/s Ra=82.06;// cm^2atm/(g mole K) A=1;//m^2 pA1=90/760;// atm pA2=20/760;// atm pB1=1-pA1; pB2=1-pA2; pBlm=(pB2-pB1)/log(pB2/pB1); G=82.06; L=3.5*10^(-3); p=1; Na=(D*A*p/(Ra*T*L))*(pA1-pA2)/pBlm; disp("gm moles/s",Na,"rate of diffusion =")
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//pathname=get_absolute_file_path('2.02.sce') //filename=pathname+filesep()+'2.02-data.sci' //exec(filename) //Thermodynamic property at T=0: p0=3; //Thermodynamic property at T=100: p100=8; //Value of a: a=(100-0)/(log(8)-log(3)) //Value of b: b=0-a*log(3) //At thermodynamic property p=6.5: t=a*log(6.5)+b/2 printf("\n\nRESULTS\n\n") printf("\n\nTemperature at the value of thermodynamic property (p=6.5)= %f \n\n",t)
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// Initilization of variables v_A=10 // m/s // velocity of body A alpha_A=60 // degree // direction of body A alpha_B=45 // degree // direction of body B // Calculations // (a) The velocity (v_B) for the same range is given by eq'n; v_B=sqrt((v_A^2*sind(2*alpha_A))/(sind(2*alpha_B))) // m/s // (b) Now velocity v_B for the same maximum height is given as, v_b=sqrt((v_A^2)*((sind(alpha_A))^2/(sind(alpha_B))^2)) // m/s // (c) Now the velocity (v) for the equal time of flight is; v=(v_A*sind(alpha_A))/(sind(alpha_B)) // m/s // Results clc printf('(a) The velocity of body B for horizontal range is %f m/s \n',v_B) printf('(b) The velocity of body B for the maximum height is %f m/s \n',v_b) printf('(c) The velocity of body B for equal time of flight is %f m/s \n',v)
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clear; clc; // Example: 7.9 // Page: 279 printf("Example: 7.9 - Page: 279\n\n"); // Solution //*****Data******// Pin = 1000;// [kPa] Tin = 600;// [K] Uin = 50;// [m/s] gama = 1.4; M = 17;// [g/mol] R = 8314;// [kJ/mol K] MachNumber = 2; //***************// // Solution (i) // Using Eqn. (7.36): Critical_Ratio = (2/(gama + 1))^(gama/(gama - 1)); printf("Critical Ratio is %.2f\n",Critical_Ratio); // Solution (ii) PV_in = R*Tin/M;// [square m] Uthroat = sqrt(Uin^2 + (2*gama*PV_in/(gama - 1))*(1-(Critical_Ratio)^((gama - 1)/gama)));// [m/s] Uout = MachNumber*Uthroat;// [m/s] printf("The discharge velocity is %.2f m/s",Uout);
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//Example No. 13_07 //Polygon Method //Pg NO. 433 clear ; close ; clc ; deff('F = f(x,y)','F = 2*y/x ') x(1) = 1 ; y(1) = 2 ; h = 0.25 ; for i = 2:3 x(i) = x(i-1) + h ; y(i) = y(i-1) + h*f( x(i-1)+ h/2 , y(i-1) + h*f( x(i-1) , y(i-1) )/2 ); mprintf('y(%f) = %f \n ',x(i),y(i)) end
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//Chapter 16, Problem 13 clc; eff = 0.8; // effficiency f = 50; // in ohm Pout = 4800; // in Watt pf1 = 0.625 // power factor pf2 = 0.95 // power factor V = 240; // in Volts //calculation: Pin = Pout/eff Im = Pin/(V*pf1) phi1 = acos(pf1) phi1d = phi1*180/%pi //When a capacitor C is connected in parallel with the motor a current Ic flows which leads V by 90°. phi2 = acos(pf2) phi2d = phi2*180/%pi Imh = Im*cos(phi1) //Ih = I*cos(phi2) Ih = Imh I = Ih/cos(phi2) Imv = Im*sin(phi1) Iv = I*sin(phi2) Ic = Imv - Iv C = Ic/(2*%pi*f*V) kvar = V*Ic/1000 printf("\n\n (a)Current taken by the motor, Im = %.0f A",Im) printf("\n\n (b)Supply current after p.f. correction, I = %.2f A ",I) printf("\n\n (c)Magnitude of the capacitor current Ic = %.0f A",Ic) printf("\n\n (d)Capacitance, C = %.0f μF ",(C/1E-6)) printf("\n\n (d)kvar rating of the capacitor = %.2f kvar ",kvar)
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// Test # 1 : No Input Arguments exec('./zpklp2xn.sci',-1); [z,p,k,n,d]=zpklp2xn(); // !--error 10000 //Number of input arguments should either be 5 or 6 //at line 37 of function zpklp2xn called by : //[z,p,k,n,d]=zpklp2xn();
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clc clear //INPUT DATA V=12000//volume of auditorium in m^3 T=1.5//The reverberation time of the auditorium in sec a=0.4//average absorption coefficient in sabine //CALCULTION S=(0.167*V)/(a*T)//area of interior surfaces in m^2 //OUTPUT printf('The area of interior surfaces is %i m^2',S)
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function [x,y,typ]=ANDBLK(job,arg1,arg2) // Copyright INRIA x=[];y=[],typ=[] select job case 'plot' then standard_draw(arg1) case 'getinputs' then [x,y,typ]=standard_inputs(arg1) case 'getoutputs' then [x,y,typ]=standard_outputs(arg1) case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then case 'define' then model = list('csuper',[],[],[1;1],1,[],[],.. list(list([600,400,0,0],'ANDBLK',[],[]),.. list('Block',.. list([194,133],[60,60],%t,[],[],10,[5;12],[],.. ['txt=[''LOGICAL'';'' '';'' AND ''];'; 'xstringb(orig(1),orig(2),txt,sz(1),sz(2),''fill'');']),.. list('andlog',[],1,[1;1],[],[],[],[],[],'d',[],[%f,%f],' ',list()),' ','ANDLOG_f'),.. list('Block',list([149,287],[20,20],%t,'1',[],[],[],5,[]),.. list('input',[],[],[],1,[],[],[],1,'d',-1,[%f,%f],' ',list()),' ','CLKIN_f'),.. list('Block',list([450,83],[20,20],%t,'1',[],[],9,[],[]),.. list('output',[],[],1,[],[],[],[],1,'d',[],[%f,%f],' ',list()),' ','CLKOUT_f'),.. list('Link',[169;214;214],[297;297;198.71429],'drawlink',' ',[0,0],[5,-1],[3,1],[2,1]),.. list('Block',list([141,330],[20,20],%t,'2',[],[],[],7,[]),.. list('input',[],[],[],1,[],[],[],2,'d',%t,[-1,-1],' ',list()),' ','CLKIN_f'),.. list('Link',[161;234;234],[340;340;275.78348],'drawlink',' ',[0,0],[5,-1],[6,1],[11,1]),.. list('Block',.. list([331,137],[60,60],%t,[],10,[],13,[9;0],.. ['txt=[''If in>=0'';'' '';'' then else''];'; 'xstringb(orig(1),orig(2),txt,sz(1),sz(2),''fill'');']),.. list('ifthel',1,[],1,[1;1],[],[],[],[],'l',[-1,-1],[%f,%f],' ',list()),' ','IFTHEL_f'),.. list('Link',[351;351;450],[131.28571;93;93],'drawlink',' ',[0,0],[5,-1],[8,1],[4,1]),.. list('Link',[262.57143;322.42857],[163;167],'drawlink',' ',[0,0],[1,1],[2,1],[8,1]),.. list('Block',list([234;275.78348],[1,1],%t,' ',[],[],7,[12;13]),.. list('lsplit',[],[],1,[1;1],[],[],[],[],'d',[-1,-1],[%t,%f],' ',list()),' ','CLKSPLIT_f'),.. list('Link',[234;234],[275.78348;198.71429],'drawlink',' ',[0,0],[5,-1],[11,1],[2,2]),.. list('Link',[234;361;361],[275.78348;275.78348;202.71429],'drawlink',' ',[0,0],[5,-1],.. [11,2],[8,1])),[],'h',%f,[%f,%f]) gr_i='xstringb(orig(1),orig(2),''ANDBLK'',sz(1),sz(2),''fill'')'; x=standard_define([3 2],model,[],gr_i) end
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//simplification of boolean expressions// //example 10.c// clc //clears the command window// clear //clears// //simplification of boolean expression// disp('given Y=C(AB''+AB)+BC') disp('Y=CA(B''+B)+BC') disp('Y=CA+BC');//B+B''=1// disp('the simplified expression is:') disp('Y=C(A+B)') //simplified boolean expression//
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clear; clc; close; clf; x=linspace(-3,3,11); y=x^2; plot2d(x,y,3); xtitle("Parabola curve","x axis","y axis") legend("y=x^2"); xgrid();
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printf("closed loop transfer function =16/(s^2+(4+16*K)*s+16)"); printf("characterstic equation of the given system is 4+16*K)*s+16=0"); printf("compare it with the standard second order characterstic equation s^2+2*d*w*s+w^2=0"); w=sqrt(16); d=0.8;//given k=(2*d*w-4)/16; mo=exp((-%pi*d)/sqrt(1-d^2))*100; disp(k,"value of K="); disp(mo,"maximum overshoot(in %)");
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0.636364 0.097561 0.4 0.533333 class1 0.369565 0.230769 0.625 0.244541 0.131868 0.0943396 0.333333 0.428571 0.25 0.185714 0.310526 0.254197 0.308176 0.157895 0.318182 0.317073 0.333333 0.366667 class1 0.26087 0.384615 0.361111 0.069869 0.0769231 0.0566038 0.235294 0.571429 0.166667 0.385714 0.2 0.16307 0.408805 0.368421 0.363636 0.0487805 0.1 0 class2 0.282609 0.384615 0.388889 0.200873 0.186813 0.132075 0.169935 0.628571 0.0833333 0.357143 0.163158 0.121103 0.408805 0.131579 0.272727 0 0.533333 0.666667 class0 0.586957 0.692308 0.888889 0.257642 0.0549451 0.150943 0.614379 0.171429 0.5 0.657143 0.457895 0.535971 0.528302 0.131579 0.227273 0.512195 0.4 0.5 class3 0.543478 0.5 0.666667 0.379913 0.175824 0.0754717 0.522876 0.228571 0.416667 0.414286 0.447368 0.454436 0.408805 0.184211 0.0909091 0.634146 0.6 0.533333 class2 0.304348 0.307692 0.5 0.266376 0.21978 0.0943396 0.235294 0.542857 0.166667 0.314286 0.215789 0.171463 0.27044 0.171053 0.318182 0.317073 0.4 0.466667 class2 0.217391 0.269231 0.180556 0.0436681 0.0659341 0.0754717 0.130719 0.771429 0.0833333 0.314286 0.0631579 0.0755396 0.301887 0.355263 0.363636 0.170732 0 0.0666667 class0 0.26087 0.192308 0.319444 0.113537 0.0879121 0.0943396 0.0653595 0.828571 0 0.171429 0.0368421 0.0419664 0.220126 0.0657895 0.909091 0.195122 0.633333 0.666667 class3 0.826087 0.769231 0.944444 0.467249 0.153846 0.169811 0.620915 0.171429 0.5 0.7 0.457895 0.541966 0.672956 0.0657895 0.954545 0.0487805 0.666667 0.8 class1 0.652174 0.884615 0.833333 0.353712 0.131868 0.169811 0.679739 0.142857 0.583333 0.785714 0.468421 0.59952 0.691824 0.210526 0.681818 0.268293 0.333333 0.433333 class3 0.413043 0.230769 0.5 0.331878 0.263736 0.0754717 0.261438 0.485714 0.166667 0.185714 0.257895 0.199041 0.213836 0.171053 0.272727 0.341463 0.633333 0.633333 class2 0.326087 0.307692 0.555556 0.187773 0.164835 0.113208 0.222222 0.542857 0.166667 0.371429 0.205263 0.160671 0.327044 0.157895 0.181818 0.390244 0.4 0.533333 class0 0.23913 0.192308 0.277778 0.104803 0.0989011 0.0566038 0.130719 0.685714 0.0833333 0.171429 0.0947368 0.0923261 0.201258 0.210526 0.363636 0.097561 0.3 0.233333 class3 0.347826 0.423077 0.555556 0.379913 0.208791 0.0754717 0.326797 0.4 0.25 0.357143 0.310526 0.254197 0.446541 0.0921053 0.590909 0.268293 0.6 0.6 class3 0.434783 0.538462 0.611111 0.441048 0.263736 0.0943396 0.418301 0.285714 0.333333 0.485714 0.315789 0.35012 0.578616 0.144737 0.318182 0.463415 0.733333 0.666667 class2 0.673913 0.730769 0.847222 0.445415 0.164835 0.150943 0.562092 0.2 0.5 0.614286 0.405263 0.483213 0.597484 0.0657895 0.0909091 0.121951 0.633333 0.766667 class3 0.173913 0.384615 0.388889 0.19214 0.186813 0.0943396 0.248366 0.542857 0.166667 0.371429 0.236842 0.17506 0.389937 0.276316 0.0454545 0.0487805 0.2 0.133333 class2 0.326087 0.461538 0.583333 0.222707 0.0989011 0.113208 0.27451 0.485714 0.166667 0.442857 0.263158 0.207434 0.383648 0.131579 0.136364 0 0.4 0.4 class1 0.652174 0.692308 0.902778 0.305677 0.0989011 0.169811 0.640523 0.171429 0.583333 0.642857 0.484211 0.558753 0.710692 0.184211 0.363636 0.219512 0.366667 0.5 class1 0.217391 0.5 0.388889 0.152838 0.131868 0.0754717 0.248366 0.514286 0.166667 0.4 0.221053 0.182254 0.465409 0.197368 0.227273 0.0731707 0.3 0.333333 class2 0.130435 0.192308 0.208333 0.069869 0.0879121 0.0566038 0.196078 0.628571 0.166667 0.142857 0.121053 0.133094 0.226415 0.289474 0.181818 0.0487805 0.133333 0.0666667 class1 0.521739 0.846154 0.875 0.406114 0.175824 0.169811 0.673203 0.142857 0.583333 0.771429 0.468421 0.591127 0.691824 0.210526 0.227273 0.585366 0.3 0.433333 class3 0.217391 0.230769 0.402778 0.100437 0.0769231 0.0566038 0.150327 0.657143 0.0833333 0.185714 0.131579 0.107914 0.333333 0.131579 0.727273 0.146341 0.366667 0.3 class3 0.543478 0.192308 0.444444 0.384279 0.241758 0.0566038 0.352941 0.342857 0.25 0.185714 0.310526 0.291367 0.18239 0.144737 0.0454545 0.0731707 0.8 0.7 class2 0.369565 0.576923 0.513889 0.122271 0.0989011 0.150943 0.294118 0.514286 0.25 0.657143 0.205263 0.203837 0.490566 0.25 0.0454545 0.0731707 0.2 0.333333 class0 0.26087 0.384615 0.361111 0.0829694 0.0879121 0.0943396 0.248366 0.542857 0.166667 0.4 0.221053 0.170264 0.402516 0.315789 0.181818 0.365854 0.133333 0.0666667 class2 0.173913 0.461538 0.388889 0.218341 0.241758 0.377358 0.254902 0.542857 0.166667 0.414286 0.294737 0.181055 0.484277 0.381579 0.0454545 0.243902 0.133333 0.133333 class2 0.369565 0.576923 0.625 0.231441 0.186813 0.169811 0.320261 0.485714 0.25 0.7 0.236842 0.229017 0.484277 0.197368 0.136364 0.390244 0.3 0.466667 class0 0.673913 0.769231 0.944444 0.436681 0.186813 0.169811 0.705882 0.142857 0.666667 0.771429 0.505263 0.627098 0.591195 0.157895 0.636364 0.731707 0.433333 0.733333 class1 0.478261 0.384615 0.777778 0.427948 0.197802 0.150943 0.503268 0.257143 0.416667 0.357143 0.457895 0.419664 0.358491 0.157895 0.272727 0.658537 0.466667 0.533333 class3 0.434783 0.346154 0.805556 0.384279 0.175824 0.132075 0.477124 0.285714 0.416667 0.285714 0.4 0.388489 0.402516 0.144737 0.454545 0.512195 0.433333 0.533333 class1 0.304348 0.192308 0.430556 0.0829694 0.0659341 0.113208 0.163399 0.657143 0.0833333 0.128571 0.147368 0.111511 0.226415 0.210526 0 0.219512 0.166667 0.166667 class1 0.673913 0.884615 0.777778 0.554585 0.296703 0.169811 0.705882 0.114286 0.666667 0.771429 0.489474 0.634293 0.685535 0.184211 0.272727 0.390244 0.333333 0.466667 class3 0.478261 0.307692 0.583333 0.28821 0.197802 0.132075 0.215686 0.571429 0.166667 0.385714 0.173684 0.155875 0.194969 0.0657895 0.181818 0.195122 0.766667 0.866667 class0 0.695652 0.807692 0.902778 0.475983 0.21978 0.150943 0.575163 0.2 0.5 0.642857 0.442105 0.495204 0.660377 0.118421 0.454545 0.487805 0.466667 0.566667 class3 0.717391 0.846154 0.777778 0.401747 0.142857 0.188679 0.712418 0.114286 0.666667 0.785714 0.5 0.639089 0.660377 0.171053 0.409091 0.317073 0.333333 0.5 class3 0.282609 0.230769 0.611111 0.196507 0.10989 0.113208 0.287582 0.485714 0.25 0.214286 0.289474 0.208633 0.301887 0.197368 0 0.560976 0.233333 0.3 class3 0.478261 0.615385 0.722222 0.388646 0.164835 0.150943 0.431373 0.314286 0.333333 0.514286 0.368421 0.352518 0.389937 0.0657895 0.0909091 0 0.733333 0.833333 class3 0.565217 0.923077 0.833333 0.318777 0.0769231 0.207547 0.732026 0.114286 0.666667 1 0.489474 0.64988 0.654088 0.171053 0.181818 0.170732 0.3 0.566667 class3 0.347826 0.346154 0.361111 0.0917031 0.0659341 0.0943396 0.124183 0.714286 0.0833333 0.371429 0.168421 0.0839329 0.333333 0.184211 0.454545 0.414634 0.4 0.333333 class0 0.478261 0.615385 0.583333 0.152838 0.0989011 0.169811 0.30719 0.485714 0.25 0.628571 0.226316 0.217026 0.477987 0.210526 0.318182 0.243902 0.2 0.333333 class0 0.521739 0.153846 0.416667 0.30131 0.208791 0.0943396 0.254902 0.485714 0.166667 0.157143 0.194737 0.194245 0.0628931 0.0789474 0 0.390244 0.833333 0.9 class2 0.586957 0.538462 0.416667 0.353712 0.252747 0.0943396 0.326797 0.4 0.25 0.5 0.257895 0.266187 0.396226 0.118421 0.409091 0.146341 0.8 0.8 class2 0.76087 0.615385 0.958333 0.436681 0.153846 0.169811 0.653595 0.142857 0.583333 0.585714 0.521053 0.576739 0.666667 0.157895 0.727273 0.268293 0.466667 0.6 class1 0.413043 0.5 0.597222 0.218341 0.0989011 0.0754717 0.313725 0.428571 0.25 0.428571 0.289474 0.23741 0.471698 0.157895 0.454545 0.121951 0.333333 0.333333 class1 0.195652 0.115385 0.152778 0.0436681 0.0659341 0.0377358 0.150327 0.685714 0.0833333 0.114286 0.105263 0.100719 0.220126 0.355263 0.681818 0.097561 0.166667 0.0333333 class1 0.826087 0.961538 0.902778 0.344978 0.043956 0.0754717 1 0 1 0.8 0.815789 1 0.918239 0.342105 0.181818 0.195122 0.166667 0.0666667 class2 0.304348 0.461538 0.361111 0.152838 0.120879 0.113208 0.183007 0.6 0.0833333 0.428571 0.2 0.131894 0.415094 0.184211 0.136364 0.292683 0.4 0.5 class0 0.456522 0.5 0.513889 0.283843 0.142857 0.113208 0.300654 0.457143 0.25 0.428571 0.268421 0.226619 0.45283 0.105263 0.545455 0.0487805 0.566667 0.6 class1 0.478261 0.384615 0.5 0.165939 0.10989 0.150943 0.254902 0.514286 0.166667 0.442857 0.226316 0.185851 0.314465 0.157895 0.0909091 0.560976 0.366667 0.633333 class0 0.369565 0.423077 0.444444 0.231441 0.186813 0.113208 0.163399 0.628571 0.0833333 0.371429 0.152632 0.118705 0.389937 0.0789474 0.409091 0.097561 0.666667 0.733333 class0 0.434783 0.0384615 0.361111 0.157205 0.0989011 0.0943396 0.117647 0.714286 0.0833333 0.0285714 0.110526 0.0803357 0.0314465 0.0394737 0.227273 0.707317 0.833333 0.866667 class3 0.434783 0.230769 0.652778 0.344978 0.186813 0.113208 0.372549 0.4 0.25 0.228571 0.368421 0.285372 0.251572 0.171053 0.318182 0.609756 0.4 0.466667 class1 0.347826 0.5 0.611111 0.257642 0.208791 0.169811 0.30719 0.485714 0.25 0.585714 0.226316 0.220624 0.421384 0.171053 0.0454545 0.487805 0.333333 0.533333 class0 0.717391 0.807692 0.847222 0.515284 0.21978 0.188679 0.718954 0.114286 0.666667 0.785714 0.515789 0.643885 0.572327 0.144737 0.136364 0.097561 0.366667 0.666667 class1 0.282609 0.115385 0.527778 0.183406 0.120879 0.0943396 0.150327 0.685714 0.0833333 0.0857143 0.131579 0.103118 0.245283 0.0921053 0 0.609756 0.466667 0.466667 class1 0.26087 0.115385 0.361111 0.0829694 0.0879121 0.0566038 0.0522876 0.857143 0 0.142857 0.0526316 0.0335731 0.138365 0.184211 0.0454545 0.439024 0.333333 0.3 class0
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Ex8_7.sce
//Optoelectronics - An Introduction, 2nd Edition by J. Wilson and J.F.B. Hawkes //Example 8.7 //OS=Windows XP sp3 //Scilab version 5.5.2 clc; clear; //given n1=1.48;//Dimensionless refractive index of fiber core n2=1.46;//Dimensionless refractive index of fiber cladding L=1e3;//Length of fiber in m c=3e8;//Speed of light in vacuum in m/s Delta=(n1^2 - n2^2)/(2* n1^2); mprintf("\n Delta = %.4f",Delta); DeltaTGI=L/c*Delta/8;//Intermodal dispersion in s mprintf("\n DeltaTGI = %.2e s",DeltaTGI); //The answers vary due to round off error
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Example_9_1.sce
clc; clear; printf("\n Example 9.1\n"); M_dot1=20; //rate of mass to be cooled M_dot2=25; //rate of cooling water Cp=4.18e3; //Heat capacity T1=360; //Initial temp. T2=340; //Final temp. theta_1=300; //Temperature of cooing water entering U=2e3; //Overall heat transfer coefficient Q=M_dot1*Cp*(T1-T2); //Heat load printf("\n Heat load = %.0f kW",Q*1e-3); //The cooling water outlet temperature is given by x=poly([0],'x'); theta_2=roots(Q-(M_dot2*Cp*(x-300))); printf("\n The cooling water outlet temperature is = %.0f K",theta_2); printf("\n (a) Counter flow") //In equation 9.9: theta_m1=((T1-theta_2)-(T2-theta_1))/(log((T1-theta_2)/(T2-theta_1))); A1=Q/(U*theta_m1) printf("\n The surface area required %.2f m^2",A1); printf("\n (b) Co-current flow") //In equation 9.9: theta_m2=((T1-theta_1)-(T2-theta_2))/(log((T1-theta_1)/(T2-theta_2))); A2=Q/(U*theta_m2) printf("\n The surface area required %.2f m^2",A2);
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/3733/CH32/EX32.12/Ex32_12.sce
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Ex32_12.sce
// Example 32_12 clc;funcprot(0); //Given data F_l=70/100;// Load factor F_c=50/100;// Capacity factor F_u=60/100;// Use factor MD=20;// Maximum demand in MW // Calculation //(a) L_a=(MD*F_l)*10^3;// Average load in kW E=L_a*365*24;// Annual energy produced in kW-hrs //(b) Pc=(L_a/1000)/F_c;// Plant capacity in MW Rc=Pc-MD;// Reserve capacity in MW //(c) t_1=E/(Pc*10^3*F_u);// hours T=8760-t_1;// Hours not in service in hrs in a year printf('\n(a)Annual energy production=%0.3e kW-hrs \n(b)Reserve capacity over and above peak load=%0.0f MW \n(c)Hours not in service=%0.0f hrs in a year',E,Rc,T); // The answer provided in the textbook is wrong
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/Toolbox Test/peak2rms/peak2rms/peak2rms1.sce
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peak2rms1.sce
//Check o/p for normal sinusoid i/p pi=3.14; x = cos(2*pi*(1:100)/100); y = peak2rms(x); disp(y); //output // 1.4142344
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Chapter9_Example4.sce
//Chapter-9, Example 9.4, Page 386 //============================================================================= clc clear //INPUT DATA l=0.5;//Wavelength at maximum intensity of radiation in micro meter //CALCULATIONS T=(0.289*10^-2)/(l*10^-6);//Temperature according to Wien's displacement law in degree C E=(5.67*10^-8*T^4)/10^6;//Emissive power using Stefan-Boltzmann law in MW/m^2 //OUTPUT mprintf('Surface temperature is %3.0f K \nEmissive power is %3.1f MW/m^2',T,E) //=================================END OF PROGRAM==============================
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// Classifica a doença de acordo com as caracteristicas colhidas no exame de // sangue // Parâmetros de entrada: // entradas: Entradas do conjunto de treinamento // pesos: Pesos iniciais da rede // Parâmetros de saída: // classes: Classificação das amostras passadas como entrada function classes = perceptron_operation(w, x) // Número de amostras [Input_Size,Samples_Size]=size(x); // Inicializa o vetor de classes (tipos classificados) classes = zeros(Samples_Size, 1); for k = 1 : Samples_Size v=w'*x(:,k); //y = sign(v); y = tanh(v); if (y <= 0) classes(k) = -1; else classes(k) = 1; end //classes(k)=y; end disp(classes); endfunction
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Name=QZChallenge PlayerCharacters=Quaker BotCharacters=QZFAST.bot IsChallenge=false Timelimit=600.0 PlayerProfile=Quaker AddedBots=QZFAST.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=1 BotTeams=2 MapName=thunderstruck-top.map MapScale=3.8125 BlockProjectilePredictors=false BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=3.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=1.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Quake 3, QuakeLive, QuakeChampions WeaponHeroTag=Lightning Gun, VQ3\VQL Movement DifficultyTag=5 AuthorsTag=fatsquirrel BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Scored by accuracy after a 10 minute high pressure training exercise. Ideally for finding sensitivity and fov settings. GameVersion=1.0.5 [Aim Profile] Name=At Feet 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=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=High Skill At Feet 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=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [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=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=QZFAST DodgeProfileNames=Mimic;Short Strafes DodgeProfileWeights=1.0;2.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;0.25;2.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=At Feet;High Skill At Feet;High Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=QuakerBot SeeThroughWalls=false [Character Profile] Name=Quaker MaxHealth=300.0 WeaponProfileNames=LG;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1300.0 MaxCrouchSpeed=500.0 Acceleration=12000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=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 [Character Profile] Name=QuakerBot MaxHealth=300.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1300.0 MaxCrouchSpeed=500.0 Acceleration=12000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=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 [Dodge Profile] Name=Mimic MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Mimic TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Short Strafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=LG Type=Hitscan ShotsPerClick=1 DamagePerShot=7.0 KnockbackFactor=2.0 TimeBetweenShots=0.05 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=7.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.05 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Quake/Source ADSAllowUserOverrideFOV=true Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false [Map Data]
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a=[1 1 1;2 2 2+%i;3 3 3]; Y=rms(a); disp(Y); //output // //1. // 1.7320508 // 3. //
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V=4*sqrt(2) w=2 R=4 L=2 Xl=w*L*%i Il=V/(R+Xl) Ic=-imag(Il)*%i C=Ic/(V*%i*w) disp(C)
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for i=1:100 b(i) = sin(i); end
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// Example 22_6 clc;funcprot(0); //Given data p_1=215;// bar T_1=500;// °C p_2=40;// bar T_2=280;// °C p_3=p_2-1;// bar p_4=8;// bar T_4=270;//°C p_5=p_4-0.5;// bar p_6=0.07;// bar m=10;// The flow of steam in kg/sec //Calculation // From h-s diagram h_1=3234;// kJ/kg h_2a=2822;// kJ/kg h_2=2910;// kJ/kg h_3=3435;// kJ/kg h_4a=2977;// kJ/kg h_4=2998;// kJ/kg h_5=3473;// kJ/kg h_6a=2444;// kJ/kg h_6=2578;// kJ/kg //From steam tables, h_f7=162;// kJ/kg W=(h_1-h_2)+(h_3-h_4)+(h_5-h_6);// Work done per kg of steam kJ/kg Q=(h_1-h_f7)+(h_3-h_2)+(h_5-h_4);// Heat supplied per kg of steam kJ/kg n_th=(W/Q)*100;//The thermal efficiency of the cycle in % P=(W*m);// Power developed by the plant in kW n_i1=((h_1-h_2)/(h_1-h_2a))*100;//Isentropic efficiency of the first stage in % n_i2=((h_3-h_4)/(h_3-h_4a))*100;//Isentropic efficiency of the second stage in % n_i3=((h_5-h_6)/(h_5-h_6a))*100;//Isentropic efficiency of the third stage in % printf('\n(a)The thermal efficiency of the cycle=%0.1f percentage \n Power developed by the plant=%0.0f kW \n(b)Isentropic efficiency of the first stage=%0.1f percentage \n Isentropic efficiency of the second stage=%0.1f percentage \n Isentropic efficiency of the third stage=%0.0f percentage',n_th,P,n_i1,n_i2,n_i3);
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clc // // // //Variable declaration lambdaa=5000*10**-10 //Wavelength muo=1.5418 //Refractive index of ordinary rays mue=1.5508 //Refractive index of extra ordinary rays t=0.032*10**-3 //thickness //Calculations orot=((2*(t*(mue-muo)))/lambdaa) //Result printf("\n The Amount of optical rotation produced is %i radians",orot)
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arc_number.sci
function [m]=arc_number(g) [lhs,rhs]=argn(0) if rhs<>1 then error(39), end ma=prod(size(g('tail'))) if g('directed')==1 then m=ma, else m=2*ma, end
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//getf('temp.sci'); getf('calculate_differentiator.sci'); getf('specgram.sci'); fileName = '../../../samples/satisfaction_15s.wav'; stacksize(50000000); // Read samples [x Fs nBits] = wavread(fileName); // We keep only the first channel x = x(1, :); wlen = Fs / 100; FFTSIZE = 512; overlap = 2/3; //.75; ignore = .5; filter_order = 10; // must always be even Nfen = wlen; Nover = round(Nfen*overlap); // overlap in samples slen = 25e-3; // length in seconds for the widening miniv = 1e-100; minimo = 0.1; m = calculate_differentiator(filter_order+1); // calculate differentiator filter Nhop = Nfen-Nover; // hop size in time Fns = Fs/(Nfen-Nover); // design of the low-pass smoothing IIR filter alpha = 0.015; betav=0.075; d = 5; c = 1; betav = betav*Fns; alpha = alpha*Fns; // Smoothing filter definition s=%s; num = [d+c, -(c*exp(-1/betav)+d*exp(-1/alpha))]; den = [1, -(exp(-1/alpha)+exp(-1/betav)), exp(-(1/alpha+1/betav))]; Hsl = sum(num .* s^[size(num, 'c') - 1: -1 : 0]) / sum(den .* s^[size(den, 'c') - 1: -1 : 0]); sl = syslin('d', Hsl); // Smoothing H = specgram(Nover, FFTSIZE * 2, 'hn', x); Ha = abs(H); for i = [1 : FFTSIZE * 2], G(:, i) = abs(flts(Ha(:, i)', sl))'; end //G = Ha; // log compression Gf = G; Gf(Gf == 0) = miniv; Gf = 20*log10(Gf(:,1:FFTSIZE)); //clear Ha //clear G //f = [0 : FFTSIZE - 1] / FFTSIZE; //t = [1 : size(Gf, 'r')]; //xset("colormap",graycolormap(128)); //grayplot(t(20:600), f, Gf(20:600,:)); //tmp = zeros(m); //tmp(size(tmp, 'c')) = 1; //s=%s //tmp = sum(m .* (s^[0 : size(m, 'c') - 1])) / s; //sl2 = syslin('d', tmp); //for i = [1 : FFTSIZE], dGf(:, i) = abs(flts(Gf(:, i)', sl2))'; end for i = [1 : FFTSIZE], dGf(:, i) = abs(convol([1, -1], Gf(:, i)'))'; end dGf(dGf<minimo) = 0; // remove small differentiation debris //df = sum(dGf); // frequency integration //f = [0 : FFTSIZE - 1] / FFTSIZE; //t = [1 : size(dGf, 'r')]; //cm = graycolormap(128); //cm = cm($:-1:1,:); //xset("colormap", cm); //grayplot(t(20:600), f, dGf(20:600,:)); for i = [1 : size(dGf, 'r')], df(i,:) = sum(dGf(i,:)); end // eliminate (?) differentiator filter transient df = df(length(m)+1:$-1); // peak widening by convolving with a cosine time window // replace by an exponential window defined above if desired //fH2 = window('hn', 2*slen+1); //fH2 = fH2(slen+1:$); //ddn = convol(fH2,df); //bn = (~isinf(ddn)) | (~isnan(ddn)); // eliminate NaN and Inf if they exist //index = find(bn == %t); //dd = zeros(size(ddn)); //dd(index) = ddn(index); dd = df/max(df); plot(dd);
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// Exa 3.13 format('v',7) clc; clear; close; // Given data del_n = 10^15;// in cm^3 Torque_p = 10 * 10^-6;// in sec R_g = del_n/Torque_p;// in hole pairs/sec/cm^3 disp(R_g,"The rate of generation of minority carrier in electron hole pairs/sec/cm^3 is ");
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printf("\t example 20.8b \n"); printf("\t approximate values are mentioned in the book \n"); m=100; // lb t1=70; t2=370; L=4; B=3; n=4; // number of air changers c1=0.12 Q1=(m*c1*(t2-t1)); printf("\t heat to steel charge : %.1e Btu \n",Q1); c2=0.25 Q2=(n*L*B*2*0.075*c2*(t2-t1)); printf("\t heat to air : %.1e Btu \n",Q2); printf("\t From Fig. 20.25a for 52ft^2 of oven outside·surface and a temperature rise of 300F the loss is 5kw for 1 in.thick insulations.For 2 in.thick insulation the loss is 2.5kw \n"); Qt=((Q1+Q2)/(3412))+(2.5); printf("\t total requirement : %.2f kw \n",Qt); // end
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// Electric Machinery and Transformers // Irving L kosow // Prentice Hall of India // 2nd editiom // Chapter 3: DC Dynamo Voltage Relations - DC Generators // Example 3-7 clear; clc; close; // Clear the work space and console. // Given data VR = 0.105; // voltage regulation V_f1 = 250; // Full load voltage of the shunt generator in V // Calculation V_n1 = V_f1 + ( V_f1 * VR ); // No-load voltage of the generator in V // Display the result disp("Example 3-7 Solution : ") printf("\n Vn1 = %.1f V ", V_n1 );
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// metodo de runge-kutta ordem 2 // metodo muito eficiente para edo's // todos algoritmos resolvem problemas de valor inicial clc; clear; function yd = rb(x, y) yd = x - 2*y + 1; endfunction // a=limite inferio, b= limite superior, h = tamanho do passo // y0=valor inicial function [vetX, vetY] = rungeKutta2(a, b, h, y0, rb) m = (b-a)/h; xt = a; yt = y0; vetX(1) = xt; vetY(1) = yt; disp([0, xt, yt]); for i = 1: m x = xt; y =yt; k1 = rb(x,y); x = xt+h; y = yt + h * k1; k2 = rb(x,y); xt = a+i*h; yt = yt + h/2 * (k1+k2); disp([i, xt, yt]); vetX(i+1) = xt; vetY(i+1) = yt; end endfunction m=10; a=0; b=1; y0=1; h = 0.1; [x,y] = rungeKutta2(a,b,h,y0,rb);
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(unwatch all) (clear) (dribble-on "dftmpcmd.out") (batch "dftmpcmd.bat") (dribble-off) (clear) (open "dftmpcmd.rsl" dftmpcmd "w") (load "compline.clp") (printout dftmpcmd "dftmpcmd.bat differences are as follows:" crlf) (compare-files dftmpcmd.exp dftmpcmd.out dftmpcmd) (close dftmpcmd)
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//volume and power// pathname=get_absolute_file_path('10.02.sce') filename=pathname+filesep()+'10.02-data.sci' exec(filename) U=0.5*(Dh+Dt)/2*1200*2*%pi/60 k=tand(alpha1)+cotd(betta1) Vn1=U/k V1=Vn1/cosd(alpha1) Vt1=V1*sind(alpha1) Vrb1=Vn1/sind(betta1) //Volume flow rate (in m^3/sec): Q=%pi/4*Vn1*(Dt^2-Dh^2) k=(U-Vn1*cotd(betta2))/Vn1 alpha2= atand(k) V2=Vn1/cosd(alpha2) Vt2=V2*sind(alpha2) //Rotor Torque (in N-m): Tz=p*Q*(Dh+Dt)/4*(Vt2-Vt1) //Power required (in W): Wm=w*2*%pi/60*Tz printf("\n\nRESULTS\n\n") printf("\n\nVolume flow rate: %.3f m^3/sec\n\n",Q) printf("\n\nRotor Torque: %.3f N-m\n\n",Tz) printf("\n\nPower required: %.3f W\n\n",Wm)
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clc,clear printf('Example 7.5\n\n') D= 8.9 //density of nickel A=200 //area of plate thickness=0.2/10 //thicknes of coating V=200*thickness //volume of material to be plated W= V* D //weight of material to be deposited Z= 0.0003043 //Electrochemical equivalent of nickel Q = W / (Z*90/100) //Q is quantity of electricity printf('Quantity of electricity = %.1f A-hr\n',Q/3600) current_density = 190*10^-4 //current density in A/ cm^2 current = current_density *A T=Q /current //time taken printf('Time taken = %f seconds\n',T) printf('or <%d hours,%d minutes,%d seconds>',T/3600,60*((T/3600)- floor(T/3600) ) , 60*((60*((T/3600)- floor(T/3600) ) )-floor(60*((T/3600)- floor(T/3600) ) )))
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x = 1:1:10; y = x.^2; plot(x,y,'r--'); title("Hello Scilab"); xlabel('x-axis'); ylabel('y-axis'); set(gca(), "grid", [1,1]); y1 = x.^3; plot(x,y1,'b-'); legend('f(x^2)', 'f(x^3)'); clf(); x = linspace(1,10,11); y = 10^(x); plot2d("nl", x,y); clf(); x = linspace(1,10,11); y = 10^(x); y1 = 10.^(-x); y2 = y1.^2; clf() x=1:0.1:10; y=sin(x); y1=cos(x); mtlb_axis([1, 16, -5, 5]); plot(x,y,x,y1); clf(); x = -2*%pi:%pi/20:2*%pi; y = sin(x); set(gca(), "grid", [1,1]); plot(x,y); mtlb_axis([0 %pi 0 1]); subplot(2,1,1); clf(); data = [-10.1, -1, 1.1, 3.5, 13, 0, -5.5, -0.5, 7.9]; bar(data, 0.5, 'yellow'); clf(); x = [1, 2, 5]; y = []; pie(x); pie(x,[0 1 0]); clf(); x = [0:%pi/16:2*%pi]'; z = sin(x)*ones(x)'; plot3d(x, x, z); clf(); x = -%pi:3*%pi/100:2*%pi; y = x; plot(x,y,'r*'); clf(); x=1:0.1:10; y = sin(x); title("sine"); xlabel('x-axis'); ylabel('y-axis'); plot(x, y); clf(); x=1:0.1:10; y = sin(x); y1 = cos(x); xlabel('x-axis'); ylabel('y-axis'); subplot(2,1,1); plot(x, y, 'b--'); subplot(2,1,2); plot(x, y1, 'r-'); legend('f(x) = sinx', 'f(x) = cosx'); clf(); x=0:0.1:10; y = sin(x); xlabel('x-axis'); ylabel('y-axis'); plot(x, y, 'b--'); legend('f(x) = sinx'); mtlb_axis([0 %pi 0 1]); clf(); a = [34 56 78 23]; pie(a, [0 0 1 0]);
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<?xml version="1.0" encoding="UTF-8" standalone="yes"?> <!DOCTYPE AUTOTEST> <AutoTest version="2.0.0" wavetype="5"> <Pulse>Pulse 4</Pulse> <Title>12V LEVEL II</Title> <Organization>BYD</Organization> <Standard>QBYDQ J01.324 2007</Standard> <Item>6.4.2.4 试验脉冲4</Item> <system> <PowerSystem>0</PowerSystem> <Ua>12</Ua> </system> <wave> <Us value="7"/> <Ua value="6"/> <Period value="1"/> <T9 value="0.5"/> <Ri index="0" text="0.02"/> <T7 value="15"/> <T8 value="50"/> <T10 value="5"/> <T11 value="5"/> <Count value="1"/> </wave> </AutoTest>
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//Example 16.5 //Non Linear Problem //Page no. 584 clc;close;clear; deff('y=f(x)','y=2/(1+x)') Y=[1,0.75,0.75,0.75,0.5];h=0.25 A=[-2,1,0;1,-2,1;0,1,-2];A_1=inv(A) disp(A_1,"Inverse of A =",A,"A =") printf('\nThe Solution of the system is: \n\n Iteration\t Y0\t\t Y1\t\t Y2\t\t Y3\t\t Y4\n----------------------------------------------------------------------------------------') for i=0:6 printf('\n %i',i) for j=1:5 if j<4 & i~=0 then Y(j+1)=y(j) end printf('\t\t%.4f',Y(j)) end x=0; for j=1:3 x=x+h if j~=2 then B(j)=h^2*f(x)*Y(j+1)^2-Y(1+2*(j-1)) else B(j)=h^2*f(x)*Y(j+1)^2 end end y=A_1*B end
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clear // r=20 l=200*10**-3 v=230 f=50 xl=314*l //314 is omega ir=v/(r) il=v/(xl) i=((ir**2)+(il**2))**0.5 printf("\n i= %0.1f A",i)
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Turbomachinery Design and Theory,Rama S. R. Gorla and Aijaz A. Khan, Chapter 8") disp("Cavitation in Hydraulic Machinery") disp("Just Theory No Solved/Unsolved Examples")
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clc // initialization of variables clear sigma_x=1400 //kg/cm^2 tau_xy=400// kg/cm^2 ep_z=-3.6*10^-6 nu=1/4 E=2*10^8 //kg/cm^2 // calculations sigma_y=(-ep_z*E/nu)-sigma_x sigma_1=(sigma_x+sigma_y)/2+sqrt((1/2*(sigma_x-sigma_y))^2+tau_xy^2) sigma_2=(sigma_x+sigma_y)/2-sqrt((1/2*(sigma_x-sigma_y))^2+tau_xy^2) th=0.5*atan(2*tau_xy/(sigma_x-sigma_y)) th=th*180/%pi printf('sigma_y is %d kg/cm^2',sigma_y) printf('\n The principal stresses are %d , %d kg/cm^2',sigma_1,sigma_2) printf('\n The direction is given by theta = %.2f degrees',th) // angle was given wrong in the text
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// Exa 4.16.11 clc; clear; close; // Given data I_o = 10;// in nA // I = I_o * ((e^(v/(Eta * V_T))) - 1) // e^(v/(Eta * V_T)<< 1, so neglecting it I = I_o * (-1);// in nA disp(I,"The Diode current in nA is ");
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//Change in air fuel ratio at altitude clc,clear //Given: ha=5000 //Altitude in m A_F=14 //Air fuel ratio at sea level P1=1.013 //Pressure of air in bar at sea level T1=27+273 //Temperature of air in K at sea level R=0.287 //Specific gas constant in kJ/kgK function t=f1(h),t=ts-0.0065*h,endfunction //Temperature(t in degreeC) as a function of altitude(h in m) function h=f2(P),h=19200*log10(1.013/P),endfunction //Altitude(h in m) as a function of pressure(P in bar) //Solution: ts=T1-273 //Sea level temperature in degreeC T2=f1(ha) //Temperature at altitude(ha = 5000 m) in degreeC T2=T2+273 //in K //Defining, y as a function of P //This function is the difference of function(f2) and ha given function y=f(P),y=f2(P)-ha,endfunction //The function f is solve for zero to get the value of P2 P2=fsolve(1,f) //Pressure at altitude(ha = 5000 m) in bar rho_a=P2/(R*T2) //Density of air at altitude in kg/m^3 rho_s=P1/(R*T1) //Density of air at sea level in kg/m^3 A_F_a=A_F*sqrt(rho_a/rho_s) //Air fuel ratio at altitude //Results: printf("\n The air fuel ratio supplied at 5000 m altitude by a carburettor = %.2f\n\n",A_F_a)
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// Example 6.5:loss clc; clear; close; format('v',5) d1=60;//micro meter na1=0.25;// alpha1=2.1;// d2=50;//in micro meter na2=0.20;// alpha2=1.9;// ncd=(d2/d1)^2;// nna=(na2/na1)^2;// nalpha1=1;// nalpha=((1+(2/alpha1))/(1+((2/alpha2))));// ncd1=1;// nna1=1;// nt=ncd*nna*nalpha1;// ltf=(-10*log10(nt));//in dB nt1=ncd1*nna1*nalpha;// ltb=(-10*log10(nt1));//in dB disp(ltf,"total loss forward direction in dB is") format('v',6) disp(ltb,"total loss backward direction in dB is")
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function [x,xsol]=Questao_4(A,b,alfa,e) //Inicialização da questão e de sua variáveis n = size(A,1) I=eye(n,n) M=(1/alfa)*I N=((1/alfa)*I)-A x=ones(n,1) crit=1 normb=norm(b) while(e<crit ) //iterações x= x + alfa*(b - A * x) xsol = M \ (N * x + b) //critério de parada crit = norm((A * x - b) / normb) end endfunction
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P7_diameter_of_rimmed_flywheel.sce
clc //Example 26.7 //Diameter of rimmed flywheel //------------------------------------------------------------------------------ //Given data P=125000 N=200 Mt=(125000*60)/(2*%pi*200) Ecycle=Mt*4*%pi Estroke=1.5*Ecycle rho=7200 St=4* 10^6 res7=mopen(TMPDIR+'7_diameter_of_rimmed_flywheel.txt','wt') mfprintf(res7,'(a)Average torque Mt=%0.2f Nm\n\n',Mt) mfprintf(res7,'(b)Energy output per cycle=%0.2f Nm\n',Ecycle) mfprintf(res7,'Energy output during power stroke=%0.2f Nm\n',Estroke) mfprintf(res7,'Energy stored in the flywheel=%0.2f Nm\n\n',Estroke-Mt) mfprintf(res7,'(c)Stress=rho*V^2\n') V=sqrt(St/rho) mfprintf(res7,'\tV=%0.2f m/s\n',V) r=(V*60)/(2*%pi*N) mfprintf(res7,'\tV=r*w\n\tr=V/w=%0.3f m\n\n',r) mfprintf(res7,'(d)Mass of rim of flywheel:\n') K=0.9 E=Estroke-Mt delta=0.03 mr=(K*E)/(V^2 *delta) mfprintf(res7,'\tmr=(K*E)/(V^2 *delta) =%0.2f kg\n\n',mr) mfprintf(res7,'(e)Dimensions of rim\n\tmr=pi*Dm*t*b*rho\n') Dm=2*r t=sqrt(mr/(%pi*Dm*rho)) mfprintf(res7,'For square rim, t=b=%0.3f m\n\n',t) t=sqrt(mr/(%pi*Dm*rho*2)) mfprintf(res7,'For rectangular rim, b=2t=%0.3f m and t=%0.3f m\n\n',2*t,t) mclose(res7) editor(TMPDIR+'7_diameter_of_rimmed_flywheel.txt') //------------------------------------------------------------------------------ //-----------------------------End of program-----------------------------------
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clear clc T1=456.15;//boiling temperature of iodine in K T2=389.65;//vapour pressure temperature of iodine in K P1=760;//pressure in torr P2=100;//vapour pressure in torr DelHm_f=15.65;//heat of fusion in kJ/mol R=8.314;//in J/K DelHm_v=(2.303*R*log10(P1/P2))/((1/T2)-(1/T1));//heat of vapourization in J/mol DelHm_s=(DelHm_f*1000)+DelHm_v;//heat of sublimation in J/mol T=311.85;//temperature at solid vapour equilibrium in K P=1;//pressure at solid vapour equilibrium in torr K1=(DelHm_s)/(2.30*R);// K2=(DelHm_v)/(2.30*R);// T0=(K1-K2)/((K1*(1/T))-(K2*(1/T2))-log10(P2));//triple point temperature in K printf('\nT0=%.1f K',T0) P0=10^(K1*((1/T)-(1/T0)));//triple point pressure in torr printf('\nP0=%.2f torr',P0) //There are some errors in the solution given in textbook //page 19
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<<<<<<< HEAD // Copyright (C) 2018 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Original Source : https://octave.sourceforge.io/signal/ // Modifieded by:Sonu Sharma, RGIT Mumbai // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in function [n, Wc] = buttord(Wp, Ws, Rp, Rs) //Minimum filter order and 3dB cutoff frequency of a digital Butterworth filter with the desired response characteristics //Calling Sequence //n = buttord(Wp, Ws, Rp, Rs) //[n, Wc] = buttord(Wp, Ws, Rp, Rs) //Parameters //Wp: scalar or vector of length 2 (passband edge(s) ) elements must be in the range [0,1] //Ws: scalar or vector of length 2, (stopband edge(s) ) elements must be in the range [0,1] //Rp: passband ripple in dB. //Rs: stopband attenuation in dB. //Description. //This function computes the minimum filter order of a Butterworth filter with the desired response characteristics. //The filter frequency band edges are specified by the passband frequency wp and stopband frequency ws. //Frequencies are normalized to the Nyquist frequency in the range [0,1]. //Rp is measured in decibels and is the allowable passband ripple, and Rs is also in decibels and is the minimum attenuation in the stop band. //If ws>wp, the filter is a low pass filter. If wp>ws, the filter is a high pass filter. //If wp and ws are vectors of length 2, then the passband interval is defined by wp the stopband interval is defined by ws. //If wp is contained within the lower and upper limits of ws, the filter is a band-pass filter. If ws is contained within the lower and upper limits of wp the filter is a band-stop or band-reject filter. //Examples //Wp = 40/500 ; //Ws = 150/500 ; //[n, Wn] = buttord(Wp, Ws, 3, 60) //Output : // Wn = // // 0.0800376 // n = // // 5. funcprot(0); [nargout nargin] = argn(); if (nargin ~= 4) error("buttord: invalid number of inputs"); else validate_filter_bands ("buttord", Wp, Ws); end if (length (Wp) == 2) warning ("buttord: seems to overdesign bandpass and bandreject filters"); end T = 2; // if high pass, reverse the sense of the test stop = find(Wp > Ws); Wp(stop) = 1-Wp(stop); // stop will be at most length 1, so no need to Ws(stop) = 1-Ws(stop); // subtract from ones(1,length(stop)) // warp the target frequencies according to the bilinear transform Ws = (2/T)*tan(%pi*Ws./T); Wp = (2/T)*tan(%pi*Wp./T); // compute minimum n which satisfies all band edge conditions // the factor 1/length(Wp) is an artificial correction for the // band pass/stop case, which otherwise significantly overdesigns. qs = log(10^(Rs/10) - 1); qp = log(10^(Rp/10) - 1); n = ceil(max(0.5*(qs - qp)./log(Ws./Wp))/length(Wp)); // compute -3dB cutoff given Wp, Rp and n Wc = exp(log(Wp) - qp/2/n); // unwarp the returned frequency Wc = atan(T/2*Wc)*T/%pi; // if high pass, reverse the sense of the test Wc(stop) = 1-Wc(stop); ======= function [n, Wc] = buttord(Wp, Ws, Rp, Rs) ///This function computes the minimum filter order of a Butterworth filter with the desired response characteristics. //Calling Sequence //n = buttord(Wp, Ws, Rp, Rs) //[n, Wc] = buttord(Wp, Ws, Rp, Rs) //Parameters //Wp: scalar or vector of length 2 //Ws: scalar or vector of length 2, elements must be in the range [0,1] //Rp: real or complex value //Rs: real or complex value //Description //This is an Octave function. //This function computes the minimum filter order of a Butterworth filter with the desired response characteristics. //The filter frequency band edges are specified by the passband frequency wp and stopband frequency ws. //Frequencies are normalized to the Nyquist frequency in the range [0,1]. //Rp is measured in decibels and is the allowable passband ripple, and Rs is also in decibels and is the minimum attenuation in the stop band. //If ws>wp, the filter is a low pass filter. If wp>ws, the filter is a high pass filter. //If wp and ws are vectors of length 2, then the passband interval is defined by wp the stopband interval is defined by ws. //If wp is contained within the lower and upper limits of ws, the filter is a band-pass filter. If ws is contained within the lower and upper limits of wp the filter is a band-stop or band-reject filter. //Examples //Wp = 40/500 //Ws = 150/500 //[n, Wn] = buttord(Wp, Ws, 3, 60) //n = 5 //Wn = 0.080038 rhs = argn(2) lhs = argn(1) if(rhs~=4) error("Wrong number of input arguments.") end select(lhs) case 1 then n = callOctave(Wp,Ws,Rp,Rs) case 2 then [n,Wc] = callOctave(Wp,Ws,Rp,Rs) end >>>>>>> 6bbb00d0f0128381ee95194cf7d008fb6504de7d endfunction
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//Caption: Measure of Skewness //Karl Pearson's coefficient of skewness //Example3.18 //Page61 clear; clc; X = [0,4;4,8;8,12;12,16;16,20;20,24;24,28;28,32]; //Absenteeism in days f = [10,76,100,150,24,36,14,2]; //No. of employees [m,n] = size(X); for i = 1:m Xi(i) = sum(X(i,:))/2; //Mid point end if (modulo(m,2)==1) then //to check even or odd mid = m/2; else mid = (m+1)/2; end A = Xi(mid); //assumed mean N = sum(f); //total frequency C = diff(X(1,:)); //class interval for i = 1:m d(i) = (Xi(i)-A)/C; fd(i)= f(i)*d(i); fd2(i) = f(i)*(d(i)^2); end Xmean = A+(sum(fd)*C/N); //Mean value [m1,n1] = max(f); //maximum frequency L = X(n1,1); //Lower limit of the modal class f1 = abs(f(n1)-f(n1-1)); //Abs difference between freq. of modal class & its //immediately preceding class f2 = abs(f(n1)-f(n1+1)); //Abs difference between freq. of modal class & its //immediately succeeding class Mode = L+((f1/(f1+f2))*C);//Mode Std = sqrt((sum(fd2)/N)-(sum(fd)/N)^2)*C;//standard deviation CS = (Xmean-Mode)/Std; //coefficient of skewness disp(Xmean,'Mean Value =') disp(Mode,'Mode value =') disp(CS,'coefficient of skewness = ') //Result if (CS<0) then disp('Since the coefficient of skewness is negative, the distribution is') disp('skewed to the left & extent of distortion is very small') end //Result //Mean Value = // // 12.679612 // // Mode value = // // 13.136364 // // coefficient of skewness = // // - 0.0832508 // // Since the coefficient of skewness is negative, the distribution is // // skewed to the left & extent of distortion is very small
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printf("w/wo\t|H|\tphase\n"); for f=0:0.2:1 // for(f=0;f<=1;f=f+0.2) H = 1 / (1 + %i*f); // relacao w/wo printf("%.2f\t%.2f\t%.2f\n",f,abs(H), (atan(imag(H),real(H)))*180/%pi); end for f=2:2:10 H = 1 / (1 + %i*f); // relacao w/wo printf("%.2f\t%.2f\t%.2f\n",f,abs(H), (atan(imag(H),real(H)))*180/%pi); end for f=20:20:100 H = 1 / (1 + %i*f); // relacao w/wo printf("%.2f\t%.2f\t%.2f\n",f,abs(H), (atan(imag(H),real(H)))*180/%pi); end
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clc //initialisation of variables Q= 0.5 //ft^3/sec d= 3 //in d1= 4 //in d2= 2 //in h= 12.7 //in g= 32.2 //ft/sec^2 s= 13.6 //kg/m^3 //CALCULATIONS k= (s-1)*(h/2)*2*g*(%pi/(Q*d^2*4))^2+((d1/d)^4-1) C= (d1/d2)^2/(sqrt(k)+1) //CALCULATIONS printf (' cntraction coefficient= %.3f ',C) //ANSWER GIVEN IN THE TEXTBOOK IS WRONG
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//Example 10.1 //page 655 //Control Systems: Principles and Design //M Gopal, Second Edition, Tata McGraw-Hill //Chapter:Compensator design using Bode Plots xdel(winsid())//close all graphics Windows clear; clc; s=poly(0,"s") w=poly(0,'w') G=1/(s*(s+1)) Kv=10 pm=45 //degrees K=Kv/horner(s*G,0) G1=syslin('c',K*G) [gm,frg]=g_margin(G1) [pm0,frp]=p_margin(G1) //Finding extra phase lead required phi=pm-pm0+3 alpha= (1-sind(phi))/(1+sind(phi)) gain_uncomp=-20*log(1/(sqrt(alpha))) wc=4.16 //New gain crossover frequency z=wc*sqrt(alpha) //z=1/T p=wc/sqrt(alpha) //p=1/(alpha*T) Kc=K/alpha D=Kc*(s+z)/(s+p) disp(D,'Lead Compensator=') Gc=syslin('c',G1*D) f=figure() bode(G1) bode_asymp(G1) title('Bode plot of uncompensated system') a=gca(); a.parent.background=8; f=figure() bode(Gc) bode_asymp(Gc) title('Bode plot of compensated system') a=gca(); a.parent.background=8; f=figure() black([G1;Gc ],0.01,100,["Plant";"Plant and Lead Compensator"]); a=gca(); a.parent.background=8; Leg=a.children(1); Leg.legend_location="in_lower_right"; nicholschart(colors=color('light gray')*[1 1])
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//Example 6.7 //What fraction of vapour woll condense . //Given Gv=20 //kg/m^2 s, mass flow rate of benzene di=0.016 //m, tube diameter muv=8.9*(10^-6) //P, viscosity Lv=391 //kj/kg., enthalpy of vaporization cpl=1.94 //kj/kg C, specific heat Tv=80 //C, normal boiling point of benzene Tw=55 //C, wall temp. g=9.8 //m/s^2, gravitational constant rhol=815 //kg/m^3, density of benzene rhov=2.7 //kg/m^3, density of benzene vapour kl=0.13 //W/m C, thermal conductivity mu=3.81*10^-4 //P, viscosity of benzene l=0.5 //m, length of tube //calculation Rev=di*Gv/muv //Reynold no. of vapour //from eq. 6.38 Lv1=Lv+(3/8)*cpl*(Tv-Tw) //heat transfer corfficient , h h=0.555*(g*rhol*(rhol-rhov)*kl^3*Lv1*10^3/(di*mu*(Tv-Tw)))^(1/4) Aavl=%pi*di*l //m^2, available area Q=Aavl*h*(Tv-Tw) //W, rate of heat transfer m=Q/(Lv1*10^3) //kg/s, rate of condensation of benzene Ratei=Gv*(%pi/4)*di^2 //kg/s rate of input of benzene vapour n=m/Ratei printf("fraction of input vapour condensed is %f",n*100)
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EXAMPLE3_1.SCE
//ANALOG AND DIGITAL COMMUNICATION //BY Dr.SANJAY SHARMA //CHAPTER 3 //RADIO TRANSMITTER clear all; clc; printf("EXAMPLE 3.1(PAGENO 132)"); //given Pm = 85//percentage modulation m = .85//modulation index P_c = 50*10^3//carrier power in watts //calculation P_t = P_c*(1+(m^2/2));//total radiated power //result printf("\n\nTotal radiated power = %.2f W",P_t);
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a=10; b=3; function xd=linear831(t,x) xd(1)=a-x(1)-((4*x(1)*x(2))/(1+x(1)^2)); xd(2)=(b*x(1))*(1-(x(2)/(1+x(1)^2))); //x(dot); x(2) means y. //y(dot); x(1) means x.; endfunction bound=[0,3,3,7]; //Bounds of x-axis and y-axis as [xmin ymin xmax ymax], change them according to your needs. nrect=25; //increase it to get more number of curves, i.e. more information will be available. set(gca(),"auto_clear","off") //hold on x=linspace(bound(1),bound(3),nrect); y=linspace(bound(2),bound(4),nrect); x0=[]; for i=1:25 x0=[x(i);y(i)]; t0=0; t=0:0.01:3000; xout=ode(x0,t0,t,linear831); plot2d(xout(1,:),xout(2,:)); end xtitle('Phase Portrait','x-axis ( x )','y-axis ( y )')
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//example 17.3 clc; funcprot(0); // Initialization of Variable u=60;//m/s Nu5=546; nu=26.41e-6; L4=0.2; L5=0.25; Pr=0.69; Re4=u*L4/nu; Re5=u*L5/nu; Nu4=0.664*Re4^0.5*Pr^0.33; h14=Nu4*0.0338/L4; Nu4=0.664*Re5^0.5*Pr^0.33; h15=Nu5*0.0338/L5; qconv=(h15*L5-h14*L4)*(230-25); disp(qconv,"heat transfer rate in W"); clear()
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// Prob 1.11 clc; clear; close; format('v',5); // Given data VL=400;//in volt Output=10;//in HP Output=Output*735.5;//in watts m=3;//no. of phase Xo=10;//in ohm/phase Eff=85;//in % Input=Output/(Eff/100);//in watts //Formula : Input=sqrt(3)*VL*IL*cosfi ILcosfi=Input/sqrt(3)/VL;//in Ampere ILmin=ILcosfi;//in Ampere disp(ILcosfi,"Minimum current by putting cosfi=1 in Ampere is : "); ER=ILmin*Xo;//in ohm V=VL/sqrt(3);//supply voltage per phase in volt E=sqrt(V^2+ER^2);//in volt LineEMF=sqrt(3)*E;//in volt disp(LineEMF,"Line Induced emf in volt : ");
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/* Eco com filtro comb. x = Sinal de entrada. d = Atraso (em amstras). t = Tempo de decaímento (em amostras). f = Feedback, controla o quanto do sinal atrasado é incluído na efeito. y = Sinal de saída com eco. */ function y = eco(x,d,t,f) N = length(x); // Dimensão do sinal. y = zeros(1,N+t); // Sinal de saida com eco. // Sinal x de entrada 'crescido', para ficar do mesmo tamanho da saída e evitar problemas no laço for. xx = zeros(1,N+t); xx(1:N) = x; // A parte inicial do sinal de saída é igual a entrada, o eco começa a partir de d. y(1:d) = x(1:d); // Filtro comb, indo até o número de amostras de atraso. for n = d:N+t y(n) = xx(n) + f*y(n-(d-1)); end endfunction
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clc clear //input data M1=0.25 //Mach number at entrance f=0.01/4 //frictional factor D=0.15 //inner pipe diameter in m p1=0.8 //Stagnation pressure ratio at exit to entry when loss in stagnation pressure is 20% M3=0.8 //Mach number at a section //calculation p2=2.4065 //Ratio of Stagnation pressure at entry from gas tables @M1,k=1.4 X1=8.537 //frictional constant fanno parameter from gas tables,fanno flow tables @M1 p3=p1*p2 //Ratio of Stagnation pressure at exit M2=0.32 //Exit mach number at p1=0.8 X2=4.447 //frictional constant fanno parameter from gas tables,fanno flow tables @M2 L1=(X1*D)/(4*f) //Length of the pipe in m L2=(X2*D)/(4*f) //Length of the pipe in m L=L1-L2 //Overall length of the duct in m p4=1.038 //Stagnation pressure ratio from M=1 to M3 PL=(1-(p4/p2))*100 //Percentage of stagnation pressure from inlet to section at which M3 in percent //output printf('(A)Length of the pipe is %3.2f m\n (B)Mach number at this exit is %3.2f\n (C)Percentage of stagnation pressure from inlet to section at which M=%3.1f is %3.2f percent\n (D)Maximum length to reach choking condition is %3.3f m',L,M2,M3,PL,L1)
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kiks_sim_prox.sci
function [res] = kiks_sim_prox(id,sample) // Ouput variables initialisation (not found in input variables) res=[]; // Number of arguments in function call [%nargout,%nargin] = argn(0) // Display mode mode(0); // Display warning for floating point exception ieee(1); // ----------------------------------------------------- // (c) 2000-2004 Theodor Storm <theodor@tstorm.se> // http://www.tstorm.se // ----------------------------------------------------- global("KIKS_SIM_PROX_NOISE","KIKS_SIM_PROX_EMAX","KIKS_SIM_PROX_EMIN","KIKS_SIM_PROX_EEXP","KIKS_SIMPROX_STEPS","KIKS_SIM_PROX_SCALE","KIKS_MMPERPIXEL","KIKS_SIM_PROX_STEP","KIKS_SIM_PROX_DIST","KIKS_1250","KIKS_ARENA_COLORMASK","KIKS_PROX_DIR","KIKS_PROX_ANG","KIKS_ROBOT_MATRIX","KIKS_PROX_POS","KIKS_WALL_WIDTH","KIKS_WALL_RENDER","KIKS_MONITOR_WIN","KIKS_MONITOR_ON","KIKS_RBT_TIME","KIKS_MAXMOVLIMIT","KIKS_sensdelay","KIKS_SIMPROX_MAXDIST","KIKS_PROX_ACCURACY","KIKS_PROX_MINRAND","KIKS_PROX_MAXRAND","KIKS_PROX_NNET1","KIKS_PROX_NNET2","KIKS_PROX_NNET3","KIKS_PROX_NNET4","KIKS_PROX_NNET5","KIKS_PROX_NNET6","KIKS_PROX_NNET7","KIKS_PROX_NNET8","KIKS_PROX_NNET_ARRAY","KIKS_PROX_USEARRAY"); if isempty(KIKS_PROX_USEARRAY) then KIKS_PROX_USEARRAY = 0;end; sincelast = mtlb_s(mtlb_double(mtlb_e(KIKS_RBT_TIME,abs(mtlb_double(id)))),mtlb_double(mtlb_e(KIKS_sensdelay,id))); if bool2s(mtlb_logic(sincelast,"<",mtlb_double(KIKS_MAXMOVLIMIT)))|bool2s(mtlb_logic(sincelast,"<",0.02)) then // According to the Khepera manual, proximity sensors update each 20 msec. return; end; prox_xvals = mtlb_a((mtlb_double(KIKS_ROBOT_MATRIX(id,2,2))+1)*cos(mtlb_s(mtlb_double(KIKS_PROX_ANG),mtlb_double(KIKS_ROBOT_MATRIX(id,1,3)))),mtlb_double(KIKS_ROBOT_MATRIX(id,1,1)))/mtlb_double(KIKS_MMPERPIXEL); prox_yvals = mtlb_a((mtlb_double(KIKS_ROBOT_MATRIX(id,2,2))+1)*sin(mtlb_s(mtlb_double(KIKS_PROX_ANG),mtlb_double(KIKS_ROBOT_MATRIX(id,1,3)))),mtlb_double(KIKS_ROBOT_MATRIX(id,1,2)))/mtlb_double(KIKS_MMPERPIXEL); prox_dirs = mtlb_a(mtlb_double(KIKS_PROX_DIR),mtlb_double(KIKS_ROBOT_MATRIX(id,1,3))); [tmp,sensors] = size(prox_xvals); if %nargin<2 then sample = [];end; res = []; proxval = [0,0,0,0,0,0,0,0]; dirs = -%pi/3:%pi/9:%pi/3; for sens = 1:sensors num = 0; proxangval = [0,0,0,0,0,0,0]; proxstep = KIKS_PROX_ACCURACY; sumres(1,sens) = 0; [ysz,xsz] = size(mtlb_double(KIKS_ARENA_COLORMASK)); for dir = -%pi/3:%pi/9:%pi/3 num = num+1; // rotate ray_xvals and ray_yvals to get sensor relative coordinates cosdir = cos(prox_dirs(sens)-dir); sindir = sin(prox_dirs(sens)-dir); ray_xvals = round(mtlb_a(mtlb_double(KIKS_1250)*cosdir,prox_xvals(sens))); ray_yvals = round(mtlb_a(-mtlb_double(KIKS_1250)*sindir,prox_yvals(sens))); idx = mtlb_a(mtlb_s(ray_xvals,1)*ysz,ray_yvals); // calculate index values for these points idx = mtlb_i(idx,mtlb_find(bool2s(mtlb_logic(idx,">",ysz*xsz))),ysz*xsz); idx = mtlb_i(idx,mtlb_find(bool2s(mtlb_logic(idx,"<",1))),1); // ! L.49: abs(mtlb_double(mtlb_e(KIKS_ARENA_COLORMASK,idx))) may be replaced by: // ! --> mtlb_double(mtlb_e(KIKS_ARENA_COLORMASK,idx)) if mtlb_double(mtlb_e(KIKS_ARENA_COLORMASK,idx)) is real obst = mtlb_find(abs(mtlb_double(mtlb_e(KIKS_ARENA_COLORMASK,idx)))); // get all non-zero entries if ~isempty(obst) then dist = min(obst,"m"); xp = mtlb_e(ray_xvals,dist); yp = mtlb_e(ray_yvals,dist); c = KIKS_ARENA_COLORMASK(floor(yp),floor(xp)); oldc = c; back = 0; while bool2s(mtlb_logic(mtlb_double(c),">",0))&bool2s(mtlb_logic(back,"<",mtlb_double(KIKS_SIM_PROX_STEP))) back = back+1; oldc = c; xp = mtlb_s(xp,cosdir); yp = mtlb_a(yp,sindir); c = KIKS_ARENA_COLORMASK(floor(yp),floor(xp)); end; c = oldc; %v0_1 = mtlb_a(mtlb_s(mtlb_double(KIKS_SIM_PROX_DIST),(dist*mtlb_double(KIKS_MMPERPIXEL))*ceil(mtlb_double(KIKS_SIM_PROX_STEP)/mtlb_double(KIKS_MMPERPIXEL))),back); proxangval(1,num) = (%v0_1(:)).'; // Color sensitive falloff proxangval = mtlb_i(proxangval,num,mtlb_s(proxangval(num),(proxangval(num)*0.5)*(mtlb_s(255,mtlb_double(c))/255))); end; sumres = mtlb_i(sumres,sens,sumres(sens)+proxangval(num)); end; res(sens,1:length(proxangval)) = proxangval; end; // Error settings Emax = KIKS_SIM_PROX_EMAX;// Max relative error caused by noise when sensor reading is 1 Emin = KIKS_SIM_PROX_EMIN;// Max relative error caused by noise when sensor reading is 1000 Eexp = KIKS_SIM_PROX_EEXP;// The larger Eexp, the less frequent large errors are. // Eexp=1 ==> Errors are evenly distributed across the error range, // Eexp=Inf ==> No errors, // Eexp>1 ==> Large errors are less common than small errors, // Eexp<1 ==> Large errors are more common than small errors. for sens = 1:sensors if sumres(sens)>0 then if mtlb_logic(mtlb_double(KIKS_PROX_USEARRAY),"==",0) then // calculate neural network select pmodulo(sens-1,8) case 0 then // !! L.90: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET1,(res(sens,:))'); case 1 then // !! L.92: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET2,(res(sens,:))'); case 2 then // !! L.94: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET3,(res(sens,:))'); case 3 then // !! L.96: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET4,(res(sens,:))'); case 4 then // !! L.98: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET5,(res(sens,:))'); case 5 then // !! L.100: Matlab toolbox(es) function sim not converted, original calling sequence used smsens = sim(KIKS_PROX_NNET6,(res(sens,:))'); case 6 then // !! L.102: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET7,(res(sens,:))'); case 7 then // !! L.104: Matlab toolbox(es) function sim not converted, original calling sequence used simsens = sim(KIKS_PROX_NNET8,(res(sens,:))'); end; else // find values in array ix = round(res(sens,:)/mtlb_double(KIKS_SIM_PROX_SCALE)); if mtlb_logic(sum(ix,"m"),">",0) then ix = mtlb_a(ix,1); ix = mtlb_i(ix,mtlb_find(bool2s(mtlb_logic(ix,">",mtlb_double(KIKS_SIMPROX_STEPS)))),KIKS_SIMPROX_STEPS); ix = mtlb_i(ix,mtlb_find(bool2s(mtlb_logic(ix,"<",1))),1); simsens = mtlb_double(KIKS_PROX_NNET_ARRAY(ix(1),ix(2),ix(3),ix(4),ix(5),ix(6),ix(7)))*(1023/255); else simsens = 0; end; end; errQ = mtlb_s(mtlb_double(Emax),(mtlb_double(simsens)/1000)*mtlb_s(mtlb_double(Emax),mtlb_double(Emin))); // randQ=KIKS_PROX_MINRAND/KIKS_PROX_MAXRAND; minrand = -mtlb_double(KIKS_PROX_MINRAND)*errQ; maxrand = mtlb_double(KIKS_PROX_MAXRAND)*errQ; if mtlb_logic(mtlb_double(rand()),"<",0.5) then rdir = maxrand;else rdir = minrand;end; randval = mtlb_a(1,rdir*(mtlb_double(rand())^mtlb_double(Eexp))); proxval(sens) = mtlb_min(1023,round(mtlb_double(simsens)*randval)); end; end; KIKS_sensdelay = mtlb_i(KIKS_sensdelay,id,mtlb_e(KIKS_RBT_TIME,abs(mtlb_double(id)))); //if KIKS_ROBOTTYPE==2 // baseval=90+rand(1,8)*20; // proxval=round(baseval+proxval); // proxval(find(proxval>1023))=1023; //end; [rows,cols] = size(proxval); noiseval = rand(rows,cols)*1023; KIKS_ROBOT_MATRIX(id,KIKS_PROX_POS,:) = mtlb_min(1023,round(mtlb_a(proxval*(mtlb_s(100,mtlb_double(KIKS_SIM_PROX_NOISE))/100),noiseval*(mtlb_double(KIKS_SIM_PROX_NOISE)/100)))); endfunction
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funcprot(0) function A = circulante(n) A = zeros(n,n) A(1,n)=1 // coef en haut à droite for k=1:n-1 A(k+1,k)=1 // sous-diagonale end endfunction //n=6 //p=.8 //A = circulante(n) //I = eye(n,n) //transition = p * A + (1-p) * I ////disp(transition)
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// Calculate the resistance of the cell clc; Ri=30; Rf=100; t=10; tc=72; Rt=Ri+(Rf-Ri)*[1-exp(-t/tc)]; disp(Rt,'resistance of the cell (K ohm)')
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clc// // // //Variable declaration H=10^6; //magnetic field(amp/m) chi=1.5*10^-3; mew0=4*%pi*10^-7; //Calculation M=chi*H; //magnetisation of material(A/m) B=mew0*(M+H); //flux density(T) //Result printf("\n magnetisation of material is %0.3f *10^3 A/m",M/10^3) printf("\n flux density is %0.4f T",B) printf("\n answer given in the book varies due to rounding off errors")
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//Example 2.2.1 //Geostationary Satellite Look Angles //Variable Declaration Le=52.0 le=0 longs=66.0 //Calculation y=acosd(cosd(Le)*cosd(longs-le)) printf("Central Angle is %f degrees\n",y) El=atand((6.6107345-cosd(y))/sind(y))-y printf("Elevation Angle is %f degrees\n",(El)) alpha=atand(tand(longs-le)/sind(Le)) printf("Intermediate Angle is %f degrees\n",alpha) Az=180-alpha printf("Azimuth Angle is %f degrees (clockwise from true north )",Az)
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// Scilab Code Ex9.2.4: Page-415 (2008) clc; clear; lambda1 = 3333e-010; // First wavelength of the incident light, m lambda2 = 2400e-010; // Second wavelength of the incident light, m c = 3e+008; // Speed of light in free space, m/s e = 1.6e-019; // Energy equivalent of 1 eV, J E1 = 0.6; // Kinetic energy of the emitted photoelectrons for the first wavelength, eV E2 = 2.04; // Kinetic energy of the emitted photoelectrons for the second wavelength, eV h = (E2 - E1)*lambda1*lambda2*e/(c*(lambda1 - lambda2)); // Planck's constant, Js W0 = (E2*lambda2 - E1*lambda1)/(lambda1 - lambda2); // Work function of the metal, eV printf("\nThe value of Planck constant = %3.1e Js", h); printf("\nThe work function of the metal = %3.1f eV", W0); // Result // The value of Planck constant = 6.6e-034 Js // The work function of the metal = 3.1 eV
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//Example 2.7.1 Page 31 //Non-Linear Dynamics and Chaos, First Indian Edition Print 2007 //Steven H. Strogatz clear; clc; close; set(gca(),"auto_clear","off") //hold on //x(dot) = f(x) = -x // On Integrating we get V(x) = (1/2)x^2 + C ; C = 0. //Now, Plotting the potential i.e. V(x) for x = -5:0.5:5 V = (1/2)*x^2; plot2d(x,V,style=-2) end plot2d(0,0,style=-4) //Just to show that the fixed point is Stable. set(gca(),"grid",[2,5]) xtitle("Potential Diagram","x-Axis(x)","y-Axis (V(x))") disp("From graph of V(x) v/s x itself, it is clear that :-") disp("The only equilibrium point is at x=0") disp(" And from the flow we can conclude that the x*=0 point is Stable.") disp("OR") disp("f(dot)(x) = -1 for all x; Thus every equilibrium point which exists is Stable.") //End of Example.
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// Chapter 4_Carrier Transport Phenomenon //Caption_The Einstein relation //Ex_6//page 155 T=300 mu=1000 //mobility of a particular carrier kT=0.0259 e=1.6*(10^-19) D=(kT)*mu printf('Diffusion coefficient is %1.2fd cm^2/s ',D)
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function strBody = hrtFrameBody(strFrame) tokensFrame = tokens(part(strFrame,hrtFrameIni(strFrame):$),' ') count = hrtFrameType(strFrame)*4; strNBBody = tokensFrame(4+count); nBBody = hex2dec(strNBBody); if nBBody == 0 then strBody = ''; else strBody = tokensFrame(5+count:4+count+nBBody); end endfunction
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//example 6.11 clear; clc; //Given: W=1000;//Total mass of a solution[gm] x1=0.5;//mole fraction of Chloroform x2=0.5;//mole fraction of Acetone V1m=80.235;//Partial molar volume of chloroform[cm3/mol] V2m=74.166;//Partial molar volume of Acetone[cm3/mol] M1=119.59;//molecular weight of chloroform[gm/mol] M2=58;//molecular weight of Acetone[gm/mol] //To find the Volume of the solution nT=W/(x1*M1+x2*M2);//Total no. of moles V=nT*(x1*V1m+x2*V2m);//Total volume[cm3] printf("The volume of the solution is %f cm3",V);
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//Lista de exercício 3 - 2º Tarefa //Dados pi = %pi; r_e = 0.001; // raio da esfera em metros r = 1; // raio da pista circular rho = 7850; //densidade do aço em kg/m^3 g = 9.8; //m/s^2 m = (4/3)*pi*(r_e^3)*7850 // massa em kg //Condições 1 theta_1 = [0;0]; //Condições 2 theta_2 = [-pi/180;0]; //Condições 3 theta_3 = [pi/4;1.8]; //Condições 4 theta_4 = [5*pi/6;0]; //Condições 5 theta_5 = [pi/2;2]; //Condições 6 theta_6 = [pi*2/3;0]; //Condições 7 theta_7 = [0;3]; //Condições 8 theta_8 = [pi/10;0.5]; //Condições 9 theta_9 = [pi*14/15;-2]; //Condições 10 theta_10 = [pi/3;6]; //Condições 10 theta_11 = [pi/3;6]; //Condições 10 theta_12 = [pi/3;6]; //Condições 10 theta_13 = [pi/3;6]; //Condições 10 theta_14 = [pi/45;1.9]; //Condições 10 theta_15 = [pi/2;0.35]; //Vetor tempo t0 = 0; tf = 10; //Vamos integrar pelo tempo de 0 a 10 segundos dt = 0.01; //Define o passo, quanto menor mais preciso t = t0:dt:tf; //Espaço de estados function dtheta = f(t,v) //s é o vetor de estado, ou seja, s = [s, ds/dt] dtheta1 = v(2); dtheta2 = -g*sin(v(1))/r; dtheta = [dtheta1; dtheta2]; endfunction theta1 = ode(theta_1,0,t,f); theta2 = ode(theta_2,0,t,f); theta3 = ode(theta_3,0,t,f); theta4 = ode(theta_4,0,t,f); theta5 = ode(theta_5,0,t,f); theta6 = ode(theta_6,0,t,f); theta7 = ode(theta_7,0,t,f); theta8 = ode(theta_8,0,t,f); theta9 = ode(theta_9,0,t,f); theta10 = ode(theta_10,0,t,f); //Plotar gráficos clf() scf(0) xtitle('Retrato do espaço de fases'); plot(theta1(1,:), theta1(2,:), 'k'); plot(theta2(1,:), theta2(2,:), 'k'); plot(theta3(1,:), theta3(2,:), 'k'); plot(theta4(1,:), theta4(2,:), 'k'); plot(theta5(1,:), theta5(2,:), 'k'); plot(theta6(1,:), theta6(2,:), 'k'); plot(theta7(1,:), theta7(2,:), 'k'); plot(theta8(1,:), theta8(2,:), 'k'); plot(theta9(1,:), theta9(2,:), 'k'); plot(theta10(1,:), theta10(2,:), 'k');
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// Calculating Difference mode, Common mode gain and CMRR clc; Vo=3; Vd=30*10^-3; Ad=Vo/Vd; disp(Ad,'difference mode gain=') Vo=5*10^-3; Vc=500*10^-3; Ac=Vo/Vc; disp(Ac,'Common mode gain=') CMRR=Ad/Ac; disp(CMRR,'Common mode rejection ratio=')
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// Scilab Code Ex1.10: Page-1.8 (2009) clc; clear; m = 1.67e-027; // Mass of the proton, kg c = 3e+08; // Speed of light, m/s v = 1/20*c; // Velocity of the proton, m/s h = 6.626e-034; // Planck's constant, Js lambda = h/(m*v); // de Broglie wavelength of the neutron, m printf("\nThe de Broglie wavelength associated with moving proton = %5.3e m", lambda); // Result // The de Broglie wavelength associated with moving proton = 2.645e-14 m
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x=0:5; y=[0 10 25 36 52 59]; x_new=0:.01:5; y_new=interp1(x,y,x_new,'spline'); plot(x,y,'d'); legend off; plot(x_new,y_new) title('Velocity versus Time','fontsize',5) ylabel('Miles per Hour','fontsize',5) xlabel('Time, seconds','fontsize',5) legend('Data Points','Cubic Spline Interpolation')
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 14.1w //calculation of the extension of the wire //given data L=2//lengh(in m)of the wire A=.2*10^-4//area(in m^2) m=4.8//mass(in kg) Y=2*10^11//Young modulus of steel g=10//gravitational acceleration(in m/s^2) of the earth //calculation T=m*g//weight l=(T*L)/(A*Y)//exension printf('the extension of the wire is %3.1e m',l)
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//page 92 clear; close; clc; A=[1 3 3 2;2 6 9 5;-1 -3 3 0]; disp('Given matrix:') disp(A) B=A; disp('C2->C2-3*C1') A(:,2)=A(:,2)-3*A(:,1); disp(A) disp('Here,C2=3*C1,Therefore the columns are linearly dependent.') disp('R3->R3-2*R2+5*R1') B(3,:)=B(3,:)-2*B(2,:)+5*B(1,:); disp(B) disp('Here R3=R3-2*R2+5*R1,therefore the rows are linearly dependent.') //end
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//to calculate power angle,excitation emf,field current clc; j=sqrt(-1); MVA_b=300; kV_b=22; Pe=250/MVA_b; pf=.85; Vt=1; Ia=Pe/(pf*Vt); phi=acosd(pf); Iaa=Ia*complex(cosd(-phi),sind(-phi)); Xq=1.16; Xd=1.93; Ef=Vt+j*Iaa*Xq; dl=atand(imag(Ef)/real(Ef));disp(dl,'power angle'); w=phi+dl; Id=abs(Iaa)*sind(w); Ef=abs(Ef)+Id*(Xd-Xq); disp(Ef*kV_b,'excitation emf(V)'); If=338; If=If*Ef/1;disp(If,'field current(A)');
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78.92572, 11584, 9456, 11560, 10504, 11552, 9736; 78.92572, 11584, 9456, 11568, 9992, 11552, 9992; 78.92572, 11584, 10104, 11568, 10080, 11552, 10184; 78.92572, 11576, 11104, 11568, 10080, 11552, 10184; 78.92572, 11576, 11104, 11568, 9848, 11552, 9952; 78.92572, 11584, 12288, 11568, 10360, 11552, 10456; 78.92572, 11592, 10672, 11568, 10072, 11552, 10456; 78.92572, 11592, 10672, 11568, 10072, 11560, 10192; 78.92572, 11592, 9288, 11560, 10392, 11560, 10440; 78.92572, 11584, 9776, 11560, 10008, 11560, 10312; 78.92572, 11576, 10776, 11560, 10008, 11560, 10312; 78.92572, 11576, 10776, 11560, 10104, 11560, 9928; 78.92572, 11576, 11440, 11568, 10488, 11560, 9960; 78.92572, 11584, 12336, 11568, 10464, 11552, 9960; 78.92572, 11584, 12336, 11568, 10464, 11552, 10008; 78.92572, 11584, 12112, 11568, 10488, 11552, 9856; 78.92572, 11592, 9744, 11568, 9848, 11552, 9856; 78.92572, 11592, 9432, 11560, 9848, 11552, 10272; 78.92572, 11592, 9432, 11560, 9744, 11560, 10728; 78.92572, 11584, 9744, 11568, 10424, 11560, 10616; 78.92572, 11584, 11336, 11568, 10424, 11560, 10616; 78.92572, 11576, 11336, 11568, 10312, 11560, 10304; 78.92572, 11584, 12216, 11560, 10136, 11560, 10640; 78.92572, 11592, 11048, 11560, 9632, 11560, 10640; 78.92572, 11592, 11048, 11560, 9632, 11560, 10184; 78.92572, 11592, 9280, 11560, 10296, 11560, 9944; 78.92572, 11584, 9712, 11560, 10408, 11560, 9944; 78.92572, 11584, 10544, 11560, 10408, 11552, 10040; 78.92572, 11576, 10544, 11568, 10296, 11552, 10008; 78.92572, 11576, 11520, 11568, 10048, 11552, 10008; 78.92572, 11584, 12112, 11568, 10048, 11552, 10048; 78.92572, 11584, 12112, 11568, 10088, 11552, 10400; 78.92572, 11592, 10680, 11560, 10128, 11552, 10536; 78.92572, 11592, 9672, 11560, 10128, 11552, 10536; 78.92572, 11592, 9672, 11560, 10184, 11560, 10720; 78.92572, 11584, 9280, 11560, 9920, 11560, 10896; 78.92572, 11576, 10360, 11560, 9816, 11560, 10896; 78.92572, 11576, 10360, 11560, 9816, 11560, 10744; 78.92572, 11576, 11128, 11560, 10440, 11560, 10232; 78.92572, 11584, 11768, 11560, 9960, 11560, 10232; 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78.92572, 11576, 10992, 11560, 10440, 11560, 10632; 78.92572, 11576, 11968, 11568, 10448, 11552, 10576; 78.92572, 11592, 11104, 11568, 10440, 11552, 10576; 78.92572, 11592, 9456, 11568, 10440, 11560, 10792; 78.92572, 11592, 9456, 11560, 9808, 11560, 10600; 78.92572, 11584, 9768, 11560, 9904, 11560, 10600; 78.92572, 11576, 11120, 11560, 9904, 11560, 10456; 78.92572, 11576, 11120, 11560, 10512, 11560, 10472; 78.92572, 11592, 11632, 11568, 10232, 11552, 10040; 78.92572, 11592, 10560, 11568, 10232, 11552, 10040; 78.92572, 11592, 10560, 11560, 10128, 11552, 9752; 78.92572, 11592, 9352, 11560, 9768, 11552, 10088; 78.92572, 11584, 10016, 11560, 10424, 11552, 10088; 78.92572, 11584, 10016, 11560, 10424, 11552, 10104; 78.92572, 11576, 11176, 11568, 10456, 11552, 10376; 78.92572, 11584, 12184, 11568, 9592, 11552, 10808; 78.92572, 11592, 10496, 11568, 9592, 11552, 10808; 78.92572, 11592, 10496, 11568, 10536, 11560, 10832; 78.92572, 11592, 9664, 11568, 9904, 11560, 10376; 78.92572, 11584, 9440, 11568, 10048, 11560, 10376; 78.92572, 11584, 9440, 11560, 10048, 11560, 10168; 78.92572, 11584, 10648, 11568, 9832, 11560, 10256; 78.92572, 11576, 11480, 11568, 10376, 11560, 10256; 78.92572, 11576, 11904, 11568, 10376, 11552, 10088; 78.92572, 11584, 11904, 11568, 10240, 11552, 10512; 78.92572, 11592, 10744, 11568, 10312, 11552, 10336; 78.92572, 11592, 9528, 11568, 10056, 11560, 10336; 78.92572, 11592, 9528, 11560, 10056, 11560, 10184; 78.92572, 11584, 9736, 11568, 10608, 11560, 10488; 78.92572, 11576, 10960, 11568, 10376, 11560, 10488; 78.92572, 11576, 11888, 11568, 10376, 11560, 10008; 78.92572, 11576, 11888, 11568, 9832, 11560, 10040; 78.92572, 11584, 11760, 11568, 9512, 11560, 10040; 78.92572, 11584, 11056, 11568, 9512, 11552, 10112; 78.92572, 11592, 11056, 11568, 9992, 11552, 9944; 78.92572, 11592, 9536, 11560, 10288, 11552, 9944; 78.92572, 11584, 9656, 11560, 10288, 11552, 10112; 78.92572, 11584, 9656, 11560, 9776, 11552, 9432; 78.92572, 11576, 10504, 11560, 9928, 11552, 10096; 78.92572, 11576, 10928, 11560, 9928, 11552, 10096; 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78.92572, 11584, 9376, 11560, 10152, 11560, 10128; 78.92572, 11576, 10560, 11560, 10304, 11552, 10368; 78.92572, 11576, 11528, 11560, 10504, 11552, 10368; 78.92572, 11576, 12000, 11568, 10504, 11552, 10360; 78.92572, 11592, 12000, 11568, 10408, 11552, 10240; 78.92572, 11592, 10000, 11560, 9704, 11552, 10240; 78.92572, 11584, 9616, 11560, 9704, 11560, 10560; 78.92572, 11584, 9616, 11560, 9832, 11560, 10424; 78.92572, 11584, 9920, 11568, 9824, 11560, 10424; 78.92572, 11576, 11488, 11568, 9824, 11560, 10360; 78.92572, 11576, 11488, 11568, 10208, 11552, 10336; 78.92572, 11584, 12072, 11560, 9752, 11552, 10208; 78.92572, 11592, 11056, 11560, 9752, 11552, 10208; 78.92572, 11592, 11056, 11560, 9928, 11552, 9656; 78.92572, 11592, 9656, 11560, 10448, 11552, 10176; 78.92572, 11584, 9568, 11560, 10288, 11552, 10176; 78.92572, 11584, 9568, 11560, 10288, 11560, 10024; 78.92572, 11576, 10416, 11568, 10568, 11552, 9664; 78.92572, 11576, 11472, 11568, 9592, 11552, 9664; 78.92572, 11584, 11992, 11568, 9592, 11552, 10088; 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80.83048, 11584, 10776, 11560, 10080, 11552, 10328; 80.83048, 11584, 11152, 11568, 10136, 11552, 10880; 80.83048, 11584, 10544, 11560, 10368, 11552, 10880; 80.83048, 11584, 10800, 11560, 10368, 11552, 10928; 80.83048, 11576, 10800, 11560, 10064, 11544, 10200; 80.83048, 11576, 11032, 11560, 9976, 11544, 10416; 80.83048, 11584, 10576, 11560, 10160, 11552, 10416; 80.83048, 11584, 10576, 11560, 10160, 11552, 9968; 80.83048, 11584, 10408, 11560, 10328, 11552, 10264; 80.83048, 11584, 10616, 11560, 10272, 11552, 10264; 80.83048, 11584, 11032, 11560, 10272, 11552, 11032; 80.83048, 11584, 11032, 11560, 9960, 11552, 10888; 80.83048, 11584, 10808, 11560, 10280, 11552, 10888; 80.83048, 11584, 10504, 11560, 10280, 11544, 10104; 80.83048, 11584, 10504, 11560, 10280, 11544, 10328; 80.83048, 11584, 10456, 11560, 10280, 11552, 10400; 80.83048, 11584, 10952, 11560, 10280, 11552, 10400; 80.83048, 11584, 10952, 11560, 9952, 11552, 10496; 80.83048, 11584, 10736, 11560, 10064, 11552, 10784; 80.83048, 11576, 11392, 11560, 10160, 11552, 10784; 80.83048, 11576, 11072, 11560, 10160, 11552, 10272; 80.83048, 11576, 11072, 11560, 10096, 11544, 10280; 80.83048, 11584, 10512, 11560, 9936, 11544, 10576; 80.83048, 11584, 10960, 11560, 9936, 11552, 10576; 80.83048, 11584, 10960, 11560, 10192, 11552, 10760; 80.83048, 11584, 10768, 11560, 10160, 11552, 10648; 80.83048, 11584, 10136, 11560, 10280, 11552, 10648; 80.83048, 11584, 10512, 11560, 10280, 11552, 10512; 80.83048, 11584, 10512, 11560, 10256, 11552, 9912; 80.83048, 11584, 10584, 11560, 10320, 11552, 10224; 80.83048, 11584, 10888, 11560, 10320, 11552, 10224; 80.83048, 11584, 10888, 11560, 10232, 11552, 10872; 80.83048, 11584, 10864, 11560, 10088, 11560, 10904; 80.83048, 11584, 10944, 11560, 9952, 11560, 10904; 80.83048, 11584, 10976, 11560, 9952, 11544, 10072; 80.83048, 11584, 10976, 11560, 10240, 11552, 10360; 80.83048, 11584, 10336, 11560, 10120, 11552, 10360; 80.83048, 11584, 10632, 11560, 10120, 11552, 10696; 80.83048, 11584, 10632, 11560, 10040, 11552, 10808; 80.83048, 11576, 11096, 11560, 9984, 11552, 10384; 80.83048, 11584, 10640, 11560, 9984, 11552, 10384; 80.83048, 11584, 10640, 11560, 10192, 11552, 9984; 80.83048, 11584, 10608, 11560, 10184, 11552, 10376; 80.83048, 11584, 10592, 11560, 10152, 11552, 10376; 80.83048, 11584, 10592, 11560, 10152, 11552, 10864; 80.83048, 11584, 10800, 11560, 9960, 11560, 11000; 80.83048, 11576, 11080, 11560, 10256, 11560, 10576; 80.83048, 11576, 10928, 11560, 10256, 11552, 10576; 80.83048, 11576, 10928, 11560, 10104, 11552, 10608; 80.83048, 11576, 11216, 11560, 10104, 11552, 9960; 80.83048, 11584, 10184, 11560, 9896, 11552, 9960; 80.83048, 11584, 10184, 11560, 9896, 11552, 10400; 80.83048, 11584, 10280, 11560, 10248, 11552, 10840; 80.83048, 11576, 11136, 11560, 10184, 11552, 10840; 80.83048, 11576, 10872, 11560, 10184, 11552, 10448; 80.83048, 11576, 10872, 11560, 9888, 11552, 9976; 80.83048, 11584, 10960, 11560, 9856, 11552, 9976; 80.83048, 11584, 10656, 11560, 9856, 11544, 10400; 80.83048, 11584, 10656, 11560, 10304, 11552, 10904; 80.83048, 11584, 10200, 11560, 9952, 11552, 10600; 80.83048, 11584, 10840, 11560, 9952, 11552, 10600; 80.83048, 11584, 10840, 11560, 10024, 11544, 10120; 80.83048, 11576, 10688, 11560, 9912, 11552, 10096; 80.83048, 11584, 10888, 11560, 10416, 11552, 10096; 80.83048, 11584, 10888, 11560, 10416, 11552, 10384; 80.83048, 11584, 10368, 11560, 10248, 11552, 10832; 80.83048, 11584, 10608, 11560, 9992, 11552, 10832; 80.83048, 11584, 10776, 11560, 9992, 11552, 10952; 80.83048, 11584, 10776, 11560, 9920, 11552, 10112; 80.83048, 11584, 11104, 11560, 10304, 11552, 10248; 80.83048, 11584, 10808, 11560, 10056, 11544, 10248; 80.83048, 11584, 10808, 11560, 10056, 11552, 10272; 80.83048, 11584, 10800, 11560, 10032, 11552, 10816; 80.83048, 11584, 10528, 11560, 9936, 11552, 10816; 80.83048, 11584, 10952, 11560, 9936, 11552, 10728; 80.83048, 11584, 10952, 11560, 10312, 11552, 10768; 80.83048, 11584, 10672, 11560, 10136, 11552, 9880; 80.83048, 11584, 10168, 11560, 10192, 11552, 9880; 80.83048, 11584, 10168, 11560, 10192, 11544, 10384; 80.83048, 11584, 10648, 11560, 10120, 11552, 10880; 80.83048, 11576, 11048, 11560, 10240, 11552, 10880; 80.83048, 11576, 11072, 11560, 10240, 11552, 10776; 80.83048, 11584, 11072, 11560, 9968, 11552, 10504; 80.83048, 11584, 11016, 11560, 9968, 11552, 10504; 80.83048, 11584, 10456, 11560, 9968, 11552, 10240; 80.83048, 11584, 10456, 11560, 9912, 11552, 10192; 80.83048, 11584, 10520, 11560, 10536, 11552, 10552; 80.83048, 11584, 10256, 11560, 10536, 11552, 10552; 80.83048, 11584, 10256, 11560, 10096, 11552, 11136; 80.83048, 11576, 10840, 11560, 9904, 11552, 10424; 80.83048, 11576, 11344, 11560, 10088, 11552, 10424; 80.83048, 11576, 11344, 11560, 10088, 11544, 10384; 80.83048, 11576, 11320, 11560, 10464, 11552, 10488; 80.83048, 11584, 10704, 11560, 10232, 11552, 10384; 80.83048, 11584, 10392, 11560, 10232, 11560, 10384; 80.83048, 11584, 10392, 11560, 10120, 11552, 10712; 80.83048, 11584, 10232, 11560, 9808, 11552, 10840; 80.83048, 11584, 10520, 11560, 10360, 11552, 10840; 80.83048, 11584, 10800, 11560, 10360, 11552, 9904; 80.83048, 11584, 10800, 11560, 10128, 11544, 10288; 80.83048, 11576, 11280, 11560, 10024, 11544, 10288; 80.83048, 11576, 11376, 11560, 10024, 11552, 10952; 80.83048, 11576, 11376, 11560, 10048, 11552, 10568; 80.83048, 11576, 10784, 11560, 10472, 11552, 10568; 80.83048, 11584, 10344, 11560, 10472, 11552, 10016; 80.83048, 11584, 10344, 11560, 10152, 11552, 9920; 80.83048, 11584, 10360, 11560, 10040, 11560, 10744; 80.83048, 11584, 10320, 11560, 10040, 11560, 10744; 80.83048, 11584, 10320, 11560, 10040, 11560, 10696; 80.83048, 11584, 10880, 11560, 10464, 11552, 10664; 80.83048, 11584, 10408, 11560, 10048, 11552, 10088; 80.83048, 11576, 10952, 11560, 10048, 11552, 10088; 80.83048, 11576, 10952, 11560, 10208, 11544, 10032; 80.83048, 11576, 11032, 11560, 10272, 11544, 10520; 80.83048, 11576, 10984, 11560, 10456, 11552, 10520; 80.83048, 11576, 10824, 11560, 10456, 11552, 10880; 80.83048, 11584, 10824, 11560, 10216, 11552, 10400; 80.83048, 11584, 10344, 11560, 10136, 11552, 9992; 80.83048, 11584, 10304, 11560, 10136, 11552, 9992; 80.83048, 11584, 10304, 11560, 10176, 11552, 10640; 80.83048, 11584, 10784, 11560, 10480, 11552, 10584; 80.83048, 11584, 10496, 11560, 10312, 11552, 10584; 80.83048, 11584, 11408, 11560, 10312, 11552, 10752; 80.83048, 11576, 11408, 11560, 9976, 11552, 10496; 80.83048, 11568, 12256, 11560, 10008, 11552, 10496; 80.83048, 11568, 11816, 11560, 10008, 11544, 10024; 80.83048, 11576, 11816, 11552, 10448, 11544, 10032; 80.83048, 11584, 11120, 11560, 10480, 11544, 10488; 80.83048, 11592, 9256, 11560, 10480, 11552, 10488; 80.83048, 11592, 9256, 11568, 10136, 11560, 10952; 80.83048, 11584, 9584, 11568, 10104, 11560, 10712; 80.83048, 11592, 9592, 11568, 10472, 11552, 10712; 80.83048, 11592, 9592, 11560, 10472, 11552, 10280; 80.83048, 11584, 11232, 11560, 10216, 11552, 10128; 80.83048, 11576, 10920, 11560, 10048, 11552, 10128; 80.83048, 11576, 10968, 11560, 10048, 11552, 10232; 80.83048, 11584, 10968, 11560, 10024, 11552, 10888; 80.83048, 11584, 11120, 11560, 10288, 11552, 10456; 80.83048, 11584, 10056, 11560, 10216, 11552, 10456; 80.83048, 11584, 10056, 11560, 10216, 11544, 10440; 80.83048, 11584, 10392, 11560, 10144, 11552, 10208; 80.83048, 11576, 10976, 11560, 10256, 11552, 10208; 80.83048, 11576, 11072, 11560, 10256, 11552, 10504; 80.83048, 11576, 11072, 11560, 10216, 11552, 10816; 80.83048, 11584, 10936, 11560, 10104, 11552, 10816; 80.83048, 11576, 10784, 11560, 10104, 11552, 10720; 80.83048, 11576, 10784, 11560, 10000, 11552, 10304; 80.83048, 11584, 10624, 11560, 10152, 11552, 9952; 80.83048, 11584, 10624, 11560, 10184, 11552, 9952; 80.83048, 11584, 10624, 11560, 10184, 11552, 10720; 80.83048, 11584, 10656, 11560, 10008, 11560, 11032; 80.83048, 11584, 10888, 11560, 9928, 11560, 11032; 80.83048, 11576, 11056, 11560, 9928, 11552, 10536; 80.83048, 11576, 11056, 11560, 10168, 11544, 10320; 80.83048, 11584, 10480, 11560, 10160, 11544, 10208; 80.83048, 11584, 10752, 11560, 10168, 11544, 10208; 80.83048, 11584, 10752, 11560, 10168, 11552, 10360; 80.83048, 11584, 10304, 11560, 10000, 11552, 10728; 80.83048, 11584, 10680, 11560, 10400, 11552, 10728; 80.83048, 11584, 10944, 11560, 10400, 11552, 10376; 80.83048, 11584, 10944, 11560, 10160, 11552, 9856; 80.83048, 11576, 10800, 11560, 10376, 11552, 10376; 80.83048, 11584, 11008, 11560, 10040, 11552, 10376; 80.83048, 11584, 11008, 11560, 10040, 11552, 11048; 80.83048, 11576, 11144, 11560, 10256, 11552, 10536; 80.83048, 11584, 10424, 11560, 9984, 11552, 10536; 80.83048, 11584, 10248, 11560, 9984, 11552, 10536; 80.83048, 11584, 10248, 11560, 9944, 11552, 10400; 80.83048, 11576, 10752, 11560, 9976, 11552, 10400; 80.83048, 11584, 10704, 11560, 9976, 11552, 9680; 80.83048, 11584, 10704, 11560, 10304, 11552, 10720; 80.83048, 11584, 11080, 11560, 10032, 11552, 10328; 80.83048, 11584, 10328, 11560, 10032, 11560, 10328; 80.83048, 11584, 10328, 11560, 9912, 11552, 10720; 80.83048, 11584, 10416, 11560, 9880, 11552, 10032; 80.83048, 11576, 10736, 11560, 10280, 11552, 10032; 80.83048, 11576, 10736, 11560, 10280, 11544, 10552; 80.83048, 11576, 10936, 11560, 10056, 11552, 10496; 80.83048, 11584, 10968, 11560, 10064, 11552, 10600; 80.83048, 11584, 10856, 11560, 10064, 11552, 10600; 80.83048, 11584, 10856, 11560, 9952, 11552, 10696; 80.83048, 11584, 10448, 11560, 10360, 11552, 10128; 80.83048, 11584, 10592, 11560, 10240, 11552, 10128; 80.83048, 11584, 10608, 11560, 10240, 11552, 10232; 80.83048, 11576, 10608, 11560, 9968, 11552, 10656; 80.83048, 11584, 11264, 11560, 9992, 11552, 10656; 80.83048, 11584, 10760, 11560, 9992, 11552, 10680; 80.83048, 11584, 10760, 11560, 10304, 11552, 10520; 80.83048, 11584, 10360, 11560, 10088, 11552, 10520; 80.83048, 11584, 10656, 11560, 10088, 11552, 10360; 80.83048, 11584, 10656, 11560, 10000, 11552, 10216; 80.83048, 11584, 10096, 11560, 9992, 11552, 10632; 80.83048, 11584, 10864, 11560, 10480, 11552, 10632; 80.83048, 11584, 10864, 11560, 10480, 11552, 10960; 80.83048, 11576, 11032, 11560, 10176, 11552, 10720; 80.83048, 11576, 11320, 11560, 10128, 11552, 10720; 80.83048, 11584, 10448, 11560, 10128, 11544, 9968; 80.83048, 11584, 10448, 11560, 10056, 11552, 10472; 80.83048, 11584, 10488, 11560, 10424, 11552, 10432; 80.83048, 11584, 10608, 11560, 10104, 11552, 10432; 80.83048, 11584, 10608, 11560, 10104, 11560, 10584; 80.83048, 11584, 10872, 11560, 10216, 11552, 10816; 80.83048, 11576, 10832, 11560, 10176, 11552, 10816; 80.83048, 11576, 10496, 11560, 10176, 11552, 10344; 80.83048, 11584, 10496, 11560, 10464, 11552, 9864; 80.83048, 11584, 10904, 11560, 10472, 11552, 10480; 80.83048, 11584, 10688, 11560, 10016, 11552, 10480; 80.83048, 11584, 10688, 11560, 10016, 11552, 10496; 80.83048, 11584, 10704, 11560, 9976, 11552, 10648; 80.83048, 11584, 11000, 11560, 10360, 11552, 10648; 80.83048, 11584, 10888, 11560, 10360, 11552, 10928; 80.83048, 11584, 10888, 11560, 10120, 11552, 10288; 80.83048, 11584, 10544, 11560, 10232, 11552, 10288; 80.83048, 11576, 11104, 11560, 10232, 11544, 9560; 80.83048, 11576, 11104, 11560, 10056, 11552, 10424; 80.83048, 11576, 11280, 11560, 10440, 11552, 11072; 80.83048, 11584, 10568, 11560, 10168, 11560, 11072; 80.83048, 11584, 10568, 11560, 10168, 11552, 10632; 80.83048, 11584, 10336, 11560, 10056, 11552, 10712; 80.83048, 11584, 10648, 11560, 10112, 11552, 10712; 80.83048, 11584, 10800, 11560, 10112, 11552, 10176; 80.83048, 11576, 10800, 11560, 10464, 11544, 10056; 80.83048, 11576, 11000, 11560, 10200, 11544, 10520; 80.83048, 11584, 11192, 11560, 10000, 11552, 10520; 80.83048, 11584, 11192, 11560, 10000, 11552, 10696; 80.83048, 11576, 11056, 11560, 10176, 11552, 10712; 80.83048, 11584, 10272, 11560, 10384, 11552, 10712; 80.83048, 11584, 10160, 11560, 10384, 11552, 10424; 80.83048, 11584, 10160, 11560, 10136, 11552, 10136; 80.83048, 11584, 10256, 11560, 10088, 11552, 10136; 80.83048, 11584, 10872, 11560, 10088, 11552, 10320; 80.83048, 11584, 10872, 11560, 10352, 11552, 11088; 80.83048, 11576, 11112, 11560, 10168, 11552, 10712; 80.83048, 11576, 11040, 11560, 9976, 11552, 10712; 80.83048, 11576, 11040, 11560, 9976, 11544, 10000; 80.83048, 11576, 11208, 11560, 10016, 11552, 10200; 80.83048, 11584, 10184, 11560, 10160, 11552, 10424; 80.83048, 11592, 9952, 11560, 10160, 11552, 10424; 80.83048, 11592, 9952, 11560, 10344, 11552, 10808; 80.83048, 11584, 10688, 11560, 10296, 11552, 10808; 80.83048, 11576, 10952, 11560, 10104, 11552, 10808; 80.83048, 11576, 10952, 11560, 10104, 11544, 10336; 80.83048, 11576, 11440, 11560, 10256, 11544, 10272; 80.83048, 11584, 10416, 11560, 10168, 11544, 10272; 80.83048, 11584, 10392, 11560, 10168, 11552, 10400; 80.83048, 11584, 10392, 11560, 10008, 11552, 10816; 80.83048, 11584, 10920, 11560, 9960, 11552, 10816; 80.83048, 11576, 10960, 11560, 9960, 11552, 10512; 80.83048, 11576, 10960, 11560, 10144, 11552, 10728; 80.83048, 11584, 10792, 11560, 10064, 11552, 9984; 80.83048, 11584, 10552, 11560, 9992, 11552, 9984; 80.83048, 11584, 10696, 11560, 9992, 11552, 10248; 80.83048, 11584, 10696, 11560, 10120, 11552, 10976; 80.83048, 11576, 11088, 11560, 10352, 11552, 10976; 80.83048, 11576, 10904, 11560, 10352, 11552, 10736; 80.83048, 11576, 10904, 11560, 10072, 11544, 10040; 80.83048, 11584, 10488, 11560, 10112, 11544, 10024; ];
dc5cae0073b992aafeefc7c1934f7bf3b63abc6f
6bd47868c9c7b3e9469b27f60a4757816a62060b
/Penyelesaian Persamaan Linear/gauss.sci
e5cf7ff2ef581db5384bc924a01980ddf549ee31
[]
no_license
fahrioghanial/Program-Metode-Numerik
555401132e47516ff38ab7d38e1056c16e45ab1a
83cfe9144c72a3adbabbe71923f32ab6209b02e8
refs/heads/master
2023-02-28T16:14:24.353765
2021-02-04T08:04:46
2021-02-04T08:04:46
335,882,015
0
0
null
null
null
null
UTF-8
Scilab
false
false
945
sci
gauss.sci
/* Mohamad Fahrio Ghanial Fatihah 140810190005 */ function gauss() clear; clc; printf('\nProgram Penyelesaian SPL dengan Metode Eliminasi Gauss\n') printf('Ubah SPL menjadi matriks [A][X]=[H]\n') printf('Masukkan SPL dalam bentuk matriks\n'); A = input('Masukkan elemen matriks A : '); H = input('Masukkan elemen matriks H : '); ML = [A(1,1) A(1,2) A(1,3) H(1,1); A(2,1) A(2,2) A(2,3) H(2,1); A(3,1) A(3,2) A(3,3) H(3,1)]; printf('Matriks Lengkap\n'); disp(ML); S = ML(2,1)/ML(1,1); R = ML(3,1)/ML(1,1); for j=1:4 ML(2,j)=ML(2,j)-S*ML(1,j); ML(3,j)=ML(3,j)-R*ML(1,j); end T = ML(3,2)/ML(2,2); for j=1:4 ML(3,j)=ML(3,j)-T*ML(2,j); end x3 = ML(3,4)/ML(3,3); x2 = (ML(2,4)-ML(2,3)*x3)/ML(2,2); x1 = (ML(1,4)-ML(1,2)*x2-ML(1,3)*x3)/ML(1,1); printf('\nMatriks Lengkap yang menjadi matriks segitiga atas\n'); disp(ML); printf('Jadi Penyelesaian SPL tersebut adalah:\n x1 = %.6f\t x2 = %.6f\t x3 = %.6f', x1, x2, x3); endfunction
8a04a71e20ff2b86ca808db70f45f0e006c8f611
449d555969bfd7befe906877abab098c6e63a0e8
/3828/CH2/EX2.3/Ex2_3.sce
b41713b01d2660e50d4ec197162e173f6fb7dd0c
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
12
null
null
null
null
UTF-8
Scilab
false
false
358
sce
Ex2_3.sce
//Chapter 2 : Diffraction clear; //Variable declaration m=1 //first minimum a=90*10**-16 //slit width y=6*10**-3 //distance from central maximum D=0.98 //Screen distance //Calculations lamda=(y*a)/D/10**-17*10**3 //Result mprintf("Wavelength of incident light lamda= %d Armstrong",lamda)
e13b986f7ccd30af411e54c8eb3497ea8cd6d62b
449d555969bfd7befe906877abab098c6e63a0e8
/3131/CH19/EX19.5/Ex19_5.sce
815c307cfc63e96ac20d0c59271070cd81a424ca
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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clear all; clc; disp("Ex 19_5") //Referring figure 19-8 disp("r_p=r(bar)+ ((k_G)^2)/r(bar)")
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//Exa 2.56 clc; clear; close; //Given data : format('v',5); Output=15;//in H.P. Output=15*735.5;//in watts Vl=400;//in volt ISCat200=40;//in Ampere(at 200 volt) Efficiency=0.88;//unitless cosfi=0.85;//power factor ISCat400=ISCat200*(400/200);//in Ampere(at 400 volt) Input=Output/Efficiency;//in watts Ifl=Input/(sqrt(3)*Vl*cosfi);//in Ampere //starting line current with star delta starter Is=ISCat400/3;//in Ampere Ratio=Is/Ifl;//ratio of starting current to full load current disp(Ratio,"Ratio of line current at starting to full load current :");
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example3_11.sce
clear; clc; // Stoichiometry // Chapter 3 // Material Balances Without Chemical Reaction // Example 3.11 // Page 68 printf("Example 3.11, Page 68 \n \n"); // solution // basis : 1000 kg/h of feed // balancing H2SO4, HNO3 and H2O in all the three product streams M = [1 0 0 1 0 0 1 0 0;0 1 0 0 1 0 0 1 0;0 0 1 0 0 1 0 0 1;1 0 0 0 0 0 0 0 0;0 1 0 0 0 0 0 0 0;0 0 1 0 0 0 0 0 0;0 0 0 1 0 0 0 0 0;0 0 0 0 1 0 0 0 0;0 0 0 0 0 1 0 0 0] v = [400;100;500;4;94;60;16;6;400] s = M\v A = s(1)+s(2)+s(3) B = s(4)+s(5)+s(6) C = s(7)+s(8)+s(9) printf("Flowrates are :\n A = "+string(A)+" kg/h \n B = "+string(B)+" kg/h\n C = "+string(C)+" kg/h")
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Ex4_11.sce
//Example 4_11 clc(); clear; //To find the acceleration of the system w1=7 //units in Kg a=9.8 //units in meters/sec^2 w2=5 //units in Kg w=w1/w2 F1=29.4 //units in Newtons F2=20 //units in Newtons f=(F1+F2) //units in Newtons T1=w1*a //units in Newtons T=(T1+(w*f))/(1+w) //units in Newtons a=((w1*a)-T)/w1 //units in meters/sec^2 printf("Acceleration a=%.2f meters/sec^2",a)
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PO2.prev.tst
a^4*m11^2 - 2*a^2*b^2*m11^2 + b^4*m11^2 + 4*a^3*b*m11*m12 - 4*a*b^3*m11*m12 + 4*a^2*b^2*m12^2 + 2*a^4*m11*m13 - 2*b^4*m11*m13 + 4*a^3*b*m12*m13 + 4*a*b^3*m12*m13 + a^4*m13^2 + 2*a^2*b^2*m13^2 + b^4*m13^2 + a^4*m21^2 - 2*a^2*b^2*m21^2 + b^4*m21^2 + 4*a^3*b*m21*m22 - 4*a*b^3*m21*m22 + 4*a^2*b^2*m22^2 + 2*a^4*m21*m23 - 2*b^4*m21*m23 + 4*a^3*b*m22*m23 + 4*a*b^3*m22*m23 + a^4*m23^2 + 2*a^2*b^2*m23^2 + b^4*m23^2 - a^4*m31^2 + 2*a^2*b^2*m31^2 - b^4*m31^2 - 4*a^3*b*m31*m32 + 4*a*b^3*m31*m32 - 4*a^2*b^2*m32^2 - 2*a^4*m31*m33 + 2*b^4*m31*m33 - 4*a^3*b*m32*m33 - 4*a*b^3*m32*m33 - a^4*m33^2 - 2*a^2*b^2*m33^2 - b^4*m33^2 getVariablePowers(a,b)=a^4 + a^3*b + a^2*b^2 + a*b^3 + b^4 groupBy(a,b)= + a^4*(m11^2 + 2*m11*m13 + m13^2 + m21^2 + 2*m21*m23 + m23^2 - m31^2 - 2*m31*m33 - m33^2) + 4*a^3*b*(m11*m12 + m12*m13 + m21*m22 + m22*m23 - m31*m32 - m32*m33) + 2*a^2*b^2*( - m11^2 + 2*m12^2 + m13^2 - m21^2 + 2*m22^2 + m23^2 + m31^2 - 2*m32^2 - m33^2) + 4*a*b^3*( - m11*m12 + m12*m13 - m21*m22 + m22*m23 + m31*m32 - m32*m33) + b^4*(m11^2 - 2*m11*m13 + m13^2 + m21^2 - 2*m21*m23 + m23^2 - m31^2 + 2*m31*m33 - m33^2)