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function connected=connected_links(scs_m,k) //given a link number returns all links connected with him through split // Copyright INRIA TYPE_OBJET=1;GRAPHIQUE=2; OBJET_ORIGINE=8;OBJET_DESTINATION=9 $ENTREES=5;$SORTIES=6;$ENTREES_EVT=7;$SORTIES_EVT=8 if scs_m(k)(TYPE_OBJET)<>'Link' then error('Object is not a link') end connected = [] liaisons_a_traiter = k //- Look for connected links while liaisons_a_traiter <> [] numero_liaison = liaisons_a_traiter(1) connected = [connected, numero_liaison] bloc_amont = scs_m(scs_m(numero_liaison)(OBJET_ORIGINE)(1)) bloc_aval = scs_m(scs_m(numero_liaison)(OBJET_DESTINATION)(1)) for bloc = list(bloc_amont, bloc_aval) if is_split(bloc) then for port = [$ENTREES, $SORTIES, $ENTREES_EVT, $SORTIES_EVT] liaisons_a_traiter = [liaisons_a_traiter; bloc(GRAPHIQUE)(port)] end end end for i = connected liaisons_a_traiter = liaisons_a_traiter(find(liaisons_a_traiter <> i)) end end
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//Example 10.7 clear; clc; K=10; VT0=(273.2*10^(-3));//273.2 K for T=0 degCelsius fo0=0; R2R3rat=(1-VT0)/VT0; RC=1/((10^4)*K); C=3.9*10^(-9); R=RC/C; R3=2.74*10^3; R2=R3*R2R3rat; R1=R-((R2*R3)/(R2+R3)); printf("Designed Celsius to Frequency Converter :"); printf("\nR=%.3f kohms",R*10^(-3)); printf("\nR1=%.f ohms",R1); printf("\nR2=%.2f kohms",R2*10^(-3)); printf("\nR3=%.2f kohms",R3*10^(-3)); printf("\nC=%.1f nF",C*10^9); printf("\nTo calibrate, place the IC in a 0 deg Celsius environment and adjust R2,"); printf("\nso that the circuit is barely oscillating, say fo=1 Hz. Then move the IC to"); printf("\na 100 deg Celsius environment and adjust R1 for f0=1 kHz.");
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style.fontSize=14; style.displayedLabel="<table> <tr><td align=center>INF<br>Neuron</td></tr></table>"; pal5 = xcosPalAddBlock(pal5,"infneuron",[],style);
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//Example 4.16: clc; clear; close; //given data : A=200;//gain without feedback Beta=0.25;//feed back ratio gc=10;//percent gain change dA=gc/100;// dAf= ((1/(1+Beta*A)))*dA;// format('v',7) disp(dAf,"small change in gain is,=")
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//Bolt with reduced shank diameter g = 1.50; // inch d = 0.5; //inch t = 0.25; //inch d_r = 0.406; //inch L = 13.5; //inch ratio = ( (g*(d^2)) / ( ((g-t)*(d_r^2))+(t*(d^2))) ) //U2/U1 disp(ratio,"The energy absorbing capacity of the bolts with reduced shank diameter") // Long bolts ratio_1 = ( (((L-t)*(d_r^2))+(t*(d^2))) / ((2*(g-t)*(d_r^2))+2*(t*(d^2))) ); //U3/2U1 disp(ratio_1,"The energy absorbing capacity of the long bolts")
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clear //Given n=20 I=1 //A r=0.08 //m u=4*3.14*10**-7 //T/A m //Calculation B=u*n*I/(2*r) //Result printf("\n Magnitude of the magnetic field is %0.3f *10*4 T", B*10**4)
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// Example 14.1 // From figure 14.7(a) // Let us assume some Values to R's and C for illustration purpose R=5; C=0.1*10^-6; s=%s; // Conductance matrix from figure 14.7(b) Y_11=s*C+1/R; Y_12=-s*C; Y_21=Y_12; Y_22=Y_11; Y=[Y_11,Y_12;Y_21,Y_22]; delta=det(Y); // Solving matrix equation // Y*[V_1;V_2]=[I_1;I_2] // On application of Cramer's Rule we get // V_1=(Y_22/delta)*I_1-(Y_12/delta)*I_2 ----equqtion(1) //V_2=-(Y_21/delta)*I_1+(Y_11/delta)*I_2 ----equation(2) // comparing above equations with z-parameter matrix equation z_11=Y_11/delta; z_22=z_11; z_12=-Y_12/delta; z_21=z_12; Z=[z_11,z_12;z_21,z_22]; disp(Z,"Z-Parameters=")
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//Example 1_4 page no:5 clc clear R=10;//Resistance in ohm V=12;//Voltage in volt I=V/R; disp(I,"current flowing through resistor(in A):")
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//Ex:3.13 clc; clear; close; n1=1.48;// core refractive index n2=1.46;// cladding refractive index a=2.5;// radius in um y=0.85;// wavelength in um dl=(n1-n2)/n1;// index difference v=(2*%pi*a*n1*(2*dl)^(0.5))/y;// the normaised frequency M=(v*v)/2;// number of modes printf("The number of modes=%f", M);
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disp("Example 4.13") disp("fck=20MPa","fy=Fe250","Ast=4926mm^2","d=520mm","bw=250mm","Df=100mm","bf=850mm","Given:") bf=850 Df=100 bw=250 d=520 Ast=4926 fy=250 fck=20 Es=2*10^5 xumaxd=0.0035/(0.0055+0.87*(fy/Es)) xumax=xumaxd*d disp("mm",xumax,"xumax=") disp("First assuming xu</Df and xu</xu,max") disp("xu=(0.87*fy*Ast)/(0.362*fck*bf)") xu=(0.87*fy*Ast)/(0.362*fck*bf) disp("mm",xu,"xu=") disp("xu >Df, Hence this value of xu is not correct") disp("As xu>Df, Cuw = 0.362*fck*fy*bw*xu") Cuw=0.362*fck*fy disp("xu N", Cuw,"Cuw=") disp("ASssuming xu>/7/3*Df = 233.33mm, yf=Df=100mm and Cuf=0.447*fck*(bf-bw)*Df") Cuf=0.447*fck*(bf-bw)*Df disp("N",Cuf,"Cuf=") disp("Further assuming xu</xu,max = 276.1 mm, fst=0.87*fy, and") Tu=0.87*fy*Ast disp("N",Tu,"Tu=") disp("Applying the force equilibrium condition Cuw+Cuf=Tu") xu=(Tu-Cuf)/Cuw disp("mm",xu,"xu=") disp("which implies xu>7/3Df =233.3mm, but not xu</xu,max=276.1mm. The section is over-reinforcedas per the Code provisions") disp("Exact Solution (considering strain compatibility)") disp("mm",xu,"Corresponding to xu=") disp("Est=0.0035*(d/xu-1)") Est=0.0035*(d/xu-1) disp(Est,"Est=") strainyield=0.87*fy/Es disp("Est is greater than strain at yield for Fe250") disp(strainyield) disp("Hence the design steel stress isindeed fst=0.87*fy and the so calculated xu above, is the correct depth of the neutral axis") disp("Accordingly,MuR= Cuw*(d-0.416*xu)+Cuf*(d-Df/2)") MuR=(Cuw*xu*(d-0.416*xu)+Cuf*(d-Df/2))/10^6 disp("kNm",MuR,"MuR=") disp("APPROXIMATE SOLUTION") disp("Limiting xu to xu,max=276.1 mm and taking moments of Cuw and Cuf about the centroid of the tension steel.(Note that, following the Code procedure, Df/d=100/520=0.192<0.2, yf=Df=100mm") xumax MuRl=((Cuw*xumax*(d-0.416*xumax))+(Cuf*(d-Df/2)))/10^6 disp("kNm",MuRl,"MuR,lim=")
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// PERCEPTRON clear; clc; dados=[]; //captura da qtd de pontos da 1° classe qtd_pontos_a = input("Digite a quantidade de pontos da classe 1: "); dados(1:qtd_pontos_a, 1:4) = 0; //captura da qtd de pontos da 2° classe qtd_pontos_b = input("Digite a quantidade de pontos da classe 2: "); dados(qtd_pontos_a+1 : qtd_pontos_a+qtd_pontos_b, 1:4) = 1; //adicionando bias dados(:, 1) = -1; clc; disp("===Tabela inicial==="); disp("===Bias | Inputs | Classes==="); disp(dados); disp('===Digite os pontos da classe 1===') for count = 1:qtd_pontos_a x_ponto = input("Digite a coordenada x do ponto " + string(count) + ": "); dados(count, 2) = x_ponto; y_ponto = input("Digite a coordenada y do ponto " + string(count) + ": "); dados(count, 3) = y_ponto; end disp('===Digite os pontos da classe 2===') for count = 1:qtd_pontos_b x_ponto = input("Digite a coordenada x do ponto " + string(count) + ": "); dados(qtd_pontos_a + count, 2) = x_ponto; y_ponto = input("Digite a coordenada y do ponto " + string(count) + ": "); dados(qtd_pontos_a + count, 3) = y_ponto; end clc; disp("===Tabela final==="); disp("===Bias | Inputs | Classes==="); disp(dados) [linhas, colunas] = size(dados); //escolha dos pesos aleatoriamente w = []; for i = 1:3 w(i) = rand(); end count = 1; //índice que percorre as linhas epocas_input = input("Digite o número de épocas desejada: "); taxa_aprendizagem = input("Digite o valor da taxa de aprendizagem desejada: "); for epocas = 1:epocas_input x = dados(count, 1:3); //bias e inputs saida_esperada = dados(count, 4); //coluna das classes // somatório net = x * w; //função de ativação if net >= 0 then net = 1; else net = 0; end erro = saida_esperada - net; for i = 1:3 w(i) = w(i) + taxa_aprendizagem * erro * x(i); end count = count + 1; if count > linhas then count = 1; end disp('---Entrada---'); disp(x); disp('---Esperado---'); disp(saida_esperada); disp('---Obtido---'); disp(net); disp('==========================') end // PLOTS x_classe_a = dados(1:qtd_pontos_a, 2); y_classe_a = dados(1:qtd_pontos_a, 3); x_classe_b = dados(qtd_pontos_a+1:qtd_pontos_a+qtd_pontos_b, 2); y_classe_b = dados(qtd_pontos_a+1:qtd_pontos_a+qtd_pontos_b, 3); //plots por classe plot(x_classe_a, y_classe_a, 'o') plot(x_classe_b, y_classe_b, 'x') // reta divisora x1 = linspace(-25, 25); x2 = -((w(2)/w(3))*x1) + ((w(1)/w(3))); x2_bias = -((w(1)/w(3))*x1) + ((-1/w(2))); plot(x1, x2, 'r-');
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//Simpson Rule clc; clear; close(); format('v',10); funcprot(0); deff('[y]=f(x)','y=exp(x)'); n = [1 2 4]; a = 0; b = 2; h = (ones(1,3)*(b-a))./(2*n); s(1) = h(1)*(f(a)+f(b)+4*f(h(1)))/3; disp(s(1),'n=1'); s(2) = h(2)*(f(a)+f(b)+2*f(2*h(2))+4*(f(h(2))+f(3*h(2))))/3; disp(s(2),'n=2'); s(3) = h(3)*(f(a)+f(b)+2*(f(2*h(3))+f(4*h(3))+f(6*h(3)))+4*(f(h(3))+f(3*h(3))+f(5*h(3))+f(7*h(3))))/3; disp(s(3),'n=4'); exact = integrate('exp(x)','x',0,2); disp(exact,'The exact value of intergation is :'); exact = ones(3)*exact; err = exact-s; disp(err,'thus corresponding errors are : ');
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//Exa3.7 clc; clear; close; // given data rho_i=0.47;// in ohm-meter sigma_i=1/rho_i; miu_e=0.39;// in m^2/V-s miu_h=0.19;// in m^2/V-s e=1.6*10^-19;// in C // since sigma_i=n_i*e*(miu_e+miu_h); n_i=sigma_i/(e*(miu_e+miu_h)); // so Density of electrons = Intrinsic Concentration,n_i disp("Density of electons is :"+string(n_i)+" /m^3"); E=10^4;// in V/m v_n=miu_e*E; disp("Drift velocity of electrons is : "+string(v_n)+" m/s"); v_h=miu_h*E; disp("Drift velocity of holes is : "+string(v_h)+" m/s");
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//Example 7.7 clc clear function [I] = simp13 (fun,a,b,n) // Integrate the function over the interval using Simpson's 1/3rd rule // simp13 (fun,a,b,n) // fun - function to be integrated // a - lower limit of integration // b - upper limit of integration // n - No. of times simpson's 1/3rd rule needs to be performed N = 2 * n + 1; // N - total no. of points h = (b-a) / (N-1); x = linspace(a,b,N); y = fun(x); sum1 = y(1) + 4 * sum(y(2:2:N-1)) + 2 * sum(y(3:2:N-2)) + y(N); I = h* sum1 / 3; // Simpson's 1/3rd Integral Value endfunction n = 8; ns13 = n/2; I = simp13(log,1,5,ns13); I = round(I*10^4)/10^4; deff('[y] = true(x)',['y = x * log(x) - x']); trueVal = true(5) - true(1); err = abs(trueVal - I) / trueVal*100; err = round(err*100)/100; disp(I,"y_simp13 = ") disp(trueVal,"Actual Integral = ") disp(err,"error_simp13 = ")
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function y=log10(x) y=log(x)/log(10)
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//calculating the speed of the motor //Chapter 2 //Example 2.20 //page 125 clear; clc; disp("Example 2.20") Il=5; //current in amperes al no-load V=250; //voltage in volts Rf=250; //field resistance in ohms If1=V/Rf; //field current in amperes Ia1=Il-If1; //armature current Ra=0.2; //armature resistance in ohms disp("at a load current of 50A") Il2=50; //load current in amperes //armature reaction weakens by 3percent If2=0.97; //current in amperes Ia2=Il2-If2; N1=1000; E1=(V-(Ia1*Ra)); E2=(V-(Ia2*Ra)); N2=(N1*E2)/(0.97*E1); printf("N2=%frpm",N2)
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clear;lines(0); [s,p]=sort(rand(1,10)); //p is a random permutation of 1:10 A=[1,2,5;3,4,2]; [Asorted,q]=sort(A);A(q(:))-Asorted(:) v=1:10; sort(v) sort(v') sort(v,'r') //Does nothing for row vectors sort(v,'c')
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clc; D=50;//diameter of commutator N=1000;//speed of rotation of commutator in rpm Wb=1.5;//brush width V=%pi*D*N/60;//peripheral velocity of commutator Tc=(Wb*1000)/V;//time of commutation in ms printf('Time of commutation is %f ms.',Tc);
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clc; clear; disp(" ... NS "); disp(" PS x=0 x=1 "); disp(" A E,0 C,0 "); disp(" B C,0 A,0 "); disp(" C B,0 G,0 "); disp(" D G,0 A,0 "); disp(" E F,1 B,0 "); disp(" F E,0 D,0 "); disp(" G D,0 G,0 "); disp("Initial partition consists of all the states"); disp("P0=(ABCDEFG)"); disp("Since E only has 1 equivalent different from others,it can be partitioned from others"); disp("P1=(ABCDFG)E"); disp("now check for 2-equivalent i.e. 1-equivalent and their Ii succesors for all possible Ii are also 1 equivalent"); disp("A,F dont satisfy the 2-equivalent so they can be partitioned from others"); disp("P2=(AF)(BCDG)E"); disp("In the similar manner P3 can be obtained by splitting BD and CG since they dont have the same 3 equivalent"); disp("P3=(AF)(BD)(CG)E"); disp("In the same way P4 can be obtained by splitting A and F"); disp("P4=(A)(F)(BD)(CG)E"); disp("P4 cant be splitted more so P5 will be the same and the partition stops"); disp("P5=(A)(F)(BD)(CG)(E)"); disp("so the reduced machine is"); disp(" ... NS "); disp(" .. PS x=0 x=1 "); disp(" A----a e,0 c,0 "); disp(" F----f e,0 b,0 "); disp(" .(BD)--b c,0 a,0 "); disp(" (CG)--c b,0 c,0 "); disp(" E----e f,1 b,0 ");
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//To Determine the average KW input to the furnace //Page 288 clc; clear; M=10*(10^3); //Mass of Steel Melted t=2*3600; //Time Taken to Melt the steel eff=50/100; //Overall Efficiency I=9000; //Current Input R=0.003; //Resistance X=0.005; //Reactance SH=0.12; //Specific Heat LHF=8.89*(10^3); //Latent Heat of Fusion Tm=1371; //Melting Point Ti=20; //Room Temperature Hm=M*LHF; //Heat Required for melting Hr=M*SH*(Tm-Ti)*1000; //Heat Required to raise the temperature Ht=Hm+Hr; //Total Amount of heat required E=Ht*4.2/(3600); //Energy in Whr P=E*3600/t; //Power Pa=P/eff; //Actual Power Input to the Furnace Vt=Pa/(3*I); //V Cos theta //The Above voltage is the sum of arc drop and drop in resistance load Va=Vt-(I*R); //Arc Drop Vx=I*X; //Reactance Drop Vs=sqrt((Vt^2)+(Vx^2)); //Supply Voltage S=3*Vs*I/1000; //KVA input printf('The Average kW input to the furnance is %g kW\n',Pa/1000) printf(' The Arc Voltage is %g V\n',Va) printf(' The kVA input is %g kVA\n',S) //Accurate Answers, No rounding off.
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// ELECTRICAL MACHINES // R.K.Srivastava // First Impression 2011 // CENGAGE LEARNING INDIA PVT. LTD // CHAPTER : 4 : DIRECT CURRENT MACHINES // EXAMPLE : 4.13 clear ; clc ; close ; // Clear the work space and console // GIVEN DATA N1 = 1200; // Rotation speed of the Separately excited Generator in RPM at case (1) Ia1 = 100; // Current supplied by the Generator in Amphere V1 = 220; // Opearting Volatge of the Generator in Volts Ra = 0.08; // Armature Resistance in Ohms N2 = 1000; // Rotation speed of the Separately excited Generator in RPM at case (2) Vb = 2.0; // Total Brush drop in Volts // CALCULATIONS RL = V1/Ia1; // Load resistance in Ohms E1 = V1 + Vb + (Ra * Ia1); // Back EMF at case (1) in Volts E2 = (N2/N1)*E1; // Back EMF at case (2) in Volts (Excitation is Constant) Ia2 = (E2 - Vb)/(RL + Ra); // New load current in Amphere for case (2) // DISPLAY RESULTS disp("EXAMPLE : 4.13 : SOLUTION :-") ; printf("\n (a) New load current at %.f RPM , Ia2 = %.2f A \n",N2,Ia2);
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//para lambda newton-------------------------------------- function z = f(y) z = (y-2)^(4)-(y-2*y)^2; endfunction function t =f1(y) h=0.01; t = (f(y-h) - f(y))/h; endfunction function p =f2(y) h=0.01; p = (2*f(y-h) - f(y))/h; endfunction //------------------------------------------------------ //gradiente--------------------------------------------- function y = GradF(x1,x2) t1 = 4*(x1-2)^(3) - 2*(x1 - 2*x2); t2 = -2*(x1-2*x2); y = [-t1,-t2]; endfunction //------------------------------------------------------ //Lambda------------------------------------------------ function z = Lamb(x0,y,dk) x = x0+y*dk; contador = 0; while (contator ~= 10) b = b - (f1(x)/f2(x)); contador = contador +1; end endfunction //------------------------------------------------------- function q = desc(x1,x2,x0,y,dk,y1,y2) m = [x1,x2]; contador = 0; while (contador =~3) pont = m + lamb(x0,y,dk)*Gradf(y1,y2); m = pont; contador = contador+1; end q = pont; endfunction
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clc clear //INPUT DATA w=1.55*10^-6//wavelength of light emission in m h=6.625*10^-34// Planck's constant in m^2 Kg/sec c=3*10^8//velocity of light in m/s e=1.6*10^-19//charge of electron in coulombs //CALCULATION Eg=(h*c)/(w*e)//band gap in eV //OUTPUT printf('The band gap for lnp laser diode is %3.4f eV',Eg)
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// 08.09.21 // 13.11.01 ( __ added to varibles ) function [Zval__,Xval__,Yval__]=Evlptablepers(MS__) Nargs__=Mixlength(MS__); Eps__=10^(-3); Tmp__=Mixop(1,MS__); FdL__=Fullformfunc(Tmp__); Mdv__=50; Ndv__=50; if Nargs__>=2 Tmp__=Mixop(2,MS__); if Mixtype(Tmp__)~=1 Tmp__=Mixop(1,Tmp__); end; if length(Tmp__)>1 Mdv__=Tmp__(1,1); Ndv__=Tmp__(1,2); else Mdv__=Tmp__ if Nargs__==2 Ndv__=Mdv__ else Tmp__1=Mixop(3,MS__); if type(Tmp__1)==1 & length(Tmp__1)==1 Ndv__=Tmp__1; else Ndv__=Mdv__; end end end end; Tmp__=Mixop(5,FdL__); K__=mtlb_findstr(Tmp__,'='); Uname__=part(Tmp__,1:K__-1); Urange__=evstr(part(Tmp__,K__+1:length(Tmp__))); Tmp__=Mixop(6,FdL__); K__=mtlb_findstr(Tmp__,'='); Vname__=part(Tmp__,1:K__-1); Vrange__=evstr(part(Tmp__,K__+1:length(Tmp__))); U1__=Urange__(1); U2__=Urange__(2); V1__=Vrange__(1); V2__=Vrange__(2); Du__=(U2__-U1__)/(Mdv__-1); Dv__=(V2__-V1__)/(Ndv__-1); Xyzstr__=[Mixop(2,FdL__),Mixop(3,FdL__),Mixop(4,FdL__)]; I__=1; Zval__=[]; for v__=V1__:Dv__:V2__ v__1=v__-Eps__/2; v__2=v__+Eps__/2; ZuL__=[]; for u__=U1__:Du__:U2__; u__1=u__-Eps__/2; u__2=u__+Eps__/2; Tmp__v=strsubst(Xyzstr__,Vname__,'v__'); Tmp__=strsubst(Tmp__v,Uname__,'u__1'); P1__=evstr(Tmp__); Tmp__=strsubst(Tmp__v,Uname__,'u__2'); P2__=evstr(Tmp__); Tmp__1=Perspt(P1__); Tmp__2=Perspt(P2__); Dxu__=(Tmp__2(1)-Tmp__1(1))/Eps__; Dyu__=(Tmp__2(2)-Tmp__1(2))/Eps__; u__1=u__-Eps__/2; u__2=u__+Eps__/2; Tmp__u=strsubst(Xyzstr__,Uname__,'u__'); Tmp__=strsubst(Tmp__u,Vname__,'v__1'); P1__=evstr(Tmp__); Tmp__=strsubst(Tmp__u,Vname__,'v__2'); P2__=evstr(Tmp__); Tmp__1=Perspt(P1__); Tmp__2=Perspt(P2__); Dxv__=(Tmp__2(1)-Tmp__1(1))/Eps__; Dyv__=(Tmp__2(2)-Tmp__1(2))/Eps__; Tmp__=Dxu__*Dyv__-Dxv__*Dyu__; ZuL__=[ZuL__,Tmp__]; end; Zval__=[Zval__;ZuL__]; end; Yval__=V1__:Dv__:V2__; Xval__=U1__:Du__:U2__; endfunction;
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//Exa:1.58 clc; clear; close; T_1=240;//in N_m T_2=140;//in N-m T_3=300;//in N-m T_4=200;//in N-m t_1=20;//in minutes t_2=10;//in minutes t_3=10;//in minutes t_4=20;//in minutes T=sqrt(((t_1*T_1^2)+(t_2*T_2^2)+(t_3*T_3^2)+(t_4*T_4^2))/(t_1+t_2+t_3+t_4)); N=720;//in rpm P=T*2*%pi*N/60; disp(P,'Power rating of Motor(in KWs)=');
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clc; //page no 349 //problem no 10.13.1 del_phi_d=12;f_min=100;del_f_max_allow=15000; del_phi_rad=(12*%pi)/180; del_f_max=del_phi_rad*f_min; //Determination of freq deviation N=del_f_max_allow/del_f_max; l=del_f_max*729;//using six tripler f=0.1*729; //Determination of signal oscillator signal fo=152-f; disp('MHz',fo,'fo is best obtained by using two tripler');
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clk_sr = [0 1 0 0 0 0 0 0 0 1 0 0 0 0 0]; data_sr = [1 1 0 0 0 0 0 0 0 0 0 0 0 0 0]; wta_in=[ 2.1 2.1 2.1 1.5 1.5 1.5 1.5 2.1 2.1 2.1 2.1 1.5 1.5 1.5 1.5; 1.5 1.5 1.5 2.1 2.1 2.1 2.1 1.5 1.5 1.5 1.5 2.1 2.1 2.1 2.1;];
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//Chapter-1, Example 1.6, Page 1.18 //============================================================================= clc clear //INPUT DATA P=4;//Number of poles Z=400;//Number of conductors q=0.03;//Flux per pole in Wb Eg=250;//Generated emf in V A1=4;//Number of parallel paths in lap wound A2=2;//Number of parallel paths in wave wound //CALCULATIONS N1=(60*Eg*A1)/(q*Z*P);//Speed reqired in lap wound in rpm N2=(60*Eg*A2)/(q*Z*P);//Speed reqired in wave wound in rpm //OUTPUT mprintf('Speed reqired in lap wound is %3.0f rpm \nSpeed reqired in wave wound is %3.0f rpm',N1,N2) //=================================END OF PROGRAM==============================
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//** INRIA / SCILAB / Roberto Bucher / Simone Mannori / Paolo Gai //** 16 Jan 2008 //** // Modified by Roberto Bucher roberto.bucher@supsi.ch from the original // CodeGeneration_.sci // // Input editor function of Scicos code generator // // //** 10 Set 2007 : cleaner startup code by Simone Mannori function FlexCodeGen_() //** ------------- Preliminary I/O section ___________________________________________________________________________ k = [] ; //** index of the CodeGen source superbloc candidate xc = %pt(1); //** last valid click position yc = %pt(2); %pt = [] ; Cmenu = [] ; k = getobj(scs_m,[xc;yc]) ; //** look for a block //** check if we have clicked near an object if k==[] then return //** check if we have clicked near a block elseif typeof(scs_m.objs(k))<>"Block" then return end //** If the clicked/selected block is really a superblock //** <k> if scs_m.objs(k).model.sim(1)=="super" then XX = scs_m.objs(k); //** isolate the super block to use //----------------------------------------------------> THE REAL CODE GEN IS HERE -------------------------------- //** the real code generator is here [ok, XX, alreadyran, flgcdgen, szclkINTemp, freof] = do_compile_superblock42(XX, scs_m, k, alreadyran); //**quick fix for sblock that contains scope gh_curwin = scf(curwin) else //** the clicked/selected block is NOT a superblock message("Generation Code only work for a Super Block ! ") end endfunction
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//Chapter-5, Example 5.35, Page 198 //============================================================================= clc clear //INPUT DATA Q=250;//quality factor fr=1.5*10^6;//resonant freq in hertz //CALCULATIONS Bw=(fr)/(Q);//bandwidth in Hz hf1=fr+Bw;//half power freq 1 hf2=fr-Bw;//half power freq 2 mprintf("Thus bandwidth is %d hz\n",Bw); mprintf("Thus value of half-power frequencies are %g hz and %g hz",hf1,hf2); //=================================END OF PROGRAM======================================================================================================
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clc; //page no 193 //prob no. 5.6 //Refer fig. 5.13 //Filter method SSB generator fc=5*10^6;//filter centre freq. BW=3*10^3;//Filter bandwidth foc=4.9985*10^6;//carrier oscillator freq. disp('a)The USB will be passed');//Since carrier freq is at low end of passband disp('b)The carrier freq should be moved to the high end of filter at 5.0015MHz');//To generate the LSB
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clc // Given That a = 0.45 // distance between slit and bi prism in meter b = 0.45 // distance between screen and bi prism in meter alpha = %pi / 180 // angle of bi prism in radian Mu = 1.5 // refractive index of bi prism fringe_width = 1.56e-4 // fringe width in meter // Sample Problem 16 on page no. 1.45 printf("\n # PROBLEM 16 # \n") D = a + b // calculation for distance between screen and slit lambda = (fringe_width * 2 * a * (Mu - 1) * alpha) / D // calculation for wavelength printf("\n Standard formula used \n lambda = (2a*(mu-1)*alpha*beta)/D. \n") printf("\n Wavelength of light = %f A.", lambda*1e10)
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//Ex 3.5 clc;clear;close; format('v',5); fo=2;//kHz Ap=10;//Band pass gain C=0.1;//micro F(have to choose C, 0.01<C<1) R2=1/(2*%pi*fo*10^3*C*10^-6);//ohm R1=R2/Ap;//ohm disp("Design values are :"); disp(C,"Capacitance(micro F)"); disp(R1,"Resistance R1(ohm)"); disp(R2/1000,"Resistance R2(kohm)"); //Answer in the book is wrong.
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// Scilab code Ex2.10: Pg.86 (2008) clc; clear; // For simplicity let c = 1, i.e c = 1; // Velocity of light, m/s E = 2.40; // Total energy of electron, MeV E_r = 0.511; // Rest energy of electron, MeV // Since E^2 = (p*c)^2 + (m*c^2)^2, solving for p, we get p_e = sqrt(E^2 - (E_r^2)); // Momentum of electron in laboratory frame, MeV/c // Since 1 Mev/c = 5.34e-22 kg-m/s, so we get p = p_e*5.34e-22; // Momentum of electron in laboratory frame, kg-m/s u = p_e*c/E; // Speed of electron in labortary frame, m/s printf("\nThe momentum of electron in laboratory frame = %4.2e kg-m/s", p); printf("\nThe speed of electron in laboratory frame = %5.3fc unit", u); // Result // The momentum of electron in laboratory frame = 1.25e-021 kg-m/s // The speed of electron in laboratory frame = 0.977c unit
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//example-2.11 //page no-59 //given //dipole moment og HF is DM=6.375*10^(-30) //Cm //intermolecular distance r=0.9178*10^(-10) //m //charge on an electron e=1.67*10^(-19) //C //since the HF posses ionic characters //so //Hf in fully ionic state has dipole moment as DM2=r*e //Cm //percentage ionic characters percentage=DM/DM2*100 //% printf ("the percentage ionic character is %f approx.",percentage)
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//CHAPTER 7- SINGLE PHASE TRANSFORMER //Example 38 disp("CHAPTER 7"); disp("EXAMPLE 38"); //VARIABLE INITIALIZATION v1=220; //primary voltage in Volts v2=115; //secondary voltage in Volts f1=25; f2=50; //loads V=440 We1=100; //in Watts at 220 V, eddy losses Pc1=2*We1; //Total iron losses which equals We+Wh due to eddy and hysteresis Wh1=Pc1-We1; // //SOLUTION //since we know that We=kh.f.B^1.6 and Wh=Ke.Kf^2.f^2.B^2 //since all being constant exept frequency, we may take We2/We1=f2^2/f1^2 //and Wh2/Wh1=f2/f1 //find values for We2 and Wh2, whence Pc2=We2+Wh2 We2=f2^2*We1/f1^2; Wh2=f2*Wh1/f1; Pc2=We2+Wh2; disp(sprintf("The total no load losses at 400 V is %f W",Pc2)); disp(" "); // //END
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function [y] = pgm14(x) // y = 5; y = x^2.5 - 23*x^1.5 - 50 * x + 1150; endfunction
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//Converting current sources to voltage sources // O=[i1;i2;vx] A=[10,-3,4;-3,7,0;3,-3,-1] O=inv(A)*[16;-6;0] disp(O)
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s = poly(0,"s") //part a for a = -1:0.01:1 G = (s+5+a)/(s^2 + 11*s + 30) sys = syslin("c",G) t = 0:0.01:5 y = csim("step",t,sys) plot2d(t,y) end //when a=0 s = poly(0,"s") G1 = (s+5)/(s^2 + 11*s + 30) H1 = simp(G1) sys1 = syslin("c",H1) t = 0:0.01:5 y1 = csim("step",t,sys1) plot2d(t,y1) //part b s=poly(0,"s") G2 = syslin("c",(1/(s^2 - s -6))) t=0:0.01:10 plot2d(t,csim("step",t,G2)) //new transfer function s=poly(0,"s") G3 = syslin("c",1/(s+2)) t=0:0.01:10 plot2d(t,csim("step",t,G3)) //when we shift the zero s = poly(0,"s") for a = -3:0.1:4 G4 = syslin("c",(s-3-a)/(s^2 - s -6 )) t = 0:0.01:5 plot2d(t,csim("step",t,G4)) end
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//Example 3.3 clc; Rm=500; //Internal resistance Im=10*10^-3; //Full Scale deflection current //Case I: For Range 0-1 A I1=1; //Total current Rsh1=Im*Rm/(I1-Im); //Shunt resistance printf('\nValue of Shunt resistance for range 0-1 A = %.2f ohm\n',Rsh1) //Case II: For Range 0-5 A I2=5; //Total current Rsh2=Im*Rm/(I2-Im); //Shunt resistance printf('\nValue of Shunt resistance for range 0-5 A = %.3f ohm\n',Rsh2) //Case III: For Range 0-10 A I3=10; //Total current Rsh3=Im*Rm/(I3-Im); //Shunt resistance printf('\nValue of Shunt resistance for range 0-10 A = %.3f ohm\n',Rsh3)
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data = read("D:\AAAULTIMATELABA3\data\kf\log3.txt",-1,3); //чтение эксперимента function e = G(a,z), //функция для расчета амплитуды напряжения и частоты синусоиды МНК e = z(2) - (a(1) * sin(a(2)* z(3))); endfunction a0 = [1; 1]; amin = [1; 1]; amax = [10; 10] //[aa, error1] = datafit(G, data','b', amin, amax, a0) // расчет амплитуды напряжения и частоты синусоиды aa=[8.0538396/4 ; 1] //проверка аппроксимации построением графика disp(aa) t(:,1) = 0:0.01:20 t(:,2) = aa(1) * sin(aa(2) * t(:,1)) plot(data(:,3), data(:,2)) plot(t(:,1), t(:,2), "r-.")
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//Test - zaokraglanie wartosci do elemntu z wektora dopuszczalnych wartosci //kryterium - zaokraglenie bedzie nastepowalo do tego elementu, dla ktorego roznica miedzy obliczonym x a elementem jest najmniejsza clear x=144; dop_x=[1,2,3,4,5,6,7,8,9,11,15,22,34,45,57,71,92,113,150,220]; dim_dop_x=size(dop_x); dim_dop_x=dim_dop_x(1,2); for i=1:dim_dop_x delta(i)=abs(x-dop_x(i)); end [xmin imin]=min(delta); x=dop_x(imin);
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clc clear exec fn2.sci [y1,y2,y3]=fn2(7,9) disp(y1) disp(y2) disp(y3)
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clear; clc; Ho=10,n=200*%e^(%i*%pi/6),P=atan(3^.5),b=.5,e=10^-9 /(36*%pi); Eo=n*Ho; disp('a=w*sqrt(u*e/2*(1+(c/(w*e)^2)^.5)-1)'); disp('b=w*sqrt(u*e/2*(1+(c/(w*e)^2)^.5)+1)'); a=b*((sqrt(((1+(tan(P))^2)^.5)-1))/(sqrt(((1+(tan(P))^2)^.5)+1))); disp(a,'Value of alpha='); disp(1/a,'Skin depth = ')
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// example:-3.2,page no.-87. // program to find out load impedence. clc clear // function for smith chart for finding load impedence when reflection coefficient is given. function[]=smith_chart(tao) theta=0:0.1:2*%pi; for r=0:0.1:10 x=(1/(1+r))*cos(theta)+(r/(1+r)); y=(1/(1+r))*sin(theta); plot2d(x,y,style=2,rect=[-2,-2,2,2]) end for X=-2:0.1:2 if X==0 X=0.01; end x=1+(1/X)*cos(theta); y=(1/X)*sin(theta)+(1/X); plot2d(x,y,style=3,rect=[-2,-2,2,2]) xgrid(2) xtitle("smith chart","Tao_Real","Tao_Imaginary") end x=abs(tao)*cos(theta); y=abs(tao)*sin(theta); plot2d(x,y,style=5,rect=[-2,-2,2,2]) theta=-%pi/2:0.1:%pi/2; x=abs(tao)*cos(theta); [r angle]=polar(tao); tao=[r angle] y=x*tan(tao(1,2)); plot2d(x,y,style=5,rect=[-2,-2,2,2]) endfunction Zo=100; // characteristic impedence. tao=0.560+0.215*%i; // reflection coefficient. z=(1+tao)/(1-tao); // normalized impedence(normalized w.r.t Zo) Zl=z*Zo; // result disp(Zl,'load impedence = ') // by smith chart. smith_chart(tao) // when analyse with the help of smith chart.see the angle from x=0 axis i.e Tao_real axis.if it is above this axis take angle anticlockwise and if it is below this axis.take angle clockwise from Tao_real axis below.
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-- BD8004B.TST -- Grant of Unlimited Rights -- -- Under contracts F33600-87-D-0337, F33600-84-D-0280, MDA903-79-C-0687, -- F08630-91-C-0015, and DCA100-97-D-0025, the U.S. Government obtained -- unlimited rights in the software and documentation contained herein. -- Unlimited rights are defined in DFAR 252.227-7013(a)(19). By making -- this public release, the Government intends to confer upon all -- recipients unlimited rights equal to those held by the Government. -- These rights include rights to use, duplicate, release or disclose the -- released technical data and computer software in whole or in part, in -- any manner and for any purpose whatsoever, and to have or permit others -- to do so. -- -- DISCLAIMER -- -- ALL MATERIALS OR INFORMATION HEREIN RELEASED, MADE AVAILABLE OR -- DISCLOSED ARE AS IS. THE GOVERNMENT MAKES NO EXPRESS OR IMPLIED -- WARRANTY AS TO ANY MATTER WHATSOEVER, INCLUDING THE CONDITIONS OF THE -- SOFTWARE, DOCUMENTATION OR OTHER INFORMATION RELEASED, MADE AVAILABLE -- OR DISCLOSED, OR THE OWNERSHIP, MERCHANTABILITY, OR FITNESS FOR A -- PARTICULAR PURPOSE OF SAID MATERIAL. --* -- OBJECTIVE: -- IF A PROCEDURE CONTAINS MACHINE CODE STATEMENTS, THEN NO -- EXCEPTION HANDLER IS ALLOWED. -- APPLICABILITY CRITERIA: -- THIS TEST IS APPLICABLE ONLY TO IMPLEMENTATIONS THAT SUPPORT THE -- MACHINE CODE STATEMENTS. IF SUCH STATEMENTS ARE NOT SUPPORTED, -- THE "WITH" CLAUSE MUST BE REJECTED. -- MACRO SUBSTITUTION: -- THE MACRO MACHINE_CODE_STATEMENT IS A VALID MACHINE CODE -- STATEMENT THAT IS DEFINED IN THE PACKAGE MACHINE_CODE. IF THE -- IMPLEMENTATION DOES NOT SUPPORT MACHINE CODE THEN USE THE -- ADA NULL STATEMENT (I.E. NULL; ). -- HISTORY: -- LDC 06/15/88 CREATED ORIGINAL TEST. WITH MACHINE_CODE; -- N/A => ERROR. USE MACHINE_CODE; PROCEDURE BD8004B IS BEGIN $MACHINE_CODE_STATEMENT EXCEPTION -- ERROR: -- EXCEPTION NOT -- ALLOWED WITH -- MACHINE CODE. WHEN OTHERS => NULL; END BD8004B;
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clc Nd=10**16 //cm^-3 Ne=2.8*10**19 //cm^-3 T=300 //K //(nd/(n0+nd))=z=1/(1+(Ne/2*Nd)*exp(-(Ec-Ed)/kT)) //y=Ec-Ed y=0.045 k=8.617*10^-5 //eV/K z=1/(1+(Ne/(2*Nd))*exp(-y/(k*T))) disp(z,"the donor states is=")
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// Additional solved examples , Example 22 , pg 341 ni=1.5*10^10 //intrinsic concentration (in cm^-3) Nd=5*10^15 //donor concentration (in atoms/cm^3) T=300 //temperature (in K) e=1.6*10^-19 //charge of electron (in C) k=1.38*10^-23 //Boltzmann constant (in J/K) n0=Nd //Assuming n0=Nd ( since Nd &gt;&gt; ni) p0=ni^2/n0 //hole concentration E=k*T*log(n0/ni) // E=(Ef-Ei) location of Ef relative to Ei printf("Hole concentration (in cm^-3)") disp(p0) printf("Location of Ef relative to Ei (in eV)") disp(E/e) x = linspace(-5.5,5.5,51); y = ones(length(x),1); scf(2); clf(2); plot(x,y+0.1); plot(x,y,'ro-'); plot(x,y-0.329,'--'); plot(x,y*0,'bs:'); xlabel(["x axis";"(independent variable)"]); ylabel("Energy level (eV)"); title("Band diagram"); set(gca(),"data_bounds",matrix([-6,6,-0.1,1.1],2,-1));
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//Exa 9.8 clc; clear; close; // Given data h_sen = 417.4;// in kJ/kg h_totaldry = 2675.4;// in kJ/kg L = 2258;// in kJ/kg v = 5;// in m^3 v_v = 4.95;// in m^3 x = v_v/v; Q = h_totaldry -(h_sen +x*L);// in kJ/kg disp(Q,"Heat transfered per kg in kJ/kg is : ");
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function f=%p_d_r(n1,f2) // n1./f2 //! // Copyright INRIA f=rlist(n1.*f2('den'),ones(n1).*f2('num'),f2('dt'))
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//Ex:8.24 clc; clear; close; c=3*10^8;// speed of light in m/s h=6.64*10^-34;// plank constant Eg=1.43;// gap energy in eV y=(1.24*10^-6)/Eg;// wavelength in m dy=0.1*10^-9;// in m df=(dy*c)/y^2;// width in Hz printf("The wavelength =%f um", y*10^6); printf("\n The width =%d GHz", df/10^9);
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clear // // // //Variable declaration D=150 //slit screen distance(cm) d=0.03 //separation(cm) beta1=0.3 //fringe separation(cm) //Calculation lamda=d*beta1*10**8/D //wavelength of light(angstrom) //Result printf("\n wavelength of light is %0.0f angstrom",lamda)
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clc; clear; format('e',11) I=1; d=1*10^-3; A=(3.14*d^2/4); J=I/A; disp(J,"current density J(in A/m^2)=");
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// 4.15 clc; Fd=7.5*165*10^3/100; mf=5; Bandwidth=Fd/mf; printf("Bandwidth of intelligence =%.1f Hz ",Bandwidth) Tr=0.35/Bandwidth*10^6; printf("\nRise time=%.1f us ",Tr)
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//----trzcionka 12 //----algorytm wstecznej propagacji bledu clc; clear; adresy=["A.png","B.png","C.png","D.png","E.png","F.png","G.png","H.png","I.png","J.png",... "K.png","L.png","M.png","N.png","O.png","P.png","R.png","S.png","T.png","U.png","W.png",... "Y.png","Z.png","am.png","bm.png","cm.png","dm.png","em.png","fm.png","gm.png","hm.png",... "im.png","jm.png","km.png","lm.png","mm.png","nm.png","om.png","pm.png","rm.png","sm.png",... "tm.png","um.png","wm.png","ym.png","zm.png"] w=9; p=20; wy=46; znaki=zeros(15,15,wy); for m=1:wy znak=imread(adresy(m))/255; a2=zeros(15,15); for i=1:15//kolumny for j=1:15//rzędy a2(j,i)=znak(j,i); znaki(j,i,m)=a2(j,i) end end end mat=zeros(9,wy); mat2=zeros(wy,wy); for n=1:wy mat2(n,n)=1; end for j=1:wy i=1; for m=1:5:15 for n=1:5:15 for x=0:4 for y=0:4 if znaki(m+x,n+y,j)==0 mat(i,j)=mat(i,j)+1 end end end mat(i,j)=mat(i,j)/25 i=i+1; end end end //DO TEJ PORY BYŁA OBRÓBKA TRENERÓW //----wykreslenie obszaru klasyfikacji Licz=0; IleKrokow=80000; //----utworzenie odpowiednich tablic na dane W1= zeros(w,w+1);//wagi W2=zeros(p,w+1);//wagi W3=zeros(wy,p+1);//wagi W1b=W1 W2b=W2 W3b=W3 W1c=W1b W2c=W2b W3c=W3b //----losowa inicjalizacja wag poczatkowych for n=1:w for m=1:w+1 if(p>=n & w+1>=m ) W2(i)=rand()-0.5; end if(wy>=n & p+1>=m) W3(n,m)=rand()-0.5; end W1(n,m)=rand()-0.5; end end ro=0.3; iteracja=0; ER=zeros(IleKrokow); while(iteracja<IleKrokow) if iteracja>3 if ER(iteracja)>ER(iteracja-1) if ro+0.05<1 ro=ro+0.05 elseif ro-0.05>0 ro=ro-0.05 end end end S1=zeros(1,w);//sumy S2=zeros(1,p);//sumy S3=zeros(1,wy);//sumy U1=zeros(1,w);//wartości F aktywacyjnej U2=zeros(1,p); U3=zeros(1,wy); F1=zeros(1,w); d1=zeros(1,w);//współczynnik zmiany wagi F2=zeros(1,p); d2=zeros(1,p);//współczynnik zmiany wagi F3=zeros(1,wy); d3=zeros(1,wy);//współczynnik zmiany wagi iteracja=iteracja+1; //----losowe wybieranie wektora trenujacego i=round(rand()*(wy-1))+1;//numer od 1 do do wy bo musi być ilość liter //----faza propagacji w przod -warstwa posrednia for m=1:w for n=1:w+1 if(n>1) S1(m)=S1(m)+W1(m,n)*mat(n-1,i); else S1(m)=S1(m)+W1(m,n)*1;//bo stała 1 w każdym neuronie end end U1(m)=1/(1+exp(-S1(m))); end //WARSTWA2 for m=1:p for n=1:w+1 if(n>1) S2(m)=S2(m)+W2(m,n)*U1(n-1); else S2(m)=S2(m)+W2(m,n)*1;//bo stała 1 w każdym neuronie end end U2(m)=1/(1+exp(-S2(m))); end //WARSTWA3 for m=1:wy for n=1:p+1 if(n>1) S3(m)=S3(m)+W3(m,n)*U2(n-1); else S3(m)=S3(m)+W3(m,n)*1;//bo stała 1 w każdym neuronie end end U3(m)=1/(1+exp(-S3(m))); end //----faza propagacji w przod -warstwa wyjsciowa //----faza propagacji wstecz -warstwa wyjsciowa for m=1:wy F3(m)=U3(m)*(1-U3(m)); d3(m)=(mat2(i,m)-U3(m))*F3(m); end if(d3(i)== 0) continue; end //----faza propagacji wstecz -warstwa posrednia for m=1:p F2(m)=U2(m)*(1-U2(m)); for n=1:wy d2(m)=d2(m)+d3(n)*W3(n,m+1); end d2(m)=d2(m)*F2(m) end for m=1:w F1(m)=U1(m)*(1-U1(m)); for n=1:p d1(m)=d1(m)+d2(n)*W2(n,m+1); end d1(m)=d1(m)*F1(m) end //----uaktualnienie wag -warstwa wyjsciowa W1b=W1 W2b=W2 W3b=W3 for n=1:wy for m=1:p+1 if (m>1) W3(n,m)=W3b(n,m)+0.3*(W3b(n,m)-W3c(n,m))+(ro*d3(n)*U2(m-1)); else W3(n,m)=W3b(n,m)+0.3*(W3b(n,m)-W3c(n,m))+(ro*d3(n)*1); end end end for n=1:p for m=1:w+1 if (m>1) W2(n,m)=W2b(n,m)+0.3*(W2b(n,m)-W2c(n,m))+(ro*d2(n)*U1(m-1)); else W2(n,m)=W2b(n,m)+0.3*(W2b(n,m)-W2c(n,m))+(ro*d2(n)*1); end end end for n=1:w for m=1:w+1 if (m>1) W1(n,m)=W1b(n,m)+0.3*(W1b(n,m)-W1c(n,m))+(ro*d1(n)*mat(m-1,i)); else W1(n,m)=W1b(n,m)+0.3*(W1b(n,m)-W1c(n,m))+(ro*d1(n)*1); end end end W1c=W1b W2c=W2b W3c=W3b if(modulo(iteracja,1000)==0) disp(iteracja) ER(iteracja)=mat2(i,i)-U3(i); else if iteracja<5 ER(iteracja)=mat2(i,i)-U3(i); else ER(iteracja)=ER(iteracja-1) end end end adresy=["test1.png","test2.png","test3.png","test4.png","E.png","F.png","G.png","H.png","I.png","J.png",... "K.png","L.png","M.png","N.png","O.png","P.png","R.png","S.png","T.png","U.png","W.png",... "Y.png","Z.png","am.png","bm.png","cm.png","dm.png","em.png","fm.png","gm.png","hm.png",... "im.png","jm.png","km.png","lm.png","mm.png","nm.png","om.png","pm.png","rm.png","sm.png",... "tm.png","um.png","wm.png","ym.png","zm.png"] rozmiar=size(adresy) znaki=zeros(15,15,rozmiar(2)); for m=1:wy znak=imread(adresy(m))/255; a2=zeros(15,15); for i=1:15//kolumny for j=1:15//rzędy a2(j,i)=znak(j,i); znaki(j,i,m)=a2(j,i) end end end mat=zeros(9,rozmiar(2)); mat2=zeros(rozmiar(2),rozmiar(2)); for n=1:rozmiar(2) mat2(n,n)=1; end for j=1:rozmiar(2) i=1; for m=1:5:15 for n=1:5:15 for x=0:4 for y=0:4 if znaki(m+x,n+y,j)==0 mat(i,j)=mat(i,j)+1 end end end mat(i,j)=mat(i,j)/25 i=i+1; end end end znaki=zeros(46,47); znaki=string(znaki) for m=2:47 znaki(m-1,m)="1" end znaki(1,1)="A"; znaki(2,1)="B"; znaki(3,1)="C"; znaki(4,1)="D"; znaki(5,1)="E"; znaki(6,1)="F"; znaki(7,1)="G"; znaki(8,1)="H"; znaki(9,1)="I"; znaki(10,1)="J"; znaki(11,1)="K"; znaki(12,1)="L"; znaki(13,1)="M"; znaki(14,1)="N"; znaki(15,1)="O"; znaki(16,1)="P"; znaki(17,1)="R"; znaki(18,1)="S"; znaki(19,1)="T"; znaki(20,1)="U"; znaki(21,1)="W"; znaki(22,1)="Y"; znaki(23,1)="Z"; znaki(24,1)="a"; znaki(25,1)="b"; znaki(26,1)="c"; znaki(27,1)="d"; znaki(28,1)="e"; znaki(29,1)="f"; znaki(30,1)="g"; znaki(31,1)="h"; znaki(32,1)="i"; znaki(33,1)="j"; znaki(34,1)="k"; znaki(35,1)="l"; znaki(36,1)="m"; znaki(37,1)="n"; znaki(38,1)="o"; znaki(39,1)="p"; znaki(40,1)="r"; znaki(41,1)="s"; znaki(42,1)="t"; znaki(43,1)="u"; znaki(44,1)="w"; znaki(45,1)="y"; znaki(46,1)="z"; for q=1:rozmiar(2) i=q; S1=zeros(1,w);//sumy S2=zeros(1,p);//sumy S3=zeros(1,wy);//sumy U1=zeros(1,w);//wartości F aktywacyjnej U2=zeros(1,p); U3=zeros(1,wy); for m=1:w for n=1:w+1 if(n>1) S1(m)=S1(m)+W1(m,n)*mat(n-1,i); else S1(m)=S1(m)+W1(m,n)*1;//bo stała 1 w każdym neuronie end end U1(m)=1/(1+exp(-S1(m))); end //WARSTWA2 for m=1:p for n=1:w+1 if(n>1) S2(m)=S2(m)+W2(m,n)*U1(n-1); else S2(m)=S2(m)+W2(m,n)*1;//bo stała 1 w każdym neuronie end end U2(m)=1/(1+exp(-S2(m))); end //WARSTWA3 for m=1:wy for n=1:p+1 if(n>1) S3(m)=S3(m)+W3(m,n)*U2(n-1); else S3(m)=S3(m)+W3(m,n)*1;//bo stała 1 w każdym neuronie end end U3(m)=1/(1+exp(-S3(m))); end temp=max(U3) for n=1:length(U3) if U3(n)<temp U3(n)=0; else U3(n)=1; end end for k=1:46 if znaki(k,2:47)==string(U3) disp(znaki(k,1)); end end plot(ER) end
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// Example 6.5 : Determine 3dB frequency // High frequency response of an amplifier can be characterized by th transfer function // F_H(s)=(1-s/10^5)/(1+s/10^4)(1+s/4*10^4) w_H=1/sqrt(1/10^8+1/(16*10^8)-2/10^10); // w_H=1/sqrt(1/w_P1^2+1/w_P2^2-2/w_Z1^2-2w_Z2^2) disp(w_H,"w_H (rad/s)")
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clc,clear printf('Example 6.6\n\n') //note that a new function p2z has been defined below for direct representation of complex numbers in polar form function [FUN] = p2z(RRRR,Theeeta) FUN = RRRR.*exp(%i*%pi*Theeeta/180.); endfunction V_l=10*10^3 V_ph=V_l/sqrt(3) R_a=0.4 Z=complex(R_a,6) I_a=p2z(300,-acosd(0.8)) E=V_ph+I_a*Z phi=acos(0.8) alternator_op_ph=V_ph*abs(I_a)*cos(phi) //Power delivered to infinite bus per phase //Power deliered to the altrernator = Power delivewred to bus bar + I^2*R losses in armature alternator_power= alternator_op_ph+ abs(I_a)^2*R_a //this power developed remains constant.change pf to 1 and calculate corresponding armature current //alternator_power=V_ph*I_a1*cos(phi1)+I_a1^2*0.4 //solve the quadratic equation 0.4 I_a1^2+5773.50 I_a1- 1421640 =0 I_a1=(-1*V_ph+sqrt(V_ph^2-4*R_a*-1*alternator_power))/(2*R_a) //also as follows E1=V_ph+I_a1*Z decrease=100*(abs(E)-abs(E1))/abs(E) printf('Percentage decrease in induced e.m.f is %.1f percent',decrease)
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function y = f(x) y = 1 + x^2; endfunction function y = fp(x) y = 2*x; endfunction function [p,it] = newton_raphson(p0,tol,maxit) p = zeros(maxit,1); it = maxit; for i=1:maxit p(i) = p0 - f(p0)/fp(p0) if(abs(p(i)-p0)<tol) it = i; return; end p0 = p(i); end endfunction
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//EXAMPLE 2.16, clear; clc; //Given input sequence = [3 4 5] x=[0 3 4 5 0]; disp([3 4 5],'Input sequence = ') //determining median filter //first sequence for k=2:4 if x(k)>x(k-1) & x(k+1)>x(k-1) & x(k+1)>x(k) y(k-1)=x(k); else x(k-1)>x(k+1) & x(k)>x(k+1) & x(k)>x(k-1) y(k-1)=x(k-1); end end disp(y','The Median Filter of the given input is =');
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mode(2);errcatch(-1,"stop");driver("GIF");//Example 2.35 (a) //To draw the pole-zero plot clear; clc ; close ; z=%z H1Z=(z)/(z^2-z-1); xset('window',1); plzr(H1Z); xinit('/home/fossee/Downloads/tbc_graphs/Digital_Signal_Processing_R._Babu_52/Example2_35_a');xend();exit();
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//Ex:3.18 clc; clear; close; BLP=250*10^6;// bandwidth length product in Hz tr=0.32/BLP;// intermodel pulse width broadening md=75;// material dispersion in ps/nm.km tm=2.25;//pulse broadening due to material dispersion in ns/km tc=sqrt((tr*10^9)^2+tm^2);// combine pulse broadening in ns/km Ba=0.32/tm*10^9;// actual BLP in Hz.km Bac=Ba/10^6;// actual BLP in MHz.km printf("The intermodel pulse width broadening =%f ns/km", tr*10^9); printf("\n pulse broadening due to material dispersion =%f ns/km", tm); printf("\n The combine pulse broadening =%f ns/km", tc); printf("\n The actual BLP =%f MHz.km", Bac);
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clc; k=9*10^9; //constant in free space in N.m square/C square q1=4*10^-9; //charge in coulomb q2=5*10^-8; //charge in coulomb r=5*10^-2; //radius in metre F=(k*q1*q2)/(r*r); //calculating force in Newton disp(F,"Force in Newton = "); //displaying result
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clear all; f1 = 190; A1 = 0.5 f2 = 10; A2 = 2; fs = 200; dt = 1/fs; T = 0.5 t =0:dt:T-dt; s1 = A1*cos(2*%pi*f1*t); s2 = A2*cos(2*%pi*f2*t); figure(0) plot(t, s1, 'b'); plot(t, s2, 'r'); xlabel("Time, s", 'fontsize', 2) ylabel("Amplitude", 'fontsize', 2) title("Time domain", 'fontsize', 3) figure(1) subplot(3,1,1) f1 = (0:length(s1)-1)/length(s1)*fs plot(f1, abs(fft(s1)), 'b') xlabel("Frequency, Hz", 'fontsize', 2) ylabel("Freq amplitude", 'fontsize', 2) title("Frequency response of first signal", 'fontsize', 3) subplot(3,1,2) f2 = (0:length(s2)-1)/length(s2)*fs plot(f2, abs(fft(s2)), 'r') xlabel("Frequency, Hz", 'fontsize', 2) ylabel("Freq amplitude", 'fontsize', 2) title("Frequency response of second signal", 'fontsize', 3) subplot(3,1,3) f2 = linspace(-fs/2, fs/2, length(s2)) plot(f2, abs(fftshift(fft(s2))), 'r') f1 = (0:length(s1)-1)/length(s1)*fs plot(f2, abs(fftshift(fft(s1))), 'b') xlabel("Frequency, Hz", 'fontsize', 2) ylabel("Freq amplitude", 'fontsize', 2) title("Frequency response of final signals", 'fontsize', 3) legend(["freq = 10";"freq = 190"])
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// Example 1.3.b : relative error clc, clear // given : vm=2.65; // in volts vt=2.70; // in volts v=5;// full scale range of voltage Es=vm-vt; Er1=Es/vt; Er2=Es/v; disp("relative error as a function of true value is "+string(Er1)+" or "+string(100*Er1)+" %") disp("relative error as a function of full scale deflection is "+string(Er2)+" or "+string(100*Er2)+" %")
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clg55/Scilab-Workbench
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refs/heads/master
2023-05-31T04:06:22.931111
2022-09-13T14:41:51
2022-09-13T14:41:51
258,270,193
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sci
sci_log2.sci
function [stk,txt,top]=sci_log2() // Copyright INRIA txt=[] if lhs==1 then stk=list('log('+stk(top)(1)+')/log(2)','0',stk(top)(3),stk(top)(4),'1') else [f,e]=lhsvarsnames() k=gettempvar(0) if isname(stk(top)(1)) then v=stk(top)(1) else v=gettempvar(1) txt=v+' = '+stk(top)(1) end txt=[txt;k+' = find('+v+'<>0);' e+'('+k+') = ceil(log(abs('+v+'('+k+')))/log(2));'; f+'('+k+') = '+v+'('+k+')./(2^'+e+'('+k+'));' k+' = find('+f+'>=1);' f+'('+k+') = 0.5' e+'('+k+') = '+e+'('+k+')+1'] stk=list(list('?','-2',stk(top)(3),stk(top)(3),'?'),list('?','-2',stk(top)(3),stk(top)(3),'?')) end
731b3a037b8991c96bdd9e144487f35115a2c3b2
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/3535/CH7/EX7.6/Ex7_6.sce
286d1aa9e6e044e2f2b42a2eda62296690608ae6
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FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
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sce
Ex7_6.sce
//Chapter 7, Example 7.6, Page 206 clc clear // Energy required Z = 79 E = 700/Z printf("E = %f MeV\n",E) //Answers may vary due to round off error
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/29/CH5/EX5.9.13/exa5_9_13.sce
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FOSSEE/Scilab-TBC-Uploads
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sce
exa5_9_13.sce
//Caption:overall_transfer_function_of_two_phase_ac_motor //example 5.9.13 //page 113 syms Ka K Ktg Jeq feq N1 N2 m //where Ka=amplifier_gain; Ktg=tachometer_gain_const Jeq=moment_of_inertia; feq=coeff_of_viscous_friction; s=%s; //from torque characterstics m and K are determined Ka=20; K=0.0012; Ktg=0.2; Jeq=0.00015; feq=0.0001;m=-0.0003; a=K/(Jeq*s+(feq-m)); b=N1/N2; b=0.1; c=(Ka*a) // in series d=(c*b) // in series e=d/(1+Ktg*d); disp(e,"C(s)/R(s)=");//overall_transfer_function
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/Vertical Switching 80%.sce
4db394787e90d2e394123a23dbf3d0de7715dcce
[]
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MBHuman/Scenarios
be1a722825b3b960014b07cda2f12fa4f75c7fc8
1db6bfdec8cc42164ca9ff57dd9d3c82cfaf2137
refs/heads/master
2023-01-14T02:10:25.103083
2020-11-21T16:47:14
2020-11-21T16:47:14
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sce
Vertical Switching 80%.sce
Name=Vertical Switching 80% PlayerCharacters=VS Challenger BotCharacters=VS Target.bot IsChallenge=true Timelimit=60.0 PlayerProfile=VS Challenger AddedBots=VS Target.bot;VS Target.bot;VS Target.bot;VS Target.bot PlayerMaxLives=0 BotMaxLives=0;0;0;0 PlayerTeam=1 BotTeams=2;2;2;2 MapName=veranda_h80deg_v60deg.map MapScale=1.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=0.8 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag= WeaponHeroTag=Fully-auto DifficultyTag=2 AuthorsTag=pleasewait BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=true Description=Targets rise/fall in front of you. ---------------------------------- Note: MCA stands for "Midweek Competitive Aiming", a local event for the competitive aiming community in Japan. GameVersion=2.0.2.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=VS Target DodgeProfileNames= DodgeProfileWeights= DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=VS Target SeeThroughWalls=true NoDodging=true NoAiming=true AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=VS Challenger MaxHealth=100.0 WeaponProfileNames=VS Fully-auto;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=36.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=320.0 MaxCrouchSpeed=160.0 Acceleration=2560.0 AirAcceleration=16000.0 Friction=1.0 BrakingFrictionFactor=0.5 JumpVelocity=256.0 Gravity=1.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=0.000 Y=0.000 Z=1.000 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=72.0 MainBBRadius=12.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=72.0 ProjBBRadius=12.0 ProjBBHasHead=false ProjBBHeadRadius=10.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=512.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=VS Target MaxHealth=80.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=36.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=160.0 Acceleration=2560.0 AirAcceleration=16000.0 Friction=1.0 BrakingFrictionFactor=0.5 JumpVelocity=0.0 Gravity=0.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=0.000 Y=0.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Spheroid MainBBHeight=24.0 MainBBRadius=12.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=24.0 ProjBBRadius=12.0 ProjBBHasHead=false ProjBBHeadRadius=10.0 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=VS Vertical Movement.abilmov;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=128.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=true LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=512.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Weapon Profile] Name=VS Fully-auto Type=Hitscan ShotsPerClick=1 DamagePerShot=6.0 KnockbackFactor=0.0 TimeBetweenShots=0.05 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=1.0 ReloadTimeFromPartial=1.0 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=1.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=true ADSZoomDelay=0.0 ADSZoomSensFactor=1.0 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.001 HitSoundCooldown=0.001 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=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=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=50 ADSFOVOverride=30.0 ADSFOVScale=Vertical (1:1) ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Gunshot ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=VS Vertical Movement MaxCharges=1.0 ChargeTimer=1.85 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.0 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=0.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=false UpVelocity=320.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=true AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=-40.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=true AIReuseTimer=0.01 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=1000000.0 AIMaxTargFOV=360.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 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//Chapter-9 example 6 //============================================================================= clc; clear; //input data F = 9*10^9;//radar operating frequency in hz Vo = 3*10^8;//velocity of EM wave in m/s NNBW = 5;//Null to Null beamwidth Da = 5;//diameter of antenna in m //Calculations lamda = Vo/F;//wavelength A = (%pi*Da*Da)/4;//actural area of antenna Ac = 0.65*A;//Capture Area D = 6.4*(Da/lamda)^2;//directivity of antenna D1 = 10*log10(D)//gain in dB HPBW = 70*(lamda/Da);//half power beamwidth in deg NNBW = 2*HPBW;//null to null beamwidth //Output mprintf('HPBW of parabolic reflector is %g degrees\n NNBW of parabolic reflector is %g degrees\n Directivity is %g dB\n Capture area is %g m^2',HPBW,NNBW,D1,Ac); //=============end of the program==============================================
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状態空間表現から伝達関数を得る.sce
//状態空間表現から伝達関数を得る A=[0 1;-2 -3]; b=[0;1]; c=[1 2]; d=0; ss_sys=syslin('c',A,b,c,d); tf_sys=ss2tf(ss_sys)
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//Example 8.6.//power delivered clc; clear; close; //given data : format('v',6) Ft=35300;// in N V=48;// in kmph Po=((Ft*V*1000)/3600)*10^-3; Ft1=55180;//in N Pd=Po*sqrt(Ft1/Ft); disp("part (a)") disp(Pd,"power delivered(kW) = ") Pd1=Po*(Ft1/Ft); disp("part (b)") disp(Pd1,"power delivered(kW) = ")
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errcatch(-1,"stop");mode(2);// Display mode mode(0); // Display warning for floating point exception ieee(1); ; ; disp("Engineering Thermodynamics by Onkar Singh Chapter 9 Example 14") disp("In question no.14,various expression is derived which cannot be solved using scilab software.") exit();
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Chapter4_Example6.sce
clc clear //Input data r=8;//Compression ratio lcv=44000;//The lower heating value of the fuel in kJ/kg af=15;//The air/fuel ratio Cv=0.71;//The specific heat at constant volume in kJ/kgK p=1;//The pressure at the beginning of the compression in bar t=60;//The temperature at the beginning of the compression in degree centigrade Mo=32;//Molecular weight of oxygen Mn=28.161;//Molecular weight of nitrogen Mh=18;//Molecular weight of water n=1.3;//Polytropic index //Calculations T1=(t+273);//The temperature at the beginning of the compression in K sa=[12.5*[Mo+(3.76*Mn)]]/[(12*8)+(1*Mh)];//The stoichiometric air fuel ratio Y=af*[[(12*8)+(1*Mh)]/(Mo+(3.76*Mn))];//To balance the oxygen and nitrogen x=(12.5-Y)*2;//By oxygen balance nb=1+Y+(Y*3.76);//Number of moles before combustion na=x+7.8+9+46.624;//Number of moles after combustion Me=[(na-nb)/nb]*100;//The percentage molecular expansion in percent T2=T1*(r)^(n-1);//The temperature at point 2 in K T3=[lcv/(af+1)]*(1/Cv)+(T2);//The temperature at point 3 in K p3=r*(T3/T1)*p;//The pressure at point 3 in bar p31=p3*(na/nb);//The pressure at point 3 with molar expansion in bar //Output printf('The percentage molecular expansion is %3.0f percent \n (a) Without considering the molecular expansion \n The maximum temperature is %3.0f K \n The maximum pressure is %3.0f bar \n (b) With molecular expansion \n The maximum temperature is %3.0f K \n The maximum pressure is %3.1f bar ',Me,T3,p3,T3,p31)
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//Chapter-8, Example 8.8, Page 349 //============================================================================= clc clear //INPUT DATA D=0.2;//Outer diameter of the pipe in m Ts=100;//Surface temperature in degree C Ta=20;//Temperature of air in degree C L=3;//Length of pipe in m //CALCULATIONS Tf=(Ts+Ta)/2;//Film temperature in degree C k=0.02896;//Thermal conductivity in W/m.K v1=(18.97*10^-6);//Kinematic viscosity in m^2/s b=(1/333);//Coefficient of thermal expansion in 1/K Pr=0.696;//Prantl number Gr=((9.81*b*L^3*(Ts-Ta))/(v1^2));//Grashof number Ra=(Gr*Pr);//Rayleigh number Nu=(0.1*Ra^(1/3));//Nussults number h=(Nu*k)/L;//Heat transfer coefficient in W/m^2.K Q=(h*3.14*D*(Ts-Ta));//Rate of heat loss per meter length of pipe in W/m //OUTPUT mprintf('Rate of heat loss per meter length of pipe is %3.2f W/m',Q) //=================================END OF PROGRAM==============================
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//Example 8// Ch 3 clc; clear; close; // given data k = 1.38*10^-21; //boltzmanns constant T = 293; // temperature in K e = 1.6*10^-19; E = (1.5*k*T)/e; printf("energy of free electron %f eV",E)
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pad_out.sce
//**************************** IO PAD OUT ****************************** if(blk_name.entries(bl)=='pad_out') then fd_io= mopen (fname+'.pads','a+'); // DEDICATED PADS code for ss=1:scs_m.objs(bl).model.ipar(1) tmp_pad = strsplit(iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries," ") if tmp_pad(3) == '3' | tmp_pad(3)== '5' then tmp_pad(3) = '1'; elseif tmp_pad(3) == '2' then tmp_pad(3) = '0'; end if tmp_pad(4)=='#int[5]'|tmp_pad(4)=='#int[4]'|tmp_pad(4)=='#int[3]'|tmp_pad(4)=='#int[2]'|tmp_pad(4)=='#int[1]'|tmp_pad(4)=='#int[0]' then mputl('out:net'+ string(blk(blk_objs(bl),2)) + "_" + string(ss) + ' ' + iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries,fd_io); else mputl('out:net'+ string(blk(blk_objs(bl),2)) + "_" + string(ss) + ' ' + iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries + 'tgate[' + tmp_pad(3)+ ']',fd_io); end if scs_m.objs(blk_objs(bl)).model.rpar(ss)==56 then Counter_class=1; end // disp(iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(1+ss)).entries) // disp(scs_m.objs(blk_objs(bl)).model.rpar(1+ss)) end mclose(fd_io); end
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metodo bisección.sce
// This GUI file is generated by guibuilder version 4.2.1 ////////// f=figure('figure_position',[100,17],'figure_size',[820,700],'auto_resize','on','background',[33],'figure_name','Graphic window number %d','dockable','off','infobar_visible','off','toolbar_visible','off','menubar_visible','off','default_axes','on','visible','off'); ////////// handles.dummy = 0; handles.txt_titulo=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new Roman','FontSize',[25],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0212658,0.9412121,0.94,0.0515152],'Relief','default','SliderStep',[0.01,0.1],'String','Método de Bisección','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_titulo','Callback','') handles.frame_name=uicontrol(f,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[1,1,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.6845992,0.6833333,0.2763713,0.2357576],'Relief','default','SliderStep',[0.01,0.1],'String','UnName15','Style','frame','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','frame_name','Callback','') handles.frame_Datos=uicontrol(f,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[1,1,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0274262,0.6833333,0.6487342,0.2357576],'Relief','default','SliderStep',[0.01,0.1],'String','UnName16','Style','frame','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','frame_Datos','Callback','') handles.txt_funcion=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0437131,0.8590909,0.1360759,0.0424242],'Relief','default','SliderStep',[0.01,0.1],'String','Función:','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_funcion','Callback','') handles.txt_inferior=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0437131,0.8025252,0.1360759,0.0424242],'Relief','default','SliderStep',[0.01,0.1],'String','Límite Inferior','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_inferior','Callback','') handles.txt_superior=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0437131,0.7459596,0.1360759,0.0424242],'Relief','default','SliderStep',[0.01,0.1],'String','Límite Superior:','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_superior','Callback','') handles.txt_error=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0437131,0.6893939,0.1360759,0.0424242],'Relief','default','SliderStep',[0.01,0.1],'String','Error permitido:','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_error','Callback','') handles.input_funcion=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.1940506,0.8566667,0.2267932,0.0493939],'Relief','default','SliderStep',[0.01,0.1],'String','','Style','edit','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','input_funcion','Callback','') handles.input_inferior=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.1940506,0.8021212,0.2267932,0.0493939],'Relief','default','SliderStep',[0.01,0.1],'String','','Style','edit','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','input_inferior','Callback','') handles.input_superior=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.1940506,0.7475758,0.2267932,0.0493939],'Relief','default','SliderStep',[0.01,0.1],'String','','Style','edit','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','input_superior','Callback','') handles.input_error=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.1940506,0.6930303,0.2267932,0.0493939],'Relief','default','SliderStep',[0.01,0.1],'String','','Style','edit','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','input_error','Callback','') handles.button=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.4483122,0.7821212,0.1751055,0.0787879],'Relief','default','SliderStep',[0.01,0.1],'String','Solucionar','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','button','Callback','button_callback(handles)') handles.txt_nombre=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.7484389,0.8260606,0.17827,0.0454545],'Relief','default','SliderStep',[0.01,0.1],'String','Stephany Rivera','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_nombre','Callback','') handles.txt_codigo=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.7516034,0.7760606,0.1719409,0.0454545],'Relief','default','SliderStep',[0.01,0.1],'String','1765591-3743','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_codigo','Callback','') handles.txt_proyecto=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.7315612,0.7260606,0.2120253,0.0454545],'Relief','default','SliderStep',[0.01,0.1],'String','Proyecto Métodos Númericos','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_proyecto','Callback','') handles.frame=uicontrol(f,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','Tahoma','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[1,1,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0274262,0.0439394,0.9409283,0.6175758],'Relief','default','SliderStep',[0.01,0.1],'String','UnName14','Style','frame','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','frame','Callback','') f.visible = "on"; ////////// // Callbacks are defined as below. Please do not delete the comments as it will be used in coming version ////////// function button_callback(handles) Biseccion() endfunction ////////Método bisección function Biseccion() /* x^3+4*x^2-10 [1,2] 0.0001 */ execstr(['function y=funcion(x)'; 'y='+handles.input_funcion.string; 'endfunction']); num_iteraciones=1 a= evstr(handles.input_inferior.string); b= evstr(handles.input_superior.string); x=a:0.1:b; error_permitido=evstr(handles.input_error.string); fa=feval(a,funcion); fb=feval(b,funcion); xr=(a+b)/2; fxr=feval(xr,funcion); Error=100; tabla=[string(num_iteraciones) string(a) string(b) string(xr) string(fxr) " "]; while(Error>=error_permitido) caso1=fa*fxr; caso2=fb*fxr; if(caso1<0) b=xr; fb=fxr; valoranterior=xr; xr=(a+b)/2; valoractual=xr; end if(caso2<0) a=xr; fa=fxr; valoranterior=xr; xr=(a+b)/2; valoractual=xr; end num_iteraciones=num_iteraciones+1 fxr=feval(xr,funcion); Error=abs((valoractual-valoranterior)/valoractual); tabla=[tabla;string(num_iteraciones) string(a) string(b) string(xr) string(fxr) string(Error)]; end //resultados que se obtienen de la tabla handles.txt_Resu=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0664557,0.6,0.2732068,0.0409091],'Relief','default','SliderStep',[0.01,0.1],'String', strcat(["Valor obtenido: ",string(valoractual)]),'Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_Resu','Callback','') handles.txt_Resu1=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.3560126,0.6,0.2732068,0.0409091],'Relief','default','SliderStep',[0.01,0.1],'String',strcat(["Número iteraciones realizadas: ",string(num_iteraciones)]),'Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_Resu1','Callback','') handles.txt_Resu2=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Times new roman','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.6455696,0.6,0.2732068,0.0409091],'Relief','default','SliderStep',[0.01,0.1],'String',strcat(["Error obtenido: ",string(Error)]),'Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','txt_Resu2','Callback','') params=["n" "a" "b" "pn" "f(pn)" "Error"]; c1 = tabla(1:num_iteraciones); //Columna 1 c2 = tabla(num_iteraciones+1:num_iteraciones*2); //Columna 2 c3 = tabla(num_iteraciones*2+1:num_iteraciones*3); //Columna 3 c4 = tabla(num_iteraciones*3+1:num_iteraciones*4); //Columna 4 c5 = tabla(num_iteraciones*4+1:num_iteraciones*5); //Columna 5 c6 = tabla(num_iteraciones*5+1:num_iteraciones*6); //Columna 6 table = [params; [ c1 c2 c3 c4 c5 c6 ]] tabla_propiedades = uicontrol("style", "table",.. "string", table,.. "position", [100 130 630 250],.. "backgroundcolor", [0.9,0.9,0.9], ... "tooltipstring", "myTable"); //grafica graficas = scf(2); graficas.figure_position = [520,0] graficas.axes_size = [555 515]; graficas.figure_name = "Metodo Bisección"; xgrid(5); plot2d(x,funcion(x)); plot(valoractual,funcion(valoractual),'o'); endfunction
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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ex_1_9_a.sce
//example 1.9(a)// clc //clears the screen// clear //clears already existing variables// disp('when one of the logic input of 2-input NOR gate is 0, then when A=1, Y=0 and if A=0, Y=1') disp('Y=A''')
ae2556166538b4914b0528dd7054e6d1ca076598
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/ketpic2escifiles6/Vecnagasa2.sci
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no_license
ketpic/ketcindy-scilab-support
e1646488aa840f86c198818ea518c24a66b71f81
3df21192d25809ce980cd036a5ef9f97b53aa918
refs/heads/master
2021-05-11T11:40:49.725978
2018-01-16T14:02:21
2018-01-16T14:02:21
117,643,554
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sci
Vecnagasa2.sci
function L=Vecnagasa2(varargin) PA=varargin(1); if length(varargin)>1 PB=varargin(2); else PB=[0,0]; end Tmp=PB-PA; L=Tmp*Tmp'; endfunction
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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sce
4_10.sce
//pathname=get_absolute_file_path('4.10.sce') //filename=pathname+filesep()+'4.10-data.sci' //exec(filename) //Temperature at which heat is receieved (in K): T1=800 //Temperature maintained by the carnot engine(in K): T2=280 //Temperature at which heat is rejected(in K): T=2*T1*T2/(T1+T2) //Efficiency: n=(T1-T)/T1 //COP of refrigerator: COP=T2/(T-T2) printf("\nRESULTS\n") printf("\nEfficiency = %f",n) printf("\nC.O.P of refrigerator = %f",COP)
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/1226/CH3/EX3.1/EX3_1.sce
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
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EX3_1.sce
clc;funcprot(0);//EXAMPLE 3.1 // Initialisation of Variables t1=673;.....................//Max temp in Kelvin t3=313;;...................//Min temp in Kelvin W=130;.................//Work produced in kJ //calculations etath=(t1-t3)/t1;................//Engine thermal efficiency disp(etath*100,"Engine thermal efficiency in %:") ha=W/etath;.................//Heat added in kJ disp(ha,"Head added in kJ:") dels=(ha-W)/t3;...........//Change in entropy disp(dels,"Change in entropy in kJ/K")
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/05/PCPlusControl.tst
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no_license
eliasbagley/nand2tetris
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refs/heads/master
2020-11-29T15:24:50.945163
2020-01-20T20:39:10
2020-01-20T20:39:10
230,150,566
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PCPlusControl.tst
load PCPlusControl.hdl, output-file PCPlusControl.out, output-list time%S1.4.1 in%D1.6.1 reset%B2.1.2 j%B1.3.1 zr%B2.1.2 ng%B2.1.2 out%D1.6.1; set in 0; set reset 0; set j %B000; set zr 0; set ng 0; tick; output; tock; output; set in 1; tick; output; tock; output; set in 2; tick; output; tock; output; set in 3; set reset 1; tick; output; tock; output; set reset 0; set in 0; set zr 1; tick; output; tock; output; set in 10; set zr 1; set j %B010; tick; output; tock; output; set in 20; set zr 0; set j %B010; tick; output; tock; output;
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/compareDataOE.sce
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solothinker/compare
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2021-06-24T21:42:05.654744
2017-09-08T05:57:35
2017-09-08T05:57:35
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compareDataOE.sce
loadmatfile('data.mat') z = [data(:,1) data(:,2)]; A = 1 B = [0 0 0 2.6509 -2.0596];//[0 0 0 2.3057 -1.2170]; C = 1; D = 1; F = [1 -0.9448 0.5055];//[1 -1.1887 0.6424]; oeModel = idpoly(A,B,C,D,F,1) a = 1 b = [0 1.3366 -0.3598] c = [1 0.2959 0.0126] d = [1 -0.6273 -0.2661] f = [1 -1.2992 0.7834] bjModel = idpoly(a,b,c,d,f,1) loadmatfile('arxData.mat') a = [1 -1.1884 0.4196] b = [0 0.8726 0.8444] c = 1 d = 1 f = 1 arxModel = idpoly(a,b,c,d,f,0.1) // aPoly = poly(oeModel.a,'q','coeff'); // bPoly = poly(oeModel.b,'q','coeff'); // cPoly = poly(oeModel.c,'q','coeff'); // dPoly = poly(oeModel.d,'q','coeff'); // fPoly = poly(oeModel.f,'q','coeff'); // qG = bPoly/(aPoly*fPoly); // qH = cPoly/(aPoly*dPoly); // invqHqG = qG/qH; // invqH1 = 1-1/qH; ////------------------------------------------------------------------------------ // uCoeff = invqHqG.num*invqH1.den; // yCoeff = invqHqG.den*invqH1.num; // yCapCoeff = invqHqG.den*invqH1.den; ////-------------------------------------------------------------------------------- // lengthuCoeff = length(coeff(uCoeff)); // lengthyCoeff = length(coeff(yCoeff)); //lengthyCapCoeff = length(coeff(yCapCoeff)); ////------------------------------------------------------------------------------ // uCoeff = coeff(uCoeff); // yCoeff = coeff(yCoeff); // yCapCoeff = coeff(yCapCoeff); // yCapCoeff = -yCapCoeff(2:lengthyCapCoeff); ////------------------------------------------------------------------------------ ////initial conditions // uData = zeros(lengthuCoeff,1); // yData = zeros(lengthyCoeff,1); // yCapData = zeros(lengthyCapCoeff-1,1); // uData = [uData;data(:,2)]; // yData = [yData;data(:,1)]; // ////------------------------------------------------------------------------------ //sampleData = size(data,'r'); //uCoeff = uCoeff(lengthuCoeff:-1:1); //yCoeff = yCoeff(lengthyCoeff:-1:1); //yCapCoeff = yCapCoeff(lengthyCapCoeff-1:-1:1); //for ii = 1:sampleData+1 // //pause // tempu = uCoeff*uData(ii:ii+lengthuCoeff-1); // tempy = yCoeff*yData(ii:ii+lengthyCoeff-1); // tempyCap = yCapCoeff*yCapData(ii:ii+lengthyCapCoeff-2); // yCapData = [yCapData;tempu+tempy+tempyCap]; // //pause //end //
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/set6/s_Electrical_Measurements_Measuring_Instruments_K._Shinghal_2318.zip/Electrical_Measurements_Measuring_Instruments_K._Shinghal_2318/CH3/EX3.71.b/ex_3_71_b.sce
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hohiroki/Scilab_TBC
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2021-01-18T02:07:29.200029
2016-04-29T07:01:39
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ex_3_71_b.sce
errcatch(-1,"stop");mode(2);//Example 3.71.b:resistance and capacitance ; ; cl=10^-4;//micro-F c2=0.004;//micro-F c3=0.001;//micro-F r3=10;//killo ohms r4=5;//killo ohms f=1;//kHz rx=((c3+cl)/c2)*r4;//killo ohms cx=(r3/r4)*c2;//micro-F disp(rx,"resistance is ,(k-ohm)=") disp(cx,"capacitance is,(micro-F)=") exit();
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/Rez/bivariate-lcmsr-post_mi/bfas_ee_aspfin/~BivLCM-SR-bfas_ee_aspfin-PLin-VLin.tst
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psdlab/life-in-time-values-and-personality
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2020-03-24T22:08:27.964205
2019-03-04T17:03:26
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~BivLCM-SR-bfas_ee_aspfin-PLin-VLin.tst
THE OPTIMIZATION ALGORITHM HAS CHANGED TO THE EM ALGORITHM. ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.380813D+00 2 -0.145241D-02 0.320467D-02 3 0.338409D-01 0.184141D-04 0.532181D+00 4 0.466447D-03 0.387628D-03 -0.899567D-02 0.388610D-02 5 0.241298D-02 0.177313D-03 -0.651834D-03 -0.110690D-03 0.276628D-02 6 0.408854D-04 -0.494409D-04 -0.172966D-03 -0.299079D-04 0.470915D-04 7 -0.256868D-03 -0.969478D-04 0.416733D-03 0.308389D-03 -0.465980D-03 8 -0.689916D-03 0.137576D-03 -0.175050D-02 -0.364979D-04 0.180983D-03 9 -0.329020D+00 0.422869D-01 0.393755D-01 -0.540490D-03 0.100961D+00 10 0.876680D-01 0.137145D-01 0.356229D+00 -0.144460D-01 0.135130D+00 11 -0.579841D-01 0.129036D-01 -0.455903D+00 0.688364D-02 0.226309D-02 12 -0.793109D-01 -0.179887D-01 0.589485D+00 0.203334D-01 0.754099D-02 13 -0.160314D+00 0.544055D-02 0.128728D+00 0.799702D-02 -0.258985D-01 14 -0.866259D-01 0.126574D-01 0.136864D+00 -0.298975D-01 0.132103D-01 15 -0.807147D+00 -0.114920D+00 -0.337853D+00 -0.116139D-01 -0.168685D+00 16 -0.446095D-01 -0.103798D-01 -0.185298D-01 -0.177242D-02 -0.287006D-02 17 -0.671140D-02 -0.404677D-03 -0.555601D-03 -0.197204D-03 -0.411255D-03 18 0.119017D+00 0.939735D-02 0.486355D+00 -0.627817D-01 0.171542D-01 19 0.625566D-01 0.685236D-02 0.168771D+00 0.423138D-03 0.859420D-02 20 0.218617D+00 -0.586105D-01 0.371661D+01 0.829675D-03 -0.324171D-01 21 -0.732981D-01 -0.105462D-01 -0.119732D+00 -0.312838D-02 -0.936037D-02 22 -0.290017D-02 -0.293829D-03 -0.243057D-02 0.903576D-03 -0.288380D-03 23 0.364965D-01 -0.811123D-03 0.478673D-01 0.675376D-02 0.192222D-02 24 -0.193350D-03 0.115106D-02 -0.121050D-01 0.339392D-03 -0.544548D-03 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.892020D-03 7 0.916065D-03 0.382205D-02 8 -0.204620D-03 -0.245704D-03 0.313989D-02 9 -0.204165D-01 -0.131740D-01 -0.142926D-01 0.584624D+02 10 0.507261D-02 -0.394421D-01 0.936940D-02 0.267782D+01 0.192569D+02 11 0.103452D-01 -0.118672D-01 -0.109945D-01 -0.124120D+01 -0.369224D+00 12 0.217776D-01 -0.488577D-01 -0.535000D-01 -0.493296D+01 0.338126D+01 13 0.631582D-01 0.133188D+00 -0.335744D-02 -0.273882D+01 -0.105306D+01 14 -0.148773D-01 0.581335D-01 0.257239D+00 0.232549D+01 0.245362D+01 15 0.527041D-01 0.937785D-01 -0.107922D-01 -0.175086D+02 -0.132113D+02 16 -0.282578D-03 0.891018D-03 -0.825937D-03 0.681587D+00 -0.348545D+00 17 -0.197962D-03 -0.279998D-03 -0.589198D-04 -0.873332D-01 -0.405657D-01 18 -0.648580D-01 -0.150355D+00 0.166573D-01 -0.998989D+00 0.170025D+01 19 -0.101210D-01 -0.407954D-04 -0.137883D-02 0.272933D+01 0.579773D+00 20 -0.331686D-02 -0.348404D-01 -0.328965D+00 0.745452D+00 0.585407D+01 21 0.777667D-02 -0.488338D-02 0.383116D-02 -0.296039D+01 -0.281815D+00 22 0.597692D-04 0.148921D-03 0.455552D-04 0.256220D-01 -0.257318D-01 23 0.110281D-02 -0.168077D-02 -0.302217D-02 -0.285066D-01 0.205716D+00 24 0.692263D-04 0.213072D-03 0.349278D-03 0.110676D-01 -0.434122D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.312009D+02 12 0.472908D+01 0.126869D+03 13 -0.330578D+01 -0.182762D+00 0.159854D+02 14 -0.262877D+01 -0.182183D+02 -0.996297D+00 0.812766D+02 15 0.138875D+01 -0.657476D+01 0.620631D+01 -0.101600D+02 0.349092D+03 16 -0.238632D-01 -0.307377D+00 -0.406756D-01 -0.667681D-01 0.328453D+01 17 -0.409512D-02 0.988960D-01 -0.237010D-02 -0.130946D-01 -0.142689D+01 18 0.512978D+01 0.495464D+00 -0.832013D+01 0.732139D+00 0.182941D+02 19 0.131476D+01 -0.403844D+01 -0.814592D+00 0.112680D+00 -0.809605D+01 20 -0.729937D+01 0.879258D+01 0.153989D+01 -0.642271D+02 -0.102849D+02 21 -0.589740D+00 0.369249D+01 0.598219D+00 0.333383D+00 0.915692D+01 22 -0.671598D-01 0.187539D-01 -0.315392D-02 -0.244986D-01 0.308228D-01 23 -0.204555D+00 0.197569D+01 -0.100240D-01 -0.305882D+00 0.309077D+00 24 0.538008D-01 -0.269287D+00 0.828820D-02 0.803435D-02 -0.692931D-02 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.565696D+00 17 -0.257488D-01 0.159622D-01 18 0.369262D+00 -0.658386D-01 0.272414D+03 19 -0.162213D+00 0.325705D-01 0.578044D+01 0.664800D+01 20 0.849263D-01 0.166809D-01 0.185000D+02 0.606052D+01 0.578683D+03 21 0.264308D+00 -0.334668D-01 -0.805994D+00 -0.547063D+01 -0.643173D+01 22 0.141787D-02 0.153208D-03 -0.128162D+01 -0.559760D-01 -0.134884D+00 23 0.331471D-01 -0.408525D-02 -0.315918D+00 -0.315262D+00 0.510746D+01 24 -0.192632D-02 0.103727D-02 0.106562D-01 -0.869592D-02 -0.230170D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.641469D+01 22 -0.295058D-01 0.153652D-01 23 0.285002D+00 0.101099D-01 0.117900D+01 24 0.321679D-01 0.164867D-03 -0.923954D-01 0.274478D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.042 1.000 3 0.075 0.000 1.000 4 0.012 0.110 -0.198 1.000 5 0.074 0.060 -0.017 -0.034 1.000 6 0.002 -0.029 -0.008 -0.016 0.030 7 -0.007 -0.028 0.009 0.080 -0.143 8 -0.020 0.043 -0.043 -0.010 0.061 9 -0.070 0.098 0.007 -0.001 0.251 10 0.032 0.055 0.111 -0.053 0.585 11 -0.017 0.041 -0.112 0.020 0.008 12 -0.011 -0.028 0.072 0.029 0.013 13 -0.065 0.024 0.044 0.032 -0.123 14 -0.016 0.025 0.021 -0.053 0.028 15 -0.070 -0.109 -0.025 -0.010 -0.172 16 -0.096 -0.244 -0.034 -0.038 -0.073 17 -0.086 -0.057 -0.006 -0.025 -0.062 18 0.012 0.010 0.040 -0.061 0.020 19 0.039 0.047 0.090 0.003 0.063 20 0.015 -0.043 0.212 0.001 -0.026 21 -0.047 -0.074 -0.065 -0.020 -0.070 22 -0.038 -0.042 -0.027 0.117 -0.044 23 0.054 -0.013 0.060 0.100 0.034 24 -0.002 0.123 -0.100 0.033 -0.062 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.496 1.000 8 -0.122 -0.071 1.000 9 -0.089 -0.028 -0.033 1.000 10 0.039 -0.145 0.038 0.080 1.000 11 0.062 -0.034 -0.035 -0.029 -0.015 12 0.065 -0.070 -0.085 -0.057 0.068 13 0.529 0.539 -0.015 -0.090 -0.060 14 -0.055 0.104 0.509 0.034 0.062 15 0.094 0.081 -0.010 -0.123 -0.161 16 -0.013 0.019 -0.020 0.119 -0.106 17 -0.052 -0.036 -0.008 -0.090 -0.073 18 -0.132 -0.147 0.018 -0.008 0.023 19 -0.131 0.000 -0.010 0.138 0.051 20 -0.005 -0.023 -0.244 0.004 0.055 21 0.103 -0.031 0.027 -0.153 -0.025 22 0.016 0.019 0.007 0.027 -0.047 23 0.034 -0.025 -0.050 -0.003 0.043 24 0.014 0.021 0.038 0.009 -0.060 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 0.075 1.000 13 -0.148 -0.004 1.000 14 -0.052 -0.179 -0.028 1.000 15 0.013 -0.031 0.083 -0.060 1.000 16 -0.006 -0.036 -0.014 -0.010 0.234 17 -0.006 0.069 -0.005 -0.011 -0.604 18 0.056 0.003 -0.126 0.005 0.059 19 0.091 -0.139 -0.079 0.005 -0.168 20 -0.054 0.032 0.016 -0.296 -0.023 21 -0.042 0.129 0.059 0.015 0.194 22 -0.097 0.013 -0.006 -0.022 0.013 23 -0.034 0.162 -0.002 -0.031 0.015 24 0.058 -0.144 0.013 0.005 -0.002 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.271 1.000 18 0.030 -0.032 1.000 19 -0.084 0.100 0.136 1.000 20 0.005 0.005 0.047 0.098 1.000 21 0.139 -0.105 -0.019 -0.838 -0.106 22 0.015 0.010 -0.626 -0.175 -0.045 23 0.041 -0.030 -0.018 -0.113 0.196 24 -0.015 0.050 0.004 -0.020 -0.578 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.094 1.000 23 0.104 0.075 1.000 24 0.077 0.008 -0.514 1.000
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(a*x^4 + b*x^2*y^2 + c*y^4).degree() = 5 (a*x^4 + b*x^2*y^2 + c*y^4).degree(false) = 5
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Ex5_7.sce
//Fluid Systems- By Shiv Kumar //Chapter 5- Francis Turbine //Example 5.7 //To Determine (a) The Diameter of Wheel (b) The Quantity of Water Supplied (c) The Guide Blade Angle at Inlet (d) The Runner Vane Angles at Inlet and Exit. clc clear //Given Data:- P=368; //Shaft Power, kW H=71; //Head, m N=748; //Speed, rpm bo_by_Do=0.1; //Breadth Ratio Kf=0.15; //Flow Ratio eta_H=95/100; //Hydraulic Efficiency eta_m=85/100; //Mechanical Efficiency eta_v=100/100; //Volumetric Efficiency (Assumed to be 100%) //As Inner Diameter is Half the Outer Diameter, Di_by_Do=1/2; //Di/Do //Data Required:- rho=1000; //Density of Water, Kg/m^3 g=9.81; //Acceleration due to gravity, m/s^2 //Computations:- eta_o=eta_H*eta_m*eta_v; //Overall Efficiency Q=P*1000/(rho*g*H*eta_o); //m^3/s Vfi=Kf*sqrt(2*g*H); //m/s Vfo=Vfi; Do=sqrt(Q/(%pi*bo_by_Do*Vfi)); //m Di=Do*Di_by_Do; //m // (a) The Diameter of Wheel, Do //Calculated Above // (b) The Quantity of Water Supplied, Q //Calculated Above // (c) The Guide Blade Angle at Inlet , alpha_i ui=%pi*Do*N/60; //m/s uo= %pi*Di*N/60; //m/s Vwi=eta_H*g*H/ui; //m/s alpha_i=atand(Vfi/Vwi); //degrees // (d)Runner Vane Angles at Inlet and Outlet, beta_i, beta_o beta_i=atand(Vfi/(Vwi-ui)); //Runner Vane Angle at Inlet, degrees beta_o=atand(Vfo/uo); //Runner Vane Angle at Outlet, degrees //Results:- printf(" (a) The Diameter of Wheel, Do =%.3f m\n ",Do ) printf(" (b) The Quantity of Water Supplied, Q=%.4f m^3/s\n",Q ) printf(" (c) The Guide Blade Angle at Inlet , alpha_i=%.2f Degrees\n",alpha_i ) //The Answer Vary due to Round off Error printf(" (d)Runner Vane Angles at Inlet and Outlet are:- \n beta_i=%.2f Degrees , beta_o =%.2f Degrees \n",beta_i,beta_o ) //The Answer Vary due to Round off Error
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Ex19_3.sce
//scilab 5.4.1 //Windows 7 operating system //chapter 19 VLSI Technology and Circuits clc clear w=10//w=W/L value of the NMOS transistor in a CMOS inverter un=1350//un=electron mobility for NMOS transistor in cm^2/V s up=540//up=electron mobility for PMOS transistor in cm^2/V s //(Wpu/Lpu)*up*(VINV-VDD-VTHP)^2=(Wpd/Lpd)*un*(VINV-VTHN)^2 //For a symmetrical inverter VINV=(VDD/2) and VTHN=(-VTHP) //Also for input voltage=VDD/2 both transistors operate in saturation region //Therefore,up*(Wpu/Lpu)=un*(Wpd/Lpd) w1=(un*w)/up//w1=Wpu/Lpu=W/L value of the PMOS for a symmetrical inverter disp(w1,"W/L value of the PMOS transistor in a CMOS inverter is =")
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//Calculate current in different parts of winding of autotransformer//Chapter 3 //Example 3.32 //page 240 clear; clc; disp("Example 3.32") V1=230; //primary voltage of auto-transformer V2=75; //secondary voltage of auto-transformer r=(V1/V2); //ratio of primary to secondary turns I2=200; //load current in amperes I1=I2/r; printf("Primary current,I1=%fA",I1); printf("\nLoad current,I1=%fA",I2); printf("\ncirrent flowing through the common portion of winding=%fA",(I2-I1)); printf("\nEconomy in saving in copper in percentage=%fpercent",(100/r));
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example9_9.sce
clear; clc; //Example9.9[U-Factor of a Double-Door Window] //Given:- A_win=1.8*2.0;//[m^2] A_glazing=2*1.72*0.94;//[m^2] U_c=3.24,U_e=3.71,U_f=2.8;//U factors for the center edge and frame sections respectively [W/m^2.degree Celcius] //Solution:- A_frame=A_win-A_glazing;//[m^2] A_center=2*(1.72-0.13)*(0.94-0.13);//[m^2] A_edge=A_glazing-A_center;//[m^2] U_win=((U_c*A_center)+(U_e*A_edge)+(U_f*A_frame))/A_win;//[W/m^2.degree Celcius] disp("W/m^2.degree Celcius",U_win,"The overall U factor of the entire window is")
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//Discrete Time Fourier Transform of discrete sequence //x[n]= (a^n).u[-n], |a|>1 clear; clc; close; a1 = 3; min_limit = -20; n = min_limit:0 for i=1:length(n) x1(i) = (a1^n(i)); end Wmax = 2*%pi; K = 4; k = 0:(K/1000):K; W = k*Wmax/K; x1 = x1'; XW1 = x1* exp(-sqrt(-1)*n'*W); XW1_Mag = abs(XW1); W = [-mtlb_fliplr(W), W(2:1001)]; // Omega from -Wmax to Wmax XW1_Mag = [mtlb_fliplr(XW1_Mag), XW1_Mag(2:1001)]; [XW1_Phase,db] = phasemag(XW1); XW1_Phase = [-mtlb_fliplr(XW1_Phase),XW1_Phase(2:1001)]; subplot(3,1,1); plot2d3('gnn',n,x1); xtitle('Discrete Time Sequence x[n]','n','x[n]') subplot(3,1,2); plot2d(W,XW1_Mag); xtitle('Magnitude Response abs(X(jW))','w','|X(jW)|') subplot(3,1,3); plot2d(W,XW1_Phase); xtitle('Phase Response <(X(jW))','w','<(X(jW))')
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// Scilab code Exa12.4 : : Page-574 (2011) clc; clear; zeta = 0.209; // Moderated assembly E_change = 100/1; // Change in energy of the neutron E_thermal = 0.025; // Thermal energy of the neutron, electron volts E_n = 2*10^6; // Energy of the neutron, electron volts n = 1/zeta*log(E_change); // Number of collisions of neutrons to loss 99 percent of their energies n_thermal = 1/zeta*log(E_n/E_thermal); // Number of collisions of neutrons to reach thermal energies printf("\nThe number of collisions of neutrons to loss 99 percent of their energies = %d \nThe number of collisions of neutrons to reach thermal energies = %d",n,n_thermal) // Result // The number of collisions of neutrons to loss 99 percent of their energies = 22 // The number of collisions of neutrons to reach thermal energies = 87
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Example7_7.sce
////Example 7.7 clc; clear; close; format('v',6); //Given data : D=80/1000;//meter Q=600*10^-3/60;//m^3/sec L=1*10^3;//meter f=0.02;//coefficient of friction v=Q/(%pi/4*D^2);//m/s g=9.81;//gravity constanty hf=4*f*L*v^2/D/2/g;//meter disp(hf,"Head lost due to friction in meter : "); //Answer is wrong in the book.
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example22.sce
printf("given G(s)H(s)=(as+1)/s^2 \n we have to find the value of a for which phase margin is 45 degree\n"); printf("G(jw)H(jw)=(1+ajw)/(jw)^2 and <G(jw))H(jw)=-180+atan aw\n") aw=tan(45); a=sqrt(1/sqrt(2)); printf("the value of a is"); disp(a);
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Ex12_12.sce
//===================================================================================== //Chapter 12 example 12 clc; clear all; //variable declaration R2 = 834; //resistance of arm in Ω R3 = 100; //resistance of arm in Ω R4 = 64.9; //resistance of arm in Ω R = 0.4; //resistance in Ω C4 = 0.1*10^-6; //capacitance in F C2 = 0.124*10^-6; //capacitance in F f = 2000; //frequency in Hz //calculations L1 = R2*R3*C4; //inductance in H R1 = (R3*C4/C2); // resistance in Ω Z = R1+(2*%pi*f*L1)*%i; //effective impedance Z1 = sqrt(((real(Z))^2)+(((imag(Z))^2))); angle = (atan((imag(Z))/real(Z)))*180/%pi; //result mprintf("L1 = %3.2e",L1); mprintf("\nR1 = %3.2f",R1); mprintf("\neffective impedance of test specimen =%3.2f Ω angle %3.2f °",Z1,angle);
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ex_5.sce
// Chapter 10_Fundamentals of the Metal Oxide Semiconductor Field Effect Transistor //Caption_Threshold voltage voltage //Ex_5//page 446 T=300 eps=11.7*8.85*10^-14 eps_ox=3.9*8.85*10^-14 e=1.6*10^-19 ni=1.5*10^10 //intrinsic carrier concentration Na=10^14 //acceptor impurity concentration Qss=10^10 tox=500*10^-8 //oxide thickness phi_ms=-0.83 phi_fp=0.0259*log(Na/ni) xdt=(4*eps*phi_fp/(e*Na))^0.5 QSD_MAX=e*Na*xdt; Vtn=(QSD_MAX-Qss*e)*(tox/eps_ox)+phi_ms+2*phi_fp printf('The threshold voltage of this MOS system is %1.3f V',Vtn)
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9_1.sce
clc //initialisation of variables clear d= 2 //in V= 210 //ft/sec V1= 50 //ft/sec g= 32.2 //ft/sec^2 w= 62.4 //lb/ft^3 //CALCULATIONS M= %pi*V*w/(4*36*g) F= M*V dV= V-V1 M1= %pi*dV*w/(4*36*g) F1= M1*dV W= F1*V1 F2= M*dV W1= F2*V1 //RESULTS printf ('Force on plate = %.f lb',F+1) printf ('\n Force on plate = %.f lb',F1) printf ('\n Work done/sec = %.f ft-lb/sec',W) printf ('\n Force on plate = %.f lb',F2) printf ('\n Work done/sec = %.f ft-lb/sec',W1) //The answer is a bit different due to rounding off error in textbook
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plane1.sce
//(x/a)+(y/b)+(z/c)=1 (PLANE) a=1; b=2; c=3; x=-5:0.01:5; y=-5:0.01:3; deff('z=f(x,y)','z=(c*(1-(x)/(a)-(y)/(b)))'); fplot3d(x,y,f)
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Chap4_Ex15_R1.sce
// Y.V.C.Rao ,1997.Chemical Engineering Thermodynamics.Universities Press,Hyderabad,India. //Chapter-4,Example 15,Page 115 //Title:Final temperature and amount of gas escaping the cylinder //================================================================================================================ clear clc //INPUT V=0.1;//volume of cylinder in m^3 T0=300;//initial temperature of nitrogen in K P0=14;//initial pressure of nitrogen in MPa P=0.1;//ambient pressure in MPa Pf=2;//final pressure of nitrogen in MPa R=8.314;//universal gas constant in J/molK gaamma=1.4;//ratio of the molar heat capacities at constant pressure and constant volume for nitrogen (no unit) //CALCULATION //calculation of final temperature of the gas in the tank in K using Eq.(4.51) (and applying u=Cv*T, h=Cp*T and N=P*V/R*T as the gas is taken to be ideal) function[fn]=solver_func(Ti) //Function defined for solving the system to determine the final temperature fn=((P0*10^6)-(Pf*10^6))-((gaamma/2)*(T0+Ti)*(((P0*10^6)/T0)-((Pf*10^6)/Ti))); endfunction Tguess=300;//The final temperature guess value in K used for solving the system of equations [Tf]=fsolve(Tguess,solver_func,1e-6)//using inbuilt function fsolve for solving the system of equations //calculation of the moles of nitrogen escaping from the tank using Eq.(4.51) (and applying u=Cv*T, h=Cp*T and N=P*V/R*T as the gas is taken to be ideal) N=(V/R)*(((P0*10^6)/T0)-((Pf*10^6)/Tf)); //OUTPUT mprintf('\n The final temperature= %0.1f K\n',Tf); mprintf('\n The amount of gas that has escaped from the cylinder= %0.2f mol\n',N); //===============================================END OF PROGRAM===================================================