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// Copyright (C) 2010 - DIGITEO - Michael Baudin // Copyright (C) 1993 - 1995 - Anders Holtsberg // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt function [b,Ib,Vb]=logitfit(y,x,C) b=[];Ib=[];Vb=[]; [nargout,nargin] = argn(0) //LOGITFIT Fit a logistic regression model. // // [b, Ib, Vb] = logitfit(y,X,C) // // Fit the model log(p/(1-p)) = X*b, where p is the probability // that y is 1 and not 0. Output b is vector of point estimates, // Ib is confidence intervals, and Vb is the estimated variance // matrix of b. Input C is confidence level for the confidence // intervals, default is 0.95. // // If an intercept is not included in X it is automatically added // as an extra column. // // See also LODDS and LODDSINV. if nargin<3 then C = 0.95; end if size(y,2)>1 then error('Input y must be column vector'); end n = max(size(y)); if sum(bool2s(y==1|y==0))<n then error('Hey, only 0 or 1 as response varable y'); end one = ones(n,1); if or(abs(one-x*(x\one))>0.0000000001) then fprintf(' Intercept column added \n '); x = [x,ones(n,1)]; end nb = size(x,2); b = x\(4*y-2); for i = 1:50 z = x*b; g1 = 1+exp(-z); g0 = 1+exp(z); df1 = -1 ./ g0; df0 = 1 ./ g1; degreef = sum((y .* df1+(1-y) .* df0)*ones(1,nb) .* x)'; ddf = 1 ./ (g0+g1)*ones(1,nb) .* x'*x; b = b-ddf\degreef; if and(abs(degreef)<0.0001) then break end end if i==50 then error('No convergence'); end logL = y .* log(g1)+(1-y) .* log(g0); Vb = inv(ddf); lamda = qnorm(1-(1-C)/2); Ib = lamda*sqrt(diag(Vb)); Ib = [b-Ib,b+Ib]; endfunction
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//chapter 19 //example 19.19 //page 862 printf("\n") printf("given") Vbe=.7;R2=560;R3min=0;R3max=1*10^3;Is=2*10^-3; Ic2max=Vbe/(R2+R3min) Ic2min=Vbe/(R2+R3max) Vgsmin=(Is+Ic2min)*820 Vgsmax=(Is+Ic2max)*820
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//Chapter 8, Problem 3 clc c1=10e-12 //capacitance in farad c2=100e-12 //capacitance in farad f=100e6 //frequency in hertz //calculation w=2*%pi*f L=(1/w^2)*((1/c1)+(1/c2)) g=1+(c2/c1) printf("(a) Value of inductor = %.2f nH\n\n",L*10^9) printf("(b) Minimum voltage gain = %d ",g)
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//Chapter-4, Illustration 7, Page 138 //Title: Gears and Gear Drivers //============================================================================= clc clear //INPUT DATA N=4.5;//No. of turns //CALCULATIONS Vh=N/2;//Velocity ratio of main spring spindle to hour hand spindle Vm=12;//Velocity ratio of minute hand spindle to hour hand spindle T1=8// assumed no of teeth on gear 1 T2=32// assumed no of teeth on gear 2 T3=(T1+T2)/4// no of teeth on gear 3 T4=(T1+T2)-T3// no of teeth on gear 4 printf('no of teeth on gear 1=%d\n no of teeth on gear 2=%d\n no of teeth on gear 3=%d\n no of teeth on gear 4=%d',T1,T2,T3,T4)
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clc //to percentage contraction of a rod c=3*10^8 //light speed(m/s) v=0.8*c //velocity(m/s) //let lo be the length of the rod in the frame in which it is at rest //s' is the frame which is moving with a speed 0.8c in a direction making an angle 60 with x-axis //components of lo along perpendicular to the direction of motion are lo cos60 and lo sin60 respectively l1=cos(%pi/3)*sqrt(1-(v/c)^2) //length of the rod alond the direction of motion =lo cos(pi/3)sqrt(1-(v/c)^2) l2=sin(%pi/3) //length of the rod perpendicular to the direction of motion =lo sin60 l=sqrt(l1^2+l2^2) // length of the moving rod per=(1-l)*100/1 disp("percentage contraction of a rod is per="+string(per)+"%")
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//Exa 4.7 clc; clear; close; disp("The voltage at node X will be equal to the xvoltage across resistor R5, hence "); disp("Vx=(Vo*R5)/(R5+R6)"); disp("Vx=Vo/8"); Vz=1;//in Volt disp("writing KCL at node Y yields "); disp("(Vy-Vx)/R2+(Vy-Vz)/R3=0 or (Vy-Vx)/2+(Vy-1)/4=0"); disp("Vy=(2*Vx+1)/3"); disp("writing KCL at node X yields "); disp("(1-Vx)/R1+(Vy-Vx)/R2=0 or (1-Vx)/2+(Vy-Vx)/2=0 "); disp("Vy-2*Vx+1=0"); disp("Now substituting for Vy from above equation, we get") disp("(2*Vx-1)/3-2*Vx+1=0"); Vx=2/4;//in Volt disp(Vx,"The value of Vx in volt is :") Vo=8*Vx;//in Volt disp(Vo,"The output voltage of the circuit in volt is : ")
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clc //Initialization of variables xc=[0 0.20 0.40 0.60 0.80 1] pc=[0 35 82 142 219 293] pa=[347 270 185 102 37 0] //calculations plot(xc,pc) plot(xc,pa) xlabel('Mole fraction xc') ylabel('Pressure /Torr') disp('From the graph it is clear that KA=175 torr and KC=165 torr. They are plotted with Raoults law lines')
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//Chapter 24: Space Wave Propagation //Example 24-9.2 clc; //Variable Initialization tx_h = 144 //Transmitting antenna height (m) rx_h = 25 //Receiving antenna height (m) k = 4.0/3.0 //Equivalent earth radius/Actual earth radius (unitless) a = 6370 //Radius of earth (km) //Calculations los = 4.12*(sqrt(tx_h) + sqrt(rx_h)) //Line of sight distance (km) horz = sqrt(2*k*a*(tx_h/1000.0)) //Surface range to radio horizon from radar (km) //Result mprintf("The Radio horizon distance from radar is %.2f km",horz)
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//1a EXPERIÊNCIA: Perceptron //Aluno de Mestrado: Luiz Carlos Brandão Junior //f(u)=1 se u>0 e f(u)=0 se u <0 //y=[0 0 0 1] a saida para o AND clear; clc; //Declaração das Variaveis e seus valores b=-0.6; w1=0.4; w2=0.4; w3=0.7; w4=0.8; //declaraçã das funções function y = yperceptron(x,w,b) u=w*x+b; y=[]; for i = 1:length(u) if (u(i)>0) then y=[y 1]; elseif(u(i)<0) y=[y 0]; end end endfunction //programa principal x=[0 1 0 1;0 0 1 1]; w=[w1 w2]; y=yperceptron(x,w,b); disp(y,"Matriz AND: ") w=[w3 w4]; y=yperceptron(x,w,b); disp(y,"Matriz OR: ")
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clc; clear; //clears the console and all previously stored variables function [V0, CIl, CIr] = BS_EuCall_MC_IS (S0, r, sigma, K, T, mu, N, alpha) function V_ = f (Y) V_ = exp(-r*T-Y.*mu+mu^2/2).*max(S0*exp((r-sigma^2/2)*T+sigma*sqrt(T).*Y)-K, 0); endfunction V1(:) = f(grand(N, 1, "nor", mu, 1)); V0 = mean(V1); var_V_is = variance(V1); // function to determine the value of the standard deviation of the mean // for a given alpha (probability), since std. nor. is symetric: q=(1-alpha)/2 function std_dev = CI_std (alpha) std_dev = cdfnor("X", 0, 1, 1-(1-alpha)/2, (1-alpha)/2); endfunction epsilon = CI_std(alpha)*sqrt(var_V_is/N); CIl=V0-epsilon; CIr=V0+epsilon; endfunction // Assigning given values to variables S0=100; r=0.05; sigma=0.2; K=200; T=1; N=10000; alpha=0.95; mu=[0:0.1:6] // For-loop over all mu j=0 // auxillary index variable CI_matrix = zeros(2,length(mu)) // Initializing matrix for the CI values for i=mu [V0, CIl, CIr] = BS_EuCall_MC_IS (S0, r, sigma, K, T, i, N, alpha) j=j+1 // Increasing index variable by for each iteration of the for-loop V_plot(j) = V0 // Storing values for V0 CI_matrix(1,j) = CIl // Storing values for left CI CI_matrix(2,j) = CIr // Storing values for right CI end // Plotting the V0 in dependence on mu scf(0) clf() plot(mu, V_plot') // It can be seen that mu should probably be choosen in the range of [2,5] as // the variation of the price is lower than before or after this range // Plotting the CI in dependence on mu to see if variance is really the lowest // in the range of [2,5] plot(mu,CI_matrix(1,:),"r") plot(mu,CI_matrix(2,:),"r") // Labeling the axis and adding a legend for better overview legend(["Option Value"; string(alpha*100)+"% Confidence Intervals"]) ylabel("Value", "fontsize", 4, "color", "blue") xlabel("mu", "fontsize", 4, "color", "blue") // It is obviously the case, so mu should be chosen in the range of [3,4] as // the CI are the nearest in this region.
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function y=f(x) y=x endfunction x=linspace(0,6) plot(x,f) xlabel('t') ylabel('y') xtitle('Continuous Ramp Signal')
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//ques-25.1 //Finding pressure exerted in a vessel clc m1=2;//mass of ethane given (in g) m2=3;//mass of CO2 given (in g) M1=30;//molar mass of ethane (in g/mol) M2=44;//molar mass of CO2 (in g/mol) V=5;//volume of vessel (in L) T=273+50;//temperature (in K) R=0.0821;//(in atm L/K/mol) n=m1/M1+m2/M2;//moles of gas P=(n*R*T)/V;//pressure printf("The pressure exerted in the vessel is %.4f atm.",P);
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// Example 22_22 clc;funcprot(0); //Given data P=30;// MW p_1=0.04;// bar p_2=7;// bar p_3=60;// bar T_1=550;// °C p_c=730;// mm of Hg p_v=760;// mm of Hg n_t=90/100;// The isentropic efficiency of the turbine //Calculation p_1=((p_v-p_c)*133.3)/10^5;// bar //From h-s chart: h_1=3420;// kJ/kg h_2a=2860;// kJ/kg h_2=2900;// kJ/kg h_3=2410;// kJ/kg h_3a=2190;// kJ/kg // From steam tables h_f3=121.5;// kJ/kg(liquid heat at 0.04 bar) h_f2=697;// kJ/kg(liquid heat at 7 bar) function[X]=mass(y) X(1)= (y(1)*(h_2-h_f2))-((1-y(1))*(h_f2-h_f3)); endfunction y=[0.1]; z=fsolve(y,mass); m=z(1);// kg m_s=(P*10^3)/((h_1-h_2)+((1-m)*(h_2-h_3a)));// kg/sec printf('\n(a)Fraction of steam bled for feed heating=%0.3f kg \n(b)Boiler generating capacity=%0.1f kg/sec',m,m_s);
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//reference:https://help.scilab.org/docs/5.5.1/ja_JP/csvRead.html //http://hotic.blog129.fc2.com/blog-entry-10.html //http://scilab.kani33.com/2015/05/graphic-color/ //ファイル読み取り //filename = fullfile("/Users/makino/Desktop/scilab/check.csv"); filenamex = fullfile("C:\Users\user\Desktop\scilab\Book2.csv"); filename_out = fullfile("C:\Users\user\Desktop\scilab\out.csv"); //csv読み取り //data = csvRead(filename); datax = csvRead(filenamex); x = size(datax,1) last = datax(x,1) data_out = zeros(floor(last*100),2); for i = 1:floor(last * 100), for j =1:x, if i * 0.01 < datax(j,1) data_out(i,1) = i * 0.01; if j==1 data_out(i,2) = datax(j,2) * i*0.01/datax(j,1); data_out(i,3) = datax(j,3) * i*0.01/datax(j,1); else data_out(i,2) = datax(j-1,2) * (datax(j,1) - i*0.01) / (datax(j,1) - datax(j-1,1)) + datax(j,2) * (i*0.01 - datax(j-1,1)) / (datax(j,1) - datax(j-1,1)); data_out(i,3) = datax(j-1,3) * (datax(j,1) - i*0.01) / (datax(j,1) - datax(j-1,1)) + datax(j,3) * (i*0.01 - datax(j-1,1)) / (datax(j,1) - datax(j-1,1)); end, break end, end, end csvWrite(data_out,filename_out)
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clc clear all t=0:0.001:1; fc=input('Enter the freq of Sine Wave carrier: '); fm=input('Enter the freq of Message signal: '); amp=input('Enter the Amplitude of For Carrier & Message (Assuming then as equal): '); c=amp.*sin(2*%pi*fc*t); subplot(3,1,1); xlabel('Time') ylabel('Amplitude') title('Carrier Wave') plot(t,c); m=squarewave(2*%pi*fm*t); subplot(3,1,2); xlabel('Time') ylabel('Amplitude') title('Message') plot(t,m); x=c.*m; subplot(3,1,3); xlabel('t') ylabel('y') title('PSK') plot(t,x);
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////Ex 13.2 clc; clear; close; format('v',6); VNL=18;//V VFL=17.8;//V IL=50;//mA LR=(VNL-VFL)*100/VFL;//%(Line Regulation) LdR=LR/IL;//%/mA(Load Regulation) disp(LdR,"Load Regulation(%/mA)");
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errcatch(-1,"stop");mode(2);//Chapter 6,Example 6.4 Page 200 t = 60 C = 600*10^-12 V = 250 v = 92 R = t/(C*log(V/v)) printf (" R = %e ohm \n ",R) exit();
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//Chapter-11,Example 1,Page 275 clc(); close(); M =1000 //mass of alloy m_Cd= 0.25*M //25% of Cd in alloy //since in the eutectic system, 40% is Cd and 60% is Bi //corresponding to m_Cd Cd the content of Bi in eutectic is m_Bi = m_Cd*60/40 m= m_Cd+m_Bi printf('the mass of eutectic in 1 kg alloy is %.f gm ',m)
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//Example 19.4 clc A=%pi*(0.5)*0.5//in m I=2//in A B=0.50//in T T=B*I*A*0.5 disp(T,"The Torque in N-m=")
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//Example 9.3 //Gram-Schmidt Orthogonalization/Orthonormalization Process //Page no. 294 clc;clear;close; deff('y=f(x,a)','y=sqrt(x(1,a)^2+x(2,a)^2+x(3,a)^2+x(4,a)^2)'); deff('y=f1(g,a,h,b)','y=g(1,a)*h(1,b)+g(2,a)*h(2,b)+g(3,a)*h(3,b)+g(4,a)*h(4,b)'); U=[1/sqrt(3),-2/sqrt(7),1,0,0,0;0,1/sqrt(7),0,1,0,0;1/sqrt(3),1/sqrt(7),0,0,1,0;-1/sqrt(3),-1/sqrt(7),0,0,0,1]; for i=1:4 V(i,1)=U(i,1); end for i=1:4 if(f(V,1)~=0) W(i,1)=V(i,1)/f(V,1); else W(i,1)=0; end end for j=2:6 for i=1:4 for l=1:4 k(l,1)=0; end for l=1:j-1 for m=1:4 w(m,1)=W(m,l); end k=k-(f1(U,j,W,l))*w; end V(i,j)=U(i,j)+k(i,1); end for i=1:4 if(j~=4) if(f(V,j)~=0) W(i,j)=V(i,j)/f(V,j); else W(i,j)=0; end else W(i,j)=0; end end end disp(U,'U=') disp('W=') printf('\n') for i=1:4 for j=1:6 printf('%.4f\t\t',W(i,j)) end printf('\n') end disp('V=') printf('\n') for i=1:4 for j=1:6 printf('%.4f\t\t',V(i,j)) end printf('\n') end
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//ex7.11 V_DD=12; V_D=7; R_D=3.3*10^3; R_S=2.2*10^3; R_1=6.8*10^6; R_2=1*10^6; I_D=(V_DD-V_D)/R_D; V_S=I_D*R_S; V_G=(R_2/(R_1+R_2))*V_DD; V_GS=V_G-V_S; disp(I_D,'Drain current in amperes') disp(V_GS,'Gate to source voltage in volts')
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THE OPTIMIZATION ALGORITHM HAS CHANGED TO THE EM ALGORITHM. ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.418848D+00 2 -0.637297D-02 0.298191D-02 3 0.229505D-01 -0.123756D-02 0.338337D+00 4 -0.192249D-02 0.405919D-04 -0.297337D-02 0.277285D-02 5 -0.158442D-03 0.344223D-04 -0.210125D-02 0.306748D-03 0.432784D-02 6 0.185495D-03 0.123738D-03 0.206265D-03 -0.804582D-04 0.214016D-04 7 0.240684D-02 0.963723D-05 0.553293D-03 0.470565D-04 0.964696D-03 8 0.539381D-03 0.169923D-03 0.442054D-03 0.641062D-05 0.106976D-03 9 -0.473477D+00 0.938397D-02 0.351435D-01 0.120290D-01 0.193423D+00 10 -0.143112D+00 -0.730980D-02 -0.165008D-02 0.162704D-01 0.234094D+00 11 -0.221980D+00 0.173778D-01 -0.109608D+00 -0.126015D-02 0.346301D-01 12 -0.318433D-01 -0.109929D-01 -0.131524D+01 0.535987D-01 0.376522D-01 13 0.125727D+00 0.662432D-02 0.449957D-01 0.291413D-02 0.452996D-01 14 0.102819D+00 0.111782D-01 -0.320250D+00 0.861821D-02 0.470506D-01 15 -0.380605D+01 -0.811295D-03 -0.659256D+00 -0.401735D-01 -0.161079D+00 16 0.766721D-02 -0.131919D-01 -0.196428D-01 0.163267D-02 0.432377D-03 17 0.440530D-02 0.426396D-04 0.552144D-02 -0.111127D-03 -0.135378D-02 18 -0.978965D+00 -0.126188D-01 -0.327873D+00 -0.402914D-01 0.957409D-01 19 -0.165801D+00 0.556536D-02 0.911820D-01 0.514042D-02 0.247689D-01 20 -0.653303D-01 -0.484775D-01 -0.354546D+01 -0.423733D-01 -0.399645D-01 21 0.955123D-01 -0.477528D-03 -0.694041D-01 -0.842973D-03 -0.246516D-01 22 0.755532D-02 -0.423918D-03 0.474016D-02 0.696961D-03 -0.119319D-02 23 0.393924D-01 0.779040D-03 -0.235698D-01 -0.127447D-01 -0.624922D-02 24 0.365662D-03 0.808564D-03 0.599365D-02 -0.272073D-03 0.298521D-03 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.109111D-02 7 0.954037D-03 0.319124D-02 8 0.186471D-03 -0.211072D-03 0.267479D-02 9 0.362054D-01 0.483812D-01 0.126127D-01 0.609321D+02 10 -0.136917D-01 0.400065D-01 0.729293D-02 0.107825D+02 0.248969D+02 11 0.429741D-01 0.247146D-01 0.208285D-01 0.991406D+01 0.696722D+00 12 0.986913D-02 0.582846D-01 -0.573919D-01 0.381888D+01 0.194932D+01 13 0.711559D-01 0.150230D+00 -0.698487D-02 0.459544D+01 0.356389D+01 14 0.165800D-01 -0.219593D-01 0.248878D+00 0.228728D+01 0.566833D+01 15 -0.243336D-01 -0.900983D-01 -0.221809D-01 -0.151886D+02 -0.138566D+02 16 -0.495373D-03 -0.644664D-03 -0.381727D-02 0.104502D+01 0.124722D+00 17 0.197979D-03 0.162921D-03 0.612446D-04 -0.190683D+00 -0.938535D-01 18 -0.568530D-01 -0.790746D-01 -0.564470D-01 0.472202D+01 0.891492D+01 19 -0.132821D-01 0.386540D-02 0.925843D-03 0.664829D+00 0.137440D+01 20 0.596229D-02 0.787897D-01 -0.153144D+00 -0.213610D+01 0.114440D+01 21 0.107603D-01 -0.810044D-02 -0.159009D-02 -0.110371D+01 -0.144002D+01 22 -0.337292D-04 -0.428394D-03 0.120502D-03 -0.270227D-01 -0.909509D-01 23 0.286340D-03 0.425406D-03 0.118208D-02 -0.824046D+00 -0.265760D+00 24 -0.294804D-04 -0.355569D-03 -0.185085D-03 0.631677D-01 0.479585D-02 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.341707D+02 12 0.683523D+00 0.905301D+02 13 -0.859201D+00 0.526047D+01 0.164998D+02 14 0.200565D+01 -0.414534D+01 -0.407080D+00 0.551548D+02 15 -0.951765D+01 -0.824603D+01 -0.433078D+01 -0.745664D+01 0.487526D+03 16 0.173093D+00 -0.701814D-01 -0.609344D-01 -0.450454D+00 0.209957D+01 17 0.323819D-01 0.873192D-01 -0.167181D-01 0.579124D-01 -0.224690D+01 18 -0.902503D+01 -0.484525D+01 -0.283132D+01 -0.827966D+01 0.725616D+02 19 -0.438853D+00 -0.238463D+01 -0.881299D+00 0.805859D+00 0.286591D+01 20 -0.523399D+01 -0.148129D+01 0.297765D+01 -0.205142D+02 0.809497D+02 21 0.414265D+00 0.227232D+01 0.556357D+00 -0.582351D+00 -0.372955D+01 22 0.265528D-01 0.628641D-01 -0.384698D-01 0.188553D-01 -0.478433D+00 23 0.923625D-01 -0.357929D+00 -0.488409D-01 0.271405D+00 0.517501D+00 24 0.245998D-01 -0.100633D+00 -0.125368D-01 -0.652236D-01 -0.341178D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.779025D+00 17 -0.606088D-01 0.262888D-01 18 -0.746506D+00 -0.581074D+00 0.285504D+03 19 0.104074D-01 -0.334306D-01 0.592334D+01 0.549855D+01 20 0.578396D+00 -0.453501D+00 0.517061D+02 0.679977D+00 0.411571D+03 21 -0.153638D+00 0.557284D-01 -0.248567D+01 -0.497070D+01 -0.637970D+00 22 0.123099D-01 0.408852D-02 -0.133045D+01 -0.437574D-01 -0.361354D+00 23 0.701964D-02 0.297097D-02 -0.103422D+01 -0.400127D+00 0.364808D+01 24 0.178492D-02 0.171821D-02 -0.134673D+00 0.220849D-01 -0.193623D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.577799D+01 22 -0.388279D-02 0.121789D-01 23 0.337137D+00 -0.146249D-02 0.545275D+00 24 -0.362274D-01 0.409926D-03 -0.369302D-01 0.196775D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.180 1.000 3 0.061 -0.039 1.000 4 -0.056 0.014 -0.097 1.000 5 -0.004 0.010 -0.055 0.089 1.000 6 0.009 0.069 0.011 -0.046 0.010 7 0.066 0.003 0.017 0.016 0.260 8 0.016 0.060 0.015 0.002 0.031 9 -0.094 0.022 0.008 0.029 0.377 10 -0.044 -0.027 -0.001 0.062 0.713 11 -0.059 0.054 -0.032 -0.004 0.090 12 -0.005 -0.021 -0.238 0.107 0.060 13 0.048 0.030 0.019 0.014 0.170 14 0.021 0.028 -0.074 0.022 0.096 15 -0.266 -0.001 -0.051 -0.035 -0.111 16 0.013 -0.274 -0.038 0.035 0.007 17 0.042 0.005 0.059 -0.013 -0.127 18 -0.090 -0.014 -0.033 -0.045 0.086 19 -0.109 0.043 0.067 0.042 0.161 20 -0.005 -0.044 -0.300 -0.040 -0.030 21 0.061 -0.004 -0.050 -0.007 -0.156 22 0.106 -0.070 0.074 0.120 -0.164 23 0.082 0.019 -0.055 -0.328 -0.129 24 0.004 0.106 0.073 -0.037 0.032 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.511 1.000 8 0.109 -0.072 1.000 9 0.140 0.110 0.031 1.000 10 -0.083 0.142 0.028 0.277 1.000 11 0.223 0.075 0.069 0.217 0.024 12 0.031 0.108 -0.117 0.051 0.041 13 0.530 0.655 -0.033 0.145 0.176 14 0.068 -0.052 0.648 0.039 0.153 15 -0.033 -0.072 -0.019 -0.088 -0.126 16 -0.017 -0.013 -0.084 0.152 0.028 17 0.037 0.018 0.007 -0.151 -0.116 18 -0.102 -0.083 -0.065 0.036 0.106 19 -0.171 0.029 0.008 0.036 0.117 20 0.009 0.069 -0.146 -0.013 0.011 21 0.136 -0.060 -0.013 -0.059 -0.120 22 -0.009 -0.069 0.021 -0.031 -0.165 23 0.012 0.010 0.031 -0.143 -0.072 24 -0.006 -0.045 -0.026 0.058 0.007 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 0.012 1.000 13 -0.036 0.136 1.000 14 0.046 -0.059 -0.013 1.000 15 -0.074 -0.039 -0.048 -0.045 1.000 16 0.034 -0.008 -0.017 -0.069 0.108 17 0.034 0.057 -0.025 0.048 -0.628 18 -0.091 -0.030 -0.041 -0.066 0.194 19 -0.032 -0.107 -0.093 0.046 0.055 20 -0.044 -0.008 0.036 -0.136 0.181 21 0.029 0.099 0.057 -0.033 -0.070 22 0.041 0.060 -0.086 0.023 -0.196 23 0.021 -0.051 -0.016 0.049 0.032 24 0.030 -0.075 -0.022 -0.063 -0.110 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.424 1.000 18 -0.050 -0.212 1.000 19 0.005 -0.088 0.149 1.000 20 0.032 -0.138 0.151 0.014 1.000 21 -0.072 0.143 -0.061 -0.882 -0.013 22 0.126 0.228 -0.713 -0.169 -0.161 23 0.011 0.025 -0.083 -0.231 0.244 24 0.014 0.076 -0.057 0.067 -0.680 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.015 1.000 23 0.190 -0.018 1.000 24 -0.107 0.026 -0.357 1.000
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// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Abhilasha Sancheti & Sukul Bagai // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in // function [out] = fillConvexPoly(img, pstData, npts, r_value, g_value, b_value, linetype, shift) // This function fills a convex polygon. // // Calling Sequence // [out] = fillConvexPoly(img, pstData, npts, r_value, g_value, b_value, linetype, shift) // // Parameters // img : The input source image. // pstData : The vector of polygon vertices. // npts : The number of polygon vertices. // r_value : The red value of RGB color for the polygon. // g_value : The green value of RGB color for the polygon. // b_value : The blue value of RGB color for the polygon. // linetype : This is the type of the polygon boundaries. It has only 3 valid types: 4, 8 and 16(CV_AA). Passing any other value as lineType is not legal. // shift : This is the number of fractional bits in the vertex coordinates. // // Description // The function fillConvexPoly draws a filled convex polygon. It can fill not only convex polygons but any monotonic polygon without self-intersections, that is, a polygon whose contour intersects every horizontal line (scan line) twice at the most (though, its top-most and/or the bottom edge could be horizontal). // // Examples // // a simple example // a = imread("/images/lena.jpeg"); // b = [ 0 10; 10 0; -10 0 ]; // c = fillConvexPoly(a, b, 3, 1, 1, 1, 8, 0); // // Authors // Abhilasha Sancheti // Sukul Bagai image = mattolist(img); a = raw_fillConvexPoly(image, pstData, npts, r_value, g_value, b_value, linetype, shift) d = size(a); for i=1:d out(:,:,i) = a(i); end endfunction
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//Hougen O.A., Watson K.M., Ragatz R.A., 2004. Chemical process principles Part-1: Material and Energy Balances(II Edition). CBS Publishers & Distributors, New Delhi, pp 504 //Chapter-2, Illustration 7, Page 39 //Title: Calculation of composition and molality //============================================================================= clear clc //INPUT V = 1000; //Total volume of solution in cc rho = 1.148; //Density of solution in g/cc w1 = 230; //Weight of NaCl in solution in g MW = [58.5,18.020]; //Molecular weight of NaCl and water respectively in g/g mole rho_water = .998; //Density of water at given temperature in g/cc //CALCULATIONS W = V*rho; //Total weight of solution in g w2 = W-w1; //Weight of water in solution in g n1 = w1/MW(1); //To calculate no of moles of NaCl in g mole n2 = w2/MW(2); //To calculate no of moles of water in g mole N= n1+n2; //Total no of moles in g mole //Part(a) m1 = w1*100/W; //To compute weight percent of NaCl m2 = w2*100/W; //To compute weight percent of Water //part(b) v1 = w2/rho_water; //Volume of pure water in cc V1 = v1*100/V; //To compute volume percent of water //part(c) x1 = n1*100/N; //To calculate mole % of NaCl x2 = n2*100/N; //To calculate mole % of water //part(d) a1 = n1; //To calculate no of atoms of sodium in g atom a2 = n1; //To calculate no of atoms of chlorine in g atom a3 = 2*n2; //To calculate no of atoms of hydrogen in g atom a4 = n2; //To calculate no of atoms of oxygen in g atom A = a1+a2+a3+a4; //To calculate total no of atoms A1 = a1*100/A; //To calculate atomic percent of sodium A2 = a2*100/A; //To calculate atomic percent of chlorine A3 = a3*100/A; //To calculate atomic percent of hydrogen A4 = a4*100/A; //To calculate atomic percent of oxygen //part(e) m = n1*V/w2; //Molality of solution in lb mole NaCl/1000 lb H2O //part(f) M = w1/w2; //lb of NaCl per lb H20 //OUTPUT mprintf('\n(a) Weight percent of NaCl and water are %3.0f and %3.0f respectively',m1,m2); mprintf('\n(b) Volumetric percent of water is %3.0f',V1); mprintf('\n(c) Mole percent of NaCl and water are %3.2f and %3.1f respectively',x1,x2); mprintf('\n(d) Atomic percent of sodium,chlorine,hydrogen and oxygen are %3.2f, %3.2f, %4.1f and %3.1f respectively',A1,A2,A3,A4); mprintf('\n(e) Molality of the solution is %3.2f lb mole of NaCl/1000 lb H2O',m); mprintf('\n(f) lb of NaCl per lb of water is %4.3f',M); //=================================END OF PROGRAM==============================
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clc; V=240; // rated voltage of dc shunt motor n=800; // rated speed of dc shunt motor i=50; // rated current of dc shunt motor ra=0.2; // armature resistance pr=0.6; // reduction in load torque as a fraction of full load torque rg=2; // series resistance in armature circuit fr1=0.04; // weakening of field flux at full load fr2=0.02; // weakening of field flux at 60% of full load Ea1=V-(i*ra); // counter EMF at rated load ia2=(i*pr)*((1-fr1)/(1-fr2)); // armature current at reduced load torque Ea2=V-ia2*(rg+ra); // counter EMF at reduced load torque n2=(n*Ea2*(1-fr1))/(Ea1*(1-fr2)); printf('Motor speed at reduced load torque is %f rpm',n2);
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// Example 4.5 // Computation for position of the intrinsic fermi level and the position of the fermi level with respect to the top of the valance band for case(A),the intrinsic carrier concentration of the semiconductor for case(B), effective masses mn & mp of electrons and holes respectively for case(C)// // Page no.95 clc; clear; close; //Given data ; kT=0.0259; NC=1.5*10^18;//NC in cm^-3 NC1=1.5*10^24;//NC1 in m^-3 NV=1.3*10^19;//NV in cm^-3 NV1=1.3*10^25;//NV1 in m^-3 EG=1.43; T=300; //.................................(A)......................................// //Calculation for position of the intrinsic fermi level with respect to the centre of the bandgap// P1=-(kT/2)*log(NC/NV);//P1=(EF-E_midgap) //Thus fermi level is located at 0.028eV abov the center of the bandgap// //Calculation for position of the fermi level with respect to the top of the valance band Ev// P2=(EG/2)-((kT/2)*log(NC/NV));//P2=EF-EV //Hence the fermi level is located at 0.743eV above the valance band Ev// //Calculation for position of the fermi level with respect to the conduction band edge EC// P3=-(EG/2)-(kT/2)*log(NC/NV);//P3=EF-EC //Hence the fermi level is located at 0.687eV below EC// //.................................(B)......................................// //Calculation for intrinsic carrier concentration of the semiconductor// ni=sqrt(NC*NV*exp(-EG/kT)); //.................................(C)......................................// //Calculation for effective mass of electrons mn// mn=((NC1/(4.82*10^21))^(2/3))*(1/T); //mn in Kg: mn1=mn*9.1*10^-31; //Calculation for effective mass of holes mp// mp=((NV1/(4.82*10^21))^(2/3))*(1/T); //mp in Kg: mp1=mp*9.1*10^-31; //Displaying the result in command window printf('\n Position of the Fermi level with respect to the centre of the bandgap E-midgap= %0.3f eV',P1); printf('\n \n Position of the Fermi level with respect to the top of the valance band Ev = %0.3f eV',P2); printf('\n \n Position of the Fermi level with respect to the conduction band edge EC = %0.3f eV',P3); printf('\n \n Intrinsic carrier concentration = %0.2f x 10^6 cm^-3',ni*10^-6); printf('\n \n Effective mass of electrons in meters = %0.3f m',mn); printf('\n \n Effective mass of electrons in Kg = %0.2f x 10^-31 Kg',mn1*10^31); printf('\n \n Effective mass of holes in meters = %0.3f m',mp); printf('\n \n Effective mass of holes in Kg = %0.2f x 10^-31 Kg',mp1*10^31); //Answer given in textbook for mn is wrong// //Answers are varying due to round off error//
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//clear// //Example9.25:LTI Systems Characterized by Linear Constant //Coefficient differential Equation //Finding Transfer function H(S) of LTI system //x(t) = exp(-3t).u(t) //y(t) = [exp(-t)-exp(-2t)].u(t) syms t s; X = laplace('%e^(-3*t)',t,s); Y = laplace('%e^(-t)-%e^(-2*t)',t,s); H = Y/X; disp(H) //Result //(s+3)*(1/(s+1)-1/(s+2))
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clc //Initialization of variables Eab1=0 Eab2=5.87 //mV T1=150 //F T2=200 //F //calculations Eab= -1.12+ 0.035*T1 pi1=0.035*(T1+460) pi2=0.035*(T2+460) //results printf("Thermocouple reading at %d F = %.2f mv",T1,Eab) printf("\n Peltier coefficient at %d F = %.1f mv",T1,pi1) printf("\n Peltier coefficient at %d F = %.1f mv",T2,pi2)
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29 12 ~~~~~~~~~~~~~~~~~~~~~~~~~~ 1
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// Verify FET operation in pinch-off region // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 7-56 in page 358 clear; clc; close; // Given data Vp=-2; // Pinch off voltage in V Idss=4*10^-3; // Drain-source current in mA Rd=910; // Drain resistance in ohms Rs=3*10^3; // Source resistance in K-ohms R1=12*10^6; // R1 value in M-ohms R2=8.57*10^6; // R2 value in M-ohms Vdd=24; // Drain voltage in V // Calculation Vgg = Vdd*R2/(R1+R2); Id1=(73+sqrt(73^2-(4*9*144)))/(2*9); Id2=(73-sqrt(73^2-(4*9*144)))/(2*9); printf("Id = %0.2e A or %0.2e A\n",Id1,Id2); printf("A value of 3.39 mA is selected\n"); Vgsq=10-(3.39*10^-3*3*10^3); Vdsq=Vdd-(3.39*10^-3*3.91*10^3); Vdgq=Vdsq-Vgsq; printf("Vgsq = %0.2fV\nVdsq = %0.2fV\nVdgq = %0.3f V\n",Vgsq,Vdsq,Vdgq); printf("Vdgq>Vd.Hence the FET is in the pinch off region"); // Result // FET operates in the pinch off region
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1000 2000 1 10 3 ~~~~~~~~~~~~~~~~~~~~~~~~~~ This is impossible.
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clc clear //Initialization of variables P=200 //psia T=540 //F pow=1000 //kw ms=16000 //lb/hr //calculations disp("From mollier charts,") h1=1290 //Btu/hr h2=940 //Btu/hr dh=h1-h2 hf2=83 //Btu/lb etat=(h1-h2)/(h1-hf2) act=pow*3413/(ms*(h1-hf2)) etae=act/etat //results printf("Ideal thermal efficiency = %.1f percent",etat*100) printf("\n Actual thermal efficiency = %.1f percent",act*100) printf("\n Engine efficiency = %.1f percent",etae*100)
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clc clear //DATA GIVEN hsup=3373.7; //enthalpy of steam (at 100 bar,500 deg. celsius) in kJ/kg hf1=677; //enthalpy of feed water (at inlet temp. 160 deg. celsius) in kJ/kg hf=1407.65; //ennthalpy of saturated liquid at 100 bar in kJ/kg hg=2724.7; //ennthalpy of saturated vapout at 100 bar in kJ/kg Ms=100000; //rate of steam generation in kg/hr eta=88; //efficiency of steam generation C=21000; //calorific value of fuel in kJ/kg //eta=(heat absorbed by steam per hr)/(heat added by fuel per hour) m=Ms*(hsup-hf1)/(C*(eta/100)); //fuel burning rate in kg/hr htotal=hsup-hf1; //total heat supplied to steam formation Pec=(hf-hf1)/htotal; //% of heat absorbed in economiser Pev=(hg-hf)/htotal; //% of heat absorbed in evaporator Ps=(hsup-hg)/htotal; //% of heat absorbed in superheater printf(' (i) The Fuel burning rate, m is: %5.1f kJ/h. \n',m); printf(' (ii) The Percentage of heat absorbed in economiser is: %5.4f or %5.2f percent.\n',Pec,(Pec*100)); printf(' The Percentage of heat absorbed in evaporator is: %5.4f or %5.2f percent.\n',Pev,(Pev*100)); printf(' The Percentage of heat absorbed in superheater is: %5.4f or %5.2f percent.\n',Ps,(Ps*100));
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//example9.1 clc disp("The arrangement is shown in the Fig. 9.2") disp("Let x=0 at negative plate and x=2*10^-2 m at positive plate.") disp("The E is constant and its magnitude is given by,") e=10/(2*10^-2) disp(e,"E(in V/m)=V/d=") disp("The electron will move with constant acceleration as field is uniform,") a=(1.6*500*10^-19)/(9.107*10^-13) disp(a,"a_x(in m/sec^2)=(q*E)/m=") disp("The velocity v_x is given by,") disp("(v_x)=(a_x)*t+(V_ox) .. v_ox =0 as electron is at rest") disp("and x=(1/2 *a_x *t^2)+(V_ox *t)+(x_o)....(v_ox)=(x_o)=0") x=(1/2)*8.7844*(10^13)*((1*10^-9)^2) disp(x,"Therefore, x(in m)=(1/2)*8.7844*(10^13)*((1*10^-9)^2)=") disp("ii) When electron reaches to second plate, x=2*10^-2 m") disp("Therefore, x=(1/2)*(a_x)*t^2") disp("Therefore, 2*10^-2 = (1/2)*(8.7844*10^13)*t^2") disp("Therefore, t^2 = 4.5535*10^-16") t=sqrt(4.5535*10^-16) format(15) disp(t,"Therefore, t(in sec)=")
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clc clear //input data C1=75//Velocity of air entry in m/s a1=48//Air angle at entry in degree a2=25//Air angle at exit in degree cs=0.91//The chord-pitch ratio P0m=(11*9.81*10^3)/10^3//The stagnation pressure loss in N/m^2 d=1.25//The density of the sair in kg/m^3 //calculations Cp=(P0m/(0.5*d*C1^2))//The pressure loss coefficient am=atand((tand(a1)+tand(a2))/2)//The mean air angle in degree Cd=2*(1/cs)*(P0m/(d*C1^2))*((cosd(am))^3/(cosd(a1))^2)//The drag coefficient Cl=(2*(1/cs)*cosd(am)*(tand(a1)-tand(a2)))-(Cd*tand(am))//THe lift coefficient //output printf('(a)The pressure loss coefficient is %3.4f\n(b)The drag coefficient is %3.4f\n(c)The lift coefficient is %3.3f',Cp,Cd,Cl)
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
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EXAMPLE11_9.SCE
//ANALOG AND DIGITAL COMMUNICATION //BY Dr.SANJAY SHARMA //CHAPTER 11 //Information Theory clear all; clc; printf("EXAMPLE 11.9(PAGENO 492)"); //given Px_1 = .4//probability of first symbol Px_2 = .3//probability of second symbol Px_3 = .2//probability of third symbol Px_4 = .1//probability of fourth symbol //calculations H_X = -Px_1*log2(Px_1)-Px_2*log2(Px_2)-Px_3*log2(Px_3)-Px_4*log2(Px_4);//entropy Px1x2x1x3 = Px_1*Px_2*Px_1*Px_3;//product of probabilities Ix1x2x1x3 =-log2(Px1x2x1x3);//information of four symbols Px4x3x3x2 = Px_4*Px_3*Px_3*Px_2;//product of probabilities Ix4x3x3x2 = -log2(Px4x3x3x2);//information of four symbols //results printf("\n\ni.Entorpy = %.2f bits/symbol",H_X); printf("\n\nii.Amount of information contained in x1x2x1x3 = %.2f bits/symbol",Ix1x2x1x3); printf("\nThus,Ix1x2x1x3 < 7.4[=4*H_X]bits/symbol") printf("\n\niii.Amount of information contained in x4x3x3x2 =%.2f bits/symbol",Ix4x3x3x2); printf("\nThus we conclude that\nIx4x3x3x2 > 7.4[=4*H_X]bits/symbol")
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/446/CH12/EX12.7/12_7.sce
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no_license
FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
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12_7.sce
clear clc disp('Exa-12.7'); m236Ra=226.025403; m222Rn=222.017571; m4He=4.002603;c2=931.5; //mass of various elements and c2=c^2 Q=(m236Ra-m222Rn-m4He)*c2;//Q of the reaction A=226 K=((A-4)/A)*Q; //kinetic energy printf('The kinetic energy of the alpha particle is %.3f Mev',K);
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/test/expunge.tst
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[ "BSD-3-Clause", "BSD-2-Clause" ]
permissive
dougsong/reposurgeon
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2023-02-25T08:33:06
2023-02-25T08:33:06
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2023-02-25T08:33:08
2020-07-17T01:45:32
Go
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expunge.tst
## Test file expunge operation set interactive set echo set quiet # There's a --nobranch embedded in the test load so it can be checked standalone. # This invocation would make the load work even without that. read --nobranch <expunge.svn 1..$ expunge /^releases\/v1.0\/.*/ write
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/3472/CH7/EX7.11/Example7_11.sce
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
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Example7_11.sce
// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART I : GENERATION // CHAPTER 7: TARIFFS AND ECONOMIC ASPECTS IN POWER GENERATION // EXAMPLE : 7.11 : // Page number 76 clear ; clc ; close ; // Clear the work space and console // Given data MD = 100.0*10**3 // Maximum demand(kW) capital_cost = 200.0*10**6 // Capital cost(Rs) LF = 0.4 // Annual load factor cost_fueloil = 15.0*10**6 // Annual cost of fuel and oil(Rs) cost_tax = 10.0*10**6 // Cost of taxes, wages and salaries(Rs) interest = 0.15 // Interest and depreciation // Calculations hours_year = 365.0*24 // Total hours in a year units_gen = MD*LF*hours_year // Units generated per annum(kWh) fixed_charge = interest*capital_cost // Annual fixed charges(Rs) running_charge = cost_fueloil+cost_tax // Annual running charges(Rs) annual_charge = fixed_charge+running_charge // Total annual charges(Rs) cost_unit = annual_charge*100/units_gen // Cost per unit(Paise) // Results disp("PART I - EXAMPLE : 7.11 : SOLUTION :-") printf("\nCost per unit generated = %.f paise", cost_unit)
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/tests/getDepth/test4.sce
62f54ddfcddd4ce0df2e01438bb88cb216eb9292
[]
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rg77/Scilab-Image-Processing-And-Computer-Vision-Toolbox
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8adb116da3a9c29a32e5e0727105aff571e5b374
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2020-12-02T16:14:45.282650
2017-07-07T10:12:04
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sce
test4.sce
src = imread("../images/color2.jpeg"); //reading an image gray = rgb2gray(src); //converting to grayscale depth = getDepth(gray) ; //get the depth disp(depth) ; //view the output
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/3557/CH18/EX18.1/Ex18_1.sce
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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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Ex18_1.sce
//Example 18.1// ur=1.01; u0=4*%pi*10^-7;//henry/m H=2*10^5;//amperes/m B=ur*u0*H mprintf("B = %f weber/m^2",B) //Using second equality, we obtain M=(ur-1)*(H) mprintf("\nM = %e amperes/m",M)
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/Quick Flick.sce
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Ahmad6543/Scenarios
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sce
Quick Flick.sce
Name=Quick Flick PlayerCharacters=player_char BotCharacters=QFmain.bot;QFsub.bot IsChallenge=true Timelimit=60.0 PlayerProfile=player_char AddedBots=QFmain.bot;QFsub.bot;QFsub.bot PlayerMaxLives=1 BotMaxLives=0;0;0 PlayerTeam=1 BotTeams=2;2;2 MapName=quick_flick.map MapScale=10.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=0.0 ScorePerDamage=1.0 ScorePerKill=50.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Quick Flick WeaponHeroTag=AR DifficultyTag=3 AuthorsTag=NFNT BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=false Description=Do not drop the center target. Flick the small target around. GameVersion=2.0.0.2 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 [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=QFmain DodgeProfileNames= DodgeProfileWeights= DodgeProfileMaxChangeTime=60.0 DodgeProfileMinChangeTime=60.0 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=QFmain_char SeeThroughWalls=false NoDodging=true NoAiming=false AbilityUseTimer=1.0 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.1 UseAbilityFreqMaxTime=0.1 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=QFsub 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=QFsub_char SeeThroughWalls=false NoDodging=true NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.1 UseAbilityFreqMaxTime=0.1 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=player_char MaxHealth=100.0 WeaponProfileNames=AR;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=0.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.25 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=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=QFmain_char MaxHealth=100.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 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=2.0 AirControl=0.0 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=true BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cuboid MainBBHeight=300.0 MainBBRadius=59.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=300.0 ProjBBRadius=59.0 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=QFmain_pop.abilmov;Player_kill.abilmelee;; 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=false 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=4000.0 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=QFsub_char MaxHealth=1.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 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=256.0 Gravity=0.0 AirControl=1.0 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=50.0 MainBBRadius=25.0 MainBBHasHead=false MainBBHeadRadius=8.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=50.0 ProjBBRadius=25.0 ProjBBHasHead=false ProjBBHeadRadius=8.0 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=0.2 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=128.0 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 [Weapon Profile] Name=AR Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.25 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.1 ReloadTimeFromPartial=0.1 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.001 HitSoundCooldown=0.001 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=103.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.1 IncReloadLoopTime=0.1 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.1 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=-50.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=false 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash= ParticleWallImpact= ParticleBodyImpact= ParticleProjectileTrail= ParticleHitscanTrace= ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=0.0,0.1,0.0,0.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=0.0,0.1,0.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=QFmain_pop MaxCharges=1.0 ChargeTimer=0.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.0 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=800.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=false UpVelocity=800.0 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=0.0 AIUseInCombat=false AIUseOutOfCombat=false AIUseOnGround=false AIUseInAir=true AIReuseTimer=0.1 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=0.0 AIMaxTargFOV=360.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.1 AIDamageReactionMaxDelay=0.1 AIDamageReactionCooldown=0.1 AIDamageReactionThreshold=1.0 AIDamageReactionResetTimer=0.1 [Melee Ability Profile] Name=Player_kill MaxCharges=1.0 ChargeTimer=0.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.1 HurtboxRadius=4000.0 HurtboxDamage=100.0 HurtboxGroundKnockbackFactor=0.0 HurtboxAirKnockbackFactor=0.0 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no_license
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Ex5_9.sce
//Ex:5.9 clc; clear; close; n1=1.5;// core refractive index c=3*10^8;// the speed of light m/s w=6*10^-6;// rms spectral width in m M=200;// material dispersion parameter in ps/nm/km NA=0.25;// numerical aperture w=50;// spectral width in nm L=1;// length in m rm=w*L*M;// rms pulse broadening in s/km rM=rm/10^3;// rms pulse broadening in ns/km due to material dispersion rm1=(L*1000*(NA)^2)/(4*sqrt(3)*n1*c);//rms pulse broadening in ns/km due to material dispersion in sec/m rM1=rm1*10^9;// rms pulse broadening in ns/km due to intermodel dispersion in ns/km rmt=sqrt(rM^2+rM1^2);// total rms pulse broadening in ns/km bl=0.2/(rmt*10^-9);// bandwidth length product in Hz km bL=bl/10^6;// bandwidth length product in MHz km printf("The total rms pulse broadening =%f ns/km",rmt); printf("\n The bandwidth length product =%f MHz km",bL);
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//Ex:2.24 clc; clear; close; printf("Capacitance = 150 pF of 2%% tolerance at 100 V");
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2_36.sce
//Chapter-2,Example 2_36,Page 2-54 clc() //Given Data: n=1 //order lam=5.89*10^-7 //Wavelength of light a=0.3*10^-3 //width of slit //Calculations: //We know, a*sin(theta)=n*lam theta1=asin(n*lam/a)*180/%pi //angular position in first dark band printf('Angular position in first dark band is = %.3f degrees \n \n',theta1) //We know,for bright band a*sin(theta)=(2n+1)*lam/2 theta2=asin(1.5*lam/a)*180/%pi //angular position in first bright band printf(' Angular position in first bright band is = %.3f degrees',theta2)
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Chapter7_Example4.sce
clc clear //INPUT u=1.08; cp=8.6;//specific heat in kj/kg.K j=4.2;//joules constant in j/cal p1=1*1.013*10^6;//pressure at intial in N/sq.m p2=20*1.013*10^6;//pressure at final in N/sq.m //CALCULATIONS dh=-u*cp*j*(p1-p2);//change in enthalpy in joules //OUTPUT mprintf('the change in enthalpy is %3.2fjoules',dh)
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Ex17_7.sce
//Chapter 17: Antenna Temperature, Remote Sensing and Radar Cross Section //Example 17-5.1 clc; //Variable Initialization f = 10e9 //Frequency (Hz) wind_speed = 350 //Wind speed (km/h) c = 3e8 //Speed of light (m/s) vr = 1e3 //Differential velocity (m/h) //Calculations wave_lt = c/f //Wavelength (m) freq_shift = 2*(wind_speed*1000/3600)/wave_lt //Doppler Frequency shift (Hz) T = 1/(2*freq_shift) //Pulse repetition interval (s) prf = 1/T //Pulse repetition frequency (Hz) fmin = 2*(vr/3600)/wave_lt //Frequency resolution (Hz) N = 1/((fmin)*T) //Number of pulses //Result mprintf("The minimum pulse repetition frequency is %d Hz",prf) mprintf("\nThe number of pulses to be sampled is %d", N)
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ex6_5.sce
// Exa 6.5 clc; clear; close; format('v',6) // Given data Ao = -20; Ri = 5;// in k ohm R1 = Ri;// in k ohm disp(R1,"The value of R1 in k ohm is"); // Closed loop voltage gain for inverting amplifier, Ao = -R_F/R1 or R_F = -Ao*R1;// in k ohm disp(R_F,"The value of R_F in k ohm is");
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clear; clc; disp("--------------Example 30.7----------------") p=7; q=11; n=p*q; // formula phi=(p-1)*(q-1); // formula e=13; d=1; // not actual 'd' value; it has to be computed t=1; P=5; plaintext=P; while t==1 do // compute d such that d*e = 1 mod n if(modulo(e*d,phi)== 1) t=0; else d=d+1; end end // encryption by Alice C=modulo(P^e,n); // formula printf("Alice sends the plaintext %d to Bob. She uses the public key %d to encrypt %d.\nBob receives the ciphertext %d and uses the private key %d to decipher the ciphertext.",P,e,P,C,d); // display the result // decryption by Bob P=modulo(C^d,n); // formula printf("\n\nThe plaintext %d sent by Alice is received as plaintext %d by Bob.",plaintext,plaintext); // display the result
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5_1.sce
clc //ex5.1 R=50; t=[0:0.000001:0.05]; V_t=100*cos(100*%pi*t); V_m=100; //peak value V_rms=V_m/sqrt(2); P_avg=(V_rms^2)/R; P_t=V_t^2/R; printf(" All the values in the textbook are approximated hence the values in this code differ from those of Textbook") disp(V_rms,'RMS value of voltage in volts') disp(P_avg,'average power in watts') subplot(121) plot(t*10^3,V_t); xtitle('voltage vs time','time in ms','voltage in volts') //ms-milli seconds(10^-3) subplot(122) plot(t*10^3,P_t) xtitle('power vs time','time in ms','power in watts') //ms-milli seconds(10^-3)
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//check o/p when is of type char v=['a' 'b' 'c' 'ad']; m=cummin(v); disp(m); //output // !--error 53 //cummin: Wrong type for argument #1 (A); Real or complex entries expected //at line 70 of function cummin called by : //m=cummin(v);
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ex1_9.sce
errcatch(-1,"stop");mode(2);// Example 1.9 page no-24 k=1.76*10^11 ///e/m in C/kg eps=10^4 B=0.01 Xmax=2*eps*%pi/((B^2)*k) printf("Xmax=%.3f cm",Xmax*100) exit();
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7_8.sce
clc //initialisation of variables Q= 100 //cuses V= 2 //ft/sec n= 1.5 k= 0.006 g= 32.2 //ft/sec^2 //CALCULATIONS A= Q/V d= sqrt(A/((2*sqrt(n^2+1))-n)) m= A/d mb= m-n*d bt= m+n*d m1= d/2 f= k*(1+(4/m1)) C= sqrt(2*g/f) i= V^2/(C^2*m1) //RESULTS printf ('slope %.5f ',i)
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Ex19_2.sce
//Example 19_2 clc(); clear; //To find how large is the average EMF induced b=0.5 //Units in T a=4*10^-4 //Units in meters^2 phi2=b*a //Units in Wb phi1=0 //Units in Wb deltaPHI=phi2-phi1 //Units in Wb n=100 //Units in Constant deltaT=2*10^-2 //Units in sec emf=(n*deltaPHI)/deltaT //Units in V printf("The average emf Induced is emf=%d V",emf)
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Ex12_18_3.sce
//Section-12,Example-3,Page no.-SS.33 //To calculate distance between two adjacent atoms. clc; n=4 M=23+35.5 N=6.028*10^23 D=2.18 a=((n*M)/(N*D))^0.33 //Lattice parameter(cm) R=a/(sqrt(2)) disp(R,'Distance between two adjacent atoms(cm)') //a=5.627*10^-8,R=2*r=a/sqrt(2)=3.979 *10^-8 is wrong in the book.
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mdaq_uart_write.sci
function [x,y,typ] =mdaq_uart_write(job,arg1,arg2) uart_send_desc = ["UART write"; "This block sends data using MicroDAQ UART interface."; ""; "Max data size is 512 bytes."; ""; "MODULE:"; " 0 - UART0"; " 1 - UART1"; " 2 - UART2"; ""; "Set UART Send block parameters:"]; x=[];y=[];typ=[]; select job case 'set' then x=arg1 model=arg1.model; graphics=arg1.graphics; exprs=graphics.exprs; while %t do try getversion('scilab'); [ok,module, data_size,exprs]=.. scicos_getvalue(uart_send_desc,.. ['Module:'; 'Data Size:'],.. list('vec',1,'vec',1),exprs) catch [ok,module,data_size,exprs]=.. getvalue(uart_send_desc,.. ['Module:'; 'Data Size:'],.. list('vec',1,'vec',1),exprs) end; if ~ok then break end if module > 2 | module < 0 then ok = %f; message("Use values 0,1 or 2 to set UART module."); end if data_size > 512 | data_size < 0 then ok = %f; message("Incorrect Data size. (max 512)"); end if ok then [model,graphics,ok] = check_io(model,graphics, data_size, [], 1, []); graphics.exprs = exprs; model.rpar = []; model.ipar = [module;data_size]; model.dstate = []; x.graphics = graphics; x.model = model; break end end case 'define' then module = 0; data_size = 16; model=scicos_model() model.sim=list('mdaq_uart_write_sim',5) model.in = data_size; //intyp 8 - uint8 model.intyp=8 model.out=[] model.evtin=1 model.rpar=[]; model.ipar=[module; data_size] model.dstate=[]; model.blocktype='d' model.dep_ut=[%t %f] exprs=[sci2exp(module);sci2exp(data_size)] gr_i=['xstringb(orig(1),orig(2),['''' ; ],sz(1),sz(2),''fill'');'] x=standard_define([4 3],model,exprs,gr_i) x.graphics.in_implicit=[]; x.graphics.exprs=exprs; end endfunction
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total_physical_store_count = 0 total_physical_fetch_count = 65536 <cache info> items cached: 0/1000 regions in use: 0/0 items per region: 10000 counter: 32768 temp_read_num: 65535 temp_write_num: -1 item_req_count = 65536 item_hit_count = 0 item hit ratio = 0%
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8_25.sce
v1=220 v2=110 z1=0.32+%i*0.85 z2=0.11+%i*0.27 a=v1/v2 z=z1+a*a*z2 IHV=v1/norm(z) ILV=IHV*a disp(IHV,ILV)
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clc;funcprot(0);//Example 9.16 //Initilisation of Variables l=3,b=3,h=3;....//Sides of cube in m T1=300;....//Uniform temparature of floor in K T2=200;....//Temparature of wall & ceiling in K e1=0.9;....//Emissivity of floor e2=0.6;....//Emissivity of all ceiling e3=0.5;....//Emissivity of all side walls R=5.67*10^-8;.....//Stefens boltsman constant F12=0.2;....//shape factor of the floor and ceiling //calculations F13=1-F12;....//Shape facteor of ceiling and sidewalls A1=l*b;....//Area of floor in m^2 A2=b*h;.....//Area of Ceiling m^2 A3=h*l;....//Area of sidewalls in m^2 Eb1=(R*T1^4);....//Emissive power of ceiling as per stefen boltzman law in W/m^2 Eb2=(R*T2^4); ....//Emissive power of wall as per stefen boltzman law in W/m^2 Eb3=Eb2;....//Emissive power of wall as per stefen boltzman law in W/m^2 R1=(1-e1)/(A1*e1);.....//Resistance of floor in sq m R2=(1-e2)/(A2*e2);.....//Resistance of ceiling in sq m R3=(1-e3)/(A3*e3);.....//Resistance of side walls in sq m R12=1/(A1*F12);....//Resistance of ceiling to floor in sq m R23=1/(A1*F13);....//Resistance of ceiling to sidewalls in sq m R13=1/(A1*F13);....//Resistance of floor to side walls in sq m Q12=(Eb1-Eb2)/(R1+R12+R2);.....//Rate of heat transfer from ceiling to floor and walls in kW Q13=(Eb1-Eb2)/(R1+R13+R3);.....//Rate of heat transfer from ceiling to floor and walls in kW disp(Q12,"Rate of heat transfer to ceiling in kW:") disp(Q13,"Rate of heat transfer to sidewalls in kW:") Rtoti=R1+(1/(((1/R12)+(1/(R13+R23)))))+R2;....//Equalent resistance Q13i=(Eb1-Eb2)/Rtoti;......//Heat transfer through cieling in W disp(Q13i,"Heat transfer through side walls if they are insulated in W") a1=((1/R1)+(1/R12)+(1/R13));...// c1=((Eb1/R1)+(Eb3/R13));...// a2=1/R12;...// b1=-1/R12;...// b2=-((1/R2)+(1/R23)+(1/R12));...// c2=-(Eb2/R2)-(Eb3/R23);...// A=[a1,b1;a2,b2];...// C=[c1;c2];....// disp(inv(A)*C,"the radiocities when the walls are insulated in W/m^2")
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function[sol,niter,info]= myjacobi(A,b,nmaxit,tol) //vérification si aucun terme de la diagonal de A n'est nulle if ~and(diag(A)) then error('erreur:diagonale est nulle') end //décomposition de A: A=D-E-F D=diag(diag(A)) E=-triu(A)+D F=-tril(A)+D x=inv(A)*b sol=b niter=0 info=0 err=[] for k=1:nmaxit sol =(eye(n,n)-inv(D)*A)*sol+inv(D)*b err=[err,norm(x-sol)]; if max(abs(A*sol-b))< tol info = 1; niter= k; break end end xtitle('le graphe de convergence pour la méthode de jacobi') plot(1:niter,log(err),xtitle) endfunction n=3 A=[2 -1 0;-1 2 -1;0 -1 2] b=[1; 2; 3] [sol,niter,info]= myjacobi(A,b,100,0.01) x=inv(A)*b b=A*x; x=inv(A)*b M=eye(n,n)-(inv(diag(diag(A)))*A); R_spectral=max(abs(spec(M))); disp(R_spectral)
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//chapter 3 //example 3.14 //page 101 printf("\n") printf("given") Edc=20;vo=.24;Vo=20;Il=40*10^-3;fr=120; Eomax=(3.14*Edc)/2 Epeak=(4*Eomax)/(3*3.14) vi=Epeak; Rl=Vo/Il Xlc=(2*Rl)/3 Lc=Xlc/(2*3.14*fr) L=1.25*Lc; Xl=2*3.14*fr*L Xc=Xl/((vi/vo)+1) C1=1/(2*3.14*fr*Xc)
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//Caption: Poisson distribution //Example6.4 //Page179 clear; clc; //(a): Exactly 0 customer will arrive in 10 minutes interval X1= 0; //no. of customer Mean = 4;//mean arrival rate of 4 per 10 minutes [P1,Q1]=cdfpoi("PQ",X1,Mean) disp(P1,'Exactly 0 customer will arrive P(X=0,4) is =') //(b): Exactly 2 customers will arrive in 10 minutes interval X2 =2; //no. of customer P2 = exp(-Mean)*(Mean^X2)/(factorial(2)) disp(P2,'Exactly 2 customer will arrive P(X=2,4) is =') //(c): at most 2 customers will arrive in 10 minutes interval [P3,Q3]=cdfpoi("PQ",X2,Mean) disp(P3,'Atmost 2 customer will arrive P(X<=2,4) is =') //(d): at least 3 customers will arrive in 10 minutes interval X3 =3; P4 = 1-P3 disp(P4,'At least 3 customer will arrive P(X>=3,4) is=') //Result //Exactly 0 customer will arrive P(X=0,4) is = // // 0.0183156 // // Exactly 2 customer will arrive P(X=2,4) is = // // 0.1465251 // // Atmost 2 customer will arrive P(X<=2,4) is = // // 0.2381033 // // At least 3 customer will arrive P(X>=3,4) is= // // 0.7618967
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//Exa 9.4 clc; clear; close; //Given data : Vs=20;//kV n=3;//no. of uniits K=0.1;//shunt to mutual capacitance ratio V3=Vs;//kV V1=V3/(1+3*K+K^2);//kV disp(V1,"Voltage across top most unit(kV)"); V2=V1*(1+K);//kV disp(V2,"Voltage across middle unit(kV)"); V=V1+V2+V3;//kV Strinf_eff=V/n/V3; disp(Strinf_eff*100,"Percentage String Efficiency(%)");
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clear; clc; disp("Example 8.2"); function[]=stringtoint() num= ascii("scilab"); disp("displayin ascii codes of alphabets="); disp(num); // converting strings into unique non-negative integer and suming these unique integers. z=sum(num); disp("displayin sum of these integers"); disp(z); endfunction stringtoint()
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//Exercise 1.1Example 1.1.7 //TO Convert Binary To Ternary function[t]=bin_ter(a) b=0 b=base2dec(a,2); disp(b); [j,i]=size(a); t=[]; while(b~=0) m=modulo(b,3); t=[t(:,:) m]; b=b/3; b=b-modulo(b,10); end disp(t,"Ternary Equivalent"); endfunction //Calling Routine: a="100101101110" disp(a,"input string is"); b=bin_ter(a)
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clear μ = 0.03 k = (1/6)*10^4 β = 10^-5 δ = 1 n = 101 function f = f(M) f1 = α.*M./(M+k) f2 = 1./(1+β*n*M) f = f1.*f2 endfunction function g = g(M,γ) g = γ.*M endfunction function eqn = eqnM1(M,γ,α)//1 cohort eqn = (α*k-α*β*n*M.^2-(γ+μ)*(1+β*n*M).^2.*(M+k).^2)./((1+β*n*M).^2.*(M+k).^2) endfunction function eqn = eqnM2(M,γ,α)//2 cohort eqn = α*k/((1+β*n*M).*(M+k).^2)-μ-γ endfunction function i = termintegral(s,M,γ,α) i = exp(-(γ+μ)*s)*α*k/((1+β*n*M*exp(-γ*s))*(M*exp(-γ*s)+k)^2) endfunction function l = lambda(tau,m,γ,α) l = 1-intg(0,tau,list(termintegral,m,γ,μ)) endfunction scf() i=0 for γ = 0.0001:0.001:0.1 i=i+1 α = 2*10^3 Metoileγ(i) = fsolve(0,list(eqnM2,γ,α)) τetoileγ(i) = fsolve(0,list(lambda,Metoileγ(i),γ,α)) end j=0 for α = 500:50:3500 j=j+1 γ = 0.06 Metoileμ(j) = fsolve(0,list(eqnM2,γ,α)) τetoileμ(j) = fsolve(0,list(lambda,Metoileμ(j),γ,α)) end γ = 0.0001:0.001:0.1 α = 500:50:3500 subplot(221) plot2d(γ ,τetoileγ,color("blue")) xlabel('$γ$','fontsize',3) legend("$τ*$",-1, %f) xgrid() subplot(222) plot2d(γ ,Metoileγ,color("red")) xlabel('$γ$','fontsize',3) legend("$M*$",-1, %f) xgrid() subplot(223) plot2d(α,τetoileμ,color("blue")) xlabel('$α$','fontsize',3) legend("$τ*$",-1, %f) xgrid() subplot(224) plot2d(α,Metoileμ,color("red")) xlabel('$α$','fontsize',3) legend("$M*$",-1, %f) xgrid() scf() j=0 for α = 1000:1000:10000 // for γ = 0.0001:0.0025:0.1 j=j+1 Metoileαγ(j) = fsolve(0,list(eqnM2,γ,α)) τetoileαγ(j) = fsolve(0,list(lambda,Metoileαγ(j),γ,α)) plot(Metoileαγ(j),τetoileαγ(j),'k.') end end //plot(Metoileαγ,τetoileαγ,'k.') ylabel('$τ*$','fontsize',4) xlabel('$M*$','fontsize',4) //MOINDRES CARRES - quadratique function y = model(t, x) y = x(1)*t+x(2) //forme quadratique endfunction y = τetoileαγ t = Metoileαγ // we want to find the parameters x such that // minimize $f(x) = \sum_{i=1}^N ( f(t_i,x) - y_i )^2$ function e = aminimiser(x,t, y) e = model(t, x) - y endfunction x0 = [1;1];//CI [f,xopt] = leastsq(list(aminimiser,t,y),x0) tradeoff_M = linspace(1000,7000,5001)'; tradeoff_τ = model(tradeoff_M, xopt); plot(tradeoff_M,tradeoff_τ, 'b-','thickness',3) legend(["$0.01<γ<0.1\\ 1000<α<10000$";"$f(x)$"] ,-1, %f) title('$Moindres\ Carrés:minimiser\ f(x) = \sum_{i=1}^N ( f(t_i,x) - y_i )^2$') save("C:\Users\Julien Guégan\Documents\Cours\MAM4\STAGE\2 cohorts\Tfini\Trade-Off\tradeoff_save2",'tradeoff_τ','tradeoff_M','Metoileαγ','τetoileαγ')
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// Exa 4.11 clc; clear; close; // Given data Vrms= 10;// in mV f= 2*10^3;// in kHz C= 2*10^-6;// in F R= 50*10^3;// in ohm SF= -1/(C*R);// scale factor //Vout= -1/(R*C)*sqrt(2)*Vrms*integrate('sind(2*%pi*f*t)','t',0,t);// in mV //Vout= 1/(R*C)*sqrt(2)*Vrms/(2*%pi*f)*(cos(4000*t)-1);// in mV V= 1/(R*C)*sqrt(2)*Vrms/(2*%pi*f);// (assumed) disp("Output voltage in mV is : "+string(V)+"*(cos(4000 *t)-1)) mV")
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//============================================================================ // chapter 5 example 1 clc; clear; //input data d = 2*10^-3; //diameter in m I = 5*10^-3; //current in A e = 1.6*10^-19; //charge of electron in coulombs a = 3.61*10^-10; //side of cube in m N = 4; //number of atoms in per unit cell //formula //J=n*v*e //calculation r = d/2; //radius in m n = N/(a^3); //number of atoms per unit volume in atoms/m^3 A = %pi*(r^2); //area in m^2 J = I/A; //current density in Amp/m^2 v = J/(n*e); //average drift velocity in m/s //result mprintf('velocity=%3.2e.m/s\n',v); //=============================================================================
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//EX13_15 PG-13.10 clc clear printf("conversion of binary no 1101.1 to its decimal equivalent =") N=(1*2^3)+(1*2^2)+(0*2^1)+(1*2^0)+(1*2^(-1)); printf(" %.1f",N)
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style.fontSize=14; style.displayedLabel="<table> <tr><td align=center><b>IO Buf A</b><br>%2$s</td></tr></table>"; pal4 = xcosPalAddBlock(pal4,"pad_ina",[],style); //input pad analog buffered
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//COMO USAR: //A=[x0 x1 x2 ... xN] //B=[y0 y1 y2 ... yN] //N=grado del polinomio //difdiv(A,B,N) //Grafico f(x) //x=-10:0.1:10; //plot2d(x, f(x)); //xgrid(3,1,7); //muestra grilla function difdiv(X,Y,N) // x, y=f(x), N=grado(P(x)) for i=1:N for j=N+1:-1:i+1 Y(j)=(Y(j)-Y(j-1))/(X(j)-X(j-i)) if (i-1)==0 printf("\nf[x%d,x%d]=%12.9f",i-1,j-1,Y(j)); end end end printf("\nf[x0]=%12.9f",Y(1)); endfunction
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// Exa 6.32 clc; clear; close; // Given data P1 = 15;// in bar P2 = 0.15;// in bar T_sat = 198.3;// in degree C T_sat = T_sat + 273;// in K h_fg1 = 1947;// in kJ/kg h_fg2= 2369;// in kJ/kg h_g1 = 845;// in kJ/kg h_f2 = 232;// in kJ/kg f_g2 = 7.985;// in kJ/kg-K x1 = 0.8; Phi_f1 = 2.315;// in kJ/kg-K Phi_f2 = 0.772;// in kJ/kg-K Phi1 = Phi_f1 + ((x1*h_fg1)/T_sat);// in kJ/kg-K H1 = h_g1 + (x1*h_fg1);// in kJ/kg-K Phi2 = Phi1;// in kJ/kg-K x2 = (Phi1 - Phi_f2)/(f_g2 - Phi_f2); H2 = h_f2 + (x2*h_fg2);// in kJ/kg Eta = ((H1-H2)/(H1-h_f2))*100;// in % disp("Part (i) When the steam supply is wet and dryness fraction is 0.8") disp(Eta,"Rankine efficiency in % is"); delH = H1-H2;//theoretical work of steam in kJ/kg W = delH*60/100;// in kJ/kg Energy_Equivalent= 3600;// in kJ Steam_C = Energy_Equivalent/W;// Steam consumption in kg disp(Steam_C,"Steam consumption per kW-hr in kg is :") disp("Part (ii) When the steam supply is dry and saturated") H_1 = 2792;// in kJ/kg Phi_g1 = 6.445;// in kJ/kg-K x_2 = (Phi_g1-Phi_f2)/(f_g2-Phi_f2); H_2 = h_f2 + (x_2*h_fg2);// in kJ/kg Eta1 = (H_1-H_2)/(H_1-h_f2); disp("Rankine efficiency is "+string(Eta1)+" or "+string(Eta1*100)+" %"); W1 = (H_1-H_2)*60/100;// in kJ/kg Steam_C= Energy_Equivalent/W1;// in kg disp(Steam_C,"Steam consumption per kW-hr in kg is :") disp("Part (iii) When steam is superheated and temperature is 300°C") H_1 = 3039;// in kJ/kg Phi_1 = 6.919;// in kJ/kg-K x_2 = (Phi_1 - Phi_f2)/(f_g2-Phi_f2); H_2 = h_f2 + (x_2 * h_fg2);// in kJ/kg Eta = (H_1 - H_2)/(H_1-h_f2); disp("Rankine efficiency is "+string(Eta)+" or "+string(Eta*100)+" %"); W2 = (H_1-H_2)*60/100;// in kJ/kg Steam_C= Energy_Equivalent/W2;// in kg disp(Steam_C,"Steam consumption per kW-hr in kg is :")
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function [x, sflag] = gflineq(a, b, p) // GFLINEQ finds a solution for linear equation Ax = b over a prime Galois field. // [X, SFLAG] = GFLINEQ(A, B) returns a particular solution (X) of AX=B in GF(2). // If the equation has no solution, then X is empty and SFLAG = 0 else SFLAG = 1. // // [X, SFLAG]= GFLINEQ(A, B, P) returns a particular solution of the linear // equation A X = B in GF(P) and SFLAG=1. // If the equation has no solution, then X is empty and SFLAG = 0. // // Written by POLA LAKSHMI PRIYANKA, FOSSEE, IIT BOMBAY // // Check number of input arguments [out_a,inp_a]=argn(0) if inp_a >3 | out_a> 2 | inp_a <2 then error('comm:gflineq: Invalid number of arguments') end // Error checking . if inp_a < 3 p = 2; elseif ( isempty(p) | length(p)~=1 | abs(p)~=p | ceil(p)~=p | length(factor(p))~=1 ) error('comm:gflineq:Input argument 3 must be a positive prime integer.'); end; [row_a, col_a] = size(a); [row_b, col_b] = size(b); // Error checking - A & B. if ( isempty(a) | ndims(a) > 2 ) error('comm:gflineq:Input argument 1 must be a two-dimensional matrix.'); end if ( isempty(b) | ndims(b) > 2 | col_b > 1 ) error('comm:gflineq:Invalid dimensions of input argument 2 .'); end if ( row_a ~= row_b ) error('comm:gflineq:Dimensions of A and B are not compatible'); end if (( or( abs(a)~=a | floor(a)~=a | a>=p )) | ( or( abs(b)~=b | floor(b)~=b | b>=p )) ) error('comm:gflineq:Elements of input matrices should be integers between 0 and P-1.'); end // Solution is found by using row reduction (Reducing it to echelon form) ab = [a b]; // Composite matrix [row_ab, col_ab] = size(ab); row_i = 1; col_i = 1; row = []; col = []; while (row_i <= row_ab) & (col_i < col_ab) // Search for a non zero element in current column while (ab(row_i,col_i) == 0) & (col_i < col_ab) idx = find( ab(row_i:row_ab, col_i) ~= 0 ); if isempty(idx) col_i = col_i + 1; // No non zero element else // Swap the current row with a row containing a non zero element // (preferably with the row with value 1). idx = [ find(ab(row_i:row_ab, col_i) == 1) idx ]; idx = idx(1); temp_row = ab(row_i,:) ab(row_i,:) = ab(row_i+idx-1,:) ab(row_i+idx-1,:) = temp_row end end if ( ( ab(row_i,col_i) ~= 0 ) & ( col_i < col_ab ) ) // Set major element to 1. if (ab(row_i,col_i) ~= 1) ab(row_i,:) = pmodulo( field_inv( ab(row_i,col_i),p ) * ab(row_i,:), p ); end // The current element is a major element. row = [row row_i]; col = [col col_i]; // Find the other elements in the column that must be cleared, idx = find(ab(:,col_i)~=0); for i = idx if i ~= row_i ab(i,:) = pmodulo( ab(i,:) + ab(row_i,:) * (p - ab(i,col_i)), p ); end end col_i = col_i + 1; end row_i = row_i + 1; end if ( rank(ab) > rank( ab(:,1:col_a) ) ) disp('comm:gflineq:Solution does not exist'); x = []; sflag = 0; else x = zeros(col_a, 1); x(col,1) = ab(row,col_ab); sflag = 1; end endfunction function [x] = field_inv(a,n) t = 0; newt = 1; r = n; newr = a; while newr ~= 0 quotient = floor(r / newr); temp = t; t = newt; newt = temp -quotient*newt; temp = r; r = newr; newr = temp - quotient*newr; end if r>1 [x c] = find( pmodulo( (1:(p-1)).' * (1:(p-1)) , p ) == 1 ); end if t<0 t = t + n; end x = t; endfunction
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clc //variable Initialisation Vl=440//Voltage Input in Volts f1=50//supply frequency in Hz P=25e+3//power rating in Watts N1=950//Rotor Speed in rpm Z=0.1+(%i*3)//Rotor Impedance pole=6//No of poles f2=80//Supply 2 frequency in Hz //Solution V=Vl/sqrt(3)//Phase Voltage in Volts Wm=2*%pi*N1/60 Tfl=P/Wm//Full load Torque in N-m Ns=120*f2/pole Ws=2*%pi*Ns/60 Z2=Z*(f2/f1)//Rotor Impedance at 80 Hz S=3*(V^2)*0.5/(Ws*((abs(Z2))^2)*Tfl) Nr=Ns*(1-S) Rl=real(Z) Xl=imag(Z2) Smax=(Rl/Xl) Tmax=3*(V^2)/(Ws*2*Xl) printf('\n\n The Motor speed=%0.1f rpm\n\n',Nr)//The answers vary due to round off error printf('\n\n The Slip at which maximum torque occurs=%0.1f\n\n',Smax) printf('\n\n The maximum Torque=%0.1f\n\n',Tmax)
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s=%s;//find transfer function of the given system A =[-2 -1;-3 -2]; B =[3;4]; x =[2 1]; [r c]= size (A) p=s*eye(r,c)-A // s*I-A q=inv(p) c=x*q*B; disp(c,"required transfer function =")
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// Chapter 3 example 16 //------------------------------------------------------------------------------ clc; clear; // Given data a = 7.2 ; // width of waveguide in cm b = 3.4; // narrow dimension of waveguide in cm c = 3*10^10; // free space velocity of EM wave in cm/s f = 2.4*10^9; // frequency in Hz // Calculation lamda = c/f // free space wavelength in cm lamda_c = 2*a // cutoff wavelength in cm lamda_g = lamda/sqrt(1 - (lamda/lamda_c)^2); // guide wavelength in cm vp = (lamda_g * c)/lamda // phase velocity in cm/s vg = c^2/vp; // group velocity in cm/s // Output mprintf('Group velocity = %3.1e cm/s\n Phase Velocity = %3.1e cm/s',vg,vp); //------------------------------------------------------------------------------
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P4_16.sce
//EXAMPLE 4.16 //Design analog butterworth High pass filter clc; clear; wp=4000; ws=1000; ap=0.1; as=40; Ap=1; // assumption As=(2*%pi*wp)*Ap/(2*%pi*ws); N=ceil(log10(sqrt((10^(0.1* as)-1)/(10^(0.1*ap)-1)))/log10(As/Ap)); disp(N,'order of the filter is :'); Ac = As/((10^(0.1*as)-1)^(1/(N*2))); disp(Ac,'cutoff frequency = ') //[hs,pole,zero,gain]=analpf(N,'butt',Ac); s=%s; hs=1/((s + 1)*(s^2 + 0.61803*s + 1)*(s^2 + 1.61803*s + 1)); Hs=horner(hs,s/Ac); H1 = numer(Hs)/0.0976514; H2 = denom(Hs)/0.0976514; disp(H1/H2,'the low pass transfer function is,HLP(s) = '); Hs=horner(hs,Ac/s); H1 = numer(Hs); H2 = denom(Hs); disp(H1/H2,'the High pass transfer function is,HHP(s) = ');
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language Spanish $thermo = VirtualMaterials.Advanced_Peng-Robinson . -> $thermo cd thermo /thermo + PROPANE ISOBUTANE n-BUTANE language Portuguese /thermo - ISOBUTANE n-BUTANE /thermo + ETHANE ISOBUTANE language French /thermo + n-BUTANE ISOPENTANE cd $ cd $ thermo2 = VirtualMaterials.RK cd thermo2 $thermo2 + PROPANE ISOBUTANE n-BUTANE language Malay $thermo2 - ISOBUTANE cd / language Spanish stream = Stream.Stream_Material() cd stream language Malay /stream.In.T = 20 /stream.In.P = 101 cd /stream.In.Fraction /stream.In.Fraction = 0.0 2 3 0.0 0.0 cd / language Portuguese mix = Mixer.Mixer() cd mix /mix.In0 -> /stream.Out language English
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EX6_16.sce
// Exa 6.16 format('v',5) clc; clear; close; // Given data R_B= 10*10^3;// in Ω R_C= 5*10^3;// in Ω R_E= 10*10^3;// in Ω Beta=50; V_CC= 20;// in V V_EE= 20;// in V V_BE= 0.7;// in V V_E= -V_BE;// in V // The value of I_E1, I_E1= (V_EE-V_BE)/(R_E+R_B/Beta);// in A I_C1= I_E1;// in A V_C= V_CC-I_C1*R_C;// in V V_CE1= V_C-V_E;// in V Beta= 100; V_BE= 0.6;// in V V_E= -V_BE;// in V // The value of I_E2, I_E2= (V_EE-V_BE)/(R_E+R_B/Beta);// in A I_C2= I_E2;// in A V_C= V_CC-I_C2*R_C;// in V V_CE2= V_C-V_E;// in V // The change in collector current delta_IC= (I_C2-I_C1)/I_C1*100;// in % // The change in collector to emitter voltage delta_V_CE= (V_CE1-V_CE2)/V_CE1*100;// in % disp(delta_IC,"The change in collector current in % is : ") disp(delta_V_CE,"The change in collector to emitter voltage in % is : ")
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// Chapter 4 Example 4// clc clear // total load the consumer=tl,power factor=pf1// tl=20;// in kW// pf1=0.8; // angle of power factor=a1// a1=acosd(pf1);// in degrees// pf2=0.95;// new power factor=pf2// a2=acosd(pf2); //original reactive power=r1,reactive power with power factor pf2=r2// r1=tl/pf1; r2=tl/pf2; // rating of the capacitor required to raise the power factor=c// c=r1*sind(a1)-r2*sind(a2); printf("\n Rating of the capacitor = %.2f kVAr\n",c); // power factor of the phase advancing device=pf3// pf3=0.1; a3=acosd(pf3); a=a1-a2; b=58.87;// in degrees// c=102.45; // rating of the device=r// r=r1*sind(a)/sind(c); printf("\n Rating of the device = %.2f kVA\n",r);
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// chapter 8 // example 8.27 // Determine range of duty cycle, peak-to-peak choke ripple current and average supply current // page-523-524 clear; clc; // given Edc=24; // in V (dc source) f=50; // in KHz (switching frequency) L=500; // in uH E0=15; // in V (average output voltage) Edc_max=26; // in V (maximum voltage of dc source) Edc_min=21; // in V (maximum voltage of dc source) I0=2; // in A (average load current) // calculate f=f*1E3; // changing unit from KHz to Hz L=L*1E-6; // changing unit from uH to H // since E0=Edc*alpha/(1-alpha), therefore we get alpha_max=1/((Edc_min/E0)+1); // calculation of upper limit of duty cycle alpha_min=1/((Edc_max/E0)+1); // calculation of lower limit of duty cycle alpha_normal=1/((Edc/E0)+1); // calculation of normal duty cycle del_I=Edc*alpha_normal/(f*L); // calculation of peak-to-peak choke ripple current // since Edc*Is=E0*I0, therefore we get Is=E0*I0/Edc; // calculation of average supply current printf("\nThe duty cycle varies from \t\t\t\t\t\t %.3f to %.3f",alpha_min,alpha_max); printf("\nThe peak-to-peak choke ripple current for normal supply voltage is \t del_I=%.1f mA",del_I*1E3); printf("\nThe average supply current drawn from battery is \t\t\t Is=%.2f A",Is); // Note: the answers vary slightly due to precise calculation
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// Example 4.6.2 clc; clear; beta_c=7d-11; //isothermal compressibility n=1.46; //refractive index P=0.29; //photoelastic constat k=1.38d-23; //Boltzmnn constant T=1400; //temperature L=1000; //length lamda=0.7d-6; //wavelength gamma_r = 8*(3.14^3)*(P^2)*(n^8)*beta_c*k*T/(3*(lamda^4)); //computing coefficient attenuation=%e^(-gamma_r*L); //computing attenuation gamma_r=gamma_r*1000; printf("\nRaleigh Scattering corfficient is %.3f * 10^-3 per meter\n",gamma_r); printf("\nNOTE - in quetion they have asked for attenuation but in solution they have not calcualted\n"); printf("\nAttenuation due to Rayleigh scattering is %.3f",attenuation); //answer for Raleigh Scattering corfficient in the book is given as 0.804d-3, deviation of 0.003d-3
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printf("closed loop transfer function =16/(s^2+(4+16*K)*s+16)"); printf("characterstic equation of the given system is 4+16*K)*s+16=0"); printf("compare it with the standard second order characterstic equation s^2+2*d*w*s+w^2=0"); w=sqrt(16); d=0.8;//given k=(2*d*w-4)/16; mo=exp((-%pi*d)/sqrt(1-d^2))*100; disp(k,"value of K="); disp(mo,"maximum overshoot(in %)");
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clc // Given that mu = 1.33 // refractive index of water // Sample Problem 3 on page no. 214 printf("\n # PROBLEM 3 # \n") p = atan(mu)*180/%pi // Polarization angle printf("Standard formula used \n mu=tan(Ip)\n") printf("\n Polarization angle of water is %d degree",p)
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// chapter 7 example 17 //----------------------------------------------------------------------------- clc; clear; // Data is taken from Example 17. The beam steers towards left of the axis with all parameters remaining in Ex 17 are same c = 3*10^8; // velocity of EM waves in m/s f = 2.5*10^9; // operating frequency in Ghz S = 10*10^-2; // inter element spacing theta = -10; // steering angle // Calculations lamda = c/f // Wavelength in m phi = (360*S/lamda)*sin(theta*%pi/180) phi1 = 0*phi // phase angle for element 1 phi2 = 1*phi // phase angle for element 2 phi3 = 2*phi // phase angle for element 3 phi4 = 3*phi // phase angle for element 4 phi5 = 4*phi // phase angle for element 5 // Output mprintf('Phase angles for elements 1,2,3,4,5 are %d°, %d°, %d°, %d°, %d°',phi1,phi2,phi3,phi4,phi5); //------------------------------------------------------------------------------
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clc //initialisation of variables h1= 3892.2 //kJ/kg h2= 4102.2 //kJ/kg dh= 1015.4 //kJ/kg dh1= 448 //kJ/kg h3= 2151.1 //kJ/kg h4= 3081.1 //kJ/kg //RESULTS printf (' Specific Enthalpy= %.1f kJ/kg',h1) printf (' \n Specific Enthalpy= %.1f kJ/kg',h2) printf (' \n Specific Enthalpy= %.1f kJ/kg',h3) printf (' \n Specific Enthalpy= %.1f kJ/kg',h4) printf (' \n Enthalpy difference= %.f kJ/kg',dh) printf (' \n Enthalpy difference= %.f kJ/kg',dh1)
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EX26_24a.sce
//EXAMPLE 26.24(a) //SHUNT GENERATOR clc; funcprot(0); //Variable Initialisation V=250;..............................//Terminal voltage in Volts I=195;..............................//Load current in Amperes Ra=0.02;...........................//Armature resistance in Ohms Rsh=50;.............................//Shunt field resistance in Ohms Lif=950;............................//Iron and friction losses in Watts Ish=V/Rsh;...........//Shunt field current in Amperes Ia=I+Ish;................//Armature current in Amperes Va=Ia*Ra;................//Armature voltage drop in Volts E=V+Va;................//Generated EMF in Volts disp(E,"(a).Generated EMF in Volts:") Lacu=(Ra*Ia^2);.......//Armature copper loss in Watts Lshu=(V*Ish);.........//Shunt copper loss in Watts Lcu=Lacu+Lshu;...........//Total copper loss in Watts disp(Lcu,"(b).Total copper loss in Watts"); L=Lif+Lcu;................//Total losses in Watts Po=V*I;....................//Output power in Watts Pin=Po+L;..................//Output of prime mover in Watts disp(Pin,"(c).Output of prime mover in Watts:"); Pa=Pin-Lif;.................//Power produced in armature in Watts effm=(Pa/Pin)*100;.........//Mechanical efficiency in Percentage y=round(effm*10)/10;......//Rounding of decimal places disp(y,"(d).Mechanical efficiency in Percentage:"); effe=Po*100/(Po+Lcu);......//Electrical efficiency in Percentage y1=round(effe*10)/10;.......//Rounding of decimal places disp(y1,"Electrical efficiency in Percentage:"); effc=(Po*100/Pin);..........//Commercial efficiency in Percentage y2=round(effc*10)/10;........//Rounding of decimal places disp(y2,"Commercial efficiency in Percentage:");
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//Variable declaration: //From example 19.5: Q = -4435.2 //Heat rate with insulation (W) R2 = 0.00198 //Convection thermal resistance ( C/W) T3 = 26 //Surrounding air temperature ( C) h = 21 //Convective heat transfer coefficient between the air and the surface (W/m^2.K) k = 0.0433 //Thermal conductivity of cork board insulation (W/m.K) L = 0.00825 //Required insulation thickness (m) //Calculation: T2 = T3+Q*R2 //Interface temperature ( C) (part 1) Bi = h*L/k //Biot number (part 2) //Result: printf("1. The interface temperature is : %.2f C .",T2) printf("2. The Biot number is : %.0f ",Bi) printf("3. Theoretical part.")
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//check o/p when i/p is a vector containing imaginary values a = [%i 0.6149 0.9899 0.0000 0.0031 -0.0082]; lsf = poly2lsf(a); disp(lsf); ////output //!--error 10000 //Line spectral frequencies are not defined for complex polynomials. //at line 31 of function poly2lsf called by : //lsf = poly2lsf(a); //at line 3 of exec file called by : //Test/poly2lsf/poly2lsf3.sce', -1
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//chapter 18 //example 18.3 //page 765 printf("\n") printf("given") I4=1*10^-3;Vb2=9.8; disp(" for Vo=11V moving contact at top of R5") Vo=11; R3=(Vo-Vb2)/I4 R=Vb2/I4//R=R4+R5 disp(" for Vo=13V moving contact at bottom of R5") Vo=13; I4=Vo/(R3+R) R4=Vb2/I4 R5=R-R4
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/* Questionaire created by optica toolkit Date: Tue Mar 04 15:57:30 1997 */ question(1, 'item 6-1', 'Op welke afstand van de rechtse lens komen de lichtstralen van een divergerende lichtbundel samen?', [ 'afstand A', 'afstand B', 'afstand C', 'weet niet' ], state(state, '', [ l1 = lamp3(switch(false), angle(0), divergence(5), pos_x(0), pos_y(0)), m19 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(9.9), show_gauge(true), instrument_name(lens)), m20 = lens(label(''), radius(5), thickness(0.1), focal_distance(-5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(4.95), show_gauge(true), instrument_name(lens)), d16 = ruler(from(m19), to(m20), pos_y(6.1)), d17 = ruler(from(m20), to(centerline), pos_y(5.85)), c6 = construction_line(pos_x(14.9), instrument_name(consline)), c7 = construction_line(pos_x(19.9), instrument_name(consline)), c8 = construction_line(pos_x(24.9), instrument_name(consline)), d18 = ruler(from(m19), to(c6), pos_y(7), varname('A')), d19 = ruler(from(m19), to(c7), pos_y(6.35), varname('B')), d20 = ruler(from(m19), to(c8), pos_y(5.7), varname('C')) ])). question(2, 'item 6-2', 'Als je de lampjes aanzet hebben ze drie evenwijdige lichtstralen. Op welke afstand van de rechtse lens komen ze samen?', [ 'afstand A', 'afstand B', 'afstand C', 'weet niet' ], state(state, '', [ l1 = parlamp(switch(false), angle(0), separation(1), pos_x(0), pos_y(0), instrument_name(parlamp)), m1 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(15), show_gauge(true), instrument_name(lens)), m2 = lens(label(''), radius(5), thickness(0.1), focal_distance(-5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(10), show_gauge(true), instrument_name(lens)), c1 = construction_line(pos_x(0), instrument_name(consline)), c2 = construction_line(pos_x(19.95), instrument_name(consline)), c3 = construction_line(pos_x(24.95), instrument_name(consline)), c4 = construction_line(pos_x(29.95), instrument_name(consline)), d1 = ruler(from(c1), to(m2), pos_y(6.3)), d2 = ruler(from(m2), to(m1), pos_y(6.85)), d3 = ruler(from(m1), to(c2), pos_y(6.2), varname('A')), d6 = ruler(from(m1), to(c3), pos_y(5), varname('B')), d7 = ruler(from(m1), to(c4), pos_y(3.75), varname('C')) ])). question(3, 'item 6-3', 'De drie lampjes hebben een parallelle lichtbundel.. Hoe lopen de lichtstralen rechts van de rechtse lens?', [ 'van elkaar af', evenwijdig, 'naar elkaar toe' ], state(state, '', [ m1 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(10), show_gauge(true), instrument_name(lens)), m2 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(20), show_gauge(true), instrument_name(lens)), l1 = parlamp(switch(false), angle(0), separation(1), pos_x(0), pos_y(0), instrument_name(parlamp)), d1 = ruler(from(m2), to(m1), pos_y(6.7)), c1 = construction_line(pos_x(0), instrument_name(consline)), d2 = ruler(from(m1), to(c1), pos_y(6.35)) ])).
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clc; close(); clear(); //page no 480 //prob no. 14.7; Rin=50 //ohm Rout=50; //ohm Vrms=400; //V Zin=Rin; mprintf('(a)The input impedance is, Zin = %i ohm\n',Zin); Irms=Vrms/(Rin+Rout); //A mprintf(' (b)The rms current , Irms = %i A \n',Irms); Pin=Irms^2*Rin; mprintf(' (c)The input power is, Pin = %i W \n',Pin); Pl=Pin; mprintf(' (d)The load power is, Pl = %i W \n',Pl);
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clc clear //Input data r=1.4;//Air standard ratio p1=1.25;//Cut off ratio 1 p2=1.50;//Cut off ratio 2 p3=2.00;//Cut off ratio 3 rc=16;//Compression ratio //Calculations n1=(1-((1/rc^(r-1)*(p1^r-1)/(r*(p1-1)))))*100;//Thermal efficiency of the diesel cycle for cut off ratio 1.25 n2=(1-((1/rc^(r-1)*(p2^r-1)/(r*(p2-1)))))*100;//Thermal efficiency of the diesel cycle for cut off ratio 1.50 n3=(1-((1/rc^(r-1)*(p3^r-1)/(r*(p3-1)))))*100;//Thermal efficiency of the diesel cycle for cut off ratio 2.00 //Output printf('(a)Thermal efficiency when cut off ratio is 1.25 is %3.2f percent\n (b)Thermal efficiency when cut off ratio is 1.50 is %3.0f percent\n (c)Thermal efficiency when cut off ratio is 2.00 is %3.1f percent\n',n1,n2,n3)
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load Computer.hdl, output-file ComputerAdd.out, compare-to ComputerAdd.cmp, output-list time%S1.4.1 ARegister[0]%D1.7.1 DRegister[0]%D1.7.1 PC[]%D0.4.0 RAM16K[16]%D1.7.1 RAM16K[17]%D1.7.1 RAM16K[18]%D1.7.1 RAM16K[19]%D1.7.1; // Load a program written in the Hack machine language. ROM32K load add.hack, output; //setting a, b, c set RAM16K[16] 9, set RAM16K[17] 3, set RAM16K[18] 6; // First run (at the beginning PC=0) repeat 8 { tick, tock, output; } // Reset the PC set reset 1, set RAM16K[0] 0, tick, tock, output; set reset 0, set RAM16K[16] 8, set RAM16K[17] 7, set RAM16K[18] 5; // second run (at the beginning PC=0) repeat 8 { tick, tock, output; }
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Example1_11_b.sce
//Example 1.11(b) clear; clc; R1=1*10^6; R2=1*10^6; R3=100*10^3; R4=1*10^3; RL=2*10^3;//Load ResistanceR1=1*10^6; R2=1*10^6; R3=100*10^3; R4=1*10^3; RL=2*10^3;//Load Resistance A=-(R2/R1)*(1+(R3/R2)+(R3/R4));//Ideal Gain rd=1*10^6;//Internal input resistance a=10^5;//Open Loop Gain ro=100; RA=(R1*rd)/(R1+rd); RB=RA+R2; RC=(RB*R4)/(RB+R4); RD=RC+R3; RE=(RD*RL)/(RD+RL); RF=RE+ro; c1=-(RA/RB);//vD=c1*v1 c2=(RC/RD);//v1=c2*vo c3=(RE/RF);//vo=c3*vT c4=a*(c1*c2*c3);//vR=a*vD=a*(c1*v1)=a*(c1*c2*vo)=a*(c1*c2*c3)vT=c4*vT -> vR=c4*vT T=-c4;//T=(-vR/vT)=-c4 (Loop Gain) Trec=1/T; Atemp=1+Trec; Aactual=A/Atemp;//Actual Gain Adev=((Aactual-A)/A)*100;//Deviation in Gain printf("Actual Gain of op amp=%.1f V/V",Aactual); printf("\nPercentage Departure of Actual Gain from Ideal gain=%.2f",Adev);
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; @Harness: disassembler ; @Result: PASS section .text size=0x00000080 vma=0x00000000 lma=0x00000000 offset=0x00000034 ;2**0 section .data size=0x00000000 vma=0x00000000 lma=0x00000000 offset=0x000000b4 ;2**0 start .text: label 0x00000000 ".text": 0x0: 0x00 0x9c mul r0, r0 0x2: 0x10 0x9c mul r1, r0 0x4: 0x20 0x9c mul r2, r0 0x6: 0x30 0x9c mul r3, r0 0x8: 0x40 0x9c mul r4, r0 0xa: 0x50 0x9c mul r5, r0 0xc: 0x60 0x9c mul r6, r0 0xe: 0x70 0x9c mul r7, r0 0x10: 0x80 0x9c mul r8, r0 0x12: 0x90 0x9c mul r9, r0 0x14: 0xa0 0x9c mul r10, r0 0x16: 0xb0 0x9c mul r11, r0 0x18: 0xc0 0x9c mul r12, r0 0x1a: 0xd0 0x9c mul r13, r0 0x1c: 0xe0 0x9c mul r14, r0 0x1e: 0xf0 0x9c mul r15, r0 0x20: 0x00 0x9d mul r16, r0 0x22: 0x10 0x9d mul r17, r0 0x24: 0x20 0x9d mul r18, r0 0x26: 0x30 0x9d mul r19, r0 0x28: 0x40 0x9d mul r20, r0 0x2a: 0x50 0x9d mul r21, r0 0x2c: 0x60 0x9d mul r22, r0 0x2e: 0x70 0x9d mul r23, r0 0x30: 0x80 0x9d mul r24, r0 0x32: 0x90 0x9d mul r25, r0 0x34: 0xa0 0x9d mul r26, r0 0x36: 0xb0 0x9d mul r27, r0 0x38: 0xc0 0x9d mul r28, r0 0x3a: 0xd0 0x9d mul r29, r0 0x3c: 0xe0 0x9d mul r30, r0 0x3e: 0xf0 0x9d mul r31, r0 0x40: 0x00 0x9c mul r0, r0 0x42: 0x01 0x9c mul r0, r1 0x44: 0x02 0x9c mul r0, r2 0x46: 0x03 0x9c mul r0, r3 0x48: 0x04 0x9c mul r0, r4 0x4a: 0x05 0x9c mul r0, r5 0x4c: 0x06 0x9c mul r0, r6 0x4e: 0x07 0x9c mul r0, r7 0x50: 0x08 0x9c mul r0, r8 0x52: 0x09 0x9c mul r0, r9 0x54: 0x0a 0x9c mul r0, r10 0x56: 0x0b 0x9c mul r0, r11 0x58: 0x0c 0x9c mul r0, r12 0x5a: 0x0d 0x9c mul r0, r13 0x5c: 0x0e 0x9c mul r0, r14 0x5e: 0x0f 0x9c mul r0, r15 0x60: 0x00 0x9e mul r0, r16 0x62: 0x01 0x9e mul r0, r17 0x64: 0x02 0x9e mul r0, r18 0x66: 0x03 0x9e mul r0, r19 0x68: 0x04 0x9e mul r0, r20 0x6a: 0x05 0x9e mul r0, r21 0x6c: 0x06 0x9e mul r0, r22 0x6e: 0x07 0x9e mul r0, r23 0x70: 0x08 0x9e mul r0, r24 0x72: 0x09 0x9e mul r0, r25 0x74: 0x0a 0x9e mul r0, r26 0x76: 0x0b 0x9e mul r0, r27 0x78: 0x0c 0x9e mul r0, r28 0x7a: 0x0d 0x9e mul r0, r29 0x7c: 0x0e 0x9e mul r0, r30 0x7e: 0x0f 0x9e mul r0, r31 start .data:
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ShubhamShirsekar/GSM-System-capacity
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SystemCapacity.sce
clc disp("Exp 5, Name - Shubham Shirsekar, Roll No. 40") Asys=4200 //Area of system Acell=12 //Area of cell N=1001 //Total Channels K=7 //Cluster size Acl=K*Acell //Area of cluster M=Asys/Acl //No. of clusters disp("no. of clusters",M) J=N/K //Cell capacity disp("cell capacity in channels/cell ",J) C=N*M //System capacity disp("The system capacity in no. of channels",C) k=4 acl=k*Acell //Area of new cluster size m=Asys/acl m1=floor(m) disp("No. of clusters for reduced cluster size ",m1) j=N/k //Cell Capacity j1=floor(j) disp("New cell capacity for reduced cluster size in channels/cell",j1) c=N*m1 disp("New system capacity for reduced cluster size in no. of channels",c)
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13_10_soln.sce
clc; pathname=get_absolute_file_path('13_10_soln.sce') filename=pathname+filesep()+'13_10_data.sci' exec(filename) // Solution: // upstream temperature in Rankine, T1=T1+460; //deg R // absolute upstream pressure, p1=p1+14.7; //psia // for maximum flow-rate, // absolute downstream pressure, p2=0.53*p1; //psia // volume flow-rate, Q=floor(22.7*Cv*sqrt(((p1-p2)*p2)/T1)); //scfm // Results: printf("\n Results: ") printf("\n The maximum flow-rate is %.0f scfm of air.",Q)
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5_16.sce
//Example 5.16 //Finite Differences //Page no. 138 clc;close;clear; printf(' x\tf(x)\tdf(x) d2f(x) d3f(x) d4f(x)\n') printf('----------------------------------------------\n') x=[0,1;1,-1;2,1;3,-1;4,1;5,0;6,0;7,0]; for i=3:6 for j=1:8-i if x(j+1,i-1)~=0 then x(j,i)=x(j+1,i-1)-x(j,i-1) end end end k=-9; for i=1:8 printf(' ') for j=1:6 if i==j+k then break elseif x(i,j)==0 & j~=1 & j~=2 then printf('d%iy%i\t',j-1,i-1) elseif x(i,j)==0 & i~=1 printf('y%i\t',i-1) else printf('%i\t',x(i,j)) end end printf('\n') k=k+2 end x1=poly(0,"x") fx=x(1,2)+x1*x(1,3)+(x1^2-x1)*x(1,4)/2+(x1^3-3*x1^2+2*x1)*x(1,5)/6 for i=1:3 x(1+i,6)=16; printf('\nd5y%i = 16',i) end printf('\nElements should be constant\n\n'); i=1;k=2; for j=5:-1:2 while i<4 x(k+1,j)=x(k,j)+x(k,j+1); if j>2 then printf('\nd%iy%i = %i',j-1,k,x(k+1,j)) else printf('\ny%i = %i',k,x(k+1,j)) end k=k+1; i=i+1; end i=1;k=k-2; end
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Ex1_17.sce
//CHAPTER 1- D.C. CIRCUIT ANALYSIS AND NETWORK THEOREMS //Example 17 clc; disp("CHAPTER 1"); disp("EXAMPLE 17"); //VARIABLE INITIALIZATION v=7; //voltage source in Volts I=7; //current source in Amperes r1=1; //in Ohms r2=2; //in Ohms r3=1; //in Ohms r4=2; //in Ohms r5=3; //in Ohms //SOLUTION //deactivating the current source res=(v/4)+(v/2); vc=res/((1/4)+(1/r1)+(1/r2)); vx1=-vc; //deactivating voltage source //(4)va+(-1)vb=-21........eq (1) //(2)va+(-11)vb=0.........eq (2) //solving the equations by matrix method A=[4 -1;2 -11]; b=[-21;0]; x=inv(A)*b; va=x(1,:); //to access 1st element of 2X1 matrix vb=x(2,:); //to access 2nd element of 2X1 matrix vx2=-vb; vx=vx1+vx2; disp(sprintf("By Superposition Theorem, the value of Vx is %d V",vx)); //END