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//Solved_Ex.4.4->Determine the Trigonometric form of Fourier Series of the Full Wave Rectified sine wave clc; clear; T=8;//Defining Time Period A=2;//Defining Amplitude t=0:0.01:15; w0=2*%pi/T; function x=f(t),x=A.*abs(sin(t.*w0)) ,endfunction //given full wave rectified continuous signal plot(t,f); xlabel("time"); ylabel("x(t)"); //Check if Even Signal,if yes,then bn=0 if(f(t)==f(-1*t)) disp('even'); disp('bn=0'); function x=f(t),x=A.*abs(sin(t.*w0)) ,endfunction //given signal //Evaluation of a0 & an //Evaluation of a0: a0=4*intg(0,T/2,f)/T; //definite integral of 'f' from 0 to T/2 disp(a0,'a0'); //Evaluation of an: disp('due to convergence,for all odd values of n,a=0'); disp('for even values of n,an values are=>'); y0=a0/2+zeros(1,length(t)); for n=2:2:8 //changing the end value of n,we can get more numbers of an function xn=f1(t),xn=A.*abs(sin(t.*w0)).*cos(n.*w0.*t) ,endfunction an=4*intg(0,T/2,f1)/T; disp(n,'a'); disp(an); y0=y0+an.*cos(n*w0.*t); xset('window',1); subplot(2,2,n/2); plot(t,y0); xlabel("time"); ylabel("x(t)*cos(n*w0*t) for n="); end xset('window',2); plot(t,y0); xset('window',2); plot(t,y0); else if(f(t)==(-1*f(-1*t))) disp('odd signal=>a0=an=0'); function x=f(t),x=A.*abs(sin(t.*w0)) ,endfunction //redefining signal //Evaluation of bn=> y0=zeros(1,length(t)); for n=1:1:8 //changing the end value of n,we can get more numbers of bn function xn=f1(t),xn=A.*abs(sin(t.*w0)).*sin(n.*w0.*t) ,endfunction bn=4*intg(0,T/2,f1)/T; disp(n,'b'); disp(bn); y0=y0+bn.*sin(w0.*n.*t); xset('window',1); subplot(2,4,n); plot(t,y0); xlabel("time"); ylabel("x(t)*sin(n*w0*t) for n="); end else disp('unknown'); function xn=f1(t),xn=A.*abs(sin(t.*w0)).*sin(n.*w0.*t) ,endfunction //Evaluation of a0,an & bn //Evaluation of a0: a0=4*intg(0,T/2,f)/T; //definite integral of 'f' from 0 to T/2 disp(a0,'a0'); //Evaluation of an: y0=a0/2+zeros(1,length(t)); for n=1:1:8 //changing the end value of n,we can get more numbers of an function xn=f1(t),xn=A.*abs(sin(t.*w0)).*cos(n.*w0.*t) ,endfunction an=4*intg(0,T/2,f1)/T; disp(n,'a'); disp(an); y0=y0+an.*cos(n*w0.*t); xset('window',1); subplot(2,2,n/2); plot(t,y0); xlabel("time"); ylabel("x(t)*cos(n*w0*t) for n="); end //Evaluation of bn=> y0=zeros(1,length(t)); for n=1:1:8 //changing the end value of n,we can get more numbers of bn function xn=f1(t),xn=A.*abs(sin(t.*w0)).*sin(n.*w0.*t) ,endfunction bn=4*intg(0,T/2,f1)/T; disp(n,'b'); disp(bn); y0=y0+bn.*sin(w0.*n.*t); xset('window',1); subplot(2,4,n); plot(t,y0); xlabel("time"); ylabel("x(t)*sin(n*w0*t) for n="); end end end xset('window',2); plot(t,y0);//x(t) signal till 8 harmonics
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//Caption:Determine the (a)speed (b)Torque (c)Efficiency //Exa:2.37 clc; clear; close; V=240;//in volts P=4; Phy=0.008;//in webers Z=1000; A=2; R_f=240;//in ohms R_a=0.4;//in ohms I_1=25;//in amperes I_f=V/R_f;//in amperes I_a1=I_1-I_f;//in amperes E_b=V-I_a1*R_a;//in volts N=E_b*60*A/(P*Z*Phy); disp(N,'(a)speed (in rpm) ='); P_m=E_b*I_a1; T_g=(9.55*P_m)/N; disp(T_g,'(b)Torque (in N-m)='); P_f=P_m-800; P_i=V*I_1; Eff=P_f*100/P_i; disp(Eff,'(c)Efficiency (in %)=')
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// Scilab code Ex10.2: Pg:411 (2008) clc;clear; N = 2.7e+025; // Number of molecules per unit volume epsilon_r = 1.0024; // Dielectric constant due to electronic polarization epsilon_0 = 8.85e-012; // Permittivity of free space, force per meter // P = epsilon_0*(epsilon_r-1)*E and P = N*alpha_e*E, solving for alpha_e alpha_e = epsilon_0*(epsilon_r-1)/N; // Electronic polarizability of an argon atom, farad Sq.m printf("\nThe electronic polarizability of an argon atom = %3.1e farad Sq.m", alpha_e); // Result // The electronic polarizability of an argon atom = 7.9e-040 farad Sq.m
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// Exa 7.12 clc; clear; close; format('v',6) // Given data I_DSS = 12;// in mA V_P = 5;// in V R_D = 3.3;// in k ohm R_G = 1.5*10^3;// in k ohm R_S = 1.2;// in k ohm V_DD= 18;// in V I_D= poly(0,'I_D'); V_GS= I_D*R_S;// in V I_D= I_D-I_DSS*(1-V_GS/V_P)^2; I_D= roots(I_D); I_D= I_D(2);// in mA V_GS= I_D*R_S;// in V V_DS= V_DD-I_D*(R_S+R_D);// in V disp(I_D,"The value of I_D in mA is : ") disp(V_GS,"The value of V_GS in volts is : "); disp(V_DS,"The value of V_DS in volts is : ")
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//Example 3_31 clc; clear; close; format('v',5); //given data : I2=10;//A f=50;//Hz R1=5;//ohm L1=0.0191;//H R2=7;//ohm C2=398;//micro F R3=8;//ohm L3=0.0318;//H Z1=R1+%i*2*%pi*f*L1;//ohm Z2=R2-%i/2/%pi/f/(C2*10^-6);//ohm Z3=R3+%i*2*%pi*f*L3;//ohm VAC=I2*Z2;//V I1=VAC/Z1;//A I=I1+I2;//A VCB=I*Z3;//V VAB=VAC+VCB;//V VABmag=abs(VAB);//A VABang=atand(imag(VAB)/real(VAB));//degree disp(VABang,VABmag,"Voltage AB, magnitude(V) & Angle(degree) are"); //Answer is not accurate in the book.
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clc clear m=evstr(x_dialog('Enter a 3x3 matrix',['[0 0 0';'0 0 0';'0 0 0]']))
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//Example 4.16. clc format(6) disp("For a Hartley oscillator the frequency is given by,") disp(" f = 1 / 2*pi*sqrt(L_eq*C) where L_eq = L1+L2") leq=20+5 // in mH disp(leq,"Therefore, L__eq(in mH) = 20+5 =") f=(1/(2*%pi*sqrt(25*500*10^-15)))*10^-3 // in kHz disp(f,"Therefore, f(in kHz) =")
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//chapter27 //example27.2 //page575 R1=4 // ohm R2=4 // ohm R3=4 // ohm // for h11 and h21, imagine that output terminals are shorted hence it is clear that input impedence is equal to R1+R2*R3/(R2+R3) // this is h11 by definition so h11=R1+R2*R3/(R2+R3) // now current will divide equally at junction of 4 ohm resistors so output_current/input_current = -0.5 // but this ratio is h21 by definition. Thus h21=-0.5 // for h12 and h22 imagine a voltage source on output terminals // this voltage will be divided by a factor 2 // hence input_voltage/output_voltage = 0.5 // but this ratio is h12 by definition. Thus h12=0.5 // here output impedence looking into output terminals with input terminals open is 8 ohm. // its reciprocal is h22 by definition. Thus h22=1/8 printf("h11 = %.3f ohm \n",h11) printf("h21 = %.3f \n",h21) printf("h12 = %.3f \n",h12) printf("h22 = %.3f ohm \n",h22)
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clc; clear; format('e',11); d=0.01/0.0254; //in inches. r=d/2; l=1; //in inches. N=20; L=(r^2)*(N^2)/(9*r+10*l); //Wheeler's formula. disp(L,"The inductance of the coil by Wheelers formula,L(in micro H)=");
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// Scilab Code Ex4.5: Page-236 (2008) clc; clear; c = 3e+008; // Speed of light in vacuum, m/s t0 = 2.5e-008; // Proper life time of pi-meson, s t = 2.5e-007; // MEan life time of pi-meson, s // As t = t0/(sqrt(1-v^2/c^2)), solving for v v = sqrt(1-(t0/t)^2)*c; // Velocity of pi meson, m/s printf("\nThe velocity of pi meson = %5.3f c = %4.2e m/s", v/c, v); // Result // The velocity of pi meson = 0.995 c = 2.98e+008 m/s
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Ex2_4.sce
// Chapter 2 Example 4 //============================================================================== clc; clear; //input data h = 6.625*10^-34; // plank's constant c = 3*10^8; // vel. of light in m/s lamda = 4961*10^-10; // wavelength of light in m //Calculations E = (h*c)/lamda; // energy in joules N = 1/E //Output mprintf('Number of photons required to do one Joule of work = %3.4e /m^3',N); //==============================================================================
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Ex1_11.sce
// FUNDAMENTALS OF ELECTICAL MACHINES // M.A.SALAM // NAROSA PUBLISHING HOUSE // SECOND EDITION // Chapter 1 : REVIEW OF ELECRTIC CIRCUITS // Example : 1.11 clc;clear; // clears the console and command history // Given data Z = 3+%i*4 // impedance in Ω V_AN = 150 // voltage in V R = 3 // resistance in Ω from Z // caclulations V_AN = (150*exp(%i*(0)*(%pi/180))) //source voltage in V V_BN = (150*exp(%i*(-120)*(%pi/180))) // source voltage in V V_CN = (150*exp(%i*(120)*(%pi/180))) // source voltage in V I_Aa = V_AN/Z // line current in A I_Bb = V_BN/Z // line current in A I_Cc = V_CN/Z // line current in A pf = R/abs(Z) // power factor I = V_AN/abs(Z) // current in A P = V_AN*I*pf // power supplied in W P_t = 3*P // total power supplied in W // display the result disp("Example 1.11 solution"); printf(" \n Line currents are \n I_Aa = %.2f<%.2f A \n", abs(I_Aa),atand(imag(I_Aa),real(I_Aa)) ); printf(" I_Bb = %.2f<% 2f A \n", abs(I_Bb),atand(imag(I_Bb),real(I_Bb)) ); printf(" I_Cc = %.2f<% 2f A \n\n", abs(I_Cc),atand(imag(I_Cc),real(I_Cc)) ); printf(" Power factor \n pf = %.1f \n", pf); printf(" \n Power supplied to each phase is \n P = %.2f W \n", P); printf(" \n Total power supplied \n P_t = %.2f W \n", P_t);
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// Example 9.9 clear all; clc; // Given data fluence = 10^8; // Given fluence neutrons/cm^2 // From Figure 9.12 // To receive an dose equivalent rate of 1 mrem/hr, the fast neutron flux is 7 neutrons/cm^2-sec phi_eq = 7; // Equivalent flux in neutrons/cm^2-sec D_eq = 1; // Equivalent dose rate in mrem/hr // 1 hour = 3600 seconds fluence_eq = phi_eq*3600; // Equivalent fluence in neutrons/cm^2 // Calculation D = (fluence*D_eq)/fluence_eq; // Result printf(" \n Dose received due to exposure of accelerator source = %d mrem \n",D); // The answer given in textbook is approximated to a nearest value.
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//Part B Ex 2.14 clc;clear;close; format('v',9); dec=34.6875;//given decimal value i=floor(dec);//integer part f=dec-i;//fraction part i_bin=dec2bin(i);//binary equivalent of integer part f_bin=' ';//for initializing(string) for n=1:4 t=2*f; if t>=1 then p(n)=1; f=t-1; end if t<1 then p(n)=0; f=t; end f_bin=f_bin+string(p(n));//binary equivalent of fraction part end; bin=i_bin+'.'+f_bin;//Binary equivalent of complete no. disp(bin,"Binary equivalent of complete no. is ");
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@@emplu.pkg CREATE OR REPLACE PROCEDURE test_emplu ( counter IN INTEGER, empno_in IN emp.empno%TYPE := 7788) IS emprec employee%ROWTYPE; BEGIN sf_timer.set_factor (counter); sf_timer.start_timer; FOR i IN 1 .. counter LOOP emprec := emplu1.onerow (empno_in); END LOOP; sf_timer.show_elapsed_time ('database table'); sf_timer.set_factor (counter); sf_timer.start_timer; FOR i IN 1 .. counter LOOP emprec := emplu2.onerow (empno_in); END LOOP; sf_timer.show_elapsed_time ('index-by table'); END; / /*====================================================================== | Supplement to the third edition of Oracle PL/SQL Programming by Steven | Feuerstein with Bill Pribyl, Copyright (c) 1997-2002 O'Reilly & | Associates, Inc. To submit corrections or find more code samples visit | http://www.oreilly.com/catalog/oraclep3/ */
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//Example 1_2 clc(); clear; // To add the given vector displacements a=1 //units in meters b=3 //units in meters c=5 //units in meters d=6 //units in meters theta1=90 //units in degrees Rx_a=a*sin(theta1*%pi/180) //units in meters Rx_b=round(b*cos(theta1*%pi/180)) //units in meters theta2=37 //units in degrees Rx_c=-round(c*cos(theta2*%pi/180)) //units in meters theta3=53 //units in degrees Rx_d=-d*cos(theta3*%pi/180) Ry_a=round(a*cos(theta1*%pi/180)) //units in meters Ry_b=round(c*sin(theta2*%pi/180)) //units in meters Ry_c=round(c*sin(theta2*%pi/180)) //units in meters Ry_d=-(d*sin(theta3*%pi/180)) //units in meters Rx=Rx_a+Rx_b+Rx_c+Rx_d //units in meters Ry=Ry_a+Ry_b+Ry_c+Ry_d //units in meters R=sqrt(Rx^2+Ry^2) //units in meters phi=round(atan(Ry/-(Rx))*180/%pi) //units in degrees phi=180-phi //units in degrees printf("The Resultant R=%.2f Meters\n",R) printf("The Angle theta=%d degrees",phi)
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//Example No. 4.3 clc; clear; close; format('v',6); //Given Data : P=30;//KW theta1=54-30;//degree C t1=1;//hour theta2=67-30;//degree C t2=2;//hour(t2=2*t1) disp("theta=theta_f*(1-exp(-t/T))"); //Let exp(-t1/T)=a then exp(-t2/T)=a^2 //theta1/theta2=(1-a)/(1-a^2) //a^2*theta1-a*theta2+theta2-theta1=0 P=[theta1 -theta2 theta2-theta1];//Polynomial for a a=roots(P); a=a(2);//discarding value 1 as it cant give value of T T=-t1/log(a);//hour theta_f=theta1/(1-exp(-t1/T));//degreeC theta_steady=theta_f+30;//degreeC disp(theta_steady,"Final steady state temperature in degree C : "); disp(T,"Heating time constant in hour : "); theta2=theta_f;//degree C t=2.7;//hour theta=40-30;//degree C Tdash=-t/log(theta/theta2);//hour disp(Tdash,"Cooling time constant in hour : ");
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// //given h1=0.90,h2=1.25,h3=2.15,h4=2.50,h5=1.85,h6=1.35,h7=0.85, b=10//width in m sh=1.5//side slope in m h=40//m d1=(b+(sh*h1))*h1 d2=(b+(sh*h2))*h2 d3=(b+(sh*h3))*h3 d4=(b+(sh*h4))*h4 d5=(b+(sh*h5))*h5 d6=(b+(sh*h6))*h6 d7=(b+(sh*h7))*h7 printf("\n d1= %0.3f sq. meter,d2 = %0.3f sq. meter,d3= %0.3f sq. meter,d4= %0.3f sq. meter,d5= %0.3f sq. meter,d6= %0.3f sq. meter,d7= %0.3f sq.meter",d1,d2,d3,d4,d5,d6,d7) printf("\n by trapezoidal rule') v=(h/2)*(d1+d7+2*(d2+d3+d4+d5+d6)) printf("\n V= %0.3f meter cube',v) printf("\n by prismoidal rule') v1=(h/3)*(d1+d7+4*(d2+d4+d6)+2*(d3+d5)) printf("\n V= %0.3f meter cube',v1)
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// Exa7.14 clc; clear; close; // given : phi=5 // HPBW,half power beam width in Degrees phi_not=2*phi // BWFN, null-to-null beam width in degrees Lm=poly(0,'Lm') // defining Lm as lambda // formula : phi=70*(Lm/D_a) // where Lm is wavelength in m and D_a is mouth diameter in m D_a=(70*Lm)/phi G_p=6.4*(D_a/Lm)^2 G_p=horner(G_p,1) G_p=10*log10(G_p) // power gain in dB disp(phi_not,"BWFN, null-to-null beam width in degrees:") disp(G_p,"power gain in dB:")
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function [MTh,VTh,MSTh,VSTh] = gl_stat(N,maxp,Nu_I,Nu_O,st_j,Nu_Ma,rt_a,a,c,b,bu) // Ouput variables initialisation (not found in input variables) MTh=[]; VTh=[]; MSTh=[]; VSTh=[]; // Display mode mode(-1); // Display warning for floating point exception //ieee(1); //M and V for each phy_age MTh = zeros(maxp,6,N); VTh = zeros(maxp,6,N); //M and V for total MSTh = zeros(maxp,N); VSTh = zeros(maxp,N); Nu_A = matrix(Nu_O(4,:,:),maxp,6); // computing the mean and variance u = sum(Nu_I,2); I = ones(N,1); //survival probablity c--number of macrostate in chr_age i x~ truncated geometrical distribution Mx = zeros(maxp,N); Vx = zeros(maxp,N); for p = 1:maxp for i = 1:N n = min(i,Nu_Ma(p)); if c(p)<1 then Mx(p,i) = c(p)*(1-c(p)^n)/(1-c(p)); Vx(p,i) = c(p)*(1-(2*n+1)*(1-c(p))*c(p)^n-c(p)^(2*n+1))/(1-c(p))^2; else Mx(p,i) = n; Vx(p,i) = 0; end; end; end; //covariance between macrostate because of c MC = zeros(maxp,N,N); VC = zeros(maxp,N,N); for p = 1:maxp for i = 1:N for j = i:N if i==j then //mean and variance for existence of a single macrostate MC(p,i,i) = c(p)^i; VC(p,i,i) = c(p)^i*(1-c(p)^i); else //covariance matrix between the macrostates VC(p,i,j) = c(p)^j*(1-c(p)^i); VC(p,j,i) = VC(p,i,j); end; end; end; end; //growth probability of each macrosate --number of macrostate during one cycle y~ 0/1 distribution My = zeros(maxp,1); Vy = zeros(maxp,1); for p = 1:maxp My(p)=b(p); Vy(p)=b(p)*(1-b(p)); end; //growth probability of each microsate in a macrostate-- number of microstate in a macrostate z~ bion(Nu_I(p,k),bu(p)) distribution Mz = zeros(maxp,6); Vz = zeros(maxp,6); Mu = zeros(maxp,1); Vu = zeros(maxp,1);//sum of Mz for p = 1:maxp Mz(p,:) = Nu_I(p,:)*bu(p); Vz(p,:) = Nu_I(p,:)*bu(p)*(1-bu(p)); Mu(p)=sum(Nu_I(p,:))*bu(p); Vu(p)=sum(Nu_I(p,:))*bu(p)*(1-bu(p)); end; //branching probability of each buds in a microstate -- number of substructures in a microstate w ~ bino(Nu_A(p,k),a(k)) distribution Mw = zeros(maxp,6); Vw = zeros(maxp,6); for p = 1:maxp for k = p:maxp Mw(p,k) = Nu_A(p,k)*a(k); Vw(p,k) = Nu_A(p,k)*a(k)*(1-a(k)); end; end; //compound law of y (b) and z (bu)--if a macostate live, number of microstate inside it: yz Myz = zeros(maxp,6); Vyz = zeros(maxp,6); Myu = zeros(maxp,1); Vyu = zeros(maxp,1); for p = 1:maxp for k = p:6 Myz(p,k) = My(p)*Mz(p,k); Vyz(p,k) = My(p)*Vz(p,k)+Vy(p)*(Mz(p,k)^2); end; Myu(p)=My(p)*Mu(p); Vyu(p)=My(p)*Vu(p)+Vy(p)*Mu(p)^2; end; //compound law of y (b) and z (bu) and a--if a macostate live, number of substructures inside it: yzw //mean and var of number of substructure with phy_age j in macrostate p with chr age k Myzw = zeros(maxp,6); Vyzw = zeros(maxp,6); for p = 1:maxp for k = p:6 Myzw(p,k) = Myz(p,k)*Mw(p,k); Vyzw(p,k) = Myz(p,k)*Vw(p,k)+Vyz(p,k)*(Mw(p,k)^2); end; end; for p = maxp:-1:1 //mean and var of number of microstates(from substructure) in a macrostates for i = 1:N //chr_age of substructure p MA = zeros(maxp,6,N); VA = zeros(maxp,6,N); //number of microstates in axis (p,i), compound of c and b, bu MTh(p,p,i) = Mx(p,i)*Myu(p); VTh(p,p,i) = Mx(p,i)*Vyu(p)+Vx(p,i)*(Myu(p)^2); for k = max(1,i-mtlb_double(Nu_Ma(p,1))+1):i //lateral structure, k is chr_age of macrostate x = i-k+1; //time order when G.U. appear for j = p+1:maxp jd = (k-1)*rt_a(j,1); //the ch_age of substructure flag = 1; //(Flag_pruning(b)~=1) | (jd<=T_Pr(b)+Pruning_delay(b)) ;%not prunned if jd>0 & flag then for m = j:maxp MA(p,m,x) = MA(p,m,x)+Myzw(p,j)*MTh(j,m,jd); VA(p,m,x) = VA(p,m,x)+Myzw(p,j)*VTh(j,m,jd)+Vyzw(p,j)*(MTh(j,m,jd)^2); end; end; end; end; for m = p+1:maxp M1 = matrix(MA(p,m,:),1,N); //vector of mean of microstate m top down V1 = matrix(VA(p,m,:),1,N); //vector of var of microstate m top down MTh(p,m,i) = (M1*matrix(MC(p,:,:),N,N))*I; VTh(p,m,i) = V1*matrix(MC(p,:,:),N,N)*I+M1*matrix(VC(p,:,:),N,N)*M1'; end; //terminal structure j = st_j(p); if i>Nu_Ma(p) & j>=p & j<=maxp then jd = i-Nu_Ma(p); for m = j:maxp MTh(p,m,i) = MTh(p,m,i)+MTh(j,m,jd); VTh(p,m,i) = VTh(p,m,i)+VTh(j,m,jd); end; end; end; //i end;//p //total number for p = maxp:-1:1 //mean and var of number of microstates(from substructure) in a macrostates for i = 1:N //chr_age of substructure p MA1 = zeros(maxp,N); VA1 = zeros(maxp,N); MA2 = zeros(maxp,N); VA2 = zeros(maxp,N); MA = zeros(maxp,N); VA = zeros(maxp,N); for k = max(1,i-Nu_Ma(p,1)+1):i //lateral structure, k is chr_age of macrostate x = i-k+1; //time order when G.U. appear //number in axis MA1(p,x) = Myu(p); VA1(p,x) = Vyu(p); for j = p+1:maxp jd = (k-1)*rt_a(j,1); //the ch_age of substructure flag = 1; //(Flag_pruning(b)~=1) | (jd<=T_Pr(b)+Pruning_delay(b)) ;%not prunned if jd>0 & flag then MA2(p,x) = MA2(p,x)+Myzw(p,j)*MSTh(j,jd); VA2(p,x) = VA2(p,x)+Myzw(p,j)*VSTh(j,jd)+Vyzw(p,j)*(MSTh(j,jd)^2); end; end; MA(p,x) = MA1(p,x)+MA2(p,x); //sum of variance and covariance between number of microstate in a G.U. in axis and that in substrucutre on that G.U. VA(p,x) = VA1(p,x)+VA2(p,x)+2*(1-bu(p)+u(p)*bu(p)*(1-b(p)))*MA2(p,x); end; M1 = matrix(MA(p,:),1,N); //vector os mean of microstate m top down V1 = matrix(VA(p,:),1,N); //vector os var of microstate m top down MSTh(p,i) = (M1*matrix(MC(p,:,:),N,N))*I; VSTh(p,i) = V1*matrix(MC(p,:,:),N,N)*I+M1*matrix(VC(p,:,:),N,N)*M1'; //terminal structure j = st_j(p); if i>Nu_Ma(p) & j>=p & j<=maxp then jd = i-Nu_Ma(p); MSTh(p,i) = MSTh(p,i)+MSTh(j,jd); VSTh(p,i) = VSTh(p,i)+VSTh(j,jd); end; end; //i end;//p //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% // DISTRIBUTION //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% // MA=max(u)*N;%maximum number of microstates in axis // FA=zeros(maxp,N,MA); %distribution of number of microstate in each axis // // for k=0:m %possible number of microstates in axis // for j=0:N %possible number of macrostates in i cycles // for i=j:N-1 %possible number of cycles to survive // h(k+1)=h(k+1)+(1-c(1))*c(1)^i*binopdf(j,i,b(1))*binopdf(k,j*u(1),bu(1)); // end // h(k+1)=h(k+1)+c(1)^N*binopdf(j,N,b(1))*binopdf(k,j*u(1),bu(1));%boundary // end // end endfunction
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function [y,t] = rk4(fun,ti,tf,h,y0) // Método de Runge-Kutta para Sistema de N equações Diferenciais (interativo) - Ordem 4 // Onde -> y é o vetor solução (EDO's) // -> t é o vetor do tempo //--------------------------------------------------------------------- // -> fun é o vetor de funções do sistema (EDO's) // -> ti é o valor inicial do tempo // -> tf é o valor final do tempo // -> h é o passo de calculo (step) // -> y0 é o vator contendo as condições iniciais // //###################################################################### //Exemplo de Chamada //exec ('path\rk4.sci',-1) {-1 não mostra o código de execução} //fun = '[ya(2),9.81-(0.25/68.1)*ya(2)^2]'; // --> Caso do EX pg. 24 (Slide de Aula) // --> ya é o vetor avaliado por evstr(fun) (k1, k2, k3, k4) //y0 = '[0,0]'; --> Condições Iniciais; y1(0)=0 e y2(0)=0 //[y,t] = rk4(fun,0,10,1,[0,0]) //----------------- //Autor: Daniel HC Souza //IMPLEMENTACAÇÃO.... //Inicializações t(1) = ti; y(1,:) = y0; i = 1; ta = ti; while ta < tf do ya = y(i,:); //Calculando K1 e y(0) k1 = evstr(fun); ya = y(i,:) + k1*h/2; //Atualiza o tempo t(0 + h/2) ta = ta + h/2; //Calculando K2 e y(0,5) k2 = evstr(fun); ya = y(i,:) + k2*h/2; //Calculando K3 e y(0,5) k3 = evstr(fun); ya = y(i,:) + k3*h; //Atualiza o tempo t(0 + h/2) --> t(h) ta = ta + h/2; //Calculando K4 e y(1) k4 = evstr(fun); //Calculando Valores para y(1) - Método de Runge-Kutta 4ªOrdem phi = (k1+2*(k2+k3)+k4)/6; //Eq. de Runge-Kutta y(i+1,:) = y(i,:) + phi*h; //Atualiza Valores de y() t(i+1) = ta; //Atualiza Valores do Tempo i = i+1; //Proxima Iteração end endfunction
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errcatch(-1,"stop");mode(2);//Chapter 21, Problem 23 ; R1=150; //equivalent input resistance N=5; //turns ratio Rl=R1/(N^2); //load resistance printf("Optimum value of load resistance = %d ohm",Rl); exit();
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clear; clc; //Example - 7.30 //Page number - 267 printf("Example - 7.30 and Page number - 267\n\n"); //Given den_liq = 13690;//[kg/m^(3)] - Density of liquid mercury den_solid = 14190;//[kg/m^(3)] - Density of solid mercury mp = -38.87;//[C] - Melting point of mercury at pressure of 1 bar mp = mp + 273.15;//[K] T_req = 0;//[C] - Required temperature to which the melting point is to be raised T_req = T_req + 273.15;//[K] H_fus = 11.62;//[kJ/kg] - Latent heat of fusion of mercury V_liq = (1/den_liq);//[m^(3)/kg] - Specific volume of liquid mercury V_solid = (1/den_solid);//[m^(3)/kg] - Specific volume of solid mercury // (delta P/delta T) = ((P - 1)*100)/(T_req - mp) // delta H/(T*delta V) = (H_liq - H_solid)/(T*(V_liq - V_solid)) = del (say) del = (H_fus)/(mp*(V_liq - V_solid));//[kPa/K] - delta H/(T*delta V) //Equating the two sides and then solving we get P = (del*(T_req - mp))/100 + 1;//[bar] printf(" The required pressure should be %f bar",P);
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clear all clc close dia=0.03*1e-3;//Diameter of drop in m rho=2000;//Desnity of ink in kg/m vz=25;//velocity in z direction in m/sec L1=15*1e-3;//Length of deflection plate in m L2=12*1e-3;//distance from the exit end of the deflection plate to the print surface in m q=100*1e-15;//Charge of drop in C d=2*1e-3;//Spacing in m Vo=3500;//Charging voltage in V //Mass of drop in kg m=(4/3)*%pi*rho*(dia/2)^3; to=L1/vz; vxo=q*Vo*to/(m*d); xo=0.5*vxo*to; t1=(L1+L2)/vz; printf("time required for the drop to reach the print surface is %f s \n",t1) //Calculation of vertical displacement of the drop on the print surface in mm x1=xo+vxo*(t1-to); printf('Vertical displacement of the drop on the print surface is %f m \n',x1)
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clc; funcprot(0); // Initialization of Variable AB=31325.14//slope distance in m R=6370.0e3;//radius of earth ha=1582.15;//elevation in m h=4251.32-ha//in m //calculation AB_dash=AB-h**2/2/AB; theta=2*asin(AB_dash/2/R); AB_dash=AB-(h*sin(theta/2)+h**2/AB/2) CD=AB_dash-AB_dash*ha/R; S=CD+CD**3/24.0/R**2; disp(S,"sea level length in m") clear()
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clc;funcprot(0);//EXAMPLE 12.8 // Initialisation of Variables Vpbes=7;.................//Volume of fuel in the pump barrel before commencement of effective stroke in cc df=3;.................//Diameter of fuel line from pump to injector in mm lf=700;.................//Length of fuel line from pump to injector in mm Vfiv=2;................//Volume of fuel in the injection valve in cc Vfd=0.1;.................//Volume of fuel to be delivered in cc p1=150;..............//Pressure at which fuel is delivered in bar p2=1;.................//atmospheric pressure in bar cc=78.8*10^(-6);..........//Co - efficient of compressibility per bar dp=7;..............//Diameter of plunger in mm //calculations V1=Vpbes+(%pi/4)*((df/10)^2)*(lf/10)+Vfiv;...................//Total initial fuel volume delV=cc*(p1-p2)*V1;................//Change in volume due to compression displu=delV+Vfd;.....................//Total displacement of plunger disp(displu,"Total displacement of plunger in cc :") lp=(displu*4)/(%pi*(dp/10)^2);.............//Effective stroke of plunger disp(lp,"Effective stroke of plunger in mm:")
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//check o/p when the i/p contains negative elements impr=[-1 -2 -3 0 5]; num_ord=6; den_ord=4; [num,den]=prony(impr,num_ord,den_ord); disp(num); disp(den); //output //- 1. - 2. - 3. 0. 5. 0. // // 1. 0. 0. 0. 0.
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//example 9.4 //page 318 clc; funcprot(0); //initialisation of variable L=500; S=0.004;//slope of slope line hf=S*L; disp(hf,"head loss (ft)="); clear
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clc // Given that t = 400 // temperature in K k = 1.38e-23 // Boltzmann's constant in J/K h = 6.62e-34 // Planck constant in J-sec e = 1.6e-19 // charge on an electron in C m = 4 * 1.67e-27 // mass of helium atom in kg // Sample Problem 35 on page no. 14.34 printf("\n # PROBLEM 35 # \n") printf("Standard formula used \n ") printf(" lambda = h /(m*v)\n 1/2*m*v^2 = 3/2*k*T \n") lambda = h / sqrt(3 * m * k * t) printf("\n de-Broglie wavelength = %f Angstrom.",lambda * 1e10)
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function [psd,f_out] = pburg(x,poles,freq,Fs,range,method,plot_type,criterion) //Calculate Burg maximum-entropy power spectral density. //Calling Sequence //[psd,f_out] = pburg(x,poles,freq,Fs,range,method,plot_type,criterion) //All but the first two arguments are optional and may be empty. //Parameters // x: [vector] sampled data // poles: [integer scalar] required number of poles of the AR model // freq: [real vector] frequencies at which power spectral density is calculated [integer scalar] number of uniformly distributed frequency values at which spectral density is calculated. [default=256] // Fs: [real scalar] sampling frequency (Hertz) [default=1] // range: 'half', 'onesided' : frequency range of the spectrum is from zero up to but not including sample_f/2. Power from negative frequencies is added to the positive side of the spectrum. 'whole', 'twosided' : frequency range of the spectrum is -sample_f/2 to sample_f/2, with negative frequencies stored in "wrap around" order after the positive frequencies; e.g. frequencies for a 10-point 'twosided' spectrum are 0 0.1 0.2 0.3 0.4 0.5 -0.4 -0.3 -0.2 -0.1 'shift', 'centerdc' : same as 'whole' but with the first half of the spectrum swapped with second half to put the zero-frequency value in the middle. (See "help fftshift". If "freq" is vector, 'shift' is ignored. If model coefficients "ar_coeffs" are real, the default range is 'half', otherwise default range is 'whole'. // method: 'fft': use FFT to calculate power spectral density. 'poly': calculate spectral density as a polynomial of 1/z N.B. this argument is ignored if the "freq" argument is a vector. The default is 'poly' unless the "freq" argument is an integer power of 2. // plot_type: 'plot', 'semilogx', 'semilogy', 'loglog', 'squared' or 'db' specifies the type of plot. The default is 'plot', which means linear-linear axes. 'squared' is the same as 'plot'. 'dB' plots "10*log10(psd)". This argument is ignored and a spectrum is not plotted if the caller requires a returned value. // criterion: [optional string arg] model-selection criterion. Limits the number of poles so that spurious poles are not added when the whitened data has no more information in it (see Kay & Marple, 1981). Recognized values are 'AKICc' -- approximate corrected Kullback information criterion (recommended), 'KIC' -- Kullback information criterion 'AICc' -- corrected Akaike information criterion 'AIC' -- Akaike information criterion 'FPE' -- final prediction error" criterion The default is to NOT use a model-selection criterion. //Description //This function is being called from Octave //This function is a wrapper for arburg and ar_psd. //The functions "arburg" and "ar_psd" do all the work. //See "help arburg" and "help ar_psd" for further details. //Examples //a = [1.0 -1.6216505 1.1102795 -0.4621741 0.2075552 -0.018756746]; //[psd,f_out] = pburg(a,2); funcprot(0); lhs = argn(1) rhs = argn(2) if (rhs < 2 | rhs > 8) error("Wrong number of input arguments.") end select(rhs) case 2 then if(lhs==1) psd = callOctave("pburg",x,poless) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles) else error("Wrong number of output argments.") end case 3 then if(lhs==1) psd = callOctave("pburg",x,poles,freq) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles,freq) else error("Wrong number of output argments.") end case 4 then if(lhs==1) psd = callOctave("pburg",x,poles,freq,Fs) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles,freq,Fs) else error("Wrong number of output argments.") end case 5 then if(lhs==1) psd = callOctave("pburg",x,poles,freq,Fs,range) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles,freq,Fs,range) else error("Wrong number of output argments.") end case 6 then if(lhs==1) psd = callOctave("pburg",x,poles,freq,Fs,range,method) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles,freq,Fs,range,method) else error("Wrong number of output argments.") end case 7 then if(lhs==1) psd = callOctave("pburg",x,poles,freq,Fs,range,method,plot_type) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles,freq,Fs,range,method,plot_type) else error("Wrong number of output argments.") end case 8 then if(lhs==1) psd = callOctave("pburg",x,poles,freq,Fs,range,method,plot_type,criterion) elseif(lhs==2) [psd,f_out] = callOctave("pburg",x,poles,freq,Fs,range,method,plot_type,criterion) else error("Wrong number of output argments.") end end endfunction
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//Ex:10.7 clc; clear; close; y=860*10^-9;// wavelength in m L=5000;// length in m X=0.024; dy=20*10^-9;// spectral width in m dts=6*10^-9;// silica optical link rise time in s dtr=8*10^-9;// detector rise in s c=3*10^8;// speed of light in m/s dtm=-(L*dy*X)/(c*y);// material dispersion delay time in s id=2.5*10^-12;// intermodel dispersion in s/m dti=id*L;// intermodel dispersion delay time dtsy=sqrt((dts^2)+(dtr^2)+(dtm^2)+(dti^2));// system rise time in s Br_max=0.7/dtsy;// max bit rate for NRZ coding in bit/s Br_max1=0.35/dtsy;// max bit rate for RZ coding in bit/s printf("The system rise time =%f ns", dtsy*10^9); printf("\n The max bit rate for NRZ coding =%f Mbit/s", Br_max/10^6); printf("\n The max bit rate for RZ coding =%f Mbit/s", Br_max1/10^6);
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function mdaqDSPWait(arg1, arg2) if argn(2) == 1 then mdaqWaitUntilDone("dsp", arg1) elseif argn(2) == 2 then mdaqWaitUntilDone(arg1, "dsp", arg2) else mprintf("Description:\n"); mprintf("\tWaits until DSP application is complited\n"); mprintf("Usage:\n"); mprintf("\t[data, result] = mdaqDSPWait(linkID, timeout)\n") mprintf("\tlinkID - connection id returned by mdaqOpen() (OPTIONAL)\n"); mprintf("\ttimeout - amount of time in seconds (-1 - wait indefinitely)\n"); end endfunction
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//Example 7.2: Diffusion potential clc; clear; close; format('v',6) //given data : Na=5*10^23;// in m^-3 Nd=5*10^21;// in m^-3 T=300;// in K e=1.6*10^-19;// in J k=1.38*10^-23;// in JK^-1 V=(k*T)/e; ni=2.2*10^12;// in m^-3 Vd=V*log((Na*Nd)/ni^2); disp(Vd,"Diffusion potential,Vd(V) = ")
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//signals and systems //example4.5 // X(S) = s+3+5*exp(-2*s)/(s+1)*(s+2)) Re(s)>-1 s1 =%s ; syms t s; [A]=pfss((s1+3)/((s1+1)*(s1+2))); //partial fraction of F(s) F1 = ilaplace(A(1),s,t) F2 = ilaplace(A(2),s,t) //F3 = ilaplace(A(3),s,t) Fa = F1+F2; disp(Fa,"f1(t)=") [B]=pfss((5)/((s1+1)*(s1+2))); //partial fraction of F(s) F1 = ilaplace(B(1),s,t) F2 = ilaplace(B(2),s,t) Fb = (F1+F2)*(%e^(-2*s)); disp(Fb,"f2(t)=") disp(Fa+Fb,"f(t)=")
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EX3_11.sce
clc;funcprot(0);//EXAMPLE 3.11 // Initialisation of Variables p1=1;...................//Initial pressure in bar t1=343;..................//Initial temperature in K p2=7;....................//Pressure after adiabatic compression Qs=465;...............//Heat addition at constant volume in kJ/kg cp=1;.....................//Specific heat at constant pressure in kJ/kg cv=0.706;..................//Specific heat at constant volume in kJ/kg ga=cp/cv;.................//Ratio of specific heats //Calculations r=(p2/p1)^(1/ga);...............//Compression ratio t2=t1*(r^(ga-1));.....................//Temperature at the end of compression in K t3=t2+(Qs/cv);.............//Temperature at the end of heat addition in K disp(r,"Compression ratio:") disp(t2,"Temperature at the end of compression in K") disp(t3,"Temperature at the end of heat addition in K")
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clear clc //initialisation of variables d= 1/3 //ft g= 32.2 //ft/sec^2 d1= 4 //in d2= 1.6 //in h1= 5.7 //ft h2= -1.9 //ft Q= 0.3 //cuses H1= 34 //ft H2= 19 //ft H3= 7 //ft H4= 9.2 //ft h3= 2.9//ft h4= 3.9 //ft Et= 54 //ft-lb/lb //CALCULATIONS v1= sqrt(2*g*(h1-h2)/((d1/d2)^4-1)) Q1= %pi*v1*d^2/4 k= Q/Q1 P= (H1+H2)*H3/H4 P1= P-h3 r= P+h1-h2-h4 V= v1^2/(2*g) E= r+V dE= Et-E //RESULTS printf ('Coefficienct of venturi meter = %.4f ',k) printf ('\n Pressure of venturi throat = %.2f ft of water',P1) printf ('\n Loss in energy = %.1f ft-lb/lb',dE) //The answer is a bit different due to rounding off error in textbook
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Example3_4.sci
//Chapter 3_Semoconductor Devices Fundamentals //Caption: Hole Concentration //Example3.4: A semiconductor is doped with a concentration of 10^17 atoms/cm^3 of rsenic . What is the equilibrium hole concentration p at 300K. Given ni=1.5*10^10 cm^-3 // Solution: clear; clc; function p=holeconcentration(ni,Nd)//ni=intrinsiic concentration=1.5*10^10 cm^-3, Nd: donar concentration; since, Nd>>ni, so Nd=n=10^17 atoms/cm^3. p=ni^2/Nd disp('hole concentrartion at 300K is:') disp('per cubic cm',p) endfunction //holeconcentration(1.5*10^10,10^17);
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Ch8_8_31a.sce
clc clear disp("Example 8.31a") printf("\n") disp("perform the following binary substraction using 1s complement") disp("a)1010-0111 b)0110-1101") a=[1 0 1 0] b=~[0 1 1 1] d=0 for i=1:length(a) c(i)=a(length(a)+1-i)+b(length(a)+1-i)+d if(c(i)==1) d=0 end if[c(i)==2] d=1 c(i)=0 end end f=1 if(d==1) for i=1:length(a) g(i)=c(i)+f if(g(i)==1) f=0 end if(g(i)==2) f=1 g(i)=0 end end for i=1:length(a) c(i)=g(i) end end if(d==0) for i=1:length(a) c(i)=~c(i) end end printf("result =%d%d%d%d",c(4),c(3),c(2),c(1))
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StackTest.tst
// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/07/StackArithmetic/StackTest/StackTest.tst load StackTest.asm, output-file StackTest.out, compare-to StackTest.cmp, output-list RAM[0]%D2.6.2 RAM[256]%D2.6.2 RAM[257]%D2.6.2 RAM[258]%D2.6.2 RAM[259]%D2.6.2 RAM[260]%D2.6.2; set RAM[0] 256, repeat 1000 { ticktock; } output; output-list RAM[261]%D2.6.2 RAM[262]%D2.6.2 RAM[263]%D2.6.2 RAM[264]%D2.6.2 RAM[265]%D2.6.2; output;
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// Scilab code Ex3.15: Pg 97 (2008) clc; clear; N = 11; // Number of plates in a capacitor r = 25e-03; // Radius of circular plate, m A = (%pi*r^2); // Cross - sectional area of plate, m^2 d = 5e-04; // Distance between plates, m epsilon_r = 1; // Relative permittivity for air epsilon_o = 8.854e-12; // Relative permittivity for free space // Calculating the capacitance of the capacitor C = ((epsilon_o)*(epsilon_r)*A*(N-1))/d; // Capacitance, F printf("\n The capacitance of the capacitor = %3.2f pF", C/1e-10); // Result // The capacitance of the capacitor = 3.48 pF
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clc //Initialization of variables P=1.115 //bar //Calculations Conv_fac=1/1.01325 FinalP=Conv_fac*P //Final pressure //Results printf ('Final pressure in atmospheres (atm)= %.3f',FinalP)
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//bodeplot getf('labelbode.sci'); x=[0.001,0.0035,0.004,0.005,0.006,0.007,0.008,0.009,0.01,0.02,0.03,0.04];//Input frequency(Hz) y=[-3.87,-5.67,-7.53,-7.53,-8.17,-8.64,-8.87,-8.90,-9.11,-13.55,-15.39,-16.47];//Amplitude ratio(dB) subplot(2,1,1); plot2d(x,y,rect=[0.001,-20,0.04,0],logflag="ln"); xgrid(); y=[-25.2,-28.98,-33.11,-41.4,-60.48,-70.56,-77.76,-87.48,-90,-129.6,-151.2,-172.8];//Phase difference(degree) title = '' label(title,4,'Hz','Amplitude ratio in dB ',4); subplot(2,1,2); plot2d(x,y,rect=[0.001,-180,0.04,-20],logflag="ln"); label(title,4,'','Phase difference',4); subplot(2,1,2); xgrid(); s=poly(0,'s') h=syslin('c',(0.475/(124.827*s^2+57.26*s+1))) bode(h,0.001,0.04);
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function [y] = transpose(x) funcprot(0); y = callOctave("transpose",x) endfunction
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Ex10_2.sce
//Ex:10.2 clc; clear; close; a_fc=4;// fider cable loss in dB/km aj=0.7;// splice loss in db/km L=5;// length in km a_cr1=4;// connector losses a_cr2=3.5;// connector losses CL=(a_fc+aj)*L+(a_cr1+a_cr2);// total channel loss in dB printf("The total channel loss =%d dB", CL);
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//laplace transform of exponential function syms t s; y=laplace('%e^(-a*t)',t,s); disp(y,"ans=")
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function []=square(xmin,ymin,xmax,ymax) //definit un environnement graphique //permettant un trace isometrique. // //xmin,ymin, (xmax,ymax) specifient les abscisses et ordonnees minimum // (maximum) du dessin. defaut (-2,-2,2,2) // //square modifie le facteur d'echelle sur l'axe Ox. Pour conserver la //meme taille de dessin, utiliser plutot la macro isoview. Les extrema //sont imposes. //! // Copyright INRIA [zer,right]=argn(0); if right<=0 then right=4;xmin=-2;ymin=-2;xmax=2;ymax=2;end if right<>4 then error('0 ou 4 arguments'),end wdim=xget("wdim"); xset("wdim",maxi(wdim),maxi(wdim)); plot2d(0,0,1,"010"," ",[xmin,ymin,xmax,ymax]);
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// Problem no 10.3,Page No.252 clc;clear; close; //taking moment at pt A we get R_D=(90*6+120*3)*9**-1 //Reaction at Pt D //Joint D //Applying the summation of vertical forces we get F_GD=100*(sin(60*%pi*180**-1))**-1 //Applying the summation of horizontal forces we get F_DC=F_GD*cos(60*%pi*180**-1) //Joint G //Applying the summation of vertical forces we get F_GC=F_GD //Applying the summation of horizontal forces we get F_FG=F_GD*cos(60*%pi*180**-1)+F_GC*cos(60*%pi*180**-1) //joint C //Applying the summation of vertical forces we get F_FC=(115.5*sin(60*%pi*180**-1)-90)*(sin(60*%pi*180**-1))**-1 //Applying the summation of horizontal forces we get F_CB=F_DC+F_GC*cos(60*%pi*180**-1)+F_FC*cos(60*%pi*180**-1) //joint F //Applying the summation of vertical forces we get F_FB=F_FC //Applying the summation of horizontal forces we get F_EF=F_FG+F_FC*cos(60*%pi*180**-1)+F_FB*cos(60*%pi*180**-1) //Joint B //Applying the summation of vertical forces we get F_EB=(120-F_FB*sin(60*%pi*180**-1))*(sin(60*%pi*180**-1))**-1 //Applying the summation of horizontal forces we get F_BA=F_CB+F_FB*cos(60*%pi*180**-1)-F_EB*cos(60*%pi*180**-1) //Joint E //Applying the summation of vertical forces we get F_AE=F_EB //Result printf("Forces in Each members are as follows:F_GD %.1f kN (compression)",F_GD) printf("\n :F_DC %.2f",F_DC);printf(" KN(Tension)" ) printf("\n :F_GC %.1f kN (Tension)",F_GC) printf("\n :F_FG %.1f kN (Compression)",F_FG) printf("\n :F_FC %.1f kN(compression)",F_FC) printf("\n :F_CB %.2f",F_CB);printf(" KN(Tension)") printf("\n :F_FB %.1f kN(compression)",F_FB) printf("\n :F_EF %.2f",F_EF);printf(" KN(compression)") printf("\n :F_EB %.2f",F_EB);printf(" KN(Tension)") printf("\n :F_BA %.2f",F_BA);printf(" KN(Tension)") printf("\n :F_AE %.2f",F_AE);printf(" KN(compression)")
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566769707=6 1390748355=-1 1854083915=1 742051504=-1 710084632=3 565750963=0 1429063010=true 1459925108=5 868270416=3 1809270213=false 236938571=0 1860957759=5 1794508226=4 221507525=-2 1957337308=-1 1505728679=0 887770454=0 491728531=-1 1393501683=5 371995505=-1 914153475=-2
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function y = f(x) y = 1 - (1+x).^-9 - (140/26.5)*x //função cuja raiz é procurada endfunction function y = d(x) y = 9*(1+x).^-10 - (140/26.5) //derivada da função endfunction x = 0.12 //valor inicial de x while (1) x_ant = x //recebe valor de x da iteração anterior x = x_ant - f(x_ant)/d(x_ant) //ponto onde a reta que tangencia o x anterior toca o eixo Er = abs((x - x_ant)/x) if(Er < 10^-3) then //condição para parar de atualizar o x break end end
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 16.12w //calculation of the length of the shortest closed organ pipe that will resonate with the tunning fork //given data nu=264//frequency(in Hz)of the tunning fork v=350//speed(in m/s) of the sound in air //calculation //from the equation of the resonate frequency of the closed organ pipe....l = (n*v)/(4*nu) n=1//for l to be minimum lmin=(v)/(4*nu)//equation of the resonate frequency of the closed organ pipe printf('the length of the shortest closed organ pipe that will resonate with the tunning fork is %d cm',lmin*10^2)
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//=============================================================== //Chapter 10 Example 17 clc;clear all; //variable declaration r = 0.0250; //resistance in Ω R = 1.0125; //resistance in Ω S = 1 //sensitivity P1 = 10; //resistance in Ω Q1 = 10; //resistamce in Ω P2 = 9.95; //resistance in Ω Q2 = 10.05; //resistamce in Ω l = 100; //calculations r1 = r/100; //resistance in Ω per scale division x1 = P1/Q1; x2 = P2/Q2; //P/Q = (R+(l1*r))/(S+(l-l1)*r) //(s*x)+((l-l1)*r) = R+(l1*r) //(S*x)+(l*r)-(l1*r) = R+(L1*r) //(S*x)+(l*r)-R = (l1*r)+(l1*r) l1 = ((S*x1)+(l*r1)-R)/(r1+r1); //scale divisions l12 = ((S*x2)+(l*r1)-R)/(r1+r1); //scale divisions //result mprintf("hence the balance is obtainde at %3.0f and 75 scale divisions",l1); mprintf("\nhence the balance is obtainde at %3.0f and 95 scale divisions",l12);
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ques5.sce
//ques5 clc disp('finding the fourier series of given function'); syms x l s=0; n=input('enter the no of terms upto each of sin terms in the expansion : '); for i=1:n bi=2/%pi*integ(x*sin(i*x),x,0,%pi); s=s+float(bi)*sin(i*x); end disp(float(s));
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function [x]=solsup(U,b) n = size(U)(1); //Nombre lignes de matrice for i=n:-1:1 if abs(U(i,i)) < %eps then error("Matrice U est non inversible"); end sum_temp = 0; for j=i+1:n sum_temp = sum_temp + U(i,j)*x(j); end x(i) = 1/U(i,i)*(b(i)-sum_temp); end endfunction
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//problem 1.18 a1=1.4*2.2*1.4 x1=1.6+0.7 x11=(1.4*1.4/(12*2.3))+x1 x2=0.7 x22=(1.4*1.4/(12*0.7))+x2 z=9810 p1=z*a1*x1 p2=z*a1*x2/1.4 p=p1-p2 h=(p1*(3-x11)+p2*(1.4-x22))/p f=(p1*(3-x11)-p2*(1.4-x22))/1.4 disp(p,"resultant force") disp(f,"force acting horizontally on the top of the gate")
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Ex7_7.sce
clear // // // //Variable declaration d=0.282 //lattice spacing(nm) theta=(8+(35/60))*%pi/180 //glancing angle(radian) n=1 //order //Calculation lamda=2*d*sin(theta)/n //wavelength(nm) N=2*d/lamda //maximum order of diffraction //Result printf("\n wavelength is %0.3f nm",lamda) printf("\n maximum order of diffraction is %0.3f ",N)
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//check o/p i/p args are a matrix and a weight vector w A = [5 -4 6; 2 3 9; -1 1 2]; w = [0.5 0.25 0.25]; v=var(A,w); disp(v); // 6.1875 9.5 6.1875
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//Problem 40.22: Calculate the value of the energy stored when a current of 50 mA is flowing in a coil of inductance 200 mH. What value of current would double the energy stored? //initializing the variables: L = 0.2; // in H I = 0.05; // in Amperes u0 = 4*%pi*1E-7; ur = 1; //calculation: //energy stored in inductor W = L*I*I/2 //current I I = (2*2*W/L)^0.5 printf("\n\n Result \n\n") printf("\nenergy stored in inductor is %.2E J",W) printf("\ncurrent I is %.2E A",I)
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clear // p=30 i=10 v=p/i dt=1 dq=i*dt dw=v*dq energy=dw/i printf("\n energy of each coulomb of charge= %0.1f J",energy)
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clc //the code uses userdefined function complexstring function s=complexstring(a) if imag(a)>=0 then s=sprintf('%g+%gi',real(a),imag(a)) else s=sprintf('%g%gi',real(a),imag(a)) end funcprot(0) endfunction E1=2400 //primary voltage rating in volts E2=240 //secondary voltage rating in volts z=2 //magnitude of impedance connected to secondary terminals in ohms pha1=36.9 //phase angle of impedance connected with reference in degrees a=E1/E2 mprintf("a=%d\n",a) V1=2200 // applied primary voltage to transformer in volts V2=V1/a mprintf("|V2|=|V1|/a=%dV\n",V2) I2=V2/(z*exp(pha1*%i*3.14/180))//ans in textbook is wrong,conversion of degree to radian for calculation disp('I2='+complexstring(I2)+'A') I1=I2/a //ans may vary due to roundoff error disp('I1=I2/a='+complexstring(I1)+'A') Zin=V1/I1 disp('Zin=V1/I1='+complexstring(Zin)+'Ω') S2=V2*I2 pf=0.8 //power factor of load mprintf("|S2|=|V2||I2|=%fkVA\n",(abs(V2)*abs(I2))/1000) mprintf("P2=|S2|*cosθ2=%fkW\n",(abs(S2)*pf)/1000) mprintf("|S1|=|V2||I1|=%fkVA\n",(abs(V1)*abs(I1))/1000) mprintf("P1=|S1|cosθ1=%fkW\n",((abs(V1)*abs(I1))*cos(pha1*3.14/180))/1000)//ans may vary due to roundoff error,conversion of degree to radian for calculation
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//Initilization of variables F1=90 //lb theta1=((40*%pi)/180) //radians theta2=((30*%pi)/180) //radians //Calculations R_x=0 //lb R_y=20 //lb //Taking the sum of forces in the X-Direction P=((F1*cos(theta1))/cos(theta2)) //lb //Taking the sum of the forces in the Y-Direction F=(P*sin(theta2))+(F1*sin(theta1))-20 //lb //Results clc printf('The value of P is:%f lb\n',P) //lb printf('The value of F is:%f lb',F) //lb
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//Variable declaration chi=-0.4*10**-5; //magnetic susceptibility H=5*10**5; //magnetic field(A/m) mew0=4*%pi*10**-7; //Calculation B=mew0*H*(1+chi); //flux density(Wb/m**2) M=chi*H; //magnetic moment(A/m) //Result printf('flux density is %0.3f Wb/m**2 \n',(B)) printf('magnetic moment is %0.3f A/m \n',M)
0bad2467a8783eec84988e33efc8e05624773a5c
449d555969bfd7befe906877abab098c6e63a0e8
/2417/CH8/EX8.8/Ex8_8.sce
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no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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Ex8_8.sce
//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 8.8\n\n\n"); // Chapter 8 : Vapor Power Cycles // Problem 8.8 (page no. 387) // Solution //Neglecting the pump work,we have heatrate=3413/0.273; //Unit:Btu/kWh //0.273=efficiency //1 kWh=3413 //heat rate printf("The heat rate is %f Btu/kWh\n",heatrate); //Per pound of steam,1515-1150.5=364.5 Btu is delivered. //Because 1 kWh=3413 printf("The steam rate is %f lbm of steam per kilowatt-hour\n",3413/(1515-1150.5));
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/3050/CH2/EX2.2/Ex2_2.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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Ex2_2.sce
//calculating GCV and NCV //Example 2.2 clc clear C=90//percentage of Carbon in coal O=2//percentage of Oxygen in coal H=4//percentage of Hydrogen in coal S=2.5//percentage of Sulphur in coal N=1//percentage of Nitrogen in coal GCV=((8080*C)+(34500*(H-O/8))+(2240*S))/100//gross calorific value in kcal/kg NCV=(GCV-(0.09*H*587))//net calorific value in kcal/kg printf('Thus the gross calorific value of coal = %4.2f kcal/kg',GCV) printf('\n and the net calorific value of coal = %4.2f kcal/kg',NCV)
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/Anti Overhead Jumps Click .sce
7c4bcac4b2ef30f8f349cea5b0298f2335aa53c4
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MBHuman/Scenarios
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refs/heads/master
2023-01-14T02:10:25.103083
2020-11-21T16:47:14
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Anti Overhead Jumps Click .sce
Name=Anti Overhead Jumps Click PlayerCharacters=Quaker BotCharacters=Quaker Bot Fast Strafes.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Quaker AddedBots=Quaker Bot Fast Strafes.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=360circHighgr.map MapScale=4.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=3.0 ScorePerKill=100.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Hyperscape WeaponHeroTag=Lightning Gun, LG DifficultyTag=4 AuthorsTag=sdk BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Close quarter combat against a fast strafing bot GameVersion=2.0.0.2 ScorePerDistance=0.03 MBSEnable=false MBSTime1=0.08 MBSTime2=1.3 MBSTime3=1.3 MBSTime1Mult=20.0 MBSTime2Mult=45.0 MBSTime3Mult=45.0 MBSFBInstead=false MBSRequireEnemyAlive=false [Aim Profile] Name=Default MinReactionTime=0.1 MaxReactionTime=0.2 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.005 FlickFOV=60.0 FlickSpeed=2.0 FlickError=3.0 TrackSpeed=7.0 TrackError=1.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.1 MaxRecenterTime=0.2 OptimalAimFOV=60.0 OuterAimPenalty=0.3 MaxError=10.0 ShootFOV=50.0 VerticalAimOffset=60.0 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=Quaker Bot Fast Strafes DodgeProfileNames=Short Strafes Jumping DodgeProfileWeights=2.0 DodgeProfileMaxChangeTime=2.5 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;2.0;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=Quaker SeeThroughWalls=true NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Quaker MaxHealth=10000.0 WeaponProfileNames=;;Manwing;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1100.0 MaxCrouchSpeed=500.0 Acceleration=7500.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=1000.0 Gravity=3.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=Jump.abilmov;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=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=100.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Short Strafes Jumping MaxTargetDistance=751.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=1.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.5 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 [Weapon Profile] Name=Manwing Type=Hitscan ShotsPerClick=1 DamagePerShot=200.0 KnockbackFactor=0.1 TimeBetweenShots=0.384615 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=9999 AmmoPerShot=1 ReloadTimeFromEmpty=2.1 ReloadTimeFromPartial=2.1 DamageFalloffStartDistance=5000.0 DamageFalloffStopDistance=5000.0 DamageAtMaxRange=200.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.5 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 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=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=8 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=4.0 MinRecoilUp=4.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.025 TimeToRecoilReset=0.29 AAMode=2 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=0.5 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=Jump MaxCharges=1.0 ChargeTimer=2.5 ChargesRefundedOnKill=0.0 DelayAfterUse=4.0 FullyAuto=false AbilityDuration=0.0 LockDirectionForDuration=true NegateGravityForDuration=false MainVelocity=900.0 MainVelocityCanGoVertical=true MainVelocitySetToMovementKeys=false UpVelocity=3000.0 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=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -760.000000 664.000000 400.000000 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//Chapter 18 //Example 18_13 //Page 440 clear;clc; a=1*(cosd(120)+%i*sind(120)); r=1; vry=200; vyb=346; vbr=400; //referring to the phasor diagram //vbr is twice vry, ie, factor =2 //vyb=1.75 times vry alpha=acosd((1+1.75*cosd(90))/2); Vry=vry*(cosd(180)+%i*sind(180)); Vyb=vyb*(cosd(90)+%i*sind(90)); Vbr=vbr*(cosd(-alpha)+%i*sind(-alpha)); printf("Vry = %.2f+j(%.2f) V \n", real(Vry), imag(Vry)); printf("Vyb = %.2f+j(%.2f) V \n", real(Vyb), imag(Vyb)); printf("Vbr = %.2f+j(%.2f) V \n\n", real(Vbr), imag(Vbr)); Ir=Vry/sqrt(3); Iy=Vyb/sqrt(3); Ib=Vbr/sqrt(3); disp("Line current : "); printf("Ir = %.2f /_%.2f A \n", abs(Ir), atand(imag(Ir)/real(Ir))+180); printf("Iy = %.2f /_90 A \n", abs(Iy)); printf("Ib = %.2f /_%.2f A \n\n", abs(Ib), atand(imag(Ib)/real(Ib))); Ir0=1/3*(Ir+Iy+Ib); Ir1=1/3*(Ir+a*Iy+a^2*Ib); Ir2=1/3*(Ir+a^2*Iy+a*Ib); printf("Ir0 = %d A \n", abs(Ir0)); printf("Ir1 = %.2f /_%.2f A \n", abs(Ir1), atand(imag(Ir1)/real(Ir1))-180); printf("Ir2 = %.2f /_%.2f A \n", abs(Ir2), atand(imag(Ir2)/real(Ir2)));
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//Example 3-5, Page No - 108 clear clc It = 5.1 Ic =4.8 m=(2*((It/Ic)^2-1))^0.5 printf('The percentage of modulation is %.1f',m*100)
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clc; clear all; f = 7e6; // Ultrasonic frquency in hertz theta = 45; v = 1.5; // Blood velocity in m/s U = 1500; // Ultrasonic velocity in m/s deltaf = (2*f*v*cosd(45))/U disp('Hz',deltaf,'The frequency of the doppler flowmeter is') //Variation in anser as compared to textbook..checked in calculator also.. there is mistake in the book..
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pathname=get_absolute_file_path('17_3.sce') filename=pathname+filesep()+'17_3_data.sci' exec(filename) //Brake power bp=(2*%pi*N*T)/60000 //Friction power fp=ip-bp //Percentage losses Loss=fp/bp*100 printf("\n\nRESULTS\n\n") printf("\nPercentage losses:%f\n",Loss)
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clc; p=2; // number of poles f=50; // frequency of machine D=1.6; // diameter of cylindrical rotor l=1.8; // length of cylindrical rotor g=0.012; // air gap length rm=4000; // peak value of rotor mmf rs=6000; // peak value of stator mmf ph=140; // phase difference between stator mmf and rotor mmf uo=4*%pi*10^-7; // free space permeability0 disp('a'); rp=sqrt(rm^2+rs^2+2*rm*rs*cosd(ph)); printf('Resultant peak gap mmf is %f AT/pole\n',rp); disp('b'); Bp=(uo*rp)/g; printf('Peak gap flux density is %f T\n',Bp); disp('c'); ge=(uo*%pi*D*l*rp^2)/(4*g); printf('Total gap energy is %f Joules\n',ge); disp('d'); T=(p*uo*%pi*D*l*rs*rm*sind(ph))/(4*g); printf('Electromagnetic torque is %f Nm\n',T); disp('e'); wm=(4*%pi*f)/2; // synchronous speed P=(T*wm)/1000 printf('Electromagnetic power is %f KW',P);
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clc // Fundamental of Electric Circuit // Charles K. Alexander and Matthew N.O Sadiku // Mc Graw Hill of New York // 5th Edition // Part 2 : AC Circuits // Chapter 9 : Sinusoids and Phasors // Example 9 - 3 clear; clc; close; // // Given data Z1 = complex(40*cosd(50.0000),40*sind(50.0000)); Z2 = complex(20*cosd(-30.0000),20*sind(-30.0000)); Z3 = complex(10*cosd(-30.0000),10*sind(-30.0000)); Z4 = complex(3.0000,-4.0000); Z5 = complex(2.0000,4.0000); Z6 = conj(complex(3.0000,-5.0000)); // // Calculations Part a Ztot_a = Z1 + Z2; Ztot_a_mag = norm(Ztot_a); Ztot_a_angle = atand(imag(Ztot_a),real(Ztot_a)) Ztot_mag_a = sqrt(Ztot_a_mag); Ztot_angle_a = 0.500 * Ztot_a_angle; // Calculations Part b Ztot_b = (Z3 + Z4)/(Z5*Z6); Ztot_mag_b = norm(Ztot_b); Ztot_angle_b = atand(imag(Ztot_b),real(Ztot_b)); // disp("Example 9-3 Solution : "); disp("a. Part a : "); printf(" \n Ztot_mag_a = Magnitude of Ztot a = %.3f ",Ztot_mag_a) printf(" \n Ztot_angle_a = Angle of Ztot a = %.3f degree",Ztot_angle_a) disp("") disp("b. Part b : "); printf(" \n Ztot_mag_b = Magnitude of Ztot b = %.3f ",Ztot_mag_b) printf(" \n Ztot_angle_b = Angle of Ztot b = %.3f degree",Ztot_angle_b)
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// ch-1 page-36,37 pb-7 // // BE=50 AB=25 AEC=157.5-67.5 al=atan(BE/AB) al=al*(180/%pi) printf("\n al %0.3f ",al) bt=90-al printf("\n bt= %0.3f ",bt) k=(tan(bt*%pi/180)) printf("\n k= %0.3f ",k) BC=BE/k C=275.5+BC printf("\n chinage of c is %0.3f meters',C)
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// Scilab code Exa3.8 : : Page 125(2011) clc; clear; x = 0.25; // Thickness of Al, metre U_l = 1/x*log(50); // Linear absorption coefficient d = 2700; // density of the Al, Kg per cubic centimetre x_h = log(2)/U_l; // Half value thickness of Al, metre U_m = U_l/d; // Mass absorption coefficient, square metre per Kg printf("\nThe half value thickness of Al = %6.4f Kg per cubic metre \nThe mass absorption coefficient = %7.5f square metre per Kg ",x_h, U_m); // Result // The half value thickness of Al = 0.0443 Kg per cubic metre // The mass absorption coefficient = 0.00580 square metre per Kg
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//chapter 1 Ex 17 clc; clear; close; dividend=2010; divisor=19; mod=modulo(dividend,divisor); //remainder printf("The least number to be added is %d",(divisor-mod));
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clc //initialisation of variables ph=13.89 //pressure in bar under 36 degrees temp p1=1.447 //pressure in bar under -26 degrees temp h1=1411.4 //kj/kg s1=5.718 //kj/kgk h2=1561.7 //kj/kg h3= 150 //kj/kg h4=185.8 //kj/kg h5=1445.5 //kj/kg s5=5.327 //kj/kgk s5=5.327 //kj/kgk h6=1607.6 //kj/kg r=25 //CALCULATIONS pi=(p1*ph)^0.5 m1=(3.5164*r)/(h1-h4) mh=m1*(h2-h3)/(h5-h1) poc=m1*(h2-h1) pohc=mh*(h6-h5) pr=poc+pohc re=h1-h4 wi=(h2-h1)+(h6-h5) cop=re/wi //RESULTS printf('power of lp compressor is %2fkw',poc) printf('\npower of hp compressor is %2fkw',pohc) printf('\ntotal power required is %2fkw',pr) printf('\nrefrigerating effect is%2fkj/kg',re) printf('\ncoefficient of performance is %2f',cop)
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//Chemical Engineering Thermodynamics //Chapter 3 //First Law of Thermodynamics //Example 3.12 clear; clc; //Given W = 0;//pump work Mi = 0;//chamber is initially evacuated M2 = 0;//no exist stream H1 = 684.2;//enthalpy of steam at 200 deg cel & 3 Kgf/cm^2 //To calculate the internal energy of the steam in the chamber //Q=150*m1;.. (a) heat lost from the chamber in Kcal/Kg //m1=mf;..(b) mass of steam added from large pipe is equal to steam in chamber //H1*M1-Q=Mf*Ef; using (a)&(b) Ef = H1-150; mprintf('The internal energy of steam in chamber is %f Kcal',Ef); //end
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clear // //variable declaration P1=5.0 //Inclined at 45° down Loading at 3m distance from A,KN P2=10.0 //Inclined at 45° down Loading at 2m distance from A,KN P3=10.0 //Inclined at 45° down Loading at 1m distance from A,KN P4=5.0 //Inclined at 45° down Loading A,KN P8=5.0 //Inclined at 45° UP Loading at 3m distance from A,KN P7=10.0 //Inclined at 45° UP Loading at 2m distance from A,KN P6=10.0 //Inclined at 45° UP Loading at 1m distance from A,KN P5=5.0 //Inclined at 45° UP Loading A,KN a=1.0 theta=45.0*%pi/180.0 //The roof is inclined at 45° to horizontal and loads are at 90° to the roof. Hence, the loads are also inclined at 45° to vertical/horizontal. //assume Resulat R at distance d from A, //sum of vertical Fy & sum of horizontal forces Fx is zero //Assume direction of Fx is right //Assume direction of Fy is up Rx=(P1+P2+P3+P4+P5+P6+P7+P8)*cos(theta) Ry=-(P1+P2+P3+P4)*sin(theta)+(P5+P6+P7+P8)*sin(theta) printf("\n R= %0.3f KN",Rx) //and its direction is horizontal //Let R be at a distance d from the ridge A //moment at A d=((P1*3*cos(theta)*a+P2*cos(theta)*2*a+P3*cos(theta)*a)*2)/(Rx) printf("\n d= %0.1f m \n Resultant is a horizontal force of magnitude %0.3f at %0.1f m below A.",d,Rx,d)
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//check o/p when i/p is a vector v =[8 9 1 10 6 1 3 6 10 10]; m=cummin(v); disp(m); //output // column 1 to 7 // // 8. 8. 1. 1. 1. 1. 1. // // column 8 to 10 // // 1. 1. 1.
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// 18/04 x = linspace(0,1,100) plot(x,x^2)
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no_logfile = true; begin; picture { background_color = 153,153,153; } et_calibration; #stimulus display graphics. array { bitmap { filename = "dixie.jpg"; preload = false; scale_factor = 2.0; }; bitmap { filename = "town.jpg"; preload = false; scale_factor = 2.0; }; } graphics; #cursor for left eye ellipse_graphic { ellipse_height = 50; ellipse_width = 50; color = 0,255,0; } left_cursor; #cursor for right eye ellipse_graphic { ellipse_height = 50; ellipse_width = 50; color = 0,0,255; } right_cursor; trial { picture { # placeholder - set by PCL box { height = 1; width = 1; color = 0,0,0; }; x = 0; y = 0; } pic1; } trial1; begin_pcl; # utility function returns the last button press sub int get_last_button_press_id(string buttonstr ) begin if buttonstr.count() >0 then array <string> starr[2]; buttonstr.split(" ",starr); return int(starr[1]); end; return 0; end; int dheight = display_device.height(); int dwidth = display_device.width(); int x =0; int y =0; #initialize PresLink. eye_tracker tracker = new eye_tracker( "PresLink" ); #tracker.set_parameter("tracker_address", ""); # running as dummy mode #connect to Eyelink tracker. tracker.start_tracking(); #tracker.set_parameter("dc_err_sound", "on"); #turn on/off drift correction error sound string tracker_ver = tracker.get_parameter("tracker_version"); #tracker_ver would be something like EYELINK CL 4.48, but we want to get the 4.48 array <string> starr[5]; tracker_ver.split(" ",starr); double tr_v = double(starr[3]); #open edf file on the tracker. string edf_name = "track.edf"; if(logfile.subject().count() >0) then edf_name = logfile.subject() + ".edf"; end; tracker.set_parameter("open_edf_file",edf_name); #set preamble tracker.send_command("add_file_preamble_text 'PresLink Example 1'"); string msg_res = "0 0 "; msg_res.append(string(dwidth-1)); msg_res.append(" "); msg_res.append(string(dheight-1)); string msg_coord = "DISPLAY_COORDS 0 0 "; msg_coord.append(string(dwidth-1)); msg_coord.append(" "); msg_coord.append(string(dheight-1)); tracker.set_parameter("screen_pixel_coords", msg_res); tracker.send_message(msg_coord); tracker.set_parameter("file_event_filter", "LEFT,RIGHT,FIXATION,SACCADE,BLINK,MESSAGE,BUTTON,INPUT"); tracker.set_parameter("link_event_filter","LEFT,RIGHT,FIXATION,SACCADE,BLINK,BUTTON,INPUT"); if (tr_v >=4.0) then tracker.set_parameter("link_sample_data" ,"LEFT,RIGHT,GAZE,GAZERES,AREA,STATUS,HTARGET,INPUT"); tracker.set_parameter("file_sample_data", "LEFT,RIGHT,GAZE,AREA,GAZERES,STATUS,HTARGET,INPUT"); else tracker.set_parameter("link_sample_data","LEFT,RIGHT,GAZE,GAZERES,AREA,STATUS,INPUT"); tracker.set_parameter("file_sample_data", "LEFT,RIGHT,GAZE,AREA,GAZERES,STATUS,INPUT"); end; #program button #5 for use in drift correction tracker.send_command("button_function 5 'accept_target_fixation'"); #tell the tracker to use 9 point calibration. tracker.set_parameter("calibration_type","HV9"); #tell PresLink that we need gaze data for both eyes (if available) tracker.start_data( et_left, dt_position, false ); tracker.start_data( et_right, dt_position, false ); loop int i = 1 until i > graphics.count() begin #-----------------------CALIBRATION---------------------- # #tell PresLink to use the target.bmp as the target - taken from stimulus_directory. #otherwise the default crosshairs target will be displayed. #string target_fname = stimulus_directory +"target.bmp"; #tracker.set_parameter("target_file",target_fname); #clear out the default calibration target so that we don't get data from previous drawing. et_calibration.set_background_color(153,153,153); et_calibration.clear(); et_calibration.present(); #start calibration with camera support tracker.calibrate( et_calibrate_default, 1.0, 0.0, 0.0 ); #drift correct at (0,0) with the options to allow Camera Setup and to draw a target tracker.calibrate( et_calibrate_drift_correct, 7.0, 0.0, 0.0 ); #load the image. graphics[i].set_load_size(double(display_device.height()),double(display_device.width()),0.0); graphics[i].load(); pic1.clear(); #remove all pic1.add_part(graphics[i],0,0); # #Send viewer integration messages and tracker commands to monitor recording. # tracker.send_command("clear_screen 0"); # This supplies the title at the bottom of the eyetracker display string msg = "record_status_message 'TRIAL "; msg.append(string(i)); msg.append("/"); msg.append(string(graphics.count())); msg.append("'"); tracker.send_command(msg); # Always send a TRIALID message before starting to record. # It should contain trial condition data required for analysis. msg= "TRIALID TRIAL "; msg.append(string(i)); tracker.send_message(msg); # TRIAL_VAR message is recorded for EyeLink Data Viewer analysis # It specifies the list of trial variables value for the trial # This must be specified within the scope of an individual trial (i.e., after # "TRIALID" and before "TRIAL_RESULT") msg = "!V TRIAL_VAR TRIAL_IMAGE "; msg.append(graphics[i].filename()); tracker.send_message(msg); # IMGLOAD command is recorded for EyeLink Data Viewer analysis # It displays a default image on the overlay mode of the trial viewer screen. # Writes the image filename + path info msg = "!V IMGLOAD FILL "; msg.append(graphics[i].filename()); tracker.send_message(msg); #image transfer to EyeLink screen: #image format can be 24bit bmp, jpg, or gif. tracker.set_parameter("transfer_image",graphics[i].filename()); #set the the tracker to idle mode. tracker.send_command("set_idle_mode"); #give some time for the tracker to switch mode. wait_interval(50); #start recording tracker.set_recording(true); #present the stimulus trial1.present(); #mark the time we presented the stimulus tracker.send_message("SYNCTIME"); #get the available eye. int eye_av = int(tracker.get_parameter("eye_available")); int left_index = 2; int right_index = 3; if(eye_av == 0) then pic1.add_part(left_cursor,0,0); left_index = 2; right_index = -1; elseif(eye_av == 1) then pic1.add_part(right_cursor,0,0); right_index = 2; left_index = -1; else pic1.add_part(left_cursor,0,0); pic1.add_part(right_cursor,0,0); end; bool button_pressed = false; loop int end_time = clock.time() + 25000 until clock.time() >= end_time || button_pressed begin int modified = 0; #check for new button presses button_pressed = get_last_button_press_id(tracker.get_parameter("last_button_press"))!=0; if ((eye_av == 0 || eye_av == 2)) then #we have left data OR both eye data if(tracker.new_position_data(et_left) >0) then eye_position_data epd = tracker.last_position_data(et_left); pic1.set_part_x( left_index, epd.x()); pic1.set_part_y( left_index, epd.y()); modified = 1; end; end; if ((eye_av == 1 || eye_av == 2)) then #we have right data OR both eye data if(tracker.new_position_data(et_right) >0) then eye_position_data epd = tracker.last_position_data(et_right); pic1.set_part_x( right_index, epd.x()); pic1.set_part_y( right_index, epd.y()); modified = 1; end; end; if(modified == 1) then trial1.present(); end; modified = 0; end; pic1.clear(); pic1.set_background_color(153,153,153); pic1.present(); wait_interval(100); #stop recording. tracker.set_recording(false); msg= "TRIAL_RESULT "; msg.append(string(0)); tracker.send_message(msg); graphics[i].unload(); i = i + 1 end; #close file before transfer is required tracker.send_command("set_idle_mode"); wait_interval(500); tracker.set_parameter("close_data_file", ""); wait_interval(100); #transfer the edf file. Note Presentation places files specified without a path in the user's home directory. #in this example pres_1.edf will be placed in your home directory. (eg. in xp C:\documents and settings\<username> string edf_fname = logfile_directory + edf_name; tracker.set_parameter("get_edf_file",edf_fname); tracker.stop_tracking();
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clc; y=1.135; p1=10; pc=p1*[2/(y+1)]^[(y/(y-1))]; h1=2778; hc=2675; xc=0.962; vg=0.328; vc=xc*vg; Cc=(2*[h1-hc]*10^3)^0.5; A_m=vc/Cc*10^6; disp(A_m);
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function link_id = mdaq_open() global %microdaq; link_id = -1; result = 0; [ip_address, result] = mdaq_get_ip(); if result < 0 then disp("ERROR: Unable to get IP address - run microdaq_setup!"); return; end link_id = mdaq_connect(ip_address, 4343); if link_id == -1 then ulink(%microdaq.private.mlink_link_id); exec(mdaq_toolbox_path()+filesep()+"etc"+filesep()+.. "mlink"+filesep()+"MLink.sce", -1); link_id = mdaq_connect(ip_address, 4343); end endfunction
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Turbomachinery Design and Theory,Rama S. R. Gorla and Aijaz A. Khan, Chapter 4, Example 4") //Impeller tip diameter = 1m //Speed = 5945 rpm //Mass flow rate of air = 28 kg/s //Static pressure ratio p3/p1 = 2.2 //Atmospheric pressure = 1 bar //Atmospheric temperature = 25 degree Celcius //Slip factor = 0.90 disp("Neglect the power input factor.") disp("The impeller tip speed is given by:") D = 1; N = 5945; U2 = %pi*D*N/60 disp("The work input:") sigma = 0.9; W = sigma * U2^2 / 1000 disp("Using the isentropic P–T relation and denoting isentropic temperature by T3a, we get:") T1 = 298; r = 2.2; T3a = T1 * (r)^ 0.286 disp("Hence the isentropic temperature rise: T3a - T1") rise = T3a -T1 disp("The temperature equivalent of work done: T3 - T1") Cp = 1.005 Weq = W/Cp disp("The compressor adiabatic efficiency is given by:") etac = rise/Weq * 100 disp("The air temperature at the impeller exit is:") T3 = T1 + Weq disp("Power input:") m = 28; P = m * W
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function [i,j]=num2pos(k) //S = sudoku with 9 rows and 9 columns //k = element's position number //(i,j)=position of the entry in the sudoku i=1+pmodulo(k-1,9) j=1+(k-i)/9 endfunction
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// Exercise E3 // ------------ // Implement the cholesky analysis for a band and symmetric array // so that you avoid unnecessary calculations. // --------------------------------------------------------- function L=cholesky(A) [m,n]=size(A); if m~=n then disp('matrix u is not square'); return; end for k=1:n for i=1:k-1 s=0; if (i~=1) then s=A(i, 1:i-1)*A(k, 1:i-1)'; end A(k,i)=(A(k,i)-s)/A(i,i); end s=0; if(k~=1) then s=A(k, 1:k-1)*A(k, 1:k-1)'; end A(k,k)= (A(k,k)-s)^0.5; end L=tril(A); endfunction // --------------------------------------------------------- function L=choleskyBand(A) [m,n]=size(A); if m~=n then disp('matrix u is not square'); return; end for k=1:n for i=1:k-1 s=0; if (i~=1) then s=A(i, i-1)*A(k, i-1); end A(k,i)=(A(k,i)-s)/A(i,i); end s=0; if(k~=1) then s=A(k, k-1)*A(k, k-1); end A(k,k)= (A(k,k)-s)^0.5; end L=tril(A); endfunction // --------------------------------------------------------- // Creates a sample table for testing function A=Table(n) // n is the size of the array A=zeros(n,n); // initially fill it with zeros A(1,1)=2; A(1,2)=-1; for i=2:n-1 A(i,i-1)=-1; A(i,i)=2; A(i,i+1)=-1; end A(n,n-1)=-1; A(n,n)=2; endfunction // ---------------------------------------------------------
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clc; close(); clear(); //page no 535 //prob no. 16.13 n1=1; //refraction index of air E2=4 //material dielectric constant theta_i=50 //angle of incidence in degree (misprinted in the solution) n2=sqrt(E2); theta_r=asin(n1/n2*sin(theta_i*%pi/180)); mprintf(' The angle of refraction is %.2f \n (using angle of incidence =50)\n',theta_r*180/%pi); //misprinted angle
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Vp=3; Vm=4.5; t=0:0.01:2*10; Vm = Vm*(sin(2*3.14*t)) ; subplot(311); plot(Vm); subplot(312); plot(Vp*Vm*(sin(2*3.14*t)));
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clc; F=300 // N , given force AB=sqrt(8^2+6^2);// m Length of AB cos_alpha=8/AB; sin_alpha=-6/AB; Fx=F*cos_alpha;//N, Horizontal component Fy=F*sin_alpha;// N, Vertical Component printf("Horizontal component of F is %.2f N\n",Fx); printf("Vertial component of F is %.2f N\n",Fy); printf("We may write F as \n F = %.2f i + %.2f j",Fx,Fy);
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// // // Generates C file and corresponding headers for filters used in // C implementation // clear(); exec('sci_vor_filters.sci'); [filters] = vor_get_filters(); filter_name = [ "BP_VAR" "BP_REF" "LP_DECIM" "LP_VAR" "LP_REF" "LP_FM" ]; function print_poly(fid, name, p, header) c_p = coeff(p); l_p = length(c_p); l_ps = name+'_LEN'; if (header) fprintf(fid, '#define %s %i\n', l_ps, l_p); fprintf(fid, 'extern FLOAT_T %s[];\n', name); else fprintf(fid, 'FLOAT_T %s[%s]={\n', name, l_ps); for i=l_p:-1:1 fprintf(fid,'%10.40f,\n',c_p(i)); end fprintf(fid,'};\n'); end endfunction // // header // filename = 'vor_filter_params'; fid = mopen(filename+'.h', 'w'); fprintf(fid,'#ifndef VOR_LF_FILTER_PARAMS_H\n'); fprintf(fid,'#define VOR_LF_FILTER_PARAMS_H\n\n'); for i=1:FILTER_NB f = filters(i); fn = filter_name(i); fprintf(fid,'/* %s filter */\n', fn); print_poly(fid, fn+"_NUM", f.tf.num, 1); print_poly(fid, fn+"_DEN", f.tf.den, 1); fprintf(fid,'\n'); end fprintf(fid,'#endif /* VOR_LF_FILTER_PARAMS_H */\n'); mclose(fid); // // C // fid = mopen(filename+'.c', 'w'); fprintf(fid,'#include ""%s.h""\n\n', filename); for i=1:FILTER_NB f = filters(i); fn = filter_name(i); print_poly(fid, fn+"_NUM", f.tf.num, 0); print_poly(fid, fn+"_DEN", f.tf.den, 0); fprintf(fid,'\n'); end mclose(fid);
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clc //Example 8.13 //Calculate temperature and the velocity of air inside the shock wave //Let subscript y denote air inside the shock wave and x denote the air outside the shock wave ratio_T=1.2309//dimentionless Tx=528//R (Rankine temperature scale) Ty=ratio_T*Tx//R (Rankine temperature scale) printf("temperature of air inside the shock wave is %f R\n",Ty); My=0.7558//dimentionless cy=1249//ft/s Vy=My*cy//ft/s printf("the velocity of air inside the shock wave is %f ft/s",Vy);
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function r=mtlb_prod(a) // Copyright INRIA if type(a)==4 then a=bool2s(a);end if size(a,1)==1|size(a,2)==1 then r=prod(a) else r=prod(a,1) end
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figure(1); a = gca(); a.box = "off"; a.filled = "on"; a.isoview = "on"; a.data_bounds = [-2;2;-2;2]; a.grid=[1,1]; for t=0:0.1:1 robot1 = [t;0;0;0;0;0.3]; robot2 = [t;1;0;0;0;0.2]; delete(a.children); drawlater(); drawTurtleSide(robot1(1),robot1(3),0.6); drawTurtleSide(robot2(1),robot2(3),0.6); drawnow(); sleep(100); end
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// Example 4.6, page no-134 clear clc p=3600 //Power required t=1.2 //worst case eclipse period c=90 //capacity of each cell in Ah v=1.3 //voltage of each cell in V d=0.8 // Depth of discharge e=0.95 //Discharge efficiency E_sp=60 //specific energy specification of the battery energy=p*t n=energy/(c*v*d*e) E_b=energy/(d*e) m=E_b/E_sp printf("No of cells, n= %.0f cells\n Energy required to be stored in the battery system is %.1f Wh\n Mass of battery system = %.2f kg",n,E_b,m)
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//(Threaded Joints) Example 7.11 //Refer Fig.7.26 on page 243 //Screw pitch circle diameter 2b (mm) b = 300/2 //Flange diameter 2a (mm) a = 400/2 //External force acting on the bearing P (kN) P = 25 //Eccentricity value l (mm) l = 150 //Maximum permissible tensile stress in the cap screw sigmaMax (N/mm2) sigmaMax = 50 //Number of cap screws n n = 4
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//chapter 13 //example 13.10 //page 570 printf("\n") printf("given") hfemin=100;hfemax=400;hiemin=2*10^3;hiemax=5*10^3;Rc=12*10^3;Rl=120*10^3;Re1=150 disp(" voltage gain at extreme value ") Avmax=(hfemax*((Rc*Rl)/(Rc+Rl)))/(hiemax+Re1*(1+hfemax)) Avmin=(hfemin*((Rc*Rl)/(Rc+Rl)))/(hiemin+Re1*(1+hfemin)) disp("approximate voltage gain") Av=((Rc*Rl)/(Rc+Rl))/Re1
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//EXAMPLE 26.21(c) //4-POLE DC SHUNT GENERATOR clc; funcprot(0); //Variable Initialisation P=4;.........................//Total number of poles S=80;........................//Total number of slots C=10;.........................//Total number of conductor per slots E1=400;.........................//Generated EMF at No load in Volts N1=1000;........................//Speed of the generator in rpm N2=800;.........................//Dropped speed of the generator in rpm Al=P;.........................//Number of parallel paths in a lap wound generator Z=S*C;........................//Total number of conductors E2=220;.......................//Generated open circuit voltage in Volts //Keeping speed held cnstant while changing the flux per pole printf("(i)Keeping speed held cnstant while changing the flux per pole"); Phi1=(E1*60*Al)*1000/(P*N1*Z);...........//Flux per pole in Mili Webers at 400 Volts disp(Phi1,"Flux per pole in Mili Webers at 400 Volts:"); Phi2=(E2/E1)*Phi1;....................//Flux per pole in Mili Webers at 220 Volts disp(Phi2,"Flux per pole in Mili Webers at 220 Volts:"); if Phi2<Phi1 then printf("By increasing the shunt field circuit resistance with the help of adding external rheostatic,\n"); printf("the current in the field circuit is reduced so as to decrease the flux to %0.1f mWb",Phi2); end //Keeping the same flux per pole while changing the speed printf("\n \n(ii).Keeping the same flux per pole while changing the speed"); N=(E2*60)/((Phi1/1000)*N2);................//Speed of the generator in rpm at 30 Mili Webers disp(N,"Speed of the generator in rpm at 30 Mili Webers:"); printf("Field circuit resistance must be reduced to a new value in order to obtain"); printf("\n %0.1f mWb of flux pole from a voltage of 220 V",Phi);
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#!206A,SAV_ST,+X,!5001,I, #!206B,NF_2,+X,!0000,I, #!206C,XT_,+X,!5006,F, #!206D,XOUT_,+X,!5006,F, #!206E,IN2,+X,!5005,F, #!206F,IN1,+X,!5005,F, #!2070,MUX2,+X,!5005,F, #!2071,XMAX_,+X,!5006,F, #!2072,XMIN_,+X,!5006,F, #!2073,P0_,+X,!5006,F, #!2074,KP_,+X,!5006,F, #!2075,X0_,+X,!5006,F, #!2076,SP_,+X,!5006,F, #!2077,PV_,+X,!5006,F, @TIMERS,8 #!3001,TW_1,+X,!0000 #!3002,TW_2,+X,!0000 #!3003,TW_3,+X,!0000 #!3004,TNP_3,+X,!0000 #!3005,TNP_2,+X,!0000 #!3006,TNP_1,+X,!0000 #!3007,TNP,+X,!0000 #!3008,SAV_TM,+X,!5001 @MESSAGES,0 @USP,8 #!B001,EEP_N_R #!B002,EEP_N_W #!B003,EEP_PR #!B004,EEP_EN #!B005,REAL_INT #!B006,INT_REAL #!B007,TO_A4_20 #!B008,A4_20_TO @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @FBINSTANCES,0 @END_SYMBOLS
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//ramanujan's method //example 2.21 //page 45 clc;clear;close; deff('y=f(x)','1-((13/12)*x-(3/8)*x^2+(1/24)*x^3)'); a1=13/12,a2=-3/8,a3=1/24; b1=1; b2=a1; b3=a1*b2+a2*b1; b4=a1*b3+a2*b2+a3*b1; b5=a1*b4+a2*b3+a3*b2; b6=a1*b5+a2*b4+a3*b3; b7=a1*b6+a2*b5+a3*b4; b8=a1*b7+a2*b6+a3*b5; b9=a1*b8+a2*b7+a3*b6; printf('\n\n%f',b1/b2); printf('\n%f',b2/b3); printf('\n%f',b3/b4); printf('\n%f',b4/b5); printf('\n%f',b5/b6); printf('\n%f',b6/b7); printf('\n%f',b7/b8); printf('\n%f',b8/b9); printf('\n it appears as if the roots are converging at 2')
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hipercog/PSICAT
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Saliency.sce
/** DESCRIPTION: SCENARIO FILE PROVIDES DEFAULTS, GRAPHICAL OBJECTS, AND TRIAL DEFINITIONS FOR A BLOCKED EXPERIMENT OF PRIMED KANIZSA SHAPES Author : Ben Cowley Created: 01-05-2012 Modded : 28-03-2017 */ # FIXME TODO: can do language localisation? # FIXME TODO: check all defaults are needed? scenario = "PSICAT"; pcl_file = "PSICAT.pcl"; #code that actually runs the protocol write_codes = true; # Write all codes to parallel port (for EEG acquisition) pulse_width = 16; # Seems to work fine default_font_size = 20; default_font = "Verdana"; active_buttons = 2; button_codes = 190, 199; # Response pad buttons for 2 target classes response_port_output = true; ## Test event stimulus_properties = coords, string, cond, number, congruency, string, shape, string, pritar, string, vertices, number; event_code_delimiter = ";"; # foreground and background colors need to be defined in both SDL (as below) and # in PCL (at the beginning of pcl sequence) $fg = "255, 255, 255"; #foreground color $bg = "0, 0, 0"; #background color $transparent = "1, 0, 0"; #transparency # Fixed parallel port codes, do not use these for anything else! $TASK_START = 254; $TASK_END = 255; # PSICAT Protocol codes $SOA = 144; # Stimulus onset asynchrony (or intertrial interval) $FIXA = 143; # fixation cross display. /** Blocks are preceded by 'Start block' codes with triggers: 145, 146, 147, 148, 149 Block 1 will be as follows - 151 : shape primer for congruent shape target 152 : shape target with congruent shape primer 153 : nonshape primer for incongruent shape target 154 : shape target with incongruent nonshape primer 155 : nonshape primer for congruent nonshape target 156 : nonshape target with congruent nonshape primer 157 : shape primer for incongruent nonshape target 158 : nonshape target with incongruent shape primer All following blocks use the same pattern but add +10 to the codes. */ # Timing constants for saliency task - DUR is for saliency protocol $FIXA_DUR = 100; $SOA_DUR = 500; $INTF_DUR = 150; $KNZA_DUR = 2000; begin; #########------------#############-----------##########-----------########## # General stimuli TEXT, PICS and SOUNDS /** Native Graphics */ # Empty picture picture {} default ; # Fixation cross precedes each trial picture { line_graphic { coordinates = -30,0,30,0; line_width = 3; }; x=0;y=0; line_graphic { coordinates = 0, -30, 0, 30; line_width = 3; }; x=0;y=0; ellipse_graphic { ellipse_width = 20; ellipse_height = 20; color = 0,0,0; }; x=0; y=0; } eyes_open2; ## Line, ellipse and annuli graphics for polygons line_graphic { background_color = 120, 0, 0; transparent_color = 120, 0, 0; } lyne; ellipse_graphic { background_color = 120, 0, 0; transparent_color = 120, 0, 0; } pacman_e; annulus_graphic { background_color = 120, 0, 0; transparent_color = 120, 0, 0; } annulus1; annulus_graphic { background_color = 120, 0, 0; transparent_color = 120, 0, 0; } annulus2; /** Bitmap Graphics */ bitmap { filename = "./Stimuli/noncepad.png"; } rPadPic; #bitmap { filename = "./Stimuli/W3CON_1.png";} sCRT_instr_shapePic; #bitmap { filename = "./Stimuli/W3INCON_1.png";} sCRT_instr_nonshapePic; /** Textual Graphics */ /** Next you will be shown a series of pictures of Pacman-style objects, which together will form either an invisible 3 or 4-sided shape, or no shape. This is exactly the same as you were shown before starting. Your task is to press the RIGHT key when you see a shape, and the LEFT key when you see a non-shape. Try to be fast, but accurate. */ text { caption = "Paina OIKEAA näppäintä kun kulmista muodostuu yhtenäinen nelikulmio tai kolmio ja paina VASENTA näppäintä kun yhtenäistä kuviota ei muodostu. Koekertoja on yhteensä viisi. Voit pitää tauon koekierrosten välillä. Yritä olla mahdollisimman nopea sekä mahdollisimman tarkka. "; } sCRT_text_0; /** There will be five rounds, with a break between each - When you are ready, press any key to begin. */ text { caption = "Kun olet valmis, paina mitä tahansa näppäintä aloittaaksesi."; } sCRT_text_1c; /** Now you have a moment to rest and clear your head. Another block of stimuli will presented when you press the button, and your task will remain the same. - When you are ready, press any key to begin. */ text { caption = "Nyt sinulla on hetki aikaa levätä ja tyhjentää ajatuksesi. - Kun painat nappia, käymme taas läpi samanlaisen koetilanteen kuin äsken. Tehtäväsi pysyy edelleen samana."; } sCRT_text_2; # FIXME: provide English versions text { caption = "Jäljellä on neljä kierrosta."; font_size = 40; } sCRT_text_2a; text { caption = "Jäljellä on kolme kierrosta."; font_size = 40; } sCRT_text_2b; text { caption = "Jäljellä on kaksi kierrosta."; font_size = 40; } sCRT_text_2c; text { caption = "Jäljellä on yksi kierros."; font_size = 40; } sCRT_text_2d; /** Audio clip stimuli: */ sound{wavefile {filename = "./Stimuli/instrWavs/instructions2.wav";}; attenuation = .10;} sound1_resp; sound{wavefile {filename = "./Stimuli/instrWavs/relax.wav";}; attenuation = .10;} sound2_relax; sound{wavefile {filename = "./Stimuli/instrWavs/responsepad.wav";};attenuation = .10;} sound3_resPad; #########------------#############-----------##########-----------########## # THE TRIAL SET... # First trial: send start code to port. trial { trial_duration = 1000; stimulus_event { nothing {}; } stev; nothing {}; port_code = $TASK_START; code = "Start task"; } startAll; # Last trial: send end code to port. trial { trial_duration = 50; nothing {}; port_code = $TASK_END; code = "End task"; } endAll; ## Empty picture and trial for holding Kanizsa target stimuli trial { trial_duration = $KNZA_DUR; trial_type = first_response; stimulus_event { picture {} pyc; } ev; }Kanizsa; ## fixation period trial { trial_duration = $FIXA_DUR; # Fixation cross for eyes open measurement picture eyes_open2; port_code = $FIXA; code = "Fixation Cross"; }fixation_trial; # general SOA trial trial { trial_duration = $SOA_DUR; picture default; port_code = $SOA; code = "SOA"; } SOA_trial; # Save the thing. trial { save_logfile {}; time = 0; code = "SAVE LOGFILE"; } save_trial; # Present written instructions trial { trial_duration = stimuli_length; /* Audio instructions */ stimulus_event{ sound sound3_resPad; } sCRT_instrAud_ev; /* Text instructions */ picture { text sCRT_text_0; x=0; y=0; #text sCRT_text_1; x=-200; y=200; #y=250 #bitmap sCRT_instr_shapePic; x=250; y=190; #x=350 y=250 #text sCRT_text_1a; x=-200; y=50; #y=100 #bitmap sCRT_instr_nonshapePic; x=250; y=10; #x = 300 #text sCRT_text_1b; x=0; y=-250; #y=-200 } sCRT_instrPic; time = 0; code = "PSICAT Instructions"; } sCRT_instr_trial; trial{ trial_duration = forever; trial_type = first_response; /* Audio instructions */ stimulus_event{ sound sound1_resp; } sCRT_respAud_ev; /* Text instructions */ picture { text sCRT_text_1c; x=0; y=100; bitmap rPadPic; x=0; y=-200; } sCRT_respPic; time = 0; code = "Press to begin"; } sCRT_resp_trial;
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sortIndex.sce
// Function Name: sortIndex // Return a vector which describes the sorted order of the elements of inputvec1 (ie. it contains the indices of the elements of inputvec1) // 3rd parameter : 0/1 for ascend/descend // Calculating the sortIndex. inputvec1 = [5, 4, 3]; result = armaVec("sortIndex",inputvec1) result = armaVec("sortIndex",inputvec1,1)