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//Exa 9.2 clc; clear; close; //given data : P=200;//in KW D=20;//in Km D=D*10^3;//in m E=300*sqrt(P)/D;//in V/m disp(E*10^3,"Field Strength at 20 Km in mV/m:")
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// Functions for qualitative feature extraction //## Sample //line //to be //commented ## //## another sample //line to be commented ## exec sample_header2.sci exec abc.sce exec some_folder/yass.sci exec sample_header.sci exec sample.sci // function [NOO] = vector(something) // exec this_wont_be_expanded.sci // Some random pre-existsing comments // functions function [output1, output3] = sample_function(inputargs) endfunction function [output2] = sample_function2(inputargs) function [sum_vector, variable_with_no_return_assigned] = vector_sum(image_mat, mode_str) image_mat_size = size(image_mat); select mode_str case "cols" then // Sum of each column cols_sum = [] for i = 1 : image_mat_size(2) col_sum(1,$+1) = sum(image_mat(:,i)); // col_sum is row vector end sum_vector = col_sum; col_sum = []; case "rows" then // Sum of each row row_sum = [] for i = 1 : image_mat_size(1) row_sum(1,$+1) = sum(image_mat(i,:)); // row_sum is row vector end sum_vector = row_sum; row_sum = []; else printf("check for args"); end endfunction
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clear // // // //Variable declaration lamda=6000*10**-10 //wavelength(m) a=12*10**-7 //slit width(m) //Calculation theta=asin(lamda/a)*180/%pi //half angular width(degrees) //Result printf("\n half angular width is %0.0f degrees",theta)
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clc;funcprot(0);//EXAMPLE 7.11 //page 199 // Initialisation of Variables N=5.256*10^5;......//No. of cycles that the shaft will experience in one year F=12500;.........//applied load on shaft in lb L=96;...........//Length of Kliin produced from tool steel in in. sigma1=72000;...........//the applied stress on Shaft f=2;............//Factor of saftey of shaft sigma2=sigma1/f;......//the maximum allowed stress level //CALCULATIONS d1=(16*F*L/(sigma1*%pi))^(1/3);..........//The Diameter of Shaft in in. d2=(16*F*L/(sigma2*%pi))^(1/3);.......//The minimum diameter required to prevent failure disp(d1,"The Diameter of Shaft in in.:") disp(d2,"The minimum diameter required to prevent failure in in.:")
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clc clear //Input data W=20000 //Power developed in kW m=12 //Mass flow rate in kg/s C1=50 //Velocity of air entering in m/s T1=700+273 //Temperature of air entering in K T2=298 //Temperature of air leaving in K C2=125 //Velocity of air leaving in m/s Cp=1.005 //Specific heat capacity at constant pressure in kJ/kg-K //Calculation dh=Cp*(T2-T1) //Change in enthalpy in kJ/kg Q=((m*dh)+W-(m*(1/2000)*(C2^2-C1^2))) //The rate of heat transfer in kJ/s //Output printf('The rate of heat transfer is %3.2f kJ/s',Q)
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// 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/08/FunctionCalls/FibonacciElement/FibonacciElement.tst // FibonacciElement.asm is the result of translating both Main.vm and Sys.vm. load FibonacciElement.asm, output-file FibonacciElement.out, compare-to FibonacciElement.cmp, output-list RAM[0]%D1.6.1 RAM[261]%D1.6.1; repeat 6000 { ticktock; } output;
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clear clc //Example 5.4 MASS ACCUMULATION IN A TANK A=0.0025; //area[m^2] V=7; //velocity[m/s] rho=1000; //density[kg/m^3] mi=rho*V*A //inlet mass flow rate[kg/s] Q=0.003; //[m^3/s] mo=rho*Q //outlet mass flow rate[kg/s] //Continuity equation, mcv+mo-mi=0 mcv=mi-mo //accumulation rate[kg/s] printf("\nThe rate of water accumulating in the tank = %.1f kg/s.\n",mcv)
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clc,clear exec('milk.sce',-1) to_be_sold=zeros(500,1) //to_be_sold be the column vector that will tell us the amount of milk Akbar will decide to sell //we want to know the expected profit of akbar if he packs 1000L for (i=1:500) to_be_sold(i)=to_be_sold(i)+1000 end profit=[] //Will tell the profit of each day in Rupees for i=1:500 if demand(i)>=to_be_sold(i) x=38*to_be_sold(i)-32*to_be_sold(i) else x=38*demand(i)+30*(to_be_sold(i)-demand(i))-32*to_be_sold(i) end profit=[profit',x']' end printf('The Mean of the profit is %f\n',mean(profit))
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/tests/s/38.tst
f8f2037780255f59cd78ccb69a33e61d7f689c4d
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grenkin/compiler
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38.tst
int main(void) { int ((a)); char (b); float (*(c)); typedef int arr_int[5*2/2]; arr_int ((d)); arr_int *((d1)); arr_int (*(d2)[3-1+1]); }
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Ex4_1.sce
clc Iep=3//mA Ieh=0.01//mA Ich=0.001//mA Icp=2.99//mA gamma=Iep/(Iep+Ieh) disp(gamma,"gamma =") alphaT=Icp/Iep disp(alphaT,"alphaT =") alpha0=gamma*alphaT disp(alpha0,"alpha0 =") IE=Iep+Ieh disp(IE,"IE in mA=") IC=Icp+Ich disp(IC,"IC in mA=") ICBO=IC-alpha0*IE disp(ICBO,"ICBO in mA")
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/test/disassembler/lpmd.instr.tst
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aurelf/avrora
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lpmd.instr.tst
; @Harness: disassembler ; @Result: PASS section .text size=0x00000042 vma=0x00000000 lma=0x00000000 offset=0x00000034 ;2**0 section .data size=0x00000000 vma=0x00000000 lma=0x00000000 offset=0x00000076 ;2**0 start .text: label 0x00000000 ".text": 0x0: 0x04 0x90 lpm r0, Z 0x2: 0x14 0x90 lpm r1, Z 0x4: 0x24 0x90 lpm r2, Z 0x6: 0x34 0x90 lpm r3, Z 0x8: 0x44 0x90 lpm r4, Z 0xa: 0x54 0x90 lpm r5, Z 0xc: 0x64 0x90 lpm r6, Z 0xe: 0x74 0x90 lpm r7, Z 0x10: 0x84 0x90 lpm r8, Z 0x12: 0x94 0x90 lpm r9, Z 0x14: 0xa4 0x90 lpm r10, Z 0x16: 0xb4 0x90 lpm r11, Z 0x18: 0xc4 0x90 lpm r12, Z 0x1a: 0xd4 0x90 lpm r13, Z 0x1c: 0xe4 0x90 lpm r14, Z 0x1e: 0xf4 0x90 lpm r15, Z 0x20: 0x04 0x91 lpm r16, Z 0x22: 0x14 0x91 lpm r17, Z 0x24: 0x24 0x91 lpm r18, Z 0x26: 0x34 0x91 lpm r19, Z 0x28: 0x44 0x91 lpm r20, Z 0x2a: 0x54 0x91 lpm r21, Z 0x2c: 0x64 0x91 lpm r22, Z 0x2e: 0x74 0x91 lpm r23, Z 0x30: 0x84 0x91 lpm r24, Z 0x32: 0x94 0x91 lpm r25, Z 0x34: 0xa4 0x91 lpm r26, Z 0x36: 0xb4 0x91 lpm r27, Z 0x38: 0xc4 0x91 lpm r28, Z 0x3a: 0xd4 0x91 lpm r29, Z 0x3c: 0xe4 0x91 lpm r30, Z 0x3e: 0xf4 0x91 lpm r31, Z 0x40: 0x04 0x90 lpm r0, Z start .data:
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/Assignment 1/Decoder3To8/Decoder3To8.tst
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[]
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rohit01010/Computer-System-Design
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Decoder3To8.tst
load Decoder3To8.hdl; output-file Decoder3To8.out; output-list x2 x1 x0 y0 y1 y2 y3 y4 y5 y6 y7; set x2 0,set x1 0,set x0 0,eval,output; set x2 0,set x1 0,set x0 1,eval,output; set x2 0,set x1 1,set x0 0,eval,output; set x2 0,set x1 1,set x0 1,eval,output; set x2 1,set x1 0,set x0 0,eval,output; set x2 1,set x1 0,set x0 1,eval,output; set x2 1,set x1 1,set x0 0,eval,output; set x2 1,set x1 1,set x0 1,eval,output;
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/662/CH6/EX6.31/ex6_31.sce
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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ex6_31.sce
//Programming Example 6.31 //Averaging a list of nonnegative numbers navg=0; Sum=0; //initialize and read in a value for n printf("How many numbers ? "); n=scanf("%d"); //read in the numbers for count = 1:1:n printf("x= "); x=scanf("%f"); if x<0 then continue; end Sum=Sum+x; navg=navg+1; end //calculate the average and write out the answer average=Sum/navg; printf("\n The average is %f\n", average);
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/842/CH4/EX4.6/Example4_6.sce
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FOSSEE/Scilab-TBC-Uploads
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Example4_6.sce
//clear// //Example 4.6 // Continuous Time Fourier Transform of Symmetric // periodic Square waveform clear; clc; close; // CTFT T1 = 2; T = 4*T1; Wo = 2*%pi/T; W = -%pi:Wo:%pi; delta = ones(1,length(W)); XW(1) = (2*%pi*Wo*T1/%pi); mid_value = ceil(length(W)/2); for k = 2:mid_value XW(k) = (2*%pi*sin((k-1)*Wo*T1)/(%pi*(k-1))); end figure a = gca(); a.y_location ="origin"; a.x_location ="origin"; plot2d3('gnn',W(mid_value:$),XW,2); poly1 = a.children(1).children(1); poly1.thickness = 3; plot2d3('gnn',W(1:mid_value-1),XW($:-1:2),2); poly1 = a.children(1).children(1); poly1.thickness = 3; xlabel('W in radians/Seconds'); title('Continuous Time Fourier Transform of Periodic Square Wave')
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/1439/CH15/EX15.9/15_9.sce
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FOSSEE/Scilab-TBC-Uploads
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15_9.sce
clc //initialisation of variables pH= 4.57 M= 0.03 //mole litre^-1 M1= 0.1 //mole litre^-1 //CALCULATIONS pH1= pH+log10(M1/M) //RESULTS printf ('pH = %.2f ',pH1)
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/test_suite/strngfnx.tst
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noxdafox/clips
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(unwatch all) (clear) (set-strategy depth) (open "Results//strngfnx.rsl" strngfnx "w") (dribble-on "Actual//strngfnx.out") (batch "strngfnx.bat") (dribble-off) (load "compline.clp") (printout strngfnx "strngfnx.bat differences are as follows:" crlf) (compare-files "Expected//strngfnx.out" "Actual//strngfnx.out" strngfnx) ; close result file (close strngfnx)
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clc // Given that b_m=9.27*10^-24 // Bohr Magneton in ampere*m^2 Na=6.023*10^23 //Avogadro's Number d=8.9*10^6 // density in g/m^3 uo=4*%pi*10^-7 //Permittivity of free space A=58.71 // Atomic weight of Nickel g/mol printf("Example 18.1\n") N=d*Na/A //No. of atoms per cubic meter M=0.6*b_m*N //0.6= Bohr Magneton/atom printf("\n Part A:") printf("\n Saturation Magnetization is %.1e Ampere/m",M) M=0.6*b_m*N //0.6= Bohr Magneton/atom printf("\n\n Part B:") B=uo*M printf("\n Saturation Flux Density is %.2f Tesla\n",B);
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PL/SQL Developer Test script 3.0 13 begin --delete from DWH.DIRECT_COST_RATES; --P_DIRECT_COST_RATES(p_direct_cost_rate => .1, -- p_start_dt => date '2020-01-01'); --P_DIRECT_COST_RATES(p_direct_cost_rate => .2, -- p_start_dt => date '2020-01-02'); P_DIRECT_COST_RATES(p_direct_cost_rate => .3, p_start_dt => date '2020-01-03'); end; 0 0
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clc //initialisation of variables p= 14.7 //lbf/in^2 p1= 5 //lbf/in^2 w= 62.3 //lbf/ft^3 h= 30 //ft //CALCULATIONS hmax= (p-p1)*144/w hmin= h-hmax //RESULTS printf (' Minimum depth of the water= %.1f ft',hmin)
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dH=-57800;//Enthalpy change in cal// R=1.99;//universal gas constant// T=298;//temperture in kelvin// dn=-0.5;//change in no. of moles// dU=dH-(R*T*dn);//heat of combustion in cal// printf('The air used contains 2 mol of N2.\ndU=-57500cal.'); CpN2=8.3;//Cp value of N2// CpH2O=11.3;//Cp value of H2O// CvN2=CpN2-R;//Cv value of N2// CvH2O=CpH2O-R;//Cv value of H2O// printf('\nCv value of N2=CvN2=%fKcal deg^-1 mol^-1',CvN2); printf('\nCv value of H2O=CvH2O=%fKcal deg^-1 mol^-1',CvH2O); printf('\nSolving integration we get T2=2940K.The maximum pressure can be calculated from PV=nRT equation.'); P1=1;//initial pressure in atm// n1=3.5; n2=3; T2=2940;//final temperature in Kelvin// P2=(P1*n2*T2)/(n1*T);//maximum pressure in atm// printf('\nMaximum pressure of the reaction=P2=%fatm',P2);
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// Utility function: takes operator op // op must be a function of a vector, producing a vector // and op must be linear i.e. op(a + b) = op(a) + op(b) // and op(k*a)=k*op(b) // result: matrix m representation of op // i.e op(x) = m * x // simple linear algebra: m consists of columns op(ei) // where ei is a basis vector clc;clear function m = mkMatrix(n, op) m = zeros(n,n); e = eye(n,n); // all basis vectors for i=1:n do m(:,i) = op(e(:,i)) // apply op to e_i end endfunction function w=ff(v) n = length(v); w = zeros(n,1); for i=1:(n-1) do w(i) = 3*v(i) -v(i+1); end w(n) = v(n); endfunction m = mkMatrix(5,ff); v = [2;1;4;5;1]; sol = m \ v; // Represent each block of our system: // each block takes a incoming flow (or flows) // and produces resulting flow(s) function f2 = mixer(f1, f7) f2 = f1 + f7; endfunction function f3 = reactor(X,f2) S = [-1/3 -1 1/3 1/3 0]'; change = X * f2(2) * S; f3 = f2 + change; endfunction // takes a splitting vector Alpha function [f4, f5] = condenser(Alpha, f3) f5 = Alpha .* f3; f4 = (1 - Alpha) .* f3; endfunction // takes a purge fuctor Beta function [f6, f7] = purger(Beta, f5) f6 = Beta * f5; f7 = (1-Beta)*f5; endfunction // utility: get constituents out of the overall flow function [f1, f2, f3, f4, f5, f6, f7] = splitFlow(F) f1 = F(1:5); f2 = F(6:10); f3 = F(11:15); f4 = F(16:20); f5 = F(21:25); f6 = F(26:30); f7 = F(31:35); endfunction // A // for each block OUT = blockFunction(IN) // where IN and OUT are all parts of F // thus, mass balance is OUT - blockFunction(IN) // + constraints. In this case we specify the feed f1 // thus the constraint is simple: f1 -> f1 function b = massBalanceA(F) Alpha = [1,1,0,0,1]'; Beta = 0.12281; X = 0.6; [f1, f2, f3, f4, f5, f6, f7] = splitFlow(F); F2 = mixer(f1,f7); F3 = reactor(X, f2); [F4 F5] = condenser(Alpha,f3); [F6 F7] = purger (Beta,f5); b2 = F2 - f2; // mixer mass balance b3 = F3 - f3; // reactor mass balance b4 = F4 - f4; // condenser for f4 b5 = F5 - f5; // condenser for f5 b6 = F6 - f6; // purger for f6 b7 = F7 - f7; // purger for f7 c = f1; // constraint b = [b2;b3;b4;b5;b6;b7;c]; endfunction // RHS of mass balance feed = [0.249 0.747 0 0 0.004]'; // for all but last bit, bA must be 0 (to satisfy mass balance) bA = [zeros(30,1); feed]; AA = mkMatrix(35, massBalanceA); FA = AA \ bA; [f1A, f2A, f3A, f4A, f5A, f6A, f7A] = splitFlow(FA); factorA = 155 / f4A(3); FAfinal = factorA * FA; // B // the only change is the constraint: wwe specify f2(1), f2(2), f1(3), f1(4) // and use mol fraction of inerts in f1 (feed) x15 = 0.004 // x15 = f15/(sum f1), i.e. f15 - x15 * sum(f1) = 0 function b = massBalanceB(F) Alpha = [1,1,0,0,1]'; Beta = 0.12281; X = 0.004; [f1, f2, f3, f4, f5, f6, f7] = splitFlow(F); F2 = mixer(f1,f7); F3 = reactor(X,f2); [F4 F5] = condenser(Alpha,f3); [F6 F7] = purger (Beta,f5); b2 = F2 - f2; b3 = F3 - f3; b4 = F4 - f4; b5 = F5 - f5; b6 = F6 - f6; b7 = F7 - f7; x = 0.004; cLast = f1(5) - x * sum(f1); c = [f2(1); f2(2); f1(3); f1(4); cLast]; b = [b2;b3;b4;b5;b6;b7;c]; endfunction // f21 = 28, f22 = 70, f13=f14=0 and the constraint on inerts bB = [zeros(30,1); [28; 70; 0; 0; 0]]; AB = mkMatrix(35, massBalanceB); FB = AB \ bB; [f1B, f2B, f3B, f4B, f5B, f6B, f7B] = splitFlow(FB); factorB = 155 / f4B(3); FBfinal = factorB * FB; //================================================================= //Tutorial 7 Question 1 //================================================================= x=1:1:7;//Stream counter names=['CO2' 'H2' 'CH3OH' 'H2O' 'Inerts']';//Components flow=['Component/Flow' 'kmol/hr' 'kmol/hr' 'kmol/hr' 'kmol/hr' 'kmol/hr' 'kmol/hr' 'kmol/hr'];//Flow units frac=['Component/Molfrac' '[-]' '[-]' '[-]' '[-]' '[-]' '[-]' '[-]'];//mole frac units (dimensionless) fr=[f1B./sum(f1B) f2B./sum(f2B) f3B./sum(f3B) f4B./sum(f4B) f5B./sum(f5B) f6B./sum(f6B) f7B./sum(f7B)];//Mole fracs total=[sum(f1B) sum(f2B) sum(f3B) sum(f4B) sum(f5B) sum(f6B) sum(f7B)];//Total flows for each stream csvWrite(['Stream' string(x);flow;names string([f1B f2B f3B f4B f5B f6B f7B]);'Total' string(total);frac;names string(fr)],'streamtable_q1.csv'); //================================================================= //Tutorial 7 Question 2 //================================================================= x=[];A=[];b=[];F=[]; A=[1 1 1;0.04 0.54 0.26;0.93 0.24 0]; b=[10 2 6]'; x1=[0.2 0.6 0.2]';x2=[0.04 0.93 0.03]';x3=[0.54 0.24 0.22]';x4=[0.26 0 0.74]'; F=A\b; F1=10;F2=F(1);F3=F(2);F4=F(3); x=1:1:4; flow2=['Component/Flow' 'mol/s' 'mol/s' 'mol/s' 'mol/s']; comps=['Species 1' 'Species 2' 'Species 3']'; frac2=['Component/Molfrac' '[-]' '[-]' '[-]' '[-]']; flows=[F1.*x1 F2.*x2 F3.*x3 F4.*x4];//Species flows for each stream csvWrite(['Stream' string(x);flow2;comps string(flows);'Total' string([F1 F2 F3 F4]);frac2;comps string([x1 x2 x3 x4])],'streamtable_q2.csv');
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// This code read the KS potential and plot it potentiral profile along // a particle direction clear;clc; xdel(winsid()) // Parameter =========================================================== work_dir='C:\MyDrive\Work\CO_junc\md_cw1' // upper of td.xxxxxxxx h_par=0.2 // h parameter used in Octopus target_dir=5000 // number of target folder pot_type='Vks' // Vks, V0, Vh, Vxc, pot_line=[2,26;3,26]; // [axis1,val1;axis2,val2] line_filt=-20; pot_surf=[2,26]; //[axis, layer] surf_filt=-25; // Predef functions ==================================================== // td folder name function function name_str=td_name_conv(name_num) name_str=string(name_num); name_str='td.'+strcat(repmat('0',1,7-length(name_str)))+name_str; endfunction // Main ================================================================ // read Vks data fid=mopen(work_dir+'/'+td_name_conv(target_dir)+'/'+pot_type+'.xsf','r'); desc_lines=0 while grep(mgetl(fid,1),'DATAGRID_3D_function')==[] desc_lines=desc_lines+1 end desc_lines=desc_lines+6; data_grid=mfscanf(1,fid,'%f %f %f'); mgetl(fid,5) Vks_data=mfscanf(prod(data_grid),fid,'%f'); mclose(fid); // read Vext data fid=mopen(work_dir+'/'+td_name_conv(target_dir)+'/'+'scalar_pot-1.xsf','r'); desc_lines=0 while grep(mgetl(fid,1),'DATAGRID_3D_function')==[] desc_lines=desc_lines+1 end desc_lines=desc_lines+6; data_grid=mfscanf(1,fid,'%f %f %f'); mgetl(fid,5) Vext_data=mfscanf(prod(data_grid),fid,'%f'); mclose(fid); //Vtot_data=Vks_data+Vext_data; Vtot_data=Vks_data // reshape Vtot_data to [x,y,z] ordering Vtot_data=matrix(Vtot_data,data_grid(1),data_grid(2),data_grid(3)); // plot potetial line if prod(pot_line(:,1)==[1,2]')==1 then x=1:data_grid(3); val=squeeze(Vtot_data(pot_line(1,2),pot_line(2,2),:)); elseif prod(pot_line(:,1)==[1,3]')==1 x=1:data_grid(2); val=squeeze(Vtot_data(pot_line(1,2),:,pot_line(2,2))) elseif prod(pot_line(:,1)==[2,3]')==1 x=1:data_grid(1); val=squeeze(Vtot_data(:,pot_line(1,2),pot_line(2,2))) end val(val<=line_filt)=line_filt figure(1) plot(x,val); a=gce(); a.children.thickness=2; set(gcf(),'background',8) set(gca(),'thickness',4) set(gca(),'font_size',4); // plot potential surface select pot_surf(1) case 1 ax1=1:data_grid(2); ax2=1:data_grid(3); val=squeeze(Vtot_data(pot_surf(2),:,:)); case 2 ax1=1:data_grid(1); ax2=1:data_grid(3); val=squeeze(Vtot_data(:,pot_surf(2),:)); case 3 ax1=1:data_grid(1); ax2=1:data_grid(2); val=squeeze(Vtot_data(:,:,pot_surf(2))); end val(val<=surf_filt)=surf_filt figure(2) xset("colormap", hotcolormap(64)) Sgrayplot(ax1,ax2,val); a=gce(); a.children.thickness=2; a=gcf(); a.background=64; colorbar(min(val),max(val))
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//Variable declaration m=9.1*10**-31 k=1.38*10**-23 T=300 h=6.626*10**-34 Eg=1.1 e=1.6*10**-19 mu_e=0.48 mu_h=0.013 //Calculations ni=2*((2*%pi*m*k*T)/h**2)**(3/2)*exp(-(Eg*e)/(2*k*T)) sigma=ni*e*(mu_e+mu_h) //Result printf('Conductivity = %0.3f *10**-3 ohm**-1 m**-1 \n',(sigma*10**3))
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clear ; clc; // Example 11.3 printf('Example 11.3\n\n'); printf('Page No. 314\n\n'); //given f = 1;// feed of sodium hydroxide in kg v = 0.5;// produed vapour in kg A = 30;// in m^2 T1 = 95;// Temperature of boiling solution in deg C U = 3*10^3;// heat transfer coefficent in W/m^2-K m = 1;// feed rate in kg/s Tf = 70;// Feed temperature in deg C h_f = 260*10^3;// Enthalpy of feed in J/kg h_b = 355*10^3;// Enthalpy of boiling solution in J/kg h_v = 2.67*10^6;// Enthalpy of vapour in J/kg P1 = 0.6;// Pressure in vapour space in bar Q = (v*h_b) + (v*h_v) -(f*h_f);// in W printf('The total energy requirement is %.0f W \n',Q) // As Q = A*U*dT dT = Q/(U*A);// in degree celcius T2 = dT + T1;// in degree celcius //The temperature of the heating steam T2 corresponds to a pressure of 1.4 bar. Dry saturated steam at 1.4 bar has a total enthalpy of 2.69*10^6 J/kg //Assuming an isentropic compression of the vapour from 0.6 bar to 1.4 bar, the outlet enthalpy is 2.84*10^6 J/kg // from steam table P2 = 1.4// pressure in bar h_s = 2.69*10^6;// enthalpy of dry saturated steam in J/kg h_v2 = 2.84*10^6 ;// the outlet enthalpy of vapour in J/kg W = v*(h_v2 - h_s);// Work in W T_E = W + 60*10^3;// in W printf('The total energy consumption is %.0f W',T_E)
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// Calculating possible phase angles clc; disp ('if spot generating pattern moves in the clockwise direction') Y1=0; Y2=5; PA=asind(Y1/Y2); disp(PA,'phase angle (degree)') Y1=2.5; Y2=5; PA=asind(Y1/Y2); disp(PA,'phase angle (degree)') Y1=3.5; Y2=5; PA=asind(Y1/Y2); disp(PA,'phase angle (degree)') Y1=2.5; Y2=5; PA=180-[asind(Y1/Y2)]; disp(PA,'phase angle (degree)')
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clc; disp("Example 6.2") density= 1200 // in kg/m^3 mew= 2.25e-5 // viscosity in Pas g= 9.81 // acceleration due to gravity in m/s^2 gasdensity= 1.15 // in kg/m^3 velocity=0.2 // in m/s d=(18*mew*velocity/(g*(density-gasdensity)))^0.5 disp(d, "Maximum particle size is ")
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Ex14_23_19.sce
//Section-14,Example-3,Page no.-PC.113 //To calculate the quantity of NaOH. clc; M_m=40 //Molecular mass of NaOH pH=10 C_1=10^-pH //[H3O+] k_w=10^-14 C_2=k_w/C_1 //[OH-] C_3=C_2 //Since NaOH is a strong base [NaOH]=[OH-] A=M_m*C_3 disp(A,'Required amount of NaOH(gm)')
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Ex3_2.sce
//caption:Find change in resistance //Ex3.2 clc clear close G=2//gauge factor S=500//stress applied(in Kg/cm^2) v=2*10^6//modulus of elasticity(in Kg/cm^2) e=(S/v) R=(e*G)*100 disp(R,'change in resistance(in %)=')
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10_29.sce
clear clc a=exp(%i * 2*%pi/3) V=33 S=45 SF=2000 V2=132 Z=V2*V2/S I=S*1e6 /(sqrt(3) * V2 * 1e3) X1=.4* 60 X2=.4* 60 X0=1 * 60 x1=X1/Z x2=X2/Z x0=X0/Z xg=.0225 xt=.1 xf1=x1/2 + xg + xt xf2=x2/2 + xg + xt xf0=(x0/2 + xt)/2 xf=xf1+xf2+xf0 ia1=round(1000/xf)/1000 iF1=3*ia1 IF1=iF1*I mprintf("\n(a)Fault Current = %.2fA",IF1) IA1=ia1*-1*%i IA2=ia1*-1*%i IA0= ia1 * .5*-1*%i IA=round((IA1 +IA2 +IA0)*10000)/10000 IB=round(((IA1*a*a) + (a*IA2) +IA0)*10000)/10000 IC=round(((IA1*a) + (a*a*IA2) +IA0)*10000)/10000 mprintf("\n(b)From T1 to P: (in order - IA,IB, IC in pu)") disp(IC, IB, IA) IA1b=0 IA2b=0 IA0b=ia1 * .5*-1*%i IAb=round((IA1b +IA2b +IA0b)*10000)/10000 IBb=round(((IA1b*a*a) + (a*IA2b) +IA0b)*10000)/10000 ICb=round(((IA1b*a) + (a*a*IA2b) +IA0b)*10000)/10000 mprintf("\nFrom P to T2: (in order - IA,IB, IC in pu)") disp(ICb, IBb, IAb) //(c) Ia0=0 Ia1=IA1 * exp(%i * -1*%pi/6) Ia2=IA2 * exp(%i * 1*%pi/6) Ia=round((Ia1 +Ia2 +Ia0)*1000)/1000 Ib=round(((Ia1*a*a) + (a*Ia2) +Ia0)*1000)/1000 Ic=round(((Ia1*a) + (a*a*Ia2) +Ia0)*1000)/1000 mprintf("\n(c) Currents in lines connecting source to T1 (in order - Ia,Ib, Ic in pu)") disp(Ic, Ib, Ia) mprintf("\n(d) Currents in star wdg of T1") mprintf("\nIa= %.4fj, Ib= %.4fj, Ic= %.4fj", imag(IA), imag(IB), imag(IC)) mprintf("\nIa1= %.4fj, Ia2= %.4fj, Ia0= %.4fj", imag(IA1), imag(IA2), imag(IA0)) mprintf("\nIb1= %.4f /_%.3f, Ib2=%.4f/_%.3f, Ib0= %.4fj", abs(IA1 *a*a),atand(imag(IA1*a*a)/real(IA1*a*a))+180,abs(IA1 *a),atand(imag(IA2*a)/real(IA2*a)),imag(IA0)) mprintf("\nIc1= %.4f /_%.3f, Ic2=%.4f/_%.3f, Ic0= %.4fj", abs(IA1 *a),atand(imag(IA1*a)/real(IA1*a)),abs(IA1 *a*a),atand(imag(IA2*a*a)/real(IA2*a*a))+180,imag(IA0)) Iab1 = round(IA1*1e3 /sqrt(3))/1e3 Iab2 = round(IA2*1e3 /sqrt(3))/1e3 Iab0 = round(IA0*1e3 /sqrt(3))/1e3 Ibc1=Iab1 * a*a Ibc2=Iab2 * a Ibc0=Iab0 Ica1=Iab1 * a Ica2=Iab2 * a *a Ica0=Iab0 Iab= Iab1 +Iab2 +Iab0 Ibc= Ibc1 +Ibc2 +Ibc0 Ica= Ica1 +Ica2 +Ica0 mprintf("\n\nCurrents in delta wdg of T1") mprintf("\nIab= %.4fj, Ibc= %.4fj, Ica= %.4fj", imag(Iab), imag(Ibc), imag(Ica)) mprintf("\nIab1= %.4fj, Iab2= %.4fj, Iab0= %.4fj", imag(Iab1), imag(Iab2), imag(Iab0)) mprintf("\nIbc1= %.4f /_%.3f, Ibc2=%.4f/_%.3f, Ibc0= %.4fj", abs(Ibc1),atand(imag(Ibc1)/real(Ibc1))+180,abs(Ibc2),atand(imag(Ibc2)/real(Ibc2)),imag(Ibc0)) mprintf("\nIca1= %.4f /_%.3f, Ica2=%.4f/_%.3f, Ica0= %.4fj", abs(Ica1),atand(imag(Ica1)/real(Ica1)),abs(Ica2),atand(imag(Ica2)/real(Ica2))+180,imag(Ica0)) mprintf("\n\n Currents in star wdg of T2") mprintf("\nIa= %.4fj, Ib= %.4fj, Ic= %.4fj", imag(IAb), imag(IBb), imag(ICb)) mprintf("\nIa1= %.4f, Ia2= %.4f, Ia0= %.4fj", imag(IA1b), imag(IA2b), imag(IA0b)) mprintf("\nIb1= %.4f, Ib2= %.4f, Ib0= %.4fj", imag(IA1b *a*a), imag(IA1b *a),imag(IA0b)) mprintf("\nIc1= %.4f, Ic2= %.4f, Ic0= %.4fj", imag(IA1b *a), imag(IA1b*a *a),imag(IA0b)) Iab1b = round(IA1b*1e3 /sqrt(3))/1e3 Iab2b = round(IA2b*1e3 /sqrt(3))/1e3 Iab0b = round(IA0b*1e3 /sqrt(3))/1e3 Ibc1b=Iab1b * a*a Ibc2b=Iab2b * a Ibc0b=Iab0b Ica1b=Iab1b * a Ica2b=Iab2b * a *a Ica0b=Iab0b Iabb= Iab1b +Iab2b +Iab0b Ibcb= Ibc1b +Ibc2b +Ibc0b Icab= Ica1b +Ica2b +Ica0b mprintf("\n\nCurrents in delta wdg of T2") mprintf("\nIab= %.3fj, Ibc= %.3fj, Ica= %.3fj", imag(Iabb), imag(Ibcb), imag(Icab)) mprintf("\nIab1= %.3f, Iab2=%.3f, Iab0= %.3fj", imag(Iab1b), imag(Iab2b), imag(Iab0b)) mprintf("\nIbc1= %.3f, Ibc2=%.3f, Ibc0= %.3fj", imag(Ibc1b),imag(Ibc2b),imag(Ibc0b)) mprintf("\nIca1= %.3f, Ica2=%.3f, Ica0= %.3fj", imag(Ica1b),imag(Ica2b),imag(Ica0b))
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ch2_4.sce
// To determine the inductance of single phase Transmission line clear clc; GMDa=0.001947;// GMD of conductor in group A DSA=((.001947*6*12*.001947*6*6*0.001947*6*12)^(1/9)); DSB=sqrt(5*(10^-3)*.7788*6); Dae=sqrt((9^2)+6^2); Dcd=sqrt((12^2)+9^2); DMA=((9*10.81*10.81*9*15*10.81)^(1/6)); LA=2*(10^-7)*(10^6)*log(DMA/DSA); LB=2*(10^-7)*(10^6)*log(DMA/DSB); Tot=LA+LB; mprintf("inductance of line A,LA=%.3f mH/km\n",LA);//Answers don't match due to difference in rounding off of digits mprintf("inductance of line B,LB=%.1f mH/km\n",LB);//Answers don't match due to difference in rounding off of digits mprintf("total inductance of line =%.2f mH/km\n",Tot);//Answers don't match due to difference in rounding off of digits
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Ex7_9.sce
//Ex:7.9 clc; clear; close; V_pp=14.8-3.3; printf("Collector quiescent voltage = 9.2 V"); printf("\nCollector quiescent current = 7.3mA"); printf("\nOutput peak-peak voltage = %f V",V_pp);
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12_12.sce
clear; clc; close; Vcc =25; Rl = 4; Vl_p = Vcc; P2q_max = (2*Vcc^2)/((%pi^2)*Rl); Vl = 0.636*Vl_p; disp(P2q_max,'Maximum power dissipated(Watts) = '); disp(Vl,'Input voltage at which this occurs(Volts) = ');
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ex3_2c.sce
[s,Fs] = wavread('abc.wav') for n = 1:length(s)*2 if modulo(n,2) then z(n) = s((n+1)/2) else z(n) = s(n/2) end end S = fft(z) Ss = fftshift(S/(length(z))) wavwrite(z,Fs, 'abc_z.wav') subplot(2,1,1); plot(z); xlabel('t'); ylabel('amplitude'); a=get("current_axes"); set(a,"x_location","origin") set(a,"y_location","origin") subplot(2,1,2); p = length(Ss) plot(-p/2+1:p/2, abs(Ss)); xlabel('f'); ylabel('spectrum'); a=get("current_axes"); set(a,"x_location","origin") set(a,"y_location","origin")
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ex6_9.sce
//Page Number: 335 //Example 6.9 clc; //Given I0=500D-3; //A V0=10D+3; //V Z0=25; //ohm l=.20; //m f=5.93D+9; //Hz //Gain parameter C=((I0*Z0)/(4*V0))^(1/3); disp(C,'Gain parameter:'); N=(l*f)/(0.593D+6*sqrt(V0)); //Gain Ap=-9.54+(47.3*C*N); disp('dB',Ap,'Gain of TWT:');
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ex_9_14_1.sce
//Example 9.14.1 // peak to peak voltage and rms voltage clc; clear; close; format('v',7) vdv=1;//volts per division in V/div n=6.8;//no. of divisions Vpp=vdv*n;//peak to peak voltage in volts vrms=Vpp/(2*sqrt(2));//rms voltage in volts disp(Vpp,"peak to peak voltage in volts") disp(vrms,"rms voltage in volts")
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ex2_21_4.sce
// Exa 2.21.4 clc; clear; close; // Given data K = 1.38 * 10^-23;// in J/K T = 27;// in degree T = T + 273;// in K e = 1.6 * 10^-19;// in C Mu_e = 0.17;// in m^2/v-s Mu_e1 = 0.025;// in m^2/v-s D_n = ((K * T)/e) * Mu_e;// in m^2/s disp(D_n,"The diffusion coefficient of electrons in m^2/s is"); D_p = ((K * T)/e) * Mu_e1;// in m^2/s disp(D_p,"The diffusion coefficient of holes in m^2/s is ");
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ex5_1.sce
//Exam:5.1 clc; clear; close; //The probability that a particular quantum state at energy E is filled, is given by //f(E) =1/(1+exp(E-E_f)/kT) e=1.6*10^(-19);//charge on the electron dE=0.5*e;//E-E_f in joule //0.01=1/(1+exp(x)) //1+exp(x)=100 x=log(99); k=1.38*10^(-23);//constant T=dE/(x*k);//temperature disp(ceil(T),'temperature at which there is one per cent probability that a state with an energy 0.5 eV above the Fermi energy will be occupied by an electron(in K)=');
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Ex9_1.sce
//example 9.1 clc; funcprot(0); sall=30;//sigma allowed pi=%pi; zbar=12.1; L1=10; L2=20; Gamma=0.12; Gamma1=0.1294-0.0624; phi=40*pi/180; Ka=(tan(pi/4-phi/2))^2; Kp=(tan(pi/4+phi/2))^2; s1=Gamma*L1*Ka;//sigma1 s2=Gamma*L1*Ka+Gamma1*L2*Ka;//sigma2 L3=s2/(Gamma1*(Kp-Ka)); disp(L3,"length in ft"); P=1/2*s1*L1+s1*L2+1/2*(s2-s1)*L2+1/2*s2*L3; disp(P,"force in kip/ft"); s5=Gamma*L1*Kp+Gamma1*L2*Kp+Gamma*L3*(Kp-Ka);//sigma5 disp(s5,"pressure in kip/ft"); A1=s5/(Gamma1*(Kp-Ka)); A2=8*P/(Gamma1*(Kp-Ka)) A3=6*P*(2*zbar*(Gamma1*(Kp-Ka))+s5)/(Gamma1*(Kp-Ka))^2 A4=P*(6*zbar*s5+4*P)/(Gamma1*(Kp-Ka))^2 printf("A1,A2,A3,A4 respectively in %.2f,%.2f,%.2f,%.2f \n",A1,A2,A3,A4); disp("slight error due to rounding off error") //partb deff('y=f(x)','y=x^4+41.7*x^3-270.5*x^2-13363*x-106863'); [x]=fsolve(20,f); D=1.88+x; disp(D,"value of D, ft") TL=L1+L2+1.3*D; disp(TL,"total length in ft"); //partc z=sqrt(2*P/(Gamma1*(Kp-Ka)));//zdash Mmax=P*(z+zbar)-1/2*(Gamma1*(Kp-Ka))*z^2*z/3; S=Mmax*12/sall; disp(S,"section modulus in in^3/ft")
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TimeSeries.tst
SELECT q.* FROM( SELECT a.GroupID, a.Time, a.Value, NVL(LAG(0) OVER (PARTITION BY a.GroupID ORDER BY a.Time), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY a.GroupID ORDER BY a.Time), 1) AS end_flag FROM tblTimeSeriesTest a ) AS p, TABLE(FLARIMAUdt(p.GroupID, p.Value, 1, 0, 1, p.begin_flag, p.end_flag) ) AS q ORDER BY 1, 2, 3 LIMIT 20; ------------------------------------------------------------------------------------- SELECT q.* FROM( SELECT a.GroupID, a.Time, a.Value, NVL(LAG(0) OVER (PARTITION BY a.GroupID ORDER BY a.Time), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY a.GroupID ORDER BY a.Time), 1) AS end_flag FROM tblTimeSeriesTest a ) AS p, TABLE(FLARIMAFcstUdt(p.GroupID, p.Value, 1, 0, 1, p.begin_flag, p.end_flag) ) AS q ORDER BY 1, 2 LIMIT 20; ------------------------------------------------------------------------------------- SELECT q.* FROM( SELECT a.GroupID, a.Time, a.Value, NVL(LAG(0) OVER (PARTITION BY a.GroupID ORDER BY a.GroupID, a.Time), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY a.GroupID ORDER BY a.GroupID, a.Time), 1) AS end_flag FROM tblTimeSeriesTest AS a ) AS p, TABLE (FLAutoCorrelUdt(p.GroupID, p.Value, 10, p.begin_flag, p.end_flag) ) AS q ORDER BY 1, 2 LIMIT 20; ------------------------------------------------------------------------------------- SELECT a.* FROM(SELECT 1 AS GroupID, a.id, a.stockreturn, 1 AS q, 1 AS p, 'R' AS value_type, NVL(LAG(0) OVER (PARTITION BY GroupID ORDER BY GroupID, id), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY GroupID ORDER BY GroupID, id), 1) AS end_flag FROM tblbac_return a ) AS z, TABLE (FLGARCHpqUdt(z.GroupID, z.q, z.p, z.value_type, z.stockreturn, z.begin_flag, z.end_flag)) AS a;
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clf clc; disp('enter coordinates of the points') x=input('Enter x coordinates') y=input('Enter y coordinates') z=input('Enter z coordinates') p=[x y z 1] r=[1 0 0 0;0 1 0 0;0 0 1 0;0 0 0 1]; i=input('Enter no. of transformation'); for k=1:1:i j=input('choose transformation 1.translation 2.rotation'); select(j) case 1 tx=input('translation about x axis'); ty=input('translation about y axis'); tz=input('translation about z axis'); TM=[1 0 0 0;0 1 0 0;0 0 1 0;tx ty tz 1] r=r*TM case 2 theta=input('enter angle') theta=theta*pi/180; e=input('enter axis 1.x 2.y 3.z') select(e) case 1 RX=[1 0 0 0;0 cos(theta) -1*sin(theta) 0;0 sin(theta) 0 cos(theta) 0;0 0 0 1] r=r*RX case 2 RY=[cos(theta) 0 sin(theta) 0;0 1 0 0;-1*sin(theta) 0 cos(theta) 0;0 0 0 1] r=r*RY case 3 RZ=[cos(theta) -1*sin(theta) 0 0;sin(theta) cos(theta) 0 ;0 0 1 0;0 0 0 1] r=r*RZ end end end disp('final point q') q=p*r disp(q) figure(1) plot3(x,y,z,'b') hold on title('Original point p and transformed point q') xlabel('x axis'),ylabel('y axis'),zlabel('z axis') plot3(q(1),q(2),q(3),'r') hold off
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clear; clc; // Example: 10.9 // Page: 412 printf("Example: 10.9 - Page: 412\n\n"); // Solution //*****Data******// x1 = 0.42; x2 = 0.58; P = 760;// [mm of Hg] P1sat = 786;// [mm of Hg] P2sat = 551;// [mm of Hg] //***************// gama1 = P/P1sat; gama2 = P/P2sat; A = log(gama1)*(1 + (x2*log(gama2))/(x1*log(gama1)))^2; B = log(gama2)*(1 + (x1*log(gama1))/(x2*log(gama2)))^2; printf("Van Laar Constants\n"); printf("A = %.3f\n",A); printf("B = %.3f\n",B);
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//Example 10.11 // Scaling Calculations C=25*10^-9; R=2000; L=40*10^-3; s=%s; Z=s*L+1/(s*C+1/R); // H=I_L/V_s =1/Z ; // Required Network function H=1/Z; // since resistance is affected only by the magnitude of scale factor k_m is choosen such that R_cap will be a small integer value k_m=0.005; R_cap=0.005*(2000);// Scaled Resistance // L_cap=(k_m/k_f)*L , this equation is suggesting to choose k_f= k_m*L k_f=k_m*L; L_cap=(k_m*L)/k_f; // Scaled inductance C_cap=C/(k_m*k_f); // Scaled Capacitance // Network function for the scaled network calculated on the same base as above s_c=poly(0,'s_c') num=(s_c+4); den=(s_c^2+4*s_c+40); H_cap=num/den; K_cap=1; z_cap=roots(num); p_cap=roots(den); //hence poles and zeros for original network function will be z_1=z_cap/k_f; p_1=p_cap/k_f; // Gain factor is given by K=k_m/k_f; disp(K,"Gain for original tranfer function=") disp(z_1,"Zeros for original transfer function=") disp(p_1,"Poles for original transfer function=")
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// Exa 11.5 // To Calculate: //(a) minimum separation between frequency tones, //(b) number of frequency tones produced by a frequency synthesizer, //(c) processing gain, and //(d) hopping bandwidth. clc; clear all; R=200;//input data rate in bps Fhop=200;//per second k=1;//Multipication_Factor //solution // We have 32-FSK modulation scheme Bits_sym=log2(32); Rs=Fhop/Bits_sym; printf('There are 200 hops per second and Symbol rate is %d symbols per sec \n',Rs); disp("The hop rate is higher than symbol rate, the system is a fast FHSS system."); SDur=1/Rs; L=Fhop/Rs; CDur=SDur/L; Separation=1/CDur; M=2^Bits_sym; Hop_BW=k*M*Fhop*L; Gp=M*k*L; disp(""); printf(' Minimum separation between frequency tones should be %d Hz\n',Separation); printf(' Number of different frequency tones produced by a frequency synthesizer are %d\n',M); printf(' Processing Gain is %d\n ',Gp); printf('Hopping bandwidth is %d kHz\n',Hop_BW/1000);
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//Chapter 11 : Free Electron Theory Of Metals clear; //Variable declaration rho=1.54*10**-8 //resistivity n=5.8*10**28 //electron density e=1.602*10**-19 //charge on electron m=9.1*10**-31 //Mass of electron //Calculations tau=m/(n*(e**2)*rho)/10**-14 //Result mprintf("Relaxation time= %1.2f*10**-14 seconds",tau)
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//Chapter-13, Example 13.9, Page 390 //============================================================================= clc clear //INPUT DATA Ib=0.125;//base current in mA b=200;//common-emitter DC current gain //CALCULATIONS Ic=b*Ib;//collector current in mA Ie=Ib+Ic;//emitter current in mA mprintf("Thus emitter and collector currents are %2.3f mA and %d mA respectively",Ie,Ic); //=================================END OF PROGRAM=======================================================================================================
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clc n_O2=1; //V_O2=0.21*V; //V_N2=0.79*V; M_N2=28; M_O2=32; disp("(i) Moles of N2 per mole of O2 :") n_N2=n_O2*0.79/0.21; disp("n_N2=") disp(n_N2) disp("moles") n=n_O2+n_N2; disp("(ii) p_O2 and p_N2 :") p=1; //atm p_O2=n_O2/n*p; disp("p_O2=") disp(p_O2) disp("atm") p_N2=n_N2/n*p; disp("p_N2=") disp(p_N2); disp("atm") disp("(iii) The kg of nitrogen per kg of mixture :") x=n_N2*M_N2/(n_N2*M_N2+n_O2*M_O2); disp(" The kg of nitrogen per kg of mixture =") disp(x) disp("kg N2/kg mix")
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clc; funcprot(0); // Initialization of Variable theta=25+14.0/60;//latitude in degrees in North L1=29+15/60;//longitude in degrees in West L2=45+25/60;//longitude in degrees in West R=6370.0;//radius in km //calculation AB=cos(theta*%pi/180)*(L2-L1);//arc length in km dis=2*%pi*R*AB/360.0;//distance in km disp(dis,"distance of AB in m") clear()
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#************************************************************ # Scenario of grande_salle # # date : Fri Oct 22 17:19:29 2010 #************************************************************ p3d_sel_desc_name P3D_ENV grande_salle #p3d_sel_desc_name P3D_ROBOT BLUE_TRASHBIN #p3d_set_robot_steering_method Linear #p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 #p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 #p3d_sel_desc_name P3D_ROBOT PINK_TRASHBIN #p3d_set_robot_steering_method Linear #p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 1.255162 0.000000 0.000000 0.000000 0.000000 0.000000 #p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 #p3d_sel_desc_name P3D_ROBOT BLACK_TAPE #p3d_set_robot_steering_method Linear #p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 #p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT GREY_TAPE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.426253 -2.224680 0.783677 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT ACHILE_HUMAN1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 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0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT CHAIR1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT CHAIR2 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT TRASHBIN p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SHELF p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.500000 -2.224680 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT HRP2TABLE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SIMPLECHAIR p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT HRP2BARTable p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT ACCESSKIT p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SPACENAVBOX p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 #p3d_sel_desc_name P3D_ROBOT ORANGE_BOTTLE #p3d_set_robot_steering_method Linear #p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.426253 -2.224680 2.000000 0.000000 0.000000 0.000000 #p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT VISBALL_INTERNAL p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SAHandRight p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 6 1 5 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 0 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 10 1 9 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 1 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 14 1 13 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 2 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 18 1 17 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 3 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT JIDOKUKA_ROBOT p3d_set_robot_steering_method Multi-Localpath p3d_set_robot_radius 1.000000 p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.539823 -2.163225 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 91.692353 23.050657 -9.121951 116.585091 -144.486870 29.356629 119.281927 90.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.195229 -2.497740 0.919250 153.658537 34.243902 -25.463415 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.539823 -2.163225 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -156.840267 7.675654 1.671586 35.662741 59.466555 91.483737 77.791212 90.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 17 1 16 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 0 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 21 1 20 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 1 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 25 1 24 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 2 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 29 1 28 2 1.000000 0.000000 0 p3d_set_cntrt_Tatt2 3 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lwr_arm_ik 6 5 6 8 9 10 11 1 34 0 2 7 1 p3d_set_cntrt_Tatt 4 0.000000 0.000000 1.000000 -0.250000 -0.382683 -0.923879 0.000000 0.000000 0.923879 -0.382683 0.000000 0.000000 p3d_set_cntrt_Tatt2 4 1.000000 0.000000 0.000000 0.000000 0.000000 1.000000 0.000000 0.000000 0.000000 0.000000 1.000000 -0.105000 p3d_set_object_base_and_arm_constraints 34 1 0 1 4 p3d_set_arm_data 4 8 7 5 6 1 34 p3d_set_camera_pos 4.432160 -2.238351 0.982624 1.903393 5.641935 0.128750 0.000000 0.000000 1.000000 0.000000
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clc; //Example 19.6 //page no. 255 printf("\n Example 19.6 page no. 255\n\n"); //refer to example 19.5 //if gasoline has vapor pressure of 50000Pa ,we have to calculate flow rate at whhich cavitation to occur P1=101325//upstream pressure,Pa P2=50000//given vapor pressure,Pa D1=0.06//upstream diameter,m D2=0.02//throat diameter,m rho=680//density of gasoline v2=sqrt((2*(P1-P2))/rho*(1-D2^4/D1^4))//velocity printf("\n velocity v2=%f m/s",v2); q=(%pi/4)*D2^2*v2//flow rate printf("\n flow rate q=%f m^3/s",q);
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// Exa 3.16 clc; clear; close; // Given data V_in = 20;// in V R_S = 220;// in ohm V_Z = 10;// in V P_Z = 400;// in mW // Part (I) R_L = 200;// in ohm disp("Part (I) For R_L= 200 Ω") V_L = V_Z;// in V disp(V_L,"Load voltage in V is"); I_L = V_L/R_L;// in A disp(I_L,"Load current in A is"); I_R = (V_in-V_Z)/R_S;// in A disp(I_R,"The current through resistor in A is"); I_Z = I_R-I_L;// in A disp(I_Z,"The value of I_Z in A is"); // Part (II) R_L = 50;// in ohm disp("Part (II) For R_L= 50 Ω") V_L = V_Z;// disp(V_L,"Load voltage in V is"); I_L = V_L/R_L;// in A disp(I_L,"Load current in A is"); I_R = (V_in-V_Z)/R_S;// in A disp(I_R,"The current through resistor in A is"); I_Z = I_R-I_L;// in A disp(I_Z,"Zener current in A is"); disp("For both values of R_L, the current I_R is less than I_L and I_Z is negative. It shows that given circuit can not work successfully as a voltage regulator")
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// Exa 6.20 format('v',6) clc; clear; close; // Given data alpha_dc = 0.99; I_C = 6;// in mA I_C= I_C*10^-3;// in A I_CBO = 15;// in µA I_CBO= I_CBO*10^-6;// in A // The emitter current, I_E = (I_C - I_CBO)/alpha_dc;// in A // The base current, I_B = I_E - I_C;// in A I_B=I_B*10^6;// in µA disp(I_B,"The value of I_B in µA is");
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inf = float('inf') plant_pvt_init_data = None T = 720.0 #delta_t = 0.5 delta_t = 50 # HybridConfig initialConfig(initialSet, 2, 0, 0); # Initial Mode initial_discrete_state = [2] # Interval init_Gp = init_Gs; # init_Gp.mul_assign(1.9152); # States # idx 0 1 2 3 4 5 6 7 8 9 10 11 # name X, Isc1, Isc2, Gt, Gp, Il, Ip, I1, Id, Gs, t, uc initial_set = [[0, 72.43, 141.15, 162.45, 120*1.9152, 3.2, 5.5, 100.25, 100.25, 120, 0, 50], [0, 72.43, 141.15, 162.45, 160*1.9152, 3.2, 5.5, 100.25, 100.25, 160, 0, 90]] # prop: hypoglycemia: below 70 mg/dl. # name X, Isc1, Isc2, Gt, Gp, Il, Ip, I1, Id, Gs, t, uc hypoglycemia = [[-inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf], [inf, inf, inf, inf, inf, inf, inf, inf, inf, 70, inf, inf]] # prop: ketoacidosis: The blood glucose levels should never rise above 300 mg/dl.ketoacidosis. # name X, Isc1, Isc2, Gt, Gp, Il, Ip, I1, Id, Gs, t, uc ketoacidosis = [[-inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, 250, -inf, -inf], [inf, inf, inf, inf, inf, inf, inf, inf, inf, inf, inf, inf]] # The blood glucose should be in the euglycemic range [70; 180] mg/dl during \wakeup" t 2 [600; 720] # name X, Isc1, Isc2, Gt, Gp, Il, Ip, I1, Id, Gs, t, uc euglycemic1 = [[-inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, 180, 600, -inf], [inf, inf, inf, inf, inf, inf, inf, inf, inf, inf, 720, inf]] euglycemic2 = [[-inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, -inf, 600, -inf], [inf, inf, inf, inf, inf, inf, inf, inf, inf, 70, 720, inf]] # name X, Isc1, Isc2, Gt, Gp, Il, Ip, I1, Id, Gs, t, uc #grid_eps = [1, 1, 1, 1, 20, 1, 1, 1, 1, 20, 1, 20] grid_eps = [10]*12 num_samples = 10 error_set = ketoacidosis MAX_ITER = inf plant_description = 'python' plant_path = 'insulin_s1.py' ############################################# initial_controller_integer_state = [] initial_controller_float_state = [] num_control_inputs = 0 min_smt_sample_dist = 0 initial_private_state = [] ci = [[], []] pi = [[],[]] controller_path = None controller_path_dir_path = None
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clear; clc; //Example 4.10 b=100; Vbe=0.7; V_T=0.026;//(V) Re=2; R1=50; R2=50; Rs=0.5; Va=80; //by dc analysis Icq=0.793; Vceq=3.4; r_pi=b*V_T/Icq; printf('\nsmall signal resistance=%.3f KOhm\n',r_pi) g_m=Icq/V_T; printf('\ntransconductance=%.3f mA/V\n',g_m) ro=Va/Icq; printf('\nsmall signal output resistance=%.2f KOhm\n',ro) Rib=r_pi+(1+b)*Re*ro/(ro+Re); printf('\ninput resistance to the base=%.2f KOhm\n',Rib) //Ri=R1||R2||Rib x=R1*R2/(R1+R2); Ri=x*Rib/(x+Rib); printf('\nRi=%.2f KOhm\n',Ri) y=ro*Re/(ro+Re); Av=(1/(r_pi+(1+b)*y))*(1+b)*y*Ri/(Ri+Rs); printf('\nsmall signal voltage gain=%.3f \n',Av)
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Ex7_6.sce
//page 247 //Example 7.6 clc; clear; close; disp('A = '); disp('2 0 0'); disp('a 2 0'); disp('b c -1'); a = 1; b = 0; c = 0; A = [2 0 0;a 2 0;b c -1]; disp(A,'A = '); disp('Characteristic polynomial for A is:'); disp(poly(A,"x"),'p = '); disp('In this case, minimal polynomial is same as characteristic polynomial.'); disp('-----------------------------------------'); a = 0; b = 0; c = 0; A = [2 0 0;a 2 0;b c -1]; disp(A,'A = '); disp('Characteristic polynomial for A is:'); disp(poly(A,"x"),'p = '); disp('In this case, minimal polynomial is:'); disp('(x-2)(x+1)'); disp('or'); x = poly(0,"x"); s = (x-2)*(x+1); disp(s); disp('(A-2I)(A+I) = '); disp('0 0 0'); disp('3a 0 0'); disp('ac 0 0'); disp('if a = 0, A is similar to diagonal matrix.') //end
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// Example 2.8 // Calculation of threshold power of stimulated Brillouin scattering and Raman Scattering // Page no 52 clc; clear; close; // Given data A=0.5; // Attenuation d=5; // Core diameter lambda=1.3; // Operating wavelength v=0.7; // Bandwith of laser diode // Threshold power of stimulated Brillouin scattering Pb=4.4*10^-3*d^2*lambda^2*A*v; Pb=Pb*10^3; //Threshold power stimulated Raman Scattering Pr=5.9*10^-2*d^2*lambda*A; //Display result on command window printf("\n Threshold power of stimulated Brillouin scattering (in mW) = %0.2f ",Pb); printf("\n Threshold power stimulated Raman Scattering (in W)= %0.2f",Pr);
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Example8_1.sce
//Example 8.1 clear; clc; T0=10^4; f1=100; f2=10^6; f3=10*10^6; w1=2*%pi*f1; w2=2*%pi*f2; w3=2*%pi*f3; h=syslin('c',T0/[(1-(%s/w1))*(1-(%s/w2))*(1-(%s/w3))]); gm=g_margin(h); pm=p_margin(h); printf("(a) Gain Margin(GM)=%.2f dB",gm); printf("\n(b) Phase Margin(PM)=%.1f degrees",-pm); f=512*10^3; w=2*%pi*f; T1=T0/[(1-((%i*w)/w1))*(1-((%i*w)/w2))*(1-((%i*w)/w3))]; den=1/(abs(T1)/T0); printf("\n(c) T0 for PM=60 degrees=%.f",den);
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function x=generaliteration2(x,g,gp) R=2; PE=10^-8; maxval=10^4; A=[0 0]; k=gp(x); if abs(k)>1 then error('function chosen does not converge') abort; end for n=1:1:R x=g(x); disp(x); if abs(g(x))<=PE then break end if (abs(g(x))>maxval) then error('Solution diverges'); abort break end end disp(n," no. of iterations =") endfunction
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clc clear //input c1=2*(10^-6);// capacitance of first capacitor in farad which is connected in series with second c2=6*(10^-6);// capacitance of second capacitor in farad which is connected in series with first v=240;//d.c. voltage supply in volts //calculations ct=(c1*c2)/(c1+c2);//effective capacitance in farad q=ct*v;//total charge in coloumbs e1=(q^2)/(2*c1);// energy stored in first capacitor in joules e2=(q^2)/(2*c2);// energy stored in second capacitor in joules //output mprintf('the energy stored in first capacitor is %3.10f J \n the energy stored in second capacitor is %3.10f J',e1,e2)
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// chapter 8 // example 8.8 // Calculate the mean values of load voltage and current // page-460-462 clear; clc; // given Edc=80; // in V (dc source) T=2; // in ms (chopping period) L=8; // in mH R=4; // in ohm Ton_Toff_1= 1/1; Ton_Toff_2= 4/1; Ton_Toff_3= 1/4; // calculate L=L*1E-3; // changing unit from mH to H tou=L/R; T=T*1E-3; //part-a // since Ton/Toff=1/1 therefore Ton=Toff or Ton=T/2; Toff=Ton; I0_max=(Edc/R)*((1-exp(-Ton/tou))/(1-exp(-T/tou))); I0_min=I0_max*exp(-Toff/tou); E0=Edc*(Ton/T); I0_av=E0/R; printf("\nWhent Ton/Toff=1/1,") printf("\n\t\tThe maximum output current is \t\t I0_max=%.2f A", I0_max); printf("\n\t\tThe minimum output current is \t\t I0_min=%.2f A", I0_min); printf("\n\t\tThe mean value of load voltage is \t E0=%.f V",E0); printf("\n\t\tThe mean value of load current is \t I0_av=%.f A",I0_av); //part-b // since Ton/Toff=4/1 therefore Ton=4Toff and Ton+Toff=T or 5*Toff=T therefore we get Toff=T/5; Ton=4*Toff; I0_max=(Edc/R)*((1-exp(-Ton/tou))/(1-exp(-T/tou))); I0_min=I0_max*exp(-Toff/tou); E0=Edc*(Ton/T); I0_av=E0/R; printf("\nWhent Ton/Toff=4/1,") printf("\n\t\tThe maximum output current is \t\t I0_max=%.2f A", I0_max); printf("\n\t\tThe minimum output current is \t\t I0_min=%.2f A", I0_min); printf("\n\t\tThe mean value of load voltage is \t E0=%.f V",E0); printf("\n\t\tThe mean value of load current is \t I0_av=%.f A",I0_av); //part-c // since Ton/Toff=1/4 therefore Toff=4*Toff and Ton+Toff=T or 5*Ton=T therefore we get Ton=T/5; Toff=5*Ton; I0_max=(Edc/R)*((1-exp(-Ton/tou))/(1-exp(-T/tou))); I0_min=I0_max*exp(-Toff/tou); E0=Edc*(Ton/T); I0_av=E0/R; printf("\nWhent Ton/Toff=1/4,") printf("\n\t\tThe maximum output current is \t\t I0_max=%.2f A", I0_max); printf("\n\t\tThe minimum output current is \t\t I0_min=%.2f A", I0_min); printf("\n\t\tThe mean value of load voltage is \t E0=%.f V",E0); printf("\n\t\tThe mean value of load current is \t I0_av=%.f A",I0_av); // Note: 1 The answer for I0_min of part-b is wrong in the book due to calculation mistake. // 2.the answers varies slightly due to precise calculation
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/////////Chapter 10 Properties Of Steam ///Example 10.21 Page No:201 /// Find Final enthalpy of steam //Input data clc; clear; m=4; //Steam in Kg P=13; //Absolute pressure in bar tsup1=450; //Absolute temp in degree celsius deltaH=2.8*10^3; Cps=2.3; //loses in MJ //from steam table at 13 bar ts=191.6; //In degree celsius Vg=0.1511; //In m^3/Kg hf=814.7; //In m^3/Kg hfg=1970.7; //In KJ/Kg hg=2785.4; //In KJ/Kg ///Calculation h1=hg+Cps*(tsup1-ts); //Initial enthalpy of steam in KJ/Kg Deltah=deltaH/m; //Change in enthalpy/unit mass in KJ/Kg h2=h1-Deltah; //Final enthalpy of steam in KJ/Kg x2=(h2-hf)/hfg; //wet & dryness fraction //Output printf('Initial enthalpy of steam=%f Kj/Kg \n ',h1); printf('Change in enthalpy/unit mass=%f Kj/Kg \n ',Deltah); printf('Final enthalpy of steam= %f KJ/Kg \n',h2); printf('wet & dryness fraction=%f \n',x2);
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Reator_plug_flow_transiente_jun_20_2017.sce
clc clear function Derivada=f(t,Y,Num) for i=2:Num S=Y(i,1);X=Y(i,2);P=Y(i,3); Sb=Y(i-1,1);Xb=Y(i-1,2);Pb=Y(i-1,3); Derivada(i,1)=-U*(S-Sb)/deltaZ+X*MI*S/(S+Ks)*(1/Yxs)*(-1); Derivada(i,2)=-U*(X-Xb)/deltaZ+X*MI*S/(S+Ks); Derivada(i,3)=-U*(P-Pb)/deltaZ+X*MI*S/(S+Ks)*(Yps/Yxs) end endfunction MI=0.4;Ks=2;Yps=0.4;Yxs=0.5; Num=20;U=1;//m/s S0=100;X0=10;P0=0;t0=0;Time=0.1:0.1:7;L=20000; U=U*3600; // m/s for i=1:Num Conc0(i,1)=S0;Conc0(i,2)=X0;Conc0(i,3)=P0; end deltaZ=L/Num Ref=size(Time,2) for k=1:Ref t=Time(k); Conc=ode(Conc0,t0,t,f); Y(k,:)=Conc(Num,:); end X=Y(:,2);S=Y(:,1);P=Y(:,3); scf();a=get("current_axes");a.data_bounds=[0,0;10,100];plot(Time,S);xgrid(5);xtitle( 'Substrato' ) ; xlabel("tempo(h)");ylabel("S(g/l)"); scf();a=get("current_axes");a.data_bounds=[0,0;10,100];plot(Time,X);xgrid(5);xtitle( 'Celulas' ) ; xlabel("tempo(h)");ylabel("X(g/l)"); scf();a=get("current_axes");a.data_bounds=[0,0;10,100];plot(Time,P);xgrid(5);xtitle('Produto') ; xlabel("tempo(h)");ylabel("P(g/l)");
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clear; clc; //Example11.9[Cooling Hot Oil by Water in Multipass Heat Exchanger] //Given:- Cp_c=4.18,Cp_h=2.13;//Specific Heats of water and oil[kJ/kg] mc=0.2,mh=0.3;//Mass Flow rate of oil and water [kg/s] Th_in=150,Tc_in=20;//[degree Celcius] n=8;//No of tubes D=0.014;//[m] L=5;//[m] U=310;//Overall Heat transfer Coefficient[W/m^2.degree Celcius] //Solution:- Ch=mh*Cp_h;//[kW/degree Celcius] Cc=mc*Cp_c;//[kW/degree Celcius] if(Ch>Cc) then, Cmin=Cc; c=Cmin/Ch; else Cmin=Ch; c=Cmin/Cc; end Q_max=Cmin*(Th_in-Tc_in);//[kW] disp("kW",Q_max,"The maximum heat transfer rate is") As=n*%pi*D*L;//[m^2] disp("m^2",As,"Heat transfer Surface Area is") NTU=U*As/Cmin; disp(NTU,"The NTU of this heat exchanger is") e=0.47;//Determined from fig 11.26(c)using value of NTU and c Q=e*Q_max;//[kW] Tc_out=Tc_in+(Q/Cc);//[degree Celcius] Th_out=Th_in-(Q/Ch);//[degree Celcius] disp("degree Celcius",Tc_out,"to","degree Celcius",Tc_in,"The temperature of cooling water will rise from") disp("degree Celcius",Th_out,"to","degree Celcius",Th_in,"as it cools the hot oil from")
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clc w=1.2//lb/ft^2 u=0.3 v=3600//ft/min V=v/60//ft/sec theta=165//degrees g=32.2//ft/s^2 x=theta*%pi/180 k=%e^(u*x)//k=T1/T2=e^(u*x) To=500//lb //Solution a)Vertical drive Tc=w*V^2/g//equation 7.5 //solution a) H=2*(k-1)*(To-Tc)*V/((k+1)*550) Vmax=(To*g/(3*w))^(1/2) Hmax=2*(k-1)*(To-Tc)*Vmax/((k+1)*550) //Solution b) To1=To+Tc //from equation 7.15 2/To1^2=1/Tt^2+1/Ts^2 //T1/T2=k T2=367 //lb - from trail and error T1=k*T2 Tt=T1+Tc Ts=T2+Tc HP=(T1-T2)*V/550 printf("\nSolution a)\nHorsepower transmitted= %.1f\nMaximum Horsepower transmitted= %.1f (at velocit = %.1f ft/s^2)Solution b)\nTt=%.f lb\nTs=%.f lb\nHorsepower transmitted= %.1f",H,Hmax,Vmax,Tt,Ts,HP)
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errcatch(-1,"stop");mode(2);//Ex:2.16 ; ; temp_coeff=0.0005;//in per degree centigrade r_t1=680;//in ohm t1=20;//temperature diff. t2=90; r_o=r_t1/(1+(temp_coeff)*t1); r_t2=r_o*(1+(temp_coeff)*t2); printf("Resistance at %d degree = %f ohms",t2,r_t2); exit();
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function [x]=or(a) // and(a) returns the logical OR // for scalar matrices, an entry is TRUE if it is not zero. //! select type(a) case 1 then k=find(abs(a)>0) case 4 then k=find(a) else error('argument must be a boolean or a real matrix!') end x=k<>[]
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//EXAMPLE 3-55 PG NO-208-209 Vab=400+%i*0; Vbc=-220-%i*381.05; Vca=-220+%i*381.05; Z1=0+%i*25; Z2=13+%i*7.5; Z3=20+%i*0; IAB=Vab/Z1; disp('i) CURRENT (IAB) is in rectangular form = '+string (IAB) +' A '); IBC=Vbc/Z2; disp('i) CURRENT (IBC) is in rectangular form = '+string (IBC) +' A '); ICA=Vca/Z3; disp('i) CURRENT (ICA) is in rectangular form = '+string (ICA) +' A '); IA=IAB-ICA; disp('i) CURRENT (IA) is in rectangular form = '+string (IA) +' A '); IB=IBC-IAB; disp('i) CURRENT (IB) is in rectangular form = '+string (IB) +' A '); IC=ICA-IBC; disp('i) CURRENT (IC) is in rectangular form = '+string (IC) +' A ');
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clc //initialisation of variables w= 40 //ft h= 5 //ft P=50 // lb/ft^2 i= 1/6400 h1= 10 //ft H= 100 //ft g= 32.2 //ft/sec^2 //CAALCULATIONS m= w*h/P v= 140*sqrt(m*i) v1= v*h/h1 h2= w*h1/(H-w) a= v1^2/(140^2*h2) s= (i-a)*1000/(1-(v1^2/(g*h1))) dh= h1-s //RESULTS printf ('depth of water= %.3f ft',dh)
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considerNonPrimitive Expanding for base=2, level=4, reasons+features=base,primitive,same,similiar,evenexp Refined variables=p,q [0+1p,0+1q]: unknown -> [1] [0,0] -p²+2q² -> solution [0,0],trivial(3) ---------------- level 0 expanding queue[0]^-1,meter=[2,2]: -p²+2q² [0+2p,0+2q]: non-primitive -> solution [0,0],trivial(3) endexp[0] Proof [1] mod 2: -p²+2q²
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Dueling Apex.sce
Name=Dueling Apex PlayerCharacters=Apexer BotCharacters=Blood + Gib + Wraith BOT Rota with diff HP.rot IsChallenge=true Timelimit=60.0 PlayerProfile=Apexer AddedBots=Blood + Gib + Wraith BOT Rota with diff HP.rot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=1 BotTeams=0 MapName=boxer.map MapScale=3.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=0.0 ScorePerKill=12.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.25 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=true ScoreMultKillEfficiency=false GameTag=Apex Legends WeaponHeroTag=Wingman, Manwing, R99, R-99, Wraith, Bloodhound, Gibraltar DifficultyTag=3 AuthorsTag=Midamaru / Lyks BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Realistic Apex characters hitboxes and behaviors, with Wingman and R-99. ADS is supported and change spread and accuracy just like in game. You can download Apex sound fx here: https://tiny.cc/apexfx GameVersion=1.0.7.2 ScorePerDistance=0.0 [Aim Profile] Name=Medium Skill MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Bot Profile] Name=Bloodhound BLUE shield DodgeProfileNames=[AA]Apex Dodge;ADAD;Short Strafes;Very Short Strafes + Jump;Fast Strafes Close DodgeProfileWeights=0.6;0.2;1.5;1.4;1.0 DodgeProfileMaxChangeTime=2.0 DodgeProfileMinChangeTime=0.25 WeaponProfileWeights=1.0;0.0;0.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Medium Skill;Medium Skill;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Bloodhound BLUE shield SeeThroughWalls=false NoDodging=false NoAiming=true [Bot Profile] Name=Gibraltar PURPLE shield DodgeProfileNames=[AA]Apex Dodge;ADAD;Short Strafes;Very Short Strafes + Jump;Fast Strafes Close DodgeProfileWeights=0.6;0.2;1.5;1.4;1.0 DodgeProfileMaxChangeTime=2.0 DodgeProfileMinChangeTime=0.25 WeaponProfileWeights=1.0;0.0;0.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Medium Skill;Medium Skill;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Gibraltar PURPLE shield SeeThroughWalls=false NoDodging=false NoAiming=true [Bot Profile] Name=Wraith WHITE shield DodgeProfileNames=[AA]Apex Dodge;ADAD;Short Strafes;Very Short Strafes + Jump;Fast Strafes Close DodgeProfileWeights=0.6;0.2;1.5;1.4;1.0 DodgeProfileMaxChangeTime=2.0 DodgeProfileMinChangeTime=0.25 WeaponProfileWeights=1.0;0.0;0.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Medium Skill;Medium Skill;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Wraith WHITE shield SeeThroughWalls=false NoDodging=false NoAiming=true [Bot Rotation Profile] Name=Blood + Gib + Wraith BOT Rota with diff HP ProfileNames=Bloodhound BLUE shield;Gibraltar PURPLE shield;Wraith WHITE shield ProfileWeights=1.0;1.0;1.0 Randomized=false [Character Profile] Name=Apexer MaxHealth=200.0 WeaponProfileNames=Manwing;R-99;;;;;; MinRespawnDelay=3.0 MaxRespawnDelay=9.0 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=450.0 MaxCrouchSpeed=160.0 Acceleration=8000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=400.0 Gravity=1.8 AirControl=0.3 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=0.863 Y=0.776 Z=0.434 EnemyHeadColor=X=1.000 Y=0.888 Z=0.000 TeamBodyColor=X=0.366 Y=0.067 Z=0.371 TeamHeadColor=X=0.863 Y=0.776 Z=0.434 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=270.0 MainBBType=Cylindrical MainBBHeight=280.0 MainBBRadius=50.0 MainBBHasHead=true MainBBHeadRadius=31.0 MainBBHeadOffset=1.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=65.0 ProjBBRadius=10.0 ProjBBHasHead=true ProjBBHeadRadius=6.0 ProjBBHeadOffset=-8.0 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=Run.abilsprint;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.3 BackSpeedMult=0.9 RespawnInvulnTime=0.0 BlockedSpawnRadius=300.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=1.0 ForwardSpeedBias=1.0 HealthRegainedonkill=200.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=140.0 TPSOffset=X=0.000 Y=20.000 Z=0.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 [Character Profile] Name=Bloodhound BLUE shield MaxHealth=175.0 WeaponProfileNames=Manwing;R-99;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=9.0 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=0.8 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=450.0 MaxCrouchSpeed=160.0 Acceleration=8000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=400.0 Gravity=1.8 AirControl=0.3 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=0.420 Y=0.208 Z=0.482 EnemyHeadColor=X=0.553 Y=0.098 Z=0.000 TeamBodyColor=X=0.366 Y=0.067 Z=0.371 TeamHeadColor=X=0.863 Y=0.776 Z=0.434 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=270.0 MainBBType=Cylindrical MainBBHeight=265.0 MainBBRadius=46.0 MainBBHasHead=true MainBBHeadRadius=28.0 MainBBHeadOffset=-10.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=65.0 ProjBBRadius=10.0 ProjBBHasHead=true ProjBBHeadRadius=6.0 ProjBBHeadOffset=-8.0 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=Run.abilsprint;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=0.9 BackSpeedMult=0.9 RespawnInvulnTime=0.0 BlockedSpawnRadius=300.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=1.0 ForwardSpeedBias=1.0 HealthRegainedonkill=200.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=140.0 TPSOffset=X=0.000 Y=20.000 Z=0.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=5.0 [Character Profile] Name=Gibraltar PURPLE shield MaxHealth=200.0 WeaponProfileNames=Manwing;R-99;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=9.0 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=0.8 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=450.0 MaxCrouchSpeed=160.0 Acceleration=8000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=400.0 Gravity=1.8 AirControl=0.3 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=0.420 Y=0.208 Z=0.482 EnemyHeadColor=X=0.553 Y=0.098 Z=0.000 TeamBodyColor=X=0.366 Y=0.067 Z=0.371 TeamHeadColor=X=0.863 Y=0.776 Z=0.434 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=270.0 MainBBType=Cylindrical MainBBHeight=285.0 MainBBRadius=74.0 MainBBHasHead=true MainBBHeadRadius=28.0 MainBBHeadOffset=-18.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=65.0 ProjBBRadius=10.0 ProjBBHasHead=true ProjBBHeadRadius=6.0 ProjBBHeadOffset=-8.0 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=Run.abilsprint;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=0.9 BackSpeedMult=0.9 RespawnInvulnTime=0.0 BlockedSpawnRadius=300.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=1.0 ForwardSpeedBias=1.0 HealthRegainedonkill=200.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=140.0 TPSOffset=X=0.000 Y=20.000 Z=0.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=5.0 [Character Profile] Name=Wraith WHITE shield MaxHealth=150.0 WeaponProfileNames=Manwing;R-99;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=9.0 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=0.8 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=450.0 MaxCrouchSpeed=160.0 Acceleration=8000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=400.0 Gravity=1.8 AirControl=0.3 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=0.420 Y=0.208 Z=0.482 EnemyHeadColor=X=0.553 Y=0.098 Z=0.000 TeamBodyColor=X=0.366 Y=0.067 Z=0.371 TeamHeadColor=X=0.863 Y=0.776 Z=0.434 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=270.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=43.0 MainBBHasHead=true MainBBHeadRadius=23.0 MainBBHeadOffset=-12.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=65.0 ProjBBRadius=10.0 ProjBBHasHead=true ProjBBHeadRadius=6.0 ProjBBHeadOffset=-8.0 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=Run.abilsprint;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=0.9 BackSpeedMult=0.9 RespawnInvulnTime=0.0 BlockedSpawnRadius=300.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=1.0 ForwardSpeedBias=1.0 HealthRegainedonkill=200.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=140.0 TPSOffset=X=0.000 Y=20.000 Z=0.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=5.0 [Dodge Profile] Name=[AA]Apex Dodge MaxTargetDistance=6666.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.7 MaxLRTimeChange=2.0 MinFBTimeChange=0.7 MaxFBTimeChange=2.0 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.18 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=0.3 DamageReactionThreshold=1.0 DamageReactionResetTimer=0.2 JumpFrequency=0.25 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=0.1 MaxJumpTime=0.1 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.18 BlockedMovementReactionMax=0.25 [Dodge Profile] Name=ADAD MaxTargetDistance=2500.0 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=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.2 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.16 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.2 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Short Strafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.2 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Very Short Strafes + Jump MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.1 MaxLRTimeChange=0.3 MinFBTimeChange=0.1 MaxFBTimeChange=0.3 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.6 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Fast Strafes Close MaxTargetDistance=150.0 MinTargetDistance=50.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.1 MaxLRTimeChange=1.0 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=0.1 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.07 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.6 MaxCrouchTime=0.8 MinJumpTime=0.1 MaxJumpTime=0.1 LeftStrafeTimeMult=0.5 RightStrafeTimeMult=0.6 StrafeSwapMinPause=0.1 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Manwing Type=Projectile ShotsPerClick=1 DamagePerShot=45.0 KnockbackFactor=0.1 TimeBetweenShots=0.26 Pierces=false Category=SemiAutoNoPrehold 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=55000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=55000.000 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=8 AmmoPerShot=1 ReloadTimeFromEmpty=2.1 ReloadTimeFromPartial=2.1 DamageFalloffStartDistance=5000.0 DamageFalloffStopDistance=5000.0 DamageAtMaxRange=200.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Arrow VisualLifetime=0.5 WallParticleEffect=Flare HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.5 CanAimDownSight=true ADSZoomDelay=0.13 ADSZoomSensFactor=1.0 ADSMoveFactor=0.8 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=275.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=Smoke 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=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=70 ADSFOVOverride=77.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=150.0 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=1.0,10.0,0.0,5.3 SpreadSCA=1.0,2.0,0.0,1.3 SpreadMSA=1.0,2.0,0.0,1.3 SpreadMCA=1.0,2.0,0.0,1.3 SpreadSSH=4.0,4.0,1.35,3.7 SpreadSCH=4.0,4.0,1.4,3.8 SpreadMSH=4.0,4.0,1.65,3.7 SpreadMCH=4.0,4.0,1.4,3.8 MaxRecoilUp=3.3 MinRecoilUp=1.65 MinRecoilHoriz=0.2 MaxRecoilHoriz=1.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.25 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 [Weapon Profile] Name=R-99 Type=Projectile ShotsPerClick=1 DamagePerShot=12.0 KnockbackFactor=0.0 TimeBetweenShots=0.05 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=42000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=42000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=1.5 MagazineMax=25 AmmoPerShot=1 ReloadTimeFromEmpty=0.7 ReloadTimeFromPartial=0.7 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=12.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Arrow VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=true ADSZoomDelay=0.13 ADSZoomSensFactor=1.0 ADSMoveFactor=0.8 ADSStartDelay=0.0 ShootSoundCooldown=0.05 HitSoundCooldown=0.05 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=1 DecalSize=25.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=100.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.1 TaggingMaxFactor=0.25 TaggingHitFactor=0.4 ProjectileTrail=Smoke RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=0.7 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=3.0 AimPunchResetTime=0.25 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=true PSRAutoReset=true AimPunchUpTime=0.1 AmmoReloadedOnKill=25 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=70 ADSFOVOverride=77.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=0.5,3.0,1.0,1.5 SpreadSCH=0.5,3.0,0.8,3.0 SpreadMSH=0.5,3.0,1.4,2.5 SpreadMCH=0.5,3.0,0.8,3.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.3 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=true PSRLoopStartIndex=0 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no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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//=========================================================================== //chapter 5 example 22 clc; clear all; //variable declaration Irms = 32; //measured reading reading in A Ir = 30; //rectifier ammeter reading in A Ks = 1.11; //form factor for sinusoidal wave //calculations Iav = Ir/(Ks); //average value of current under measurement in A e = ((Irms)/(Iav)); //percentage errror in % //result mprintf("form factor = %3.3f ",e);
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tpyrun $p/bin/util/dictdiff_test
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//consider the CJ-1 at sea level. b=16.25;//wingspan(meter) S=29.54;//wingarea(m^2) AR=b^2/S;//aspect ratio D=1.225;//density at sea level(Kg/m^3) W=88176.75;//normal gross weight(N) Tf=2*16245//thrust (N) provided by two turbofan engine Cdo=0.02;//parasite drag coefficient e=0.81;//oswald efficiency factor V=linspace(40,300,500);//velocity over which we have to find thrust(40 to 300 m/s and over 500 points)
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clear; clc; //Example14.12[Evaporative Cooling of a Canned Drink] //Given:- //Water is species A and air is species B M_A=18,M_B=29;;//Molar Masses of water and air[kg/kmol] D_AB=2.5*10^(-5);//Diffusivity of water vapor in air[m^2/s] T_inf=30;//Ambient Temperature[degree Celcius] T_avg=(20+T_inf)/2;//Average temperature P=101.325;//Atmospheric Pressure[kPa] //Properties of A at 20 degree Celcius h_fg=2454;//[kJ/kg] Pv1=2.34;//Saturation vapor pressure[kPa] Pv2=4.25;//Vapor Pressure at 30 degree Celcius[kPa] //Properties of air at average temperature and 1 atm Cp=1.007;//[kJ/kg] a=2.141*10^(-5);//[m^2/s] phi=0.4;//Relative Humidity //Solution:- Le=a/D_AB; disp(Le,"The Lewis Number is") Pv_inf=phi*Pv2;//[kPa] disp("kPa",Pv_inf,"The vapor pressure of air away from the surface is") Ts=T_inf-(h_fg*M_A*(Pv1-Pv_inf)/(Cp*(Le^(2/3))*M_B*P)); disp("degree Celcius",Ts,"The temperature of the drink can be lowered to")
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//developed in windows XP operating system //platform Scilab 5.4.1 clc;clear all; //example 9.3 //calculation of dielectric constant and complex permittivity of bakelite //given data C=147*10^-12//capacitance(in Farad) Ca=35*10^-12//air capacitance(in Farad) tandelta=0.0012 epsilon0=(36*%pi*10^9)^-1//electrical permittivity(in F/m) of free space //calculation epsilonr=C/Ca//dielectric constant Kdash=epsilonr Kdashdash=tandelta*Kdash Kim=complex(Kdash,-Kdashdash) epsilonast=epsilon0*Kim printf('The dielectric constant is %3.1f ',epsilonr) disp(epsilonast,'The complex permittivity(in F/m)is ')
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//Example 7_1_u2 clc(); clear; //To calculate the mean free path mn=0.26*0.91*10^-30 un=1000*10^-4 e=1.6*10^-19 tc=(mn*un)/e vth=10^7 meanfreepath=vth*tc*10^7 //units in nm printf("The mean free path is given by L=%.1f nm",meanfreepath)
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//Exa6.7 clc; clear; close; // given : G=12 // required gain in dB f=200 // frequency in MHz f=200*10^6 // frequency in Hz c=3*10^8 // speed of light in m/s lambda=c/f // wavelength in m La=0.46*lambda // length of driven element in m (note: in book La is given 0.416*lambda misprint) Lr=0.475*lambda // length of reflector in m Ld1=0.44*lambda // length of director1 in m Ld2=0.44*lambda // length of director2 in m Ld3=0.43*lambda // length of director3 in m Ld4=0.40*lambda // length of director4 in m SL=0.25*lambda // spacing between reflector and driver in m Sd=0.31*lambda // spacing director and driving element in m d=0.01*lambda // diameter of elements in m l=1.5*lambda // length of array in m disp(La,"length of driven element in m:") disp(Lr,"length of reflector in m:") disp(Ld1,"length of director1 in m:") disp(Ld2,"length of director2 in m:") disp(Ld3,"length of director3 in m:") disp(Ld4,"length of director4 in m:") disp(SL,"spacing between reflector and driver in m:") disp(Sd,"spacing director and driving element in m:") disp(d,"diameter of elements in m:") disp(l,"length of array in m:")
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clc; clear; e=0.001; D=0.50; l=0.20; lg=0.005; A1=12800;//Stator peak current densities A2=9600;//Rotor peak current densities lamda=(%pi/3);//torque angle F1=A1*D*(1/2);//mmf per pole F2=A2*D*(1/2);//mmf per pole Fo=4450;//Resultant gap mmf per pole Mewo=1.25*10^(-7); Bm=(Fo*Mewo)/lg; disp(Bm,'The sine distributed flux density of peak value:') Mp=((D*l)/(3*Mewo))*(Bm^2);//Magnetic pull per pole disp(Mp,'The magnetic pull per pole is :') e1=0.001/0.005;//Eccentricity after displacement of 'e' Mu=((%pi*D*l)/(4*Mewo))*(Bm^2)*e1; disp(Mu,'The resultant u.m.p is:') M=260; F=M/0.25; disp(M,'The useful torque of machine is:') disp(F,'The pheripheral force is:')
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java -ea trip.Main -m trip-tests/autograder_map01 trip-tests/autograder_request01
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//Example 2.15 //To determine area of triangle when 3 sides are given clc,clear c=7 //side oposite to vertex C a=5 //side opposite to vertex A b=4 //side opposite to vertex B s= (a+b+c)/2 //semi perimeter area_K = sqrt(s*(s-a)*(s-b)*(s-c)) //using herons formula printf('Area of triangle ABC = %.2f square units',area_K)
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//Ball is dropped from height u1=sqrt(2*9.81*1) //m/sec v1=-sqrt(2*9.81*0.810) //m/sec //There is no movement of the floor before and after striking //u2=0 //v2=0 //From the defination of coefficient of restitution e=(3.987/4.429) //Let the velocity of the ball after second bounce be v2 v2=e*3.987 //m/sec upward //Expected height h2 h2=(3.576^2)/(2*9.81) //m printf("\nCoefficient of restitution=%.3f \nExpected height of second bounce h2=%.4f m",e,h2)
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// chapter14 // example14.12 // page 307 Rin=1d3 // ohm Rc= 10d3 // ohm Rl=100 // ohm gain_beta=100 // effective collector load is R_AC=Rc*Rl/(Rc+Rl) Av=gain_beta*R_AC/Rin printf("voltage gain = %.3f \n",Av) printf("comment : load is only 100 ohm so efective load of amplifier is too much reduced.\nThus voltage gain is very small.\n") printf("In such cases we can use a step down transformer to serve the purpose. \n")
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//Variable declaration: NPS = 2 //Nominal pipe size (inch) SN = 40 //Schedule number //Calculation: //From Table 6.2, we obtain that the inside diameter of steel pipe is ID = 2.067 in. ID = 2.067 //Result: printf("The inside diameter of steel pipe is : %f in.",ID)
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clc // Given that v = 6.6e4 // speed of electron in m/sec a = 0.01 // percentage accuracy in measurement of speed e = 1.6e-19 // charge on an electron in C m = 9.1e-31 // mass of electron in kg h = 6.6e-34 // Planck constant in J-sec // Sample Problem 9 on page no. 15.27 printf("\n # PROBLEM 9 # \n") printf("Standard formula used \n") printf(" del_x*del_p = h/(4*pi) \n") delta_v = v * a / 100 delta_p = m * delta_v delta_x = h / (4 * %pi * delta_p) printf("\n Uncertainty in determining the position is %e m.",delta_x)
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clear clc //initialisation of variables l= 5000 //ft l1= 2000 //ft d= 12 //in f= 0.005 d1= 24 //in f1= 0.0045 l2= 3000 //ft Q= 1800 //gal/min w= 6.24 //lb/ft^3 g=32.2 //ft/s^2 //CALCULATIONS F= Q/(60*w) v1= F*4/(%pi*(d/12)^2) v2= v1/(d1/d)^2 H= (f*l1*F^2/(10*(d/12)^5))+(f1*l2*F^2/(10*(d1/12)^5))+(v1^2/(4*g))+((v1-v2)^2/(2*g))+(v2^2/(2*g)) //RESULTS printf ('Available Head = %.2f ft',H)
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// C-Exercise 22, SS 2017 // Density of the Beta distribution. function y = Beta_density (x, alpha1, alpha2) y = 1/beta(alpha1,alpha2) * x^(alpha1-1) .* (1-x)^(alpha2-1) .* (x>=0) .* (x<=1); endfunction function X = Sample_Beta_AR (alpha1, alpha2, N) // Mode of the density of the Beta distribution. x_max = (alpha1-1) / (alpha1+alpha2-2); // Constant C for the acceptance/rejection method. C = Beta_density(x_max, alpha1, alpha2); // Generate one sample by the acceptance/rejection method. function x = SingleSample() success = %F while ~success U = rand(2,1); success = ( C*U(2) <= Beta_density(U(1), alpha1, alpha2) ); end x = U(1); endfunction // Generate N samples. X = zeros(N,1); for n=1:N X(n) = SingleSample(); end endfunction // Test parameters. alpha1 = 2; alpha2 = 3; N = 2000; // Generate N samples. X = Sample_Beta_AR (alpha1, alpha2, N); // Plot histogram of samples and density of the Beta distribution. scf(0); clf(); histplot(50,X); // Divide density by the number of bins such that they have the same scale. x = 0:0.01:1; plot(x, 1/50*Beta_density(x,alpha1,alpha2)); legend("Acceptance/rejection method", "True density *1/50"); xlabel("x"); ylabel("Frequency / density"); title("Illustration of the acceptance/rejection method to sample from the Beta distribution");
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/* Gauss-Seidel Method by Keivalya Pandya on SciLab */ // FUNCTION for Gauss Seidel Method function C = seidel(a, x, b) n = size(a, "r"); for j = 1:n d = b(j); for i = 1:n if j~=i d = d - a(j,i)*x(i); end x(j) = d/a(j,j); end end C = x; endfunction // FUNCTION to give number of iterations. Here, 10 is enough. function K(a, x, b) for i = 1:10 x = seidel(a, x, b); disp(x); end endfunction // Q8 printf("\n\t Q8 Output\n") x = [0,0,0,0]; a = [4, 2, 0, 0; 2, 8, 2, 0; 0, 2, 8, 2; 0, 0, 2, 4]; b = [4, 0, 0, 14]; K(a, x, b);
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// Example 5_6 clc;funcprot(0); // Given data m=2;// The mass flow rate in kg/s V_e=200;// The rocket exhaust velocity in m/s // Calculation F=m*V_e;// The restraining force required to hold the rocket in place in N printf("\nThe restraining force required to hold the rocket in place,F_c=%0.0f N",F);
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//Chapter 4, Exmaple 11, page 146 //Claculate the first Townsend's ionization coefficient clc clear t = 0.2*10**-6 // transit time of electrons in seconds d = 0.05 // m ve = d/t TC = 35*10**-9 // Time constant a = 1/(ve*TC) printf("\n Electron drift velocity = %e m/s",ve) printf("\n alpha = %e m^-1",a) // Answers may vary due to round of error
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Ex1_40_15.sce
//Ex 1.40.15 clc;clear;close; format('v',9); //Given : ND=4.5*10^15;//per cm^3 A=1*10^-2;//cm^2 l=10;//cm tau_p=1*10^-6;//sec tau_n=1*10^-6;//sec Dp=12;//cm^2/sec Dn=30;//cm^2/sec q=1.6*10^-19;//Coulomb del_p=10^21;//electron hole pair/cm^3/sec x=34.6*10^-4;//cm Kdash=26;//mV(Kdash is taken as K*T/q) ni=1.5*10^10;//per cm^3 no=ND;//per cm^3//ND<<ni po=ni^2/no;//per cm^3 ln=sqrt(Dn*tau_n);//cm lp=sqrt(Dp*tau_p);//cm dpBYdx=del_p*exp(-x/lp);//per cm^4 dnBYdx=del_p*exp(-x/ln);//per cm^4 Jp=-q*Dp*dpBYdx;//A/cm^2 Ip=Jp*A;//A disp(Ip,"Hole diffusion current (A) : "); Jn=q*Dn*dnBYdx;//A/cm^2 In=Jn*A;//A disp(In,"Electron diffusion current (A) : "); //Solution is not complete in the book and value of Jp & Jn is due to wrong calculation for dpBYdx and dnBYdx.
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//Problem 35.10: An ac. source of 30/_0° V and internal resistance 20 kohm is matched to a load by a 20:1 ideal transformer. Determine for maximum power transfer (a) the value of the load resistance, and (b) the power dissipated in the load. //initializing the variables: rv = 30; // in volts thetav = 0; // in degrees r = 20000; // in ohms tr = 20; // turn ratio //calculation: //voltage V = rv*cos(thetav*%pi/180) + %i*rv*sin(thetav*%pi/180) //The network diagram is shown in Figure 35.13. //For maximum power transfer, r1 must be equal to r1 = r //load resistance RL RL = r1/tr^2 //The total input resistance when the source is connected to the matching transformer is RT = r + r1 //Primary current I1 = V/RT //N1/N2 = I2/I1 I2 = I1*tr //Power dissipated in load resistance RL is given by P = RL*I2^2 printf("\n\n Result \n\n") printf("\n (a)the value of the load resistance is %.0f ohm",RL) printf("\n (b) Power dissipated in the load resistance is %.2E W",P)
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Power_Law_Transform.sce
clc; clear all; a=imread('color.jpg'); subplot(1,5,1); title('Original image'); imshow(a); b=rgb2gray(a); c=im2double(b); subplot(1,5,2); title('Grayscale image'); imshow(b); s1=c.^0.2; x=255/(max(max(s1))); s4=x.*s1; u1=uint8(s4); subplot(1,5,3); title('power law image with gamma 0.2'); imshow(u1); s2=c.^0.6; x2=255/(max(max(s2))); s5=x2.*s2; u2=uint8(s5); subplot(1,5,4); title('power law image with gamma 0.6'); imshow(u2); s3=c.^4; x3=255/(max(max(s3))); s6=x3.*s3; u2=uint8(s6); subplot(1,5,5); title('power law image with gamma 4'); imshow(u2);
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//6.1 clc; r=250; s=1000; l=1000; x=r*l/s; printf("Position of the fault=%.1fm",x)
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f=50 w=2*%pi*f T=1/f Iav=1/(T/2)*integrate('sin(w*t)','t',0,T/2) disp(Iav)
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// Exa 9.4 clc; clear; close; //given data f=700;// in Hz // R_A= R_B // T_on = T_off = T/2 // Frequency is given by equation f= 1.44/((R_A+R_B)*C) C=0.01;// in micro F (assumed value) C=C*10^-6;// in F R_A= 1.44/(2*f*C);// in ohm R_A=R_A*10^-3;// in k ohm R_A=ceil(R_A); R_B= R_A; disp("Resistors required : "+string(R_A)+" k ohm (100 ohm standart value)");
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example12_2.sce
im=50*10^(-6); rm=3000; it1=10^(-3); it2=10*10^(-3); it3=100*10^(-3); it4=1; is1=it1-im; is2=it2-im; is3=it3-im; is4=it4-im; disp("Part a"); rs1=rm*im/is1; disp("for a range of 1 mA the shunt resistance (in Ω) is"); disp(rs1); rs2=rm*im/is2; disp("for a range of 10 mA the shunt resistance (in Ω) is"); disp(rs2); rs3=rm*im/is3; disp("for a range of 100 mA the shunt resistance (in Ω) is"); disp(rs3); rs4=rm*im/is4; disp("for a range of 1 A the shunt resistance (in Ω) is"); disp(rs4); disp("Part b"); vm=im*rm; disp("at full-scale deflection the voltage drop (in V) is"); disp(vm); disp("Part c"); rt1=vm/it1; disp("for a range of 1 mA the total resistance (in Ω) is"); disp(rt1); rt2=vm/it2; disp("for a range of 10 mA the total resistance (in Ω) is"); disp(rt2); rt3=vm/it3; disp("for a range of 100 mA the total resistance (in Ω) is"); disp(rt3); rt4=vm/it4; disp("for a range of 1 A the total resistance (in Ω) is"); disp(rt4);
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example6.sce
// Example 2-6, page 51 clear;clc; close; // Given data I(1)=5;// saturation current at given temperature in nano amperes T(1)=25;// temperature in degree celcius at which saturation current is known T(2)=100;// temperature in degree celcius at which saturation current is to be found // Calculations I(2)=(2^7)*I(1);// 7 doublings between 25 and 95 degree celcius I(3)=((1.07)^5)*I(2); // additional 5 degree between 95 and 100 degree celcius disp("Amperes",I(3),"Saturation Current =") // Result // saturation current at 100 degree celcius is 898 nano amperes.
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TK_EvalStr.man.tst
clear;lines(0); TK_EvalStr('toplevel .foo'); // creates a toplevel TK window. TK_EvalStr('label .foo.l -text ""TK married Scilab !!!""'); // create a static label TK_EvalStr('pack .foo.l'); // pack the label widget. It appears on the screen. text='button .foo.b -text close -command {destroy .foo}'; TK_EvalStr(text); TK_EvalStr('pack .foo.b');
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7_5.sce
//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 7.5 //calculation of the normal contact force by the side wall of the groove //given data r=25*10^-2//radius(in m) of the cirlce m=.1//mass(in kg) of the block t=2//time(in s) taken by the block //calculation v=2*%pi*r/t//speed of the block a=(v*v)/r//acceleration of the block N=m*a//newton's second law printf('the normal contact force by the side wall of the groove is %3.2f N',N)
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1_5.sce
// Example 1.5 clc; //Given A = [3 5 -7]; B = [2 7 1]; //Solution C = A+B; D = A-B; E = (A(1,1)^2 + A(1,2)^2 + A(1,3)^2)^0.5; F = (B(1,1)^2 + B(1,2)^2 + B(1,3)^2)^0.5; G = (A(1,1)*B(1,1) + A(1,2)*B(1,2) + A(1,3)*B(1,3)); H = G/(E*F); // where C=A+B and D=A-B and E =|A| and F = |B| and G = A.B and H =cos(A,B) disp("A+B ="); disp(C); disp("A-B ="); disp(D); disp("|A|="); disp(E); disp("|B|="); disp(F); disp("A.B="); disp(G); disp("cos(A,B)="); disp(H);