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function X_ech=decimation(X, k_ech) // Fonction downsampling facteur k_ech [n,l]=size(X) n_ech=int(n/k_ech) X_ech=zeros(n_ech,l); for i = 1:n_ech X_ech(i,:)=X(i*k_ech,:); end endfunction // //X=read('bunny.asc',-1,3); //[n,l]=size(X) //X_ech=decimation(X,10) //write('bunny_ech.asc',X_ech); //figure(1); //clf //param3d1(X_ech(:,1), X_ech(:,2), list(X_ech(:,3), -4));

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clc; //e.g 16.4 Vdc=30; RL=600; Rf=25; Idc=(Vdc/RL); disp('A',Idc*1,"Idc="); Im=%pi*Idc; disp('A',Im*1,"Im="); Vin=Im*(Rf+RL); disp('V',Vin*1,"Vin=");

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example_11.sce

clc clear printf("example 5.11 page number 192\n\n") //to find the equilibrium temperature R=6.92*10^5 //in km l=14.97*10^7 //in km Ts=6200; //in K To=(R^2/l^2)^0.25*Ts; printf("Equilibrium temperature = %f K",To)

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// Exa 4.15 clc; clear; close; // Given data V_CC = 18;// in V bita = 90; R_C = 2.2 * 10^3;// in ohm R_E = 1.8*10^3;// in ohm R_B = 510*10^3;// in ohm I_B = V_CC/( (bita*(R_C+R_E))+R_B );// in A I_C = bita*I_B;// in A disp(I_C*10^3,"The value of I_C in mA is"); V_CE = I_B*R_B;// in V disp(V_CE,"The value of V_CE in V is");

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errcatch(-1,"stop");mode(2);; ; //To determine the number of guided modes NA=0.28; //numerical aperture a=30; //core radius lambda=0.8; //wavelength in micro meter f=(2*%pi*a*NA)/lambda; //normalised frequency Ng=f^2/2 //number of guided modes printf("The number of guided modes is %f",Ng); exit();

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clc; Vgs1=-0.5 Vgs2=-5; Gm01=0.002; Gm02=0.006; Vgsoff1=-2; Vgsoff2=-8; Gm1=Gm01*(1-(Vgs1/Vgsoff1)); Gm2=Gm02*(1-(Vgs2/Vgsoff2)); Rs=5100; RL=20000; rS=(Rs*RL)/(Rs+RL); Avmin=rS/(rS+(1/Gm1)); Avmax=rS/(rS+(1/Gm2)); disp(' ',Avmax,"Avmax=")//The answers vary due to round off error disp(' ',Avmin,"Avmin=")//The answers vary due to round off error Gm11=1/667; Gm22=1/444; Zoutmax=(Rs/Gm11)/(Rs+(1/Gm11)); Zoutmin=(Rs/Gm22)/(Rs+(1/Gm22)); disp('Ohm',Zoutmax,"Zoutmax=")//The answers vary due to round off error disp('Ohm',Zoutmin,"Zoutmin=")//The answers vary due to round off error R1=1000000; R2=1000000; Zin=(R1*R2)/(R1+R2); disp('KOhm',Zin/1000,"Zin=")//The answers vary due to round off error

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// Example 24_25 clc;funcprot(0); //Given data p_r=4.5;// Pressure ratio m_a=82;// kg/min m_f=1.4;// kg/min W_o=200;// kW W_c=230// kW p_1=1;// bar T_1=15+273;// K T_3=765+273;// K r_c=1.4;// The index of compression r_e=1.34;// The index of expansion C_pa=1;// kJ/kg.K C_pg=1.13;// kJ/kg.K n_m=0.98;// Mechanical efficiency of the compressor //Calculation W_t=(W_o+W_c)/n_m;// kW m_a=(m_a)/60;// kg/sec m_f=(m_f)/60;// kg/sec AF=m_a/m_f;// Air fuel ratio //(a) T_2a=T_1*(p_r)^((r_c-1)/r_c);// K n_c=(m_a*C_pa*((T_2a-T_1)/W_c))*100;// Isentropic efficiency of compressor in % //(b) T_4a=T_3/(p_r)^((r_e-1)/r_e);// K n_t=(W_t/((m_a+m_f)*C_pg*(T_3-T_4a)))*100;// Isentropic efficiency of turbine in % //(c) T_2=T_1+((T_2a-T_1)/(n_c/100));// K n_o=(W_o/((m_a+m_f)*C_pg*(T_3-T_2)))*100;// The over all efficiency of the plant in % printf('\n(a)Isentropic efficiency of compressor=%0.0f percentage \n(b)Isentropic efficiency of turbine=%0.1f percentage \n(c) The over all efficiency of the plant=%0.1f percentage',n_c,n_t,n_o); // The answers provided in the textbook is wrong

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ex1_38.sce

//Exa:1.38 clc; clear; close; V=230;//in volts I_a=100;//in amperes R_a=0.05;//in ohms E_b=V-I_a*R_a;//in volts N=870;//in rpm T=E_b*I_a/(2*%pi*N/60);//torque developed (in N-m) T_l=400;//in N-m I_an=I_a*T_l/T;//in amperes E=V+I_an*R_a;//in volts N1=N*E/230; disp(N1,'Speed (in rpm)=')

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EX7_2.sce

//EXAMPLE 7-2 PG NO-437-438 Z11=99+%i*99; Z12=-%i*100; Z21=20-%i*102.26; Z22=90.06-%i*120; Z1=Z11-Z12; disp('i) Impedance (Z1) is in rectangular form = '+string (Z1) +'ohm '); Z2=Z22-Z12; disp('ii) Impedance (Z2) is in rectangular form = '+string (Z2) +'ohm '); Z3=Z21-Z12; disp('iii) Impedance (Z3) is in rectangular form = '+string (Z3) +'ohm ');

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//Exa:3.17 clc; clear; close; V=200;//in volts I_a=100;//in amperes R_a=0.02;//in ohms N1=940;//in rpm N2=500;//in rpm E_b1=V-(I_a*R_a);//in volts E_b2=E_b1*N2/N1;//in volts V_a=E_b2+(I_a*R_a);//in volts alpha=V_a/V; disp(alpha,'Duty Cycle Of The Chopper=')

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gaussjordon.sce

a = [3 4 -2 2 2 4 9 -3 5 8 -2 -3 7 6 10 1 4 6 7 2]; for j=1:m-1 for z=2:m if a(j,j)==0 t=a(j,:);a(j,:)=a(z,:); a(z,:)=t; end end for i=j+1:m a(i,:)=a(i,:)-a(j,:)*(a(i,j)/a(j,j)); end end x=zeros(1,m); for s=m:-1:1 c=0; for k=2:m c=c+a(s,k)*x(k); end x(s)=(a(s,n)-c)/a(s,s); end disp('Gauss elimination method:'); for j=1:m-1 for z=2:m if a(j,j)==0 t=a(1,:);a(1,:)=a(z,:); a(z,:)=t; end end for i=j+1:m a(i,:)=a(i,:)-a(j,:)*(a(i,j)/a(j,j)); end end for j=m:-1:2 for i=j-1:-1:1 a(i,:)=a(i,:)-a(j,:)*(a(i,j)/a(j,j)); end end for s=1:m a(s,:)=a(s,:)/a(s,s); x(s)=a(s,n); end disp('Gauss-Jordan method:');

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Example1_11.sce

//Example 1.11 //MAXIMA SCILAB TOOLBOX REQUIRED FOR THIS PROGRAM //Testing Stability of Given System clear; clc ; close ; syms n; x =(1/2)^n X= symsum (x,n ,0, %inf ); //Display the result in command window disp (X,"Summation is :"); disp('Hence Summation < infinity. Given System is Stable');

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@relation abalone @attribute Sex{M,F,I} @attribute Length real[0.075,0.815] @attribute Diameter real[0.055,0.65] @attribute Height real[0.0,1.13] @attribute Whole_weight real[0.002,2.8255] @attribute Shucked_weight real[0.001,1.488] @attribute Viscera_weight real[5.0E-4,0.76] @attribute Shell_weight real[0.0015,1.005] @attribute Rings{15,7,9,10,8,20,16,19,14,11,12,18,13,5,4,6,21,17,22,1,3,26,23,29,2,27,25,24} @inputs Sex,Length,Diameter,Height,Whole_weight,Shucked_weight,Viscera_weight,Shell_weight @outputs Rings @data 12 7 10 7 15 7 5 7 4 7 8 7 20 7 11 7 16 7 12 7 8 7 12 7 11 7 9 7 18 7 7 7 9 7 16 7 13 7 13 7 12 7 8 7 13 7 7 7 11 7 15 7 11 7 9 7 10 7 16 7 8 7 19 7 19 7 10 7 10 7 10 7 12 7 14 7 11 7 11 7 13 7 17 7 11 7 5 7 10 7 14 7 8 7 14 7 11 7 15 7 21 7 9 7 16 7 11 7 11 7 11 7 5 7 12 7 4 7 13 7 13 7 17 7 17 7 15 7 9 7 10 7 12 7 7 7 10 7 9 7 8 7 15 7 12 7 11 7 4 7 8 7 7 7 5 7 7 7 7 7 6 7 7 7 6 7 6 7 8 7 10 7 9 7 7 7 8 7 10 7 12 7 11 7 6 7 6 7 6 7 7 7 6 7 8 7 8 7 7 7 8 7 8 7 8 7 8 7 9 7 9 7 9 7 7 7 8 7 8 7 11 7 8 7 8 7 7 7 9 7 7 7 13 7 10 7 9 7 9 7 11 7 10 7 10 7 11 7 9 7 10 7 11 7 12 7 10 7 15 7 10 7 10 7 11 7 14 7 6 7 6 7 8 7 6 7 9 7 8 7 6 7 8 7 9 7 9 7 8 7 10 7 10 7 11 7 6 7 5 7 8 7 8 7 8 7 9 7 10 7 12 7 10 7 9 7 8 7 9 7 11 7 10 7 12 7 9 7 12 7 12 7 10 7 10 7 10 7 9 7 11 7 9 7 4 7 7 7 11 7 8 7 8 7 10 7 10 7 7 7 9 7 9 7 9 7 10 7 10 7 9 7 11 7 11 7 13 7 11 7 7 7 7 7 7 7 8 7 9 7 9 7 9 7 8 7 8 7 11 7 8 7 10 7 14 7 7 7 8 7 10 7 9 7 16 7 9 7 12 7 9 7 6 7 5 7 11 7 7 7 18 7 13 7 8 7 13 7 13 7 15 7 10 7 10 7 10 7 8 7 10 7 17 7 23 7 12 7 18 7 11 7 3 7 12 7 10 7 5 7 9 7 10 7 9 7 9 7 11 7 7 7 5 7 8 7 12 7 8 7 7 7 7 7 6 7 9 7 8 7 8 7 9 7 9 7 10 7 11 7 4 7 6 7 8 7 8 7 9 7 9 7 10 7 10 7 11 7 10 7 10 7 12 7 9 7 9 7 7 7 9 7 9 7 6 7 7 7 9 7 8 7 8 7 11 7 11 7 12 7 11 7 11 7 9 7 11 7 14 7 6 7 8 7 9 7 7 7 9 7 9 7 11 7 10 7 10 7 14 7 11 7 11 7 7 7 7 7 9 7 13 7 24 7 10 7 15 7 12 7 5 7 9 7 6 7 15 7 16 7 8 7 13 7 14 7 5 7 11 7 18 7 15 7 14 7 12 7 9 7 17 7 16 7 13 7 8 7 19 7 9 7 10 7 5 7 6 7 10 7 13 7 6 7 7 7 13 7 7 7 8 7 9 7 11 7 10 7 10 7 6 7 8 7 8 7 12 7 11 7 3 7 6 7 7 7 7 7 9 7 9 7 10 7 8 7 12 7 10 7 7 7 8 7 9 7 9 7 7 7 10 7 10 7 14 7 10 7 11 7 10 7 11 7 7 7 9 7 9 7 13 7 8 7 10 7 9 7 10 7 9 7 10 7 14 7 6 7 8 7 4 7 7 7 12 7 11 7 5 7 13 7 14 7 17 7 10 7 15 7 12 7 20 7 14 7 13 7 13 7 9 7 12 7 6 7 7 7 6 7 9 7 11 7 10 7 11 7 10 7 11 7 9 7 9 7 8 7 10 7 8 7 9 7 10 7 8 7 10 7 6 7 7 7 7 7

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//chapter6,Example6_4,pg 122 sig=3.82*10^7 L=1000*12*2.54*10^-2//converting into m r=0.4*2.54*10^-2 V=1.2 Jc=sig*(V/L) A=3.14*(r^2) Ic=Jc*A P=Ic*V printf("current density\n") printf("Jc=%.f A/m2",Jc) printf("\ntotal current\n") printf("Ic=%.2f A",Ic) printf("\npower dissipation\n") printf("P=%.2f watt",P)

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example18.sce

//Example 1.8 //Find the power of the signal x(t)=Acos(Wot+theeta) clc; A=20; Wo=(2*%pi)/4; for i=1:50 x(i)=A*cos(Wo*i); end p=0; for i=1:4 p=p+(abs(x(i)^2))/4; end disp(p,'The power of the given signal is =');

a9ec2f7a445cad4da4e20337977e7195fba21317

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/Positive_Negative_test/Netezza-Functions/function1/MLE.tst

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[]

no_license

kamleshm/intern_fuzzy

c2dd079bf08bede6bca79af898036d7a538ab4e2

aaef3c9dc9edf3759ef0b981597746d411d05d34

refs/heads/master

2021-01-23T06:25:46.162332

2017-07-12T07:12:25

93,021,923

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7,200

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MLE.tst

INFO: Reading startup configuration from file PulsarLogOn.act_ssl_config -- Fuzzy Logix, LLC: Functional Testing Script for DB Lytix functions on Teradata Aster -- -- Copyright (c): 2016 Fuzzy Logix, LLC -- -- NOTICE: All information contained herein is, and remains the property of Fuzzy Logix, LLC. -- The intellectual and technical concepts contained herein are proprietary to Fuzzy Logix, LLC. -- and may be covered by U.S. and Foreign Patents, patents in process, and are protected by trade -- secret or copyright law. Dissemination of this information or reproduction of this material is -- strictly forbidden unless prior written permission is obtained from Fuzzy Logix, LLC. -- Functional Test Specifications: -- -- Test Category: Maximum Likelihood Estimation of Distribution Parameters -- -- Last Updated: 05-30-2017 -- -- Author: <kamlesh.meena@fuzzyl.com> -- -- BEGIN: TEST SCRIPT \timing on Timing is on -- BEGIN: TEST(s) -----**************************************************************** ---FLMLEBinomialUdt -----**************************************************************** CREATE VIEW view_binom_1000 AS SELECT 1 AS GroupID, 5 AS NumOfTrials, FLSimBinomial(a.RandVal, 0.77, 5) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumOfTrials , vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_binom_1000 vw) AS z, TABLE(FLMLEBinomialUdt(z.GroupID, z.NumOfTrials, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_binom_1000; ------------------------------------------------------------------------------------- -----**************************************************************** ---FLMLEChiSqUdt -----**************************************************************** CREATE VIEW view_chisq_1000 AS SELECT 1 AS GroupID, FLSimChiSq(a.RandVal, 6) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_chisq_1000 vw) AS z, TABLE (FLMLEChiSqUdt(z.GroupID, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_chisq_1000; ------------------------------------------------------------------------------------- -----**************************************************************** ---FLMLEExpUdt -----**************************************************************** CREATE VIEW view_exp_1000 AS SELECT 1 AS GroupID, FLSimExp(a.RandVal, 0, 6.08) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_exp_1000 vw) AS z, TABLE(FLMLEExpUdt(z.GroupID, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_exp_1000; ------------------------------------------------------------------------------------- -----**************************************************************** ---FLMLENormalUdt -----**************************************************************** CREATE VIEW view_normal_1000 AS SELECT 1 AS GroupID, FLSimNormal(a.RandVal, -3.75, 1.5) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_normal_1000 vw) AS z, TABLE (FLMLENormalUdt(z.GroupID, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_normal_1000; ------------------------------------------------------------------------------------- -----**************************************************************** ---FLMLEPoissonUdt -----**************************************************************** CREATE VIEW view_poisson_1000 AS SELECT 1 AS GroupID, CAST(FLSimPoisson(a.RandVal, 2.1) AS INTEGER) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_poisson_1000 vw) AS z, TABLE (FLMLEPoissonUdt(z.GroupID, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_poisson_1000; ------------------------------------------------------------------------------------- -----**************************************************************** ---FLMLEWeibullUdt -----**************************************************************** CREATE VIEW view_weibull_1000 AS SELECT 1 AS GroupID, FLSimWeibull(a.RandVal, 0, 1.8, 4.8) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_weibull_1000 vw) AS z, TABLE(FLMLEWeibullUdt(z.GroupID, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_weibull_1000; ------------------------------------------------------------------------------------- -----**************************************************************** ---FLMLEStudentsTUdt -----**************************************************************** CREATE VIEW view_student_1000 AS SELECT 1 AS GroupID, FLSimStudentsT(a.randval,0,1,35.6895) AS NumVal FROM fzzlSerial a WHERE a.SerialVal <= 1000; SELECT a.* FROM(SELECT vw.GroupID, vw.NumVal, NVL(LAG(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS begin_flag, NVL(LEAD(0) OVER (PARTITION BY vw.GroupID ORDER BY vw.GroupID), 1) AS end_flag FROM view_student_1000 vw) AS z, TABLE (FLMLEStudentsTUdt(z.GroupID, z.NumVal, z.begin_flag, z.end_flag)) AS a; DROP VIEW view_student_1000;

2b900d2fbb28372aa4fc2179bbdd3ae75486cec8

a56536320fd14b35e21c2b9997d8aac037da6124

/FOCA/FOCA.sce

878c9038439938fd4d071c38608109e0ea868190

[]

no_license

HigorKolecha/OtimizacaoDeRedes

97869a5d4593b2e765304a23edcb4e825883eacb

f0057b6a4d9c1f00734fecdf9ea5b4a859abf433

refs/heads/master

2023-05-12T12:11:43.074997

2021-06-04T23:44:25

369,598,892

1

0

null

UTF-8

Scilab

false

23,379

sce

FOCA.sce

//---------------------------------------------- // Algorítimo OCF responsável pela otimização na // corrente injetada na rede distribuição. // Projeto de Pesquisa FAPESP // Projeto número: #2019/24128-2 // @date 01/07/2020 // @author Higor de Paula Kolecha // @author Adolfo Blengini Neto // @author Marcius Fabius Henriques de Carvalho. // @version 1.0 //---------------------------------------------- // Responsável pela limpeza toda memória clear; // Responsável pela limpeza de tela clc; // Solicitação ao usuário do endereço para obtenção do arquivo de entrada. entradaDeDados=input("Digite o endereço com localização do arquivo de entrada de dados. Obs: seguir instruções no arquivo Guideline. "); // Arquivo de Entrada com a estrutura da Rede de Distribuição. M = fscanfMat(entradaDeDados, "%lg"); // Importa arquivo que apresenta os dados de entrada da rede. // Inicio de contagem de timer para tempo de resolução da rede. tic(); // Salva o número de ramos. NR=M(1,1); // Salva o número de barras. NB=M(1,2)+M(1,3); // Valor de refencia de tensão inicial Real. vf=1.0; // Valor de refencia de tensão inicial Imaginário. vfi=0; // -------------------------------------------------------------------- // Funcao responsável pela construçao do laço externo. // Entrada : Estrutura do arquivo completo. // Saida : Matriz de lacos externos, informação de quantos laços foram // criados. // ------------------------------------------------------------------- function [LE,quantosLacos,barraLaco,barraLacoImag]=lacosExternos(M) // Ajuste da variável M para retirada de informações gerais. mAux=M(2:NR+1,1:size(M,'c')); // Criação de vetores auxiliares O=mAux(:,1); // Criação do vetor origem. D=mAux(:,2); // Criação do vetor destino. // Criação do caminho que a corrente faz para poder criar um laço para a parte real e imaginária da rede. quaisLacos=[]; // Real. quaisLacosImag=[];// Imaginária. // Quais barras tiveram seus laços criados para a parte real e imaginária da rede. barraLaco=[]; // Real. barraLacoImag=[]; // Imaginária. // Definição de posições das barras geradoras na matriz mAux. geradores=find(mAux(:,7)==1); // Criação uma matriz com todas barras geradoras da rede. geradores=mAux(geradores,1); // Estrutura de repetição para criação de laços da rede. for i=NR:-1:1 // Definição da barra inicial que posteriormente será verificada a existência de laços. buss=mAux(i,2); // Laços para parte real da rede. if (mAux(i,3)~=0) // Verificação da existencia de carga. laco=zeros(NR+M(1,3),1); // Criação da matriz referente ao caminho que a corrente faz para poder criar um laço. barraLaco=cat(1,barraLaco,i); // Faz a concatenação da matriz "barralaco" a fim de serem adicionadas apenas as barras com laços existentes. // Busca amontante até feeder. while (1>0) origem=find(D(:,1)==buss); // Mostra as possíveis posições onde se encontra o próximo ramo para formação de laços. laco(origem(1,1),1)=mAux(origem(1,1),5); // Monta o vetor caminhos, mostrando os laços feitos. buss=O(origem(1,1),1); // Recebe o valor que se encontra na posição acima destacada dentro do vetor origem. parada=find(O(:,1)==buss(1,1)); // Procura onde está a origem do buss, retornando a posição da matriz O. parou=mAux(parada,1); // Atribui o valor referente a posição da matriz O encontrada na linha superior. condicaoDeParada=find(geradores(:,:)==parou); // Procura na matriz geradores, se já chegou em algum deles. if(condicaoDeParada~=[]) // Caso o valor da condicaoDeParada seja diferente de vazio, quer dizer que ainda não estamos em um gerador, desta forma, a função while deverá continuar. Caso contrário, deverá parar. break end end buss=mAux(i,2); // Retorna o valor inicial referente a barra a ser utilizada neste momento, para que possa ser criados outros laços futuramente. quaisLacos=cat(2,quaisLacos,laco); // Concatenação horizontal, inserindo todos laços 'reais' criados em apenas uma matriz. end // Laços para parte imaginária da rede. if (mAux(i,4)~=0) // Verificação da existencia de carga. lacoImag=zeros(NR+M(1,3),1); // Criação do caminho que a corrente faz para poder criar um laço. barraLacoImag=cat(1,barraLacoImag,i); // Faz a concatenação da matriz "barralaco" a fim de serem adicionadas apenas as barras com laços existentes. // Busca amontante até feeder, ou seja, barra de geração. while (1>0) origem=find(D(:,1)==buss); // Mostra a posição onde se encontra o próximo ramo para formação de laços. lacoImag(origem(1,1),1)=mAux(origem(1,1),6); // Monta o vetor caminhos, mostrando os laços feitos. buss=O(origem(1,1),1); // Recebe o valor que se encontra na posição acima destacada dentro do vetor origem. parada=find(O(:,1)==buss(1,1)) // Procura onde está a origem do buss, retornando a posição da matriz O. parou=mAux(parada,1); // Atribui o valor referente a posição da matriz O encontrada na linha superior. condicaoDeParada=find(geradores(:,:)==parou); // Procura na matriz geradores, se já chegou em algum deles. if(condicaoDeParada~=[]) // Caso o valor da condicaoDeParada seja diferente de vazio, quer dizer que ainda não estamos em um gerador, desta forma, a função while deverá continuar. Caso contrário, deverá parar. break end end buss=mAux(i,2); // Retorna o valor inicial referente a barra a ser utilizada neste momento, para que possa ser criados outros laços futuramente. quaisLacosImag=cat(2,quaisLacosImag,lacoImag); // Concatenação horizontal, inserindo todos laços 'imaginários' criados em apenas uma matriz. end end // Criação da matriz auxiliar. quaisLacos2=quaisLacos; // Junção das informações de quais barras geraram laço para parte real e imaginária. // barraLaco=cat(1,barraLaco,barraLacoImag); // Junção de laços reais e imaginários. quaisLacos=cat(2,quaisLacos,quaisLacosImag); // Junção dos laços para calculo de tensão imaginária. quaisLacosImag=cat(2,quaisLacosImag*(-1),quaisLacos2); // Junção de todos laços reais e imaginários para calculo da tensão de barra parte real e imaginária. quaisLacos=cat(1,quaisLacos,quaisLacosImag); // Transposição da matriz para concatenação com a matriz indicencia posteriormente. quaisLacos=quaisLacos'; // Expansão da matriz para resolução da rede. quaisLacos=cat(2,quaisLacos,eye(size(quaisLacos,'r'),size(quaisLacos,'r'))); // Nomeação de nova variável, recebendo a matriz de laços criada. LE=quaisLacos; // Dimensão de quantos laços ao todo foram criados. quantosLacos=size(LE,'r'); endfunction // --------------------------------------------------------------- // Funcao responsavel pela construção da Matriz incidência C. // Entrada : Estrutura do arquivo completo e Matriz laços externos. // Saída : Matriz incidência C, informação de colunas para resolução // de caso real, informação de colunas para resolução de caso completo // de rede. //---------------------------------------------------------------- function [C,qnt_coluna_MC_incidencia,qnt_coluna_MC] = MatrizC(M,LE,quantosLacos) AuxC=1; // Auxiliar para criação da matriz inciência de "carga", endereço da coluna. AuxG=1; // Auxiliar para criação da matriz inciência de "geração", endereço da coluna. MAg=zeros(M(1,2),M(1,3)); // Criação de variáveis novas para descartar restrições de desigualdade. for i=2:(NR+1) // Orientação. origem=M(i,1); destino=M(i,2); // Parte real matriz incidencia (A). C(origem,AuxC)=1; C(destino,AuxC)=-1; AuxC=AuxC+1; // Complemento da matriz incidencia (A) com as barras de geração. if(M(i,7)==1) MAg(origem,AuxG)=1; AuxG=AuxG+1; end end // Concatenação da Matriz indicencia com variáveis de folga. C=cat(2,C,MAg); // Criação da matriz que será responsável por receber quais ramos devem estar normalmente abertas ou fechadas. matrizRestricao=zeros(NB,size(C,"c")); // Estrutura de repetição responsável pela criação da matriz responsável pela identificação das linhas abertas, assim como ligar ou desligar ramos da rede. for i=2:(NR+1) if M(i,8)==1 matrizRestricao(i-1,i-1)=1; end end // Ajuste para inserção da variável de folga. matrizRestricao=cat(1,matrizRestricao,zeros(M(1,3),size(matrizRestricao,"c"))); // Informação do tamanho da matriz incidência A. Definição para a quantidade de valores presentes na matriz Q. qnt_coluna_MC_incidencia=size(C,'c'); // Criação de matriz auxiliar de mesmo tamanho que a matriz incidencia após a concatenação com variáveis de folga. C1=zeros(size(C,'r'),size(C,'c')); // Criação da parte imaginária da matriz incidencia. // A concatenção é feita desta forma para que sejam inseridas novas variáveis, sendo responsáveis pela parte imaginária. C2=cat(2,C1,C); // Junção da matriz incidecia real com seu complemento de zeros. // Esta concatenação é feita para que possam ser feita posteriormente a junção com a parte imaginária da rede. C=cat(2,C,C1); // Junção da matriz incidecia real com a parte imaginária. C=cat(1,C,C2); // Ajuste para desligamento de ramo. C=cat(2,C,zeros(size(C,"r"),size(LE,"c")-size(C,"c"))); // Junção de restrição para desligar ramos para partes Real e Imaginária. matrizRestricaoAux=matrizRestricao; matrizRestricao=cat(2,matrizRestricao,zeros(size(matrizRestricao,"r"),size(matrizRestricao,"c"))); matrizRestricaoAux=cat(2,zeros(size(matrizRestricaoAux,"r"),size(matrizRestricaoAux,"c")),matrizRestricaoAux); matrizRestricao=cat(1,matrizRestricao,matrizRestricaoAux); // matrizRestricao=cat(2,matrizRestricao,zeros(size(matrizRestricao,"r"),size(matrizRestricao,"c"))); matrizRestricao=cat(2,matrizRestricao,zeros(size(matrizRestricao,"r"),size(LE,"c")-size(matrizRestricao,"c"))); // Junção da matriz Indicência com a matriz restrição. C=cat(1,C,matrizRestricao); // Inserção da matriz de laço junto à matriz incidência C. // C=cat(1,C,LE); // Inserção de novas colunas para que as restrições de laço funcionem. C=cat(2,C,zeros(size(C,"r"),size(C,"r")-size(C,"c"))); //Valor responsável para a criação da matriz P futuramente. qnt_coluna_MC=size(C,'c'); endfunction // -------------------------------------------------------------------- // Funcao responsavel pela contrução da Matriz de carga b. // Entrada: Estrutura do arquivo completo, informação de colunas para // resolução de caso real, informação de colunas para resolução de caso // completo de rede. // Saída : Matriz de carga b. //--------------------------------------------------------------------- function [b] = MatrizB(M,quantosLacos,qnt_coluna_MC_incidencia,barraLaco,barraLacoImag) // Criação da matriz B com todos valores negativos. for i=1:NR // Matriz b parte real da carga. b(i)=(-1)*(M(i+1,3))//+M((i+1),9)); // Matriz B parte imaginário da carga. b1(i)=(-1)*M(i+1,4); end // Ajuste para casos onde o número de barras é maior que o número de ramos. if NB>NR then b=cat(1,b,zeros(M(1,3),1)); b1=cat(1,b1,zeros(M(1,3),1)); end // Atualização de sinais da matriz B. // Sendo positivo o que é gerado e negativo o que é consumido. for i=1:NR if(M(i+1,7)==1) // Correção para a parte Real. origem=M(i+1,1); b(origem)=b(origem)*(-1); // Correção para a parte imaginária. b1(origem)=b1(origem)*(-1); end end // Complemento referente a barras inseridas de folga e restrições de abertura/fechamento de ramos. if(NB==NR) // Fora necessário inserir esta comparação pois no caso da rede de 400barras, haviam na verdade 402 barras e 402 ramos, mas como 1 ramo era feeder e é considerado que neste caso seja inserido uma barra nova, a quantidade de barras e ramos era diferente, ou seja 403 barras e 402 ramos no total. // Junção da matriz Solicitação de carga partes Real e Imaginária. b=cat(1,b,b1); // Inserção de restrições de laço pela lei de Kirchoff para a parte Real da rede. b=cat(1,b,zeros(2*(NR+M(1,3)),1)); // Inserção de tensão inicial de barra. // b=cat(1,b,vf*ones(size(barraLaco,"r"),1)); // b=cat(1,b,vfi*ones(size(barraLacoImag,"r"),1)); elseif(NB<NR) // Ajuste de tamanho para matriz referente a Solicitação de Carga parte Real e Imaginária b=b(1:NB);// Real b1=b1(1:NB);// Imaginária // Junção da matriz Solicitação de carga partes Real e Imaginária. b=cat(1,b,b1); // Inserção de restrições de laço pela lei de Kirchoff para a parte Real da rede. b=cat(1,b,zeros(2*(NR+M(1,3)),1)); // Inserção de tensão inicial de barra. // b=cat(1,b,vf*ones(size(barraLaco,"r"),1)); // b=cat(1,b,vfi*ones(size(barraLacoImag,"r"),1)); // pause else // Ajuste de tamanho para matriz referente a Solicitação de Carga parte Real e Imaginária. b=b(1:NB);// Real. b1=b1(1:NB);// Imaginária. // Ajuste caso o número de barras for superior ao número de ramos para parte imaginária b=cat(1,b,zeros(M(1,3),1)); // Inserção das solicitações de carga para parte imaginária da rede. b=cat(1,b,b1); // Ajuste caso o número de barras for superior ao número de ramos para parte imaginária b=cat(1,b,zeros(M(1,3),1)); // Inserção de restrições de laço pela lei de Kirchoff para a parte Real da rede. b=cat(1,b,zeros(2*(NR+M(1,3)),1)); // Inserção de tensão inicial de barra. // b=cat(1,b,vf*ones(size(barraLaco,"r"),1)); // b=cat(1,b,vfi*ones(size(barraLacoImag,"r"),1)); end endfunction //------------------------------------------------------------------- // Função responsável pela criação da matriz Q. // Entrada : Estrutura do arquivo completo, informação de colunas para // resolução de caso real, informação de colunas para resolução de caso // completo de rede. // Saída : Matriz simétrica para resistência e reatância Q. //------------------------------------------------------------------- function [Q]=MatrizQ(M,qnt_coluna_MC_incidencia,quantosLacos) // Dimensionamento de tamanho para matriz Q. Q=zeros(NR,qnt_coluna_MC_incidencia); Q2=zeros(NR,qnt_coluna_MC_incidencia); Q3=zeros(NR,qnt_coluna_MC_incidencia); // Criação da matriz simétrica para resistência e reatância de cada barra. for i=2:(NR+1) // Matriz simétrica para resistência. Q(i-1,i-1)=M(i,5); // Matriz simétrica para reatância. Q2(i-1,i-1)=M(i,6); end // Criação de complemento que será responsável pela resistência e impedância das as barras de geração. AuxQ=0.0000001*eye(M(1,3),M(1,3)); // Responsável pela criação de uma matriz complementar, irá possibilitar a concatenação posteriormente das variáveis de folga da rede. Q1=zeros(M(1,3),NR); // Concatenação de incremento para as variáveis com baixa resistencia referentes às variáveis de folga. Q1=cat(2,Q1,AuxQ); // Incremento da matriz auxiliar Q1 à matriz principal real e imaginária. Q=cat(1,Q,Q1); //Real. Q2=cat(1,Q2,Q1); //Imaginária. // Complemento à matriz Q (dobrando seu tamanho) para que seja possível, posteriormente, fazer a concatenação com a parte referente a reatancias da rede. // Parte real (resistencias) Q=cat(2,Q,zeros(size(Q,'r'),size(Q,'c'))); // Complemento à matriz Q (dobrando seu tamanho) para que seja possível, posteriormente, fazer a concatenação com a parte referente a reatancias da rede. Q2=cat(2,zeros(size(Q2,"r"),size(Q2,"c")),Q2); // Junção da matriz responsáveis pela resistencia dos ramos da rede e dos pesos para religamento da rede com a matriz responsável pela reatância dos ramos da rede. Q=cat(1,Q,Q2); // Expanção de colunas decorrente da inserção das equações de laço. Q=cat(2,Q,zeros(size(Q,"r"),size(C,"c")-size(Q,"c"))); // Expanção de linhas decorrente da inserção das equações de laço. Q=cat(1,Q,zeros(size(C,"c")-size(Q,"r"),size(Q,"c"))); // Correção para que a matriz se torne simétrica, ou seja, diferente de zero diagonal princial. for i=1:size(Q,"c") if Q(i,i)==0 Q(i,i)=0.00000000001; end end endfunction //---------------------------------------------------- // Criação matriz p. // Entrada : Valor de colunas da matriz incidência A. // Saída : Matriz peso p. //---------------------------------------------------- function [p]=MatrizP(qnt_coluna_MC) //Dimensão desta matriz deve ser igual a quantidade de colunas da matriz incidência A. a=0; for i=1:qnt_coluna_MC p(i,1)=0; end endfunction //---------------------------------------------------------------- // Função responável por inserção de restrições para abertura e // fechamento de ramos. // Entrada : Matriz incidência C e Estrutura do arquivo completo. // Saída : Matriz incidência C com restrições. //--------------------------------------------------------------- function [C]=restricao(C,M) while 1>0 do // Comunicação ao usuário. disp("Houve um Defeito Falha em algum ramo?"); algumRamoFalhou=input("Digite 1 (um) para sim ou 0 (zero) para não. "); // Verificação se houve Defeito Falha if algumRamoFalhou==0 break; elseif algumRamoFalhou==1 // Comunicação ao usuário. defeitoFalha=input("Digite o ramo com Defeito Falha: "); // Verificação de possibilidade de existir o Defeito Falha informado. if(defeitoFalha>NB) disp("Você digitou um valor inválido"); elseif(defeitoFalha~=0) // Inserção de valor 1 para iniciar uma restrição capaz de desligar o ramo informado tanto para parte real quanto imaginária. C(2*NB+M(1,3)+defeitoFalha,M(1,3)+defeitoFalha)=1; C(2*NB+NR+M(1,3)+defeitoFalha,NR+defeitoFalha+M(1,3))=1; elseif(defeitoFalha==0) continue; end // Comunicação com o usuário. on_off=input("Deseja ligar alguma linha? 1 para sim, 0 para não. ") // Confirmação do usuário para ligar algum ramo manualmente. if(on_off==1) // Demonstração de opções para religamento. disp("As opções são:"); for i=1:NR if(M(i+1,8)==1) a=M(i+1,1); b=M(i+1,2); c="-"; disp("Origem Destino - Número da linha"); disp(a, b, c, i); end end // Possibiliade de fechamento das opções já fornecidas ao usuário. while 1>0 ligar=input("Quais linhas que deseja ligar? Quando já colocou todas suas opções, digite 0. "); if(ligar==0) // Foram fechadas todas que o usuário quis. break; elseif(ligar>NR) // Usuário digitou informação inválida. disp("Você digitou um valor inválido") else // Usuário digitou informação válida. // Inserção de valor 0 para iniciar uma restrição capaz de ativar o ramo informado tanto para parte real quanto imaginária. C(2*NB+ligar,ligar)=0; C(2*NB+M(1,3)+NR+ligar,NR+ligar+M(1,3))=0; end end break; elseif(on_off==0) break; else disp("Você não digitou um valor válido."); end else disp("Você digitou uma informação inválida"); end end endfunction // ------------------------------------------------ // Estutura principal do Algoritimo para Otimização. // do fluxo de Corrente Alternada com Contingência. // ------------------------------------------------ // Instrução para criação da matriz responsável pela criação dos laços externos da rede. [LE,quantosLacos,barraLaco,barraLacoImag]=lacosExternos(M); // Instrução para criação da matriz incidência A. [C,qnt_coluna_MC_incidencia,qnt_coluna_MC]=MatrizC(M,LE,quantosLacos); // Instrução para criação da matriz incidência Q. [Q]=MatrizQ(M,qnt_coluna_MC_incidencia,quantosLacos); // Instrução para criação da matriz incidência P. [p]=MatrizP(qnt_coluna_MC); // Instrução para inserção de desligamento de barras em casa de Defeito Falha. [C]=restricao(C,M); // Instrução para criação da matriz incidência B. [b]=MatrizB(M,quantosLacos,qnt_coluna_MC_incidencia,barraLaco,barraLacoImag); // Limite inferior. ci=(-5)*ones(size(C,"c"),1); // Limite superior. cs=ci*(-1); // Função de otimização QPSOLVE - objetivo: Minimização de perdas na rede. [xopt,iact,iter,fopt]=qpsolve(Q,p,C,b,ci,cs,qnt_coluna_MC); // Término de contagem de timer para tempo de resolução da rede. toc(); // Informação ao usuário da resolução da rede. if xopt~=[] disp("Solução Ótima Encontrada!"); disp(fopt,"O valor ótimo encontrado para a função objetivo."); disp(iter,"Foram necessárias esta quantidade de iterações para convergir."); disp("O primeiro valor se refere às iterações e o segundo às restrições desativadas para resolução da rede."); disp(ans,"CPU time (s)."); else disp("Solução não encontrada.") end // Variáveis de resolução de rede. xopt=xopt(1:((2*(NR+M(1,3))+(size(LE,'r'))),1));

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// Scilab code Ex12.5: Pg:468 (2008) clc;clear; // Define function to convert degrees to degree, minute and second function [deg, minute, second] = deg2dms(theta) deg = floor(theta); minute = floor((theta-deg)*60); second = floor(((theta-deg)*60-minute)*60); endfunction n1 = 1.480; // Core refractive index of an optical fibre n2 = 1.47; // Cladding refractive index of an optical fibre lambda_0 = 850e-09; // wavelength of light, m V = 2.405; // Normalized frequency for single mode propagation of the fibre // As V = %pi*d*sqrt(n1^2-n2^2)/lambda_0, solving for d d = V*lambda_0/(%pi*sqrt(n1^2-n2^2)*1e-006); // Core radius, micro-metre NA = sqrt(n1^2-n2^2); // Numerical aperture of the fiber // Since sind(theta_0) = NA, solving for theta_0 theta_0 = asind(NA); // The maximum acceptance angle of fiber, degree [deg, m, s] = deg2dms(theta_0); // Call conversion function printf("\nThe core radius of the fiber = %4.2f micro-meter", d); printf("\nThe numerical aperture of fiber = %6.4f ", NA); printf("\nThe maximum acceptance angle = %d deg %d min %d sec", deg, m, s); // Result // The core radius of the fiber = 3.79 micro-meter // The numerical aperture of fiber = 0.1718 // The maximum acceptance angle = 9 deg 53 min 23 sec

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// Grob's Basic Electronics 11e // Chapter No. I // Example No. I_16 clc; clear; // Find the squareroot of 90*10^5. Express the answer in scientific notation. // Given data A = 90*10^5; // Variable 1 B = sqrt(A); disp (B,'The squareroot of 90*10^5 is') disp ('i.e 3.0*10^3')

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//control systems by Nagoor Kani A //Edition 3 //Year of publication 2015 //Scilab version 6.0.0 //operating systems windows 10 // Example 5.23 clc; clear; s=poly(0,'s')//defines s as poly nomial variable h=syslin('c',(48/(s*(s+2)*(s+4))))//the given transfer function assigned to variable h assume K=1 scf() evans(h) //calculation of K disp('the characterstic equation is given by : s^3+6*s^2+8*s+K') //put s=jw and equate real and imaginary parts //K=4*w^2 K=6*8 disp(K,'the value of K is ')

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clc; close(); clear(); //page no 288 //prob no. 8.7 //All frequencies in kHz k=7; W=1; Bt=k*W; printf('Minimum Bandwidth is %i kHz',Bt);

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// Scilab Code Ex4.12:: Page-4.23 (2009) clc; clear; lambda = 5893e-008; // Wavelength of light used, m t = 0.005; // Thickness of the crystal, cm // As for quarter wave plate, mu_diff*t = (mu_o - mu_e)*t = lambda/4, solving for mu_diff mu_diff = lambda/(4*t); // The difference in refractive indices of rays, cm printf("\nThe least thickness of plate for which emergent beam is plane polarised = %4.2e cm", mu_diff); // Result // The least thickness of plate for which emergent beam is plane polarised = 2.95e-003 cm

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//To Find the Moment of Inertia clc //Given: m=85 //kg h=0.1 //m //Solution: //Calculating the Frequency of Oscillation n=100/145 //Hz //Calculating the Equivalent Length of Simple Pendulum L=(1/(2*%pi)/.69*sqrt(9.81))^2 //Calculating the Radius of Gyration kG=sqrt((L-h)*h) //Calculating the Moment of Inertia of the Flywheel through the Centre of Gravity I=m*kG^2 //kg-m^2 //Results: printf("\n\n The Moment of Inertia of the Flywheel Through its c.g., I = %.1f kg-m^2.\n\n",I)

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//The value mentioned in the part 'c' of the question is 45MN^3 but that assumed in the solved problem is 50MN^3 clear all; clc; disp("Ex 1_1") disp("Part a :-") a=10//magnitude of force 1 in mN a1=10*10^-3//magnitude of force 1 in N b=5//magnitude of force 2 in GN b1=5*10^9//magnitude of force 2 in N k1=a1*b1//answer in N^2 k=k1/10^6//answer in kN^2 printf('The answer is %g kN^2',k) disp("Part b :-") c=100//magnitude of length in mm c1=100*10^-3//magnitude of length in m d=0.5//magnitude of force in MN d1=0.5*10^6//magnitude of force in N l1=c1*d1^2//answer in mN^2 l=l1/10^9//answer in GmN^2 printf('The answer is %g GmN^2',l) disp("Part c :-") e=50//magnitude of force in MN^3 e1=50*10^6//magnitude of force in N^3 f=500//magnitude of weight in Gg f1=500*10^6//magnitude of weight in kg m1=e1/f1//answer in N^3/kg m=m1*10^3//answer in kN^3/kg printf('The answer is %g kN^3/kg',m)

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// Exa 3.19 format('v',5);clc;clear;close; // Given data V1 = 100;// in V V2 = 0;// in V e1= 0;// in V e2= 100;// in V T=2;// in sec T1 = 0;// in sec T2 = 2;// in sec // Slope of ramp A= (e2-e1)/(T2-T1);// in V/sec e= 'A*t';// in sec Erms= sqrt(1/T*integrate('(A*t)^2','t',0,T));// in V Eav= 1/T*integrate('(A*t)','t',0,T);// in V Kf= Erms/Eav;// form factor Kf_sine= 1.11;// form factor of sine wave True_reading= 1;// true reading Meas_reading= Kf_sine/Kf;// measured reading PerError= (True_reading-Meas_reading)/True_reading*100;//percentage error in the reading in % disp(PerError,"The percentage error in the reading in % is : ")

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//ex7.1 V_GS_off=-4; I_DSS=12*10^-3; R_D=560; V_P=-1*V_GS_off; V_DS=V_P; I_D=I_DSS; V_R_D=I_D*R_D; //voltage across resistor V_DD=V_DS+V_R_D; disp(V_DD,'The value of V_DD required to put the device in the constant current area of operation of JFET')

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//Chapter 12 //page no 444 //given clc; clear all; L=200; //in km dL=1550; //in nm R=10; //in Gb/s Cd=17; //in ps/nm-km w=0.1; //Assused bandwidth Cd200=Cd*L; printf("\n Dispersion by 200km ofc = %0.1f*10^3 ps/nm",Cd200/10^3); TCd=w*Cd200; printf("\n total chromatic dispersion = %0.2f*10^3 ps",TCd/10^3);

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// chapter 1 , Example1 13 , pg 25 V=15000//volume(in m^3) T1=1.3//initial reverberation time(in sec) aS=(0.165*V)/T1 //total absorption of hall (in Sabine) T2=(0.165*V)/(aS+300)//revrberation time of hall after adding 300 chairs each having absorption of 1 Sabine printf("Reverberation time of hall after adding 300 chairs\n") printf("T2=%.3f sec",T2)

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exec('readpbm.sci') exec('display_gray.sci') img = readpbm('Europa_surface.pbm'); //gray = display_gray(img); max_gray=max(img); disp(max_gray); //216 colonne=512; ligne=384; //si point le plus blanc if img(j,i) > 200 //si point le plus noir if img(j,i) < 50 for i=1:ligne for j=1:colonne if img(j,i) > 253 img(j,i)=255; else img(j,i)=0; end end end

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//Chapter 10 Electmotive Force clc; clear; //Initialisation of Variables E= -0.771 //v R= 8.31 //J/mol K T= 25 //C F= 96500 //coloums M= 0.02 //m M1= 0.1 //m //CALCULATIONS E1= E-(R*(273+T)*2.3*log10(M/M1)/F) //RESULTS mprintf("Oxidation potential of copper electrode = %.2f v",E1)

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//Chapter-3,Example 3_17,Page 3-25 clc() //Given Data: n1=1.48 //R.I. of core delta=0.055 //Realtive R.I. lam=1*10^-6 //Wavelength of light a=50*10^-6 //core radius //Calculations: //Delta=(u1-u2)/u1 n2=n1-(n1*delta) //R.I. of cladding NA=n1*sqrt(2*delta) //Formula to find Numerical Aperture printf('Numerical Aperture of Fibre is =%.4f \n \n',NA) theta0=asin(NA)*180/%pi //Acceptance angle of fibre printf(' Acceptance angle of Fibre is =%.2f degrees \n \n',theta0) V=2*%pi*a*NA/lam //V number N=(V^2)/2 //Number of guided modes //In book,instead of NA , value of delta is taken into calculation. //Thus there is calculation mistake in values of V and N. printf(' V number of Fibre is =%.3f \n \n',V) printf(' Number of guided mode of Fibre is =%.3f \n',N) printf('(Calculation mistake in book)')

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function [out]=unipolar(in) if in > 0 then out = 1; else out = 0; end endfunction function [out]=bipolar(in) if in > 0 then out = 1; else out = -1; end endfunction function [out]=activate(in, expression, display_messages) [rows, cols] = size(in); if rows * cols <> 1 then out = zeros(rows, cols) for row = 1:rows for col = 1:cols out(row, col) = activate(in(row, col)) end end if display_messages then disp(out.', 'Wygenerowane potencjały wyjściowe') end else out = expression(in); end endfunction function [stop_condition]=verify_finished(last_steps, display_messages) stop_condition = %T [rows_size, cols_size] = size(last_steps) col_results = ones(1, cols_size) if rows_size == cols_size then for col_index = 1:cols_size col_value = sum(last_steps(:, col_index)) / rows_size for row_index = 1:rows_size row_value = last_steps(row_index, col_index) col_results(col_index) = col_results(col_index) & col_value == last_steps(row_index, col_index) end end stop_condition = sum(col_results) <> cols_size end if display_messages then disp(col_results, 'Poprawność potencjałów') disp(last_steps, 'W ostatnich wykonaniach') disp(stop_condition, 'Kontynuuj') end endfunction function [last_steps] = apply_execution(input_steps, new_execution) last_steps = [input_steps; new_execution] [rows_size, cols_size] = size(last_steps) if rows_size > cols_size then last_steps(1, :) = [] end endfunction function hopfield_network(input_network, input_values, expression, display_messages) last_steps = [] output_values = [] [rows, cols] = size(input_values) if display_messages then disp(input_values, 'Punkty wejściowe') disp(input_network, 'Sieć wejściowa') end for row_index = 1:rows input_point = input_values(row_index, :) output_point = input_point.'; if display_messages then disp(input_point, 'Potencjały wejściowe:') end continue_work = %T while continue_work for col_index = 1:cols if display_messages then disp(col_index, 'KROK') disp(output_point.', 'Potencjały wejściowe w kroku') end result = input_network * output_point result_activated = activate(result, expression, display_messages) output_point(col_index, 1) = result_activated(col_index, 1) step = output_point.' last_steps = apply_execution(last_steps, step) if display_messages then disp(step, 'Potencjały wyjściowe w kroku') end end continue_work = verify_finished(last_steps, display_messages) end input_point = output_point.' if display_messages then disp(input_point, 'Potencjały wyjściowe') end output_values(row_index, :) = input_point end convergent_points = [] for row_index = 1:rows if input_values(row_index, :) == output_values(row_index, :) then convergent_points = [convergent_points; output_values(row_index, :)] end end disp(input_network, 'Sieć') disp(input_values, 'Dla punktów wejściowych') disp(output_values, 'Generuje punkty wyjściowe') disp(convergent_points, 'Posiada punkty zbieżne') endfunction

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clc; clear all; rho = 7860;//Density of alpha-iron in Kg/m^3 M = 55.85e-3; // Atomic weight of alpha-iron in Kg n = 2;// Number of atoms per unit cell of BCC N = 6.022e26; // Avagadro constant a = ((n*M)/(N*rho))^(1/3);//Lattice constant r = ((a*sqrt(3))/4); disp('m',r,'The atomic radius of alpha-iron is')

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function Calcul_Exponentielle(lambda,iteration) esperance_expo = 1/lambda; var_expo = 1/lambda^2; sigma_expo = sqrt(var_expo); Xn = [] for i=1:iteration Xi = grand(i,1,'exp',esperance_expo) // Prend l'esperance de la loi expo, pas lambda. Somme(i) = sum(Xi); Xn(i) = (1/i)*Somme(i); end plot2d(Xn); endfunction

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clc;funcprot(0);//EXAMPLE 17.36 // Initialisation of Variables n=6;....................//No of cylinders D=0.125;................//Engine bore in m L=0.125;...............//Engine stroke in m N=2400;.................//Engine rpm W=490;...............//Load on the dynamometer in N CD=16100;...............//Dynamometer constant d0=0.055;...................//Air orifice diameter in m Cd=0.66;...................//Co efficient of discharge hw=310;.................//Head causing flow through prifice in mm of water br=760;................//Barometer reading in mm of Hg t=298;..................//Ambient temperature in Kelvin fc=22.1;..................//Fuel consumption per hour in kg C=45100;..................//Calorific value of fuel used in kJ/kg perc=85;...................//Percentage of carbon in the fuel perh=15;...................//Percentage of hydrogen in the fuel p1=1.013;....................//Pressure of air at the end of suction stroke in bar t1=298;......................//Temperature of air the the end of suction stroke in Kelvin k=0.5;.......................//Four stroke engine R=287;.......................//Gas constant in J/kgK //calculations BP=W*(N/CD);................//Brake power in kW pmb=(BP*6)/(L*D*D*k*10*N*n*(%pi/4));................//Brake mean effective pressure in bar disp(pmb,"Brake mean effective pressure (in bar):") bsfc=fc/BP;.......................//Brake specific fuel consumption in kg/kWh disp(bsfc,"Brake specific fuel consumption (in kg/kWh):") etathb=BP/((fc/3600)*C);......................//Brake thermal efficiency disp(etathb*100,"Brake thermal efficiency (in %):") Vst=(%pi/4)*D*D*L;..............//Stroke volume in m^3 Val=840*(%pi/4)*d0*d0*Cd*sqrt((hw/10)/((p1*10^5)/(R*t1)));............//Volume of air passing through orifice of air box per min Vac=Val/n;.........................//Actual volume of air per cylinder in m^3/min asps=Vac/(N/2);.......................//Air supplied per stroke per cylinder in m^3 etav=asps/Vst;....................//Volumetric efficiency disp(etav*100,"Volumetric efficiency (in %)") Qa=(100/23)*(((perc/100)*(8/3))+((perh/100)*(8/1)));.....................//Quantity of air required per kg of fuel combustion aqas=(Val*((p1*10^5)/(R*t1))*60)/fc;....................//Actual quantity of air supplied per kg of fuel pe=(aqas-Qa)/Qa;....................//Fraction of excess air supplied to engine disp(pe*100,"Percentage of excess air supplied :")

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// Scilab code Ex6.12: Pg:262 (2008) clc;clear; t = 0.003; // Thickness of the crystal slice, cm Lambda = 6e-005; // Wavelength of linearly polarized light, cm d_mu = Lambda/(4*t); // Difference in the refractive indices of two rays printf("\nThe difference in the refractive indices of two rays = %1.0e ", d_mu ); // Result // The difference in the refractive indices of two rays = 5e-003

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function [i]=modulo(n,m) //i=modulo(n,m) returns n modulo m. //! // Copyright INRIA if size(m,'*')==1 then m=ones(n)*m, elseif size(n,'*')==1 then n=ones(m)*n, end i=n-int(n./m).*m // n - m .* fix (n ./ m)

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Rv1=60/1000*10000 Rv2=120/1000*10000 Rx=(Rv2-Rv1)*(1/(27.5/30*2-1)-1) I=27.5/1000/600*(Rx+600)/Rx Vact=Rx*I disp(Vact)

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//ques-5.30 //Calculating hydrolysis constant and dissociation constant of acetic acid clc Kb=1.8*10^-5; Kw=10^-14; h=5.5*10^-3;//degree of hydrolysis Kh=h^2;//hydrolysis constant Ka=Kw/(Kh*Kb);//dissociation constant printf("Hydrolysis constant of acetic acid is %.2f*10^-5 and Dissociation constant is %.2f*10^-5.",Kh*100000,Ka*100000);

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<?xml version="1.0" encoding="utf-8" ?> <test> <description>Structured grid generation from NekMesh wrapper</description> <executable python="true">LoadCAD.py</executable> <parameters>3d_sphere.stp output.xml</parameters> <files> <file description="STEP file input">../../../../../utilities/NekMesh/Tests/MeshGen/STEP/3d_sphere.stp</file> </files> <metrics> <metric type="regex" id="1"> <regex>^.*Total negative Jacobians: (\d+)</regex> <matches> <match> <field id="0">0</field> </match> </matches> </metric> </metrics> </test>

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//Chapter-13, Example 13.17, Page 391 //============================================================================= clc clear //INPUT DATA b=49;//common-emitter DC current gain Ie=3*10^-3;//emitter current in A //CALCULATIONS a=b/(1+b);//common-base DC current gain Ic=a*Ie;//collector current in A mprintf("Thus common-base DC current gain and ccollector current are %1.2f and %g A respectively",a,Ic); //=================================END OF PROGRAM=======================================================================================================

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// Example no 4.6 // To find a)the length and effective aperture of receiving antenna b)the received power at mobile // Page no. 125 clc; clear; // Given data d=5*10^3; // distance of mobile from base station in m E0=1*10^-3; // E-field at 1Km from transmitter in V/m d0=1*10^3; // Distance from transmitter in m f=900*10^6; // Carrier frequency used for the system in Hz c=3*10^8; // Speed of ligth in m/s gain=2.55; // Gain of receiving antenna in dB G=10^(gain/10); // Gain of receiving antenna // a)To find the length and effective aperture of receiving antenna lambda=c/f; // Wavelength L=lambda/4; // Length of antenna Ae=(G*lambda^2)/(4*%pi); // Effective aperture of receiving antenna // Displaying the result in command window printf('\n Length of antenna = %0.4f m',L); printf(' = %0.2f cm',L*10^2); printf('\n Effective aperture of receiving antenna = %0.3f m^2',Ae); // b)To find the received power at mobile // Given data ht=50; // Heigth of transmitting antenna hr=1.5; // Heigth of receiving antenna ERd=(2*E0*d0*2*%pi*ht*hr)/(d^2*lambda); // Electic field at distance d in V/m Prd=((ERd^2/377)*Ae); // The received power at mobile in W PrddB=10*log10(Prd); // The received power at mobile in dBW PrddBm=10*log10(Prd/10^-3); // The received power at mobile in dBm Prd=((ERd^2/377)*Ae)*10^13; // The received power at mobile in 10^-13W // Displaying the result in command window printf('\n \n The received power at mobile = %0.1f X 10^-13 W',Prd); printf(' = %0.2f dBW',PrddB); printf(' = %0.2f dBm',PrddBm);

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//Example 10_10 clc(); clear; //To findout how fast the nitrogen molecule moving in air M=28 //Units in Kg/Mol Na=6.02*10^26 //Units in K mol^-1 mo=M/Na //Units in Kg k=1.38*10^-23 //units in J/K T=27+273 //Units in K v2=(3*k*T)/mo //unit in Meter^2/Sec^2 v=sqrt(v2) //Units in meter/sec printf("The nitrogen molecule goes at a speed of V=%d meter/sec",v) //In text book the answer is printed wrong as v=517 m/sec the correct answer is v=516 meter/ sec

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function [Obs,U,m]=observer(Sys,flag,alfa) //Obs=observer for (observable part of) linear system Sys //Obs is a linear system with matrices [Ao,Bo,Identity]. //where Ao is no x no, Bo is no x (nu+ny) and Co is no x no //and no=nx-m; //input to Obs is [u,y] (assuming Sys: dotx=A x + Bu, y=Cx + Du) //output of Obs is: // xhat=estimate of x modulo unobservable subsp. (case 'pp') // or // xhat=estimate of x modulo unstable unobservable subsp. (case 'st') // //case flag='st': // z=H*x can be estimated with stable observer iff H*U(:,1:m) = 0 // assignable poles of the observer are set to alfa(1),alfa(2),... // //case flag='pp': // z=H*x can be estimated with given error spectrum iff H*U(:,1:m)=0 //all poles of the observer are assigned and set to alfa(1),alfa(2),... // //If H satifies the constraint: H*U(:,1:m)=0 (ker(H) contains unobs-subsp //of Sys) one has H*U=[0,H2] and the observer for // z=H*x is is H2*Obs with H2=H*U(:,m+1:nx) i.e. Co, the C-matrix of the // observer for H*x, is Co=H2. // //EXAMPLE: // nx=5;nu=1;ny=1;un=3;us=2;Sys=ssrand(ny,nu,nx,list('dt',us,us,un)); // nx=5 states, nu=1 input, ny=1 output, // un=3 unobservable states, us=2 of them unstable. // [Obs,U,m]=observer(Sys); Stable observer (default) // W=U';H=W(m+1:nx,:);[A,B,C,D]=abcd(Sys); //H*U=[0,eye(no,no)]; // Sys2=ss2tf(syslin('c',A,B,H)) //Transfer u-->z // Idu=eye(nu,nu);ss2tf(Obs*sysdiag(Idu,Sys)*[Idu;Idu]) // Transfer u-->[u;u]-->w=[u;y=Sys*u]-->Obs*w i.e. u-->output of Obs // this transfer must equal Sys2, the u-->z transfer (H2=eye). //FD. [nx,nx]=size(Sys(2)); td=Sys(7);x0=Sys(6); [LHS,RHS]=argn(0); if RHS<>2 then [m1,m2,U,sl2]=dt_ility(Sys);end if RHS==1 then flag='st';alfa=-ones(1,nx); end if RHS==2 then //poles are not given-->set to -ones alfa=-ones(1,nx); [A,B,C,D]=abcd(Sys); // J=flag; // F=A+J*C;G=[B+J*D,-J]; // Obs=syslin(td,A+J*C,[B+J*D,-J],eye(A));U=[];m=[];return; //Ao end if RHS==3 then if prod(size(alfa))==1 then alfa=alfa*ones(1,nx);end end select flag case 'pp' m=m2; no=nx-m; alfa=alfa(1:no); [A,B,C,D]=abcd(sl2); Ao=A(m+1:nx,m+1:nx); Bo=B(m+1:nx,:); Co=C(:,m+1:nx); Do=D; J=-ppol(Ao',Co',alfa);J=J'; F=Ao+J*Co;G=[Bo+J*Do,-J]; Obs=syslin(td,F,G,eye(Ao)); return; case 'st' m=m1; no=nx-m; alfa=alfa(1:no); [A,B,C,D]=abcd(sl2); Ao=A(m+1:nx,m+1:nx); Bo=B(m+1:nx,:); Co=C(:,m+1:nx); Do=D; J=stabil(Ao',Co',alfa);J=J'; F=Ao+J*Co;G=[Bo+J*Do,-J]; Obs=syslin(td,F,G,eye(Ao)); return; end

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sci

7_08data.sci

W=2.27*10^4;//weight of the airplane(N) S=19;//wing area (m^2) V=61;//velocity at sea level(m/s) D=1.225;//density at sea level(Kg/m^3) Cl=2*W/(D*S*V^2) //lift coefficient a=0.08;//lift slope per degree (from example 7.3) a1=Cl/a //absolute angle of attack DCmcg=-0.0133;//derivative of Cmcg w.r.t absolute angle of attack(from example 7.5) Cmo=0.06;//value of moment coefficient at zero absolute angle of attack (from example 7.5) Vh=0.34 //tail volume ratio(from example 7.4) DClt=0.04;//elevator control efficiency

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/tests/zones/invalid.records.tst

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octodns/octodns

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$ORIGIN invalid.records. @ 3600 IN SOA ns1.invalid.records. root.invalid.records. ( 2018071501 ; Serial 3600 ; Refresh (1 hour) 600 ; Retry (10 minutes) 604800 ; Expire (1 week) 3600 ; NXDOMAIN ttl (1 hour) ) ; NS Records @ 3600 IN NS ns1.invalid.records. @ 3600 IN NS ns2.invalid.records. under 3600 IN NS ns1.invalid.records. under 3600 IN NS ns2.invalid.records. ; SRV Records _srv._tcp 600 IN SRV 10 20 30 foo-1.invalid.records. _srv._tcp 600 IN SRV 10 20 30 foo-2.invalid.records. _invalid 600 IN SRV 10 20 30 foo-3.invalid.records. ; TXT Records txt 600 IN TXT "Bah bah black sheep" txt 600 IN TXT "have you any wool." txt 600 IN TXT "v=DKIM1;k=rsa;s=email;h=sha256;p=A/kinda+of/long/string+with+numb3rs" ; MX Records mx 300 IN MX 10 smtp-4.invalid.records. mx 300 IN MX 20 smtp-2.invalid.records. mx 300 IN MX 30 smtp-3.invalid.records. mx 300 IN MX 40 smtp-1.invalid.records. ; A Records @ 300 IN A 1.2.3.4 @ 300 IN A 1.2.3.5 www 300 IN A 2.2.3.6 wwww.sub 300 IN A 2.2.3.6 ; AAAA Records aaaa 600 IN AAAA 2601:644:500:e210:62f8:1dff:feb8:947a ; CNAME Records cname 300 IN CNAME invalid.records. included 300 IN CNAME invalid.records.

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/3754/CH17/EX17.1/17_1.sce

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2018-02-03T05:31:52

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clear// //Variables I = 40 //Current (in milli-Ampere) t = 15 * 10**-3 //time (in seconds) CFS = 93 //Circuit fusing rate (in Ampere-square second) //Calculation SCR = I**2 * t //Surge in the device (in Ampere-square second) //Result printf("\n Since value of SCR i.e. %0.3f A**2s is less than CFS i.e. %0.3f A**2s.",SCR,CFS) printf("\n Therefore the device will not be destroyed.")

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/2024/CH1/EX1.4/1_4.sce

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sce

1_4.sce

clc //Initialization of variables m=10 //lbm a=32.1739 //ft/sec^2 g=32.1739 //calculations F=m*a/g //results printf("Force required = %d lbf",F)

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/plots/plotter2.sce

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celebro/diploma

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2021-03-12T21:42:39.337604

2013-03-28T08:43:52

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plotter2.sce

function []=process_result(filename, s1, s2, s3, s4) M = csvRead(filename, ";") filename2 = strsubst(filename,".txt","") filename2 = strsubst(filename2,"data/results_","") fontS = 3; fontS1 = 3; disp(filename); M1 = M; M1(isnan(M1)) = 60000; disp("total times:"); disp(sum(M1, 1)/1000/60/60); disp(sum(M1)/1000/60/60); T=5000 N=6000; fact=T/N for j=1:1:size(M,2) x1 = [1:N]; for i=1:1:N x1(i) = sum(M(:,j) < i*fact); end if j == 1 then x = x1; else x = [x; x1]; end end subplot(s1,s2,s3) plot([1:N]/N*60,x); //xtitle(filename, 'čas [s]', 'št. rešenih primerov'); xtitle(filename2, 'čas [s]', 'št. rešenih primerov'); legend(['ullmann', 'vf2+subsea', 'vf2'], 4); a=gca(); a.font_size = fontS; a.x_label.font_size=fontS; a.y_label.font_size=fontS; a.title.font_size=fontS1; a.margins = [0.15, 0.05, 0.125, 0.15] subplot(s1,s2,s4) plot("ln",[1:N]/N*60,x); //xtitle(filename, 'čas [s]', 'št. rešenih primerov'); xtitle(filename2, 'čas [s]', 'št. rešenih primerov'); legend(['ullmann', 'vf2+subsea', 'vf2'], 4); a=gca(); a.font_size = fontS; a.x_label.font_size=fontS; a.y_label.font_size=fontS; a.title.font_size=fontS1; a.margins = [0.15, 0.05, 0.125, 0.15] a.log_flags="ln";// (l=) log scale on y axis //xs2png(f,strsubst(filename,".txt","")); //xs2pdf(f,strsubst(filename,".txt","")); endfunction figure(1); clf(); f = gcf(); process_result("data/results_si2_r001.txt", 3, 2, 1, 2) process_result("data/results_si2_r005.txt", 3, 2, 3, 4) process_result("data/results_si2_r01.txt", 3, 2, 5, 6) f.figure_size=[1100, 1500]; f.background=-2; f.figure_size=[1100, 1500]; xs2png(f,"results_si2"); //xs2pdf(f,"results_si2"); figure(2) clf(); f = gcf(); process_result("data/results_si4_r001.txt", 3, 2, 1, 2) process_result("data/results_si4_r005.txt", 3, 2, 3, 4) process_result("data/results_si4_r01.txt", 3, 2, 5, 6) f.figure_size=[1100, 1500]; f.background=-2; xs2png(f,"results_si4"); //xs2pdf(f,"results_si4"); figure(3) clf(); f = gcf(); process_result("data/results_si6_r001.txt", 3, 2, 1, 2) process_result("data/results_si6_r005.txt", 3, 2, 3, 4) process_result("data/results_si6_r01.txt", 3, 2, 5, 6) f.figure_size=[1100, 1500]; f.background=-2; xs2png(f,"results_si6"); //xs2pdf(f,"results_si6");

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/2096/CH6/EX6.2/EX_6_2.sce

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EX_6_2.sce

//Example 6.2// ratio error and phase angle clc; clear; dv=0;//as secondary winding power factor is unity Io=1;//in ampere Knom=200;//nominal ratio Re=1.1;//external burden in ohms Pf=0.45;//power factor d= acosd(Pf);// alpha=90-d;//in degrees Is=5;//in ampere Rs=Knom*Is;// Kact= Knom+((Io/Is)*sind(dv+alpha));//actual transformation ratio Re= ((Knom-Kact)/Kact)*100;//ratio error in percentage pa=((180/%pi)*(Io*cosd(dv+alpha))/Rs);//phase angle in degree pa1=pa-round(pa); pa2=pa*3600;// pa3= round(pa2); pa4= pa3-180;// pa5=pa2-pa4;// disp(Re,"ratio error in percentage is") disp("the phase angle is "+string(round(pa5/60))+" min and "+string(pa4)+" seconds" );

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/2912/CH5/EX5.22/Ex5_22.sce

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2018-02-03T05:31:52

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Ex5_22.sce

//chapter 5 //example 5.22 //Calculate minimum error in the energy //page 111-112 clear; clc; //given dT=2.5E-14; // in sec (average life time) h=6.63E-34; // in J-s (Planck'c constant) pi=3.14; // value of pi used in the solution e=1.6*1E-19; // in C (charge of electron) //calculate // Since dE*dt>=h/(4*pi) (uncertainty relation for energy) dE=h/(4*pi*dT); // calculation of minimum uncertainty in the energy printf('\nThe uncertainty in the energy of the photon is \tdE=%1.1E J',dE); dE=dE/e; //changing unit from J to eV printf('\n\t\t\t\t\t\t =%1.1E eV',dE);

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/Valorant sniper.sce

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MBHuman/Scenarios

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2023-01-14T02:10:25.103083

2020-11-21T16:47:14

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Valorant sniper.sce

Name=Valorant sniper PlayerCharacters=Sniper Char BotCharacters=Bot Profile long.bot;Bot Profile long.bot;Bot Profile.bot;Bot Profile.bot;Bot Profile.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Sniper Char AddedBots=Bot Profile long.bot;Bot Profile long.bot;Bot Profile.bot;Bot Profile.bot;Bot Profile.bot PlayerMaxLives=0 BotMaxLives=0;0;0;0;0 PlayerTeam=1 BotTeams=2;2;2;2;0 MapName=longrange.map MapScale=4.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=0.85 BlockHealthbars=true TimeRefilledByKill=0.0 ScoreToWin=100000.0 ScorePerDamage=0.0 ScorePerKill=1.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=TF2 WeaponHeroTag=Sniper DifficultyTag=2 AuthorsTag=snow BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=For use with zoom_sensitivity_ratio 0.7934 GameVersion=2.0.1.2 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=Bot Profile long DodgeProfileNames=Long Strafes Jumping DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=PUBG Char SeeThroughWalls=false NoDodging=false NoAiming=true AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=Bot Profile DodgeProfileNames=ADAD DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=Counter-Striker SeeThroughWalls=false NoDodging=false NoAiming=true AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Sniper Char MaxHealth=100.0 WeaponProfileNames=Sniper;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1000.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.25 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=PUBG Char MaxHealth=200.0 WeaponProfileNames=PUBG;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=5.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=2.0 MovementType=Base MaxSpeed=1000.0 MaxCrouchSpeed=500.0 Acceleration=24000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.125 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=true EnemyBodyColor=X=0.774 Y=0.000 Z=0.000 EnemyHeadColor=X=0.729 Y=0.537 Z=0.839 TeamBodyColor=X=0.000 Y=0.000 Z=0.774 TeamHeadColor=X=0.729 Y=0.537 Z=0.839 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=210.0 MainBBRadius=40.0 MainBBHasHead=true MainBBHeadRadius=30.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=230.0 ProjBBRadius=60.0 ProjBBHasHead=true ProjBBHeadRadius=30.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=0.9 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Counter-Striker MaxHealth=100.0 WeaponProfileNames=AK-47;M4A1-S;m4a4;USP-S;;;; MinRespawnDelay=0.0001 MaxRespawnDelay=0.0001 StepUpHeight=75.0 CrouchHeightModifier=0.75 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=1100.0 MaxCrouchSpeed=250.0 Acceleration=6000.0 AirAcceleration=16000.0 Friction=7.5 BrakingFrictionFactor=1.25 JumpVelocity=800.0 Gravity=2.5 AirControl=1.0 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=true EnemyBodyColor=X=0.546 Y=0.776 Z=0.546 EnemyHeadColor=X=0.608 Y=0.463 Z=0.314 TeamBodyColor=X=0.000 Y=0.000 Z=0.771 TeamHeadColor=X=0.149 Y=0.542 Z=1.000 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=250.0 MainBBRadius=35.0 MainBBHasHead=true MainBBHeadRadius=25.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=250.0 ProjBBRadius=35.0 ProjBBHasHead=true ProjBBHeadRadius=25.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=256.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Long Strafes Jumping MaxTargetDistance=3000.0 MinTargetDistance=500.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=3.0 MinFBTimeChange=0.5 MaxFBTimeChange=1.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 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=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [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 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=Sniper Type=Hitscan ShotsPerClick=1 DamagePerShot=10000.0 KnockbackFactor=4.0 TimeBetweenShots=0.01 Pierces=false Category=SemiAuto 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=67000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=67000.000 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=0.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Plasma VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.3 CanAimDownSight=true ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=90 ADSFOVOverride=20.0 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Blank WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Flare ParticleProjectileTrail=Healing Sniper B ParticleHitscanTrace=None ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.1 AAMode=0 AAPreferClosestPlayer=true AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=PUBG Type=Projectile ShotsPerClick=1 DamagePerShot=45.0 KnockbackFactor=0.0 TimeBetweenShots=0.06 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=75000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=75000.000 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=30 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=45.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=true ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=0.7 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=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=0.6 PSRADSScale=1.0 ProjectileAcceleration=-2.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.0 AimPunchCooldown=0.0 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=45000.0 PSRManualNegation=true PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,3.0,-1.0,0.5 SpreadSCA=1.0,3.0,-1.0,0.3 SpreadMSA=1.0,3.0,-1.0,0.5 SpreadMCA=1.0,3.0,-1.0,0.3 SpreadSSH=1.0,3.0,-1.0,3.0 SpreadSCH=1.0,3.0,-1.0,1.0 SpreadMSH=1.0,3.0,-1.0,3.0 SpreadMCH=1.0,3.0,-1.0,1.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=-0.6 MaxRecoilHoriz=0.6 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.3 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=true 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=3 PSRViewRecoilTracking=1.0 PSRCapUp=90.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 PSR0=0.5,0.0 PSR1=0.5,0.0 PSR2=0.5,0.0 PSR3=1.0,0.0 UsePerBulletSpread=false [Weapon Profile] Name=M4A1-S Type=Hitscan ShotsPerClick=1 DamagePerShot=33.0 KnockbackFactor=0.1 TimeBetweenShots=0.1 Pierces=false Category=FullyAuto BurstShotCount=2 TimeBetweenBursts=0.1 ChargeStartDamage=0.1 ChargeStartVelocity=X=1500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=3000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=3000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=3.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=3.0 MagazineMax=20 AmmoPerShot=1 ReloadTimeFromEmpty=1.37 ReloadTimeFromPartial=1.37 DamageFalloffStartDistance=3000.0 DamageFalloffStopDistance=7000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=true BounceFactor=0.6 BounceCount=0 HomingProjectileAcceleration=6000.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.1 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=410.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=10.3 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=true DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=true DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=5.0 BlockedByWorld=true SpreadSSA=4.0,15.0,-9.0,2.5 SpreadSCA=4.0,15.0,-9.0,2.5 SpreadMSA=4.0,15.0,-9.0,2.5 SpreadMCA=4.0,15.0,-9.0,2.5 SpreadSSH=1.5,27.0,-9.0,1.0 SpreadSCH=1.5,27.0,-9.0,0.0 SpreadMSH=100.0,1000.0,5.0,20.0 SpreadMCH=4.0,15.0,-9.0,1.8 MaxRecoilUp=0.3 MinRecoilUp=0.3 MinRecoilHoriz=-0.3 MaxRecoilHoriz=0.3 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.0001 TimeToRecoilReset=0.075 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=2.0 AADeadZone=0.0 AAFOV=15.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=true PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=90.0 PSRCapRight=90.0 PSRCapLeft=90.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=35.0 PSR0=0.4,-0.1 PSR1=0.4,0.0 PSR2=0.9,0.4 PSR3=1.0,-0.5 PSR4=1.0,0.6 PSR5=1.2,0.3 PSR6=0.7,-0.6 PSR7=0.8,-0.5 PSR8=0.3,-1.3 PSR9=0.8,0.5 PSR10=0.3,1.0 PSR11=-0.4,1.2 PSR12=0.0,1.1 PSR13=0.1,1.0 PSR14=-0.2,-0.4 PSR15=0.4,0.1 PSR16=-0.4,1.0 PSR17=0.4,-1.0 PSR18=0.0,1.0 PSR19=-0.1,-1.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=m4a4 Type=Hitscan ShotsPerClick=1 DamagePerShot=33.0 KnockbackFactor=0.2 TimeBetweenShots=0.09 Pierces=false Category=FullyAuto BurstShotCount=2 TimeBetweenBursts=0.1 ChargeStartDamage=0.1 ChargeStartVelocity=X=1500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=3000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=3000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=3.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=30 AmmoPerShot=1 ReloadTimeFromEmpty=2.7 ReloadTimeFromPartial=2.7 DamageFalloffStartDistance=3000.0 DamageFalloffStopDistance=7500.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.02 BounceOffWorld=true BounceFactor=0.6 BounceCount=0 HomingProjectileAcceleration=6000.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.1 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-40.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.2 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=410.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=10.3 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=true DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=true DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=5.0 BlockedByWorld=true SpreadSSA=4.0,15.0,-9.0,2.5 SpreadSCA=4.0,15.0,-9.0,2.5 SpreadMSA=4.0,15.0,-9.0,2.5 SpreadMCA=4.0,15.0,-9.0,2.5 SpreadSSH=4.0,27.0,-9.0,1.0 SpreadSCH=4.0,27.0,-9.0,0.0 SpreadMSH=100.0,1000.0,5.0,20.0 SpreadMCH=4.0,15.0,-9.0,1.8 MaxRecoilUp=0.3 MinRecoilUp=0.3 MinRecoilHoriz=-0.3 MaxRecoilHoriz=0.3 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.0001 TimeToRecoilReset=0.075 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.1 AAMaxSpeed=5.0 AADeadZone=0.0 AAFOV=50.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=true PSRLoopStartIndex=10 PSRViewRecoilTracking=0.45 PSRCapUp=90.0 PSRCapRight=90.0 PSRCapLeft=90.0 PSRTimeToPeak=0.16 PSRResetDegreesPerSec=35.0 PSR0=0.4,-0.25 PSR1=0.4,-0.1 PSR2=0.9,0.5 PSR3=1.2,-0.5 PSR4=1.1,0.4 PSR5=1.3,0.4 PSR6=0.9,-1.0 PSR7=0.7,-0.75 PSR8=0.5,-1.1 PSR9=0.6,-0.3 PSR10=0.7,0.5 PSR11=-0.4,1.5 PSR12=0.1,1.7 PSR13=-0.3,1.3 PSR14=0.2,1.0 PSR15=0.2,-0.9 PSR16=-0.1,0.0 PSR17=0.3,0.5 PSR18=0.2,0.5 PSR19=-0.2,0.5 PSR20=-0.2,-0.75 PSR21=0.5,-2.0 PSR22=-0.2,-0.7 PSR23=0.2,-0.6 PSR24=-0.1,-0.75 PSR25=-0.1,-0.5 PSR26=0.3,0.3 PSR27=0.3,-0.4 PSR28=0.1,-0.2 PSR29=0.15,-0.2 PSR30=0.15,-0.2 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=USP-S Type=Hitscan ShotsPerClick=1 DamagePerShot=35.0 KnockbackFactor=1.0 TimeBetweenShots=0.17 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=12 AmmoPerShot=1 ReloadTimeFromEmpty=2.2 ReloadTimeFromPartial=2.2 DamageFalloffStartDistance=300.0 DamageFalloffStopDistance=1000.0 DamageAtMaxRange=33.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=1.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=400.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=5.0,25.0,0.2,7.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=1.0,25.0,2.0,7.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.3 MinRecoilUp=0.0 MinRecoilHoriz=-0.2 MaxRecoilHoriz=0.2 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.0001 TimeToRecoilReset=0.075 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.1 AAMaxSpeed=5.0 AADeadZone=0.0 AAFOV=50.0 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=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -576.000000 0.000000 256.000000 448.000000 0.000000 256.000000 448.000000 0.000000 -768.000000 -576.000000 0.000000 -768.000000 -576.000000 -16.000000 256.000000 448.000000 -16.000000 256.000000 448.000000 -16.000000 -768.000000 -576.000000 -16.000000 -768.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 5 4 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 2 1 5 6 0x00000000 0.000000 0.000000 1.000000 1.000000 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1d69f34610aafa41f17640ae87f3b340dca8e77c

449d555969bfd7befe906877abab098c6e63a0e8

/3821/CH14/EX14.5/Example14_5.sce

16faa5a575a218e440a74c18398df21d1131604b

[]

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FOSSEE/Scilab-TBC-Uploads

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Example14_5.sce

////Chapter No 14 Air Standard Cycles ////Example No 14.5 Page No 308 ///Find compression ratio ///Input data clc; clear; P1=1; //Isentropic Compression in bar P2=20; //Isentropic Compression in bar //Consider air as the working fluid therefore gamma1=1.4; //Calculation r=(P2/P1)**(1/gamma1); //Isentropic process eta=100*(1-(1/(r^(gamma1-1)))); //Otto cycle air standard effeciency in % //Output printf('compression ratio= %f \n ',r); printf('standard efficiency= %f percent \n',eta);

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// Chapter 11 example 17 //------------------------------------------------------------------------------ clc; clear; // Given data r = 42164; // orbital radius in kms Dlamda_max = 500; // max displacement due to latitude deviation // Calculations i = Dlamda_max/r; // angle of inclination in radians i_deg = i*180/%pi // rad to deg conv // Output mprintf('Angle of inclination = %3.2f°',i_deg); //------------------------------------------------------------------------------

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19_07.sce

//Problem 19.07: Three coils each having resistance 3 ohm and inductive reactance 4 ohm are connected (i) in star and (ii) in delta to a 415 V, 3-phase supply. Calculate for each connection (a) the line and phase voltages and (b) the phase and line currents. //initializing the variables: R = 3; // in ohms XL = 4; // in ohms VL = 415; // in Volts //calculation: //For a star connection: //IL = Ip //VL = Vp*(3^0.5) VLs = VL Vps = VLs/(3^0.5) //Impedance per phase, Zp = (R*R + XL*XL)^0.5 Ips = Vps/Zp ILs = Ips //For a delta connection: //VL = Vp //IL = Ip*(3^0.5) VLd = VL Vpd = VLd Ipd = Vpd/Zp ILd = Ipd*(3^0.5) printf("\n\n Result \n\n") printf("\n (a)the line voltage for star connection is %.0f V and the phase voltage for star connection is %.0f V and the line voltage for delta connection is %.0f V and the phase voltage for delta connection is %.0f V",VLs,Vps,VLd,Vpd) printf("\n (b)the line current for star connection is %.0f A and the phase current for star connection is %.0f A and the line current for delta connection is %.0f A and the phase current for delta connection is %.0f A",ILs,Ips,ILd,Ipd)

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Ex3_11_1.sce

//Chapter-3,Example 3_11_1,Page 3-25 clc() //Given Data: u1=1.52 //R.I. of Core u2=1.5189 //R.I.of Cladding lam=1.3*10^-6 //wavelength in meter d=29*10^-6 //core diameter in meter a=d/2 //Calculations: NA=sqrt(u1^2-u2^2) //Formula to find Numerical Aperture V=2*%pi*a*NA/lam //Normalised frequency Nm=(V^2)/2 //Number of modes printf('Normalised frequency of Fibre is (V)=%.3f \n \n',V) printf(' The Maximum Number of modes the Fibre will support is (Nm) =%.0f \n',Nm)

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bubble-sort.tst

.( Loading Bubble Sort benchmark...) cr \ A classical benchmark of an O(n**2) algorithm; Bubble sort \ \ Part of the programs gathered by John Hennessy for the MIPS \ RISC project at Stanford. Translated to forth by Marty Fraeman \ Johns Hopkins University/Applied Physics Laboratory. \ MM forth2c doesn't have it ! : mybounds over + swap ; variable seed ( -- addr) : initiate-seed ( -- ) 74755 seed ! ; : random ( -- n ) seed @ 1309 * 13849 + 65535 and dup seed ! ; 6000 constant elements ( -- int) align create list elements cells allot : initiate-list ( -- ) list elements cells + list do random i ! cell +loop ; : dump-list ( -- ) list elements cells + list do i @ . cell +loop cr ; : verify-list ( -- ) list elements 1- cells mybounds do i 2@ > abort" bubble-sort: not sorted" cell +loop ; : bubble ( -- ) ." bubbling..." cr 1 elements 1 do list elements i - cells mybounds do i 2@ > if i 2@ swap i 2! then cell +loop loop ; : bubble-sort ( -- ) initiate-seed initiate-list bubble verify-list ; : bubble-with-flag ( -- ) 1 elements 1 do -1 list elements i - cells mybounds do i 2@ > if i 2@ swap i 2! drop 0 then cell +loop if leave then loop ; : bubble-sort-with-flag ( -- ) initiate-seed initiate-list bubble-with-flag verify-list ; : main ( -- ) bubble-sort \ bubble-sort-with-flag ;

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Exa2_27.sce

//Exa 2.27 clc; clear; close; //Given data : format('v',6); V=500;//in volt Pout_rotor=20;//Power output of rotor in H.P. phase=3;//no. of phase P=6;//no. of poles f=50;//in Hz N=995;//in rpm(Actual speed of motor) cosfi=0.87;//powerfactor(unitless) Ns=120*f/P;//synchronous speed in rpm S=(Ns-N)/Ns;//unitless disp(S,"Slip : "); RotorCuLoss=(S/(1-S))*Pout_rotor*735.5;//in watts disp(RotorCuLoss,"Rotor Cu Loss(in watts) : "); Pin_rotor=RotorCuLoss/S;//in watts disp(Pin_rotor/10^3,"Power input to rotor(in KW) :"); LineCurrent=Pin_rotor/(sqrt(3)*V*cosfi);//in Ampere disp(LineCurrent,"Line Current(in A) :"); RotorFreq=S*f;//in Hz disp(RotorFreq,"Rotor Frequency(in Hz) :");

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Example1.sce

clear flag=1 mode(-1) clc printf("Example 1 : Show the method of using arrays in advanced shellscripting \n") disp("****************************************************************") disp("Answer : ") disp("INSTRUCTIONS : ") printf("\n1. Here all instructions are preloaded in the form of a demo\n\nInitially the whole perl script is displaying and then \n the result of the same can be seen in the command line interpreter.\n\n2. PLEASE MAKE SURE THAT THE PERLSCRIPT INTERPRETER\nEXISTS IN THE SYSTEM\nOR THE COMMAND WOULD NOT WORK \n\n3. PRESS ENTER AFTER EACH COMMAND to see its RESULT\n\n5. PRESS ENTER AFTER EACH RESULT TO GO TO THE NEXT COMMAND\n") halt('.............Press [ENTER] to continue.....') halt("") clc printf("\tUNIX SHELL SIMULATOR(DEMO VERSION WITH PRELOADED COMMANDS)\n\n\n") halt('') clc i=0 i=i+1;f(i)='#!/usr/bin/ksh' i=i+1;f(i)='# Script: dateval.sh - validates a date field using an array' i=i+1;f(i)='IFS='+ascii(34)+'/'+ascii(34)+'' i=i+1;f(i)='n='+ascii(34)+'[0-9][0-9]'+ascii(34)+'' i=i+1;f(i)='set -A month arr 0 31 29 31 30 31 30 31 30 31 30 31' i=i+1;f(i)='while echo '+ascii(34)+'Enter a date: \c'+ascii(34)+' ; do' i=i+1;f(i)=' read value' i=i+1;f(i)=' case '+ascii(34)+'$value'+ascii(34)+' in' i=i+1;f(i)=' '+ascii(34)+''+ascii(34)+') echo '+ascii(34)+'No date entered'+ascii(34)+' ; continue ;;' i=i+1;f(i)=' $n/$n/$n) set $value' i=i+1;f(i)=' let rem='+ascii(34)+'$3 % $4'+ascii(34)+'' i=i+1;f(i)=' if [ $2 -gt 12 -o $2 -eq 0 ] ; then' i=i+1;f(i)=' echo '+ascii(34)+'Illegal month'+ascii(34)+' ; continue' i=i+1;f(i)=' else' i=i+1;f(i)=' case '+ascii(34)+'$value'+ascii(34)+' in' i=i+1;f(i)=' 29/02/??) [ $rem -gt 0 ] &&' i=i+1;f(i)=' { echo '+ascii(34)+'20$3 is not a leap year'+ascii(34)+' ; continue ; } ;;' i=i+1;f(i)=' *) [ $1 -gt ${month_arr[$2]} -o $1 -eq 0 ] &&' i=i+1;f(i)=' { echo '+ascii(34)+'Illegal day'+ascii(34)+' ; continue ; } ;;' i=i+1;f(i)=' esac' i=i+1;f(i)=' fi;;' i=i+1;f(i)=' *) echo '+ascii(34)+'Invalid date'+ascii(34)+' ; continue ;;' i=i+1;f(i)=' esac' i=i+1;f(i)=' echo '+ascii(34)+'$1/$2/$3'+ascii(34)+' is a valid date' i=i+1;f(i)='done' n=i printf("\n# Enter the name of the shellscript file whichever you desire \n\n") nam=input('$ cat ','s') halt(' ') for i=1:n printf("%s\n",f(i)) end halt(' ') clc i=0 i=i+1;f(i)='@echo off' i=i+1;f(i)='set chc=y' i=i+1;f(i)=':loop' i=i+1;f(i)='if /I '+ascii(34)+'%chc%'+ascii(34)+'=='+ascii(34)+'n'+ascii(34)+' goto endloop' i=i+1;f(i)='set /P dat=Enter a date: ' i=i+1;f(i)='if '+ascii(34)+'%dat%'+ascii(34)+' equ '+ascii(34)+''+ascii(34)+' echo No date entered&&goto chci' i=i+1;f(i)='if exist testt del testt' i=i+1;f(i)='echo %dat%>testt' i=i+1;f(i)='for /F '+ascii(34)+'tokens=1,2,3 delims=/'+ascii(34)+' %%i in (testt) do set dd=%%i&&set mm=%%j&&set yy=%%k' i=i+1;f(i)='if %mm% gtr 12 echo Illegal month&&goto chci' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'01'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'03'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'04'+ascii(34)+' set ulim=30&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'05'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'06'+ascii(34)+' set ulim=30&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'07'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'08'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'09'+ascii(34)+' set ulim=30&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'10'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'11'+ascii(34)+' set ulim=30&&goto printing' i=i+1;f(i)='if '+ascii(34)+'%mm%'+ascii(34)+'=='+ascii(34)+'12'+ascii(34)+' set ulim=31&&goto printing' i=i+1;f(i)='set /a rem=yy%%4' i=i+1;f(i)='if %rem% neq 0 set ulim=28&&goto nlpyear' i=i+1;f(i)='set ulim=29' i=i+1;f(i)='goto printing' i=i+1;f(i)=':nlpyear' i=i+1;f(i)='if '+ascii(34)+'%dd%'+ascii(34)+'=='+ascii(34)+'29'+ascii(34)+' echo 20%yy% is not a leap year&&goto chci' i=i+1;f(i)=':printing' i=i+1;f(i)='if %dd% leq %ulim% echo %dat% is a valid date&&goto chci' i=i+1;f(i)='echo Illegal day ' i=i+1;f(i)=':chci' i=i+1;f(i)='set /p chc=Do you want to continue ? (y/n) : ' i=i+1;f(i)='goto loop' i=i+1;f(i)=':endloop' i=i+1;f(i)='pause>NUL&&del testt' n=i if getos()=='Linux' then printf("\n\nPlease Switch to windows and then execute using the instructions\n\nThank You \n\n") halt(' ') exit end v=mopen(nam+'.sh.bat','wt') for i=1:n mfprintf(v,"%s\n",f(i)) end mclose(v) printf("\n# type the following command in the command line interpreter as soon as it appears") printf(" \n %c %s.sh %c [COMMANDLINE ARGUMENTS][ENTER]\n\n",ascii(34),nam,ascii(34)) printf("\n$ %s.sh [COMMANDLINE ARGUMENTS] #to execute the perlscript",nam) halt(' ') dos('start') printf("\n\n\n") halt(' ---------------->Executing ShellScript in Command Line Prompt<-------------- ') printf("\n\n\n$ exit #To exit the current simulation terminal and return to Scilab console\n\n") halt("........# (hit [ENTER] for result)") //clc() printf("\n\n\t\t\tBACK TO SCILAB CONSOLE...\nLoading initial environment') sleep(1000) mdelete(nam+'.sh.bat') mdelete('emp.lst')

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14_3.sce

k=0.025852; //say k=K*T/q Na=3*10^14; Nv=3.08*10^19; a=4.05; //say a=χsi c=k*log(Nv/Na); //say c=Ef-Ev printf('\n The value of Ef-Ev is %fV',c); b=1.125; //say b=Eg d=a+b-c; //say d=φs printf('\n The value of φs is %fV\n',d); e=11.7*8.854*10^-14; //say e=Єs Vt=0.025852; q=1.6*10^-19; Na=3*10^14; Ld=sqrt(e*Vt/(q*Na)); printf('\n The value of Ld is %f*10^-5cm\n',Ld*10^5); eox=3.9*8.854*10^-14; //say eox=Єox dox=350*10^-7; cox=eox/dox; printf('\n The oxide capacitance per unit area is %f*10^-9F/cm^2',cox*10^9); esi=11.7*8.854*10^-14; Cdiffb=1/((dox/eox)+(Ld/esi)); printf('\n The capacitance per unit area at the flat band condition is %f*10^-9F/cm^2\n',Cdiffb*10^9); Vfb1=a-d; printf('\n The value of Vfb1 is %fV\n',Vfb1); ni=1*10^10; f=k*log(ni/Na); //say f=φb printf('\n The value of φb is %1.3f\n',f); Xdmax=sqrt(2*e*2*(-f)/(q*Na)); printf('\n The value of Xdmax is %f*10^-4cm\n',Xdmax*10^4); Qdmax=-q*Na*Xdmax; printf('\n The value of Qdmax is %f*10^-9C/cm^2\n',Qdmax*10^9); Emax=-Qdmax/e; printf('\n The value of Emax is %fV/cm\n',Emax); VT=Vfb1-(2*f)-(Qdmax/cox); printf('\n The value of Threshold voltage is %fV\n',VT);

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2016-04-13T09:24:27

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buildmacros.sce

// ==================================================================== // Allan CORNET // Simon LIPP // INRIA 2008 // This file is released into the public domain // ==================================================================== tbx_build_macros(TOOLBOX_NAME, get_absolute_file_path('buildmacros.sce')); clear tbx_build_macros;

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Ex11_19.sce

// Variable declaration n = 5 k = 1 // Calculation X = [1 0 ; 1 1 ; 1 2 ; 1 3 ; 1 4] Y = [8 ; 9 ; 4 ; 3 ; 1] XT = X' XTX = XT*X XTXI = [0.6 -0.2; -0.2 0.1] XTY = XT*Y b = XTXI*XTY Y1 = X*b MMT = ((Y-Y1)')*(Y-Y1) MMT = int(MMT) Se_square = (1.0/(n-k-1))*MMT Final = Se_square*XTXI // Result printf ( "var(bo): %.2f",Final(1,1)) printf ( "var(b1): %.2f",Final(2,2) )

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function y = trapecio(func1, a, b) y = ((b - a) / 2) * (func1(a) + func1(b)); //error = f''(c) * (h^3 / 12) c tal que la f'' sea máxima endfunction function y = trapeciocompuesto(func1, a, b, n) h = (b - a) / n y = 0 for x = a: h: (b - h) y = y + trapecio(func1, x, x + h); end //error = f''(c) * (h^3 / (12 * n^2)) c tal que la f'' sea máxima endfunction function y = err_trap(a, b, n, maxder2) //google: 4chan trap thread y = -maxder2 * (((b - a)^3) / (12 * n^2)) endfunction function y = simpson(func, a, b) y = ((b - a) / 6) * (func(a) + 4 * func((a + b) / 2) + func(b)); //error = (h^5 / 90) * f''''(c) c tal que la f'''' sea máxima endfunction function y = simpsoncompuesto(func, a, b, n) h = (b - a) / n y = 0 for x = a: h: (b - h) y = y + simpson(func, x, x + h); end //error = (b - a) * (h^4 / 180) * f''''(c) c tal que la f'''' sea máxima endfunction function y = err_simp(a, b, n, maxder4) h = (b - a) / n; y = (b - a) * ((h^4) / 180) * maxder4; endfunction function y = trap_aux(func, x, a, b) [p1, p2, p3] = string(func) y = ((b - a) / 2) * (func(x, a) + func(x, b)); //error = f''(c) * (h^3 / 12) c tal que la f'' sea máxima endfunction function y = trap_comp_aux(func, x, a, b, n) h = (b - a) / n y = 0 for i = a: h: (b - h) y = y + trap_aux(func, x, i, i + h); end //error = f''(c) * (h^3 / (12 * n^2)) c tal que la f'' sea máxima endfunction function y = simp_aux(func2, x, a, b) y = ((b - a) / 6) * (func2(x, a) + 4 * func2(x, (a + b) / 2) + func2(x, b)); //error = (h^5 / 90) * f''''(c) c tal que la f'''' sea máxima endfunction function y = simp_comp_aux(func2, x, a, b, n) h = (b - a) / n y = 0 for i = a: h: (b - h) y = y + simp_aux(func2, x, i, i + h); end //error = (b - a) * (h^4 / 180) * f''''(c) c tal que la f'''' sea máxima endfunction function y = trapecio_ext(func, a, b, fC, fD, n) //deff("r = G(x)", "r = trap_comp_aux(func, x, fC(x), fD(x), n)"); function r = G(x) r = trap_comp_aux(func, x, fC(x), fD(x), n) endfunction y = trapeciocompuesto(G, a, b, n); endfunction function y = simpson_ext(func1, a, b, fC, fD, n) //deff("r = G(x)", "r = trap_comp_aux(func, x, fC(x), fD(x), n)"); function r = G(x) r = simp_comp_aux(func1, x, fC(x), fD(x), n) endfunction y = simpsoncompuesto(G, a, b, n); endfunction

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syms G1 G2 G3 G4 H1 H2 a= G1*G2 //shifting the take off point b= a/(1+(a*H2)) c=(1+(G3/G2)) Y= b*c*(G4/(1+G4*H1)) disp(Y,"C/R = ")

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//Given that C = 1.5*10^-6 //in F V = 57 //in volts L = 12*10^-3 //in H //Sample Problem 33-1 printf("**Sample Problem 33-1**\n") Imax = V*sqrt(C/L) printf("The maximum current in the circuit is %1.2eA", Imax)

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// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Vinay Bhat, Rohan Gurve // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in // function[dstImg] = regionFill(srcImg,inpaintRadius,varargin) // This function restores the selected region in an image using the region neighborhood. // This function restores the selected region in an image using the region neighborhood. // // // Calling Sequence // src = imread(location-for-image) // x = [x1 x2 ...........xn ] //x coordinates of polygon covering the region that you want to fill // y = [y1 y2 ...........yn ] //corresponding y coordinates of polygon covering the region that you want to fill // dstImg 1= regionFill(srcImg,inpaintRadius,x,y) // // mask = roiFreeHand(srx) //making a mask - you can also use other function to make the mask // dstImg2 = regionFill(srcImg,inpaintRadius,mask) // // Parameters // // srcImg: input source imge //it is converted to 8 bit internally // inpaintRadius: Radius of a circular neighborhood of each point inpainted that is considered by the algorithm(Double) // mask: Inpainting mask. Non-zero pixels indicate the area that needs to be inpainted. // x: 1xn matrix denoting x coordinates of polygon covering the region that you want to fill // y: 1xn matrix denoting y coordinates of polygon covering the region that you want to fill // // Examples // src= imread("../images/color2.jpeg"); // p=regionFill(src,1,[100 110 110 100],[150 150 200 200]); // imshow(p); // // Examples // src= imread("../images/color2.jpeg"); //reading an image // mask=roiFreeHand(src); //making a mask // p=regionFill(src,5,mask); // imshow(p); // //Authors //Vinay Bhat //Rohan Gurve [lhs, rhs] = argn(0) if rhs < 3 error(msprintf("input arguments missing")); elseif rhs > 4 error(msprintf(" Too many input arguments")); end srcMat = mattolist(srcImg) if rhs == 3 then maskMat = mattolist(varargin(1)) out = raw_regionFill(srcMat,inpaintRadius, maskMat) elseif rhs == 4 then x= varargin(1) y= varargin(2) out = raw_regionFill(srcMat,inpaintRadius, x, y) end channels = size(out) for i = 1:channels dstImg(:,:,i) = out(i) end endfunction

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//Chapter-5,Example5_3_4,pg 5-7 E=0.025 //energy of neutron h=6.63*10^-34 //Plancks constant m=1.676*10^-27 //mass of a neutron e=1.6*10^-19 //charge on electron wavelength=h/sqrt(2*m*E*e) //The Wavelength of a beam of neutron printf("\nThe Wavelength of a beam of neutron is\n") disp(wavelength) printf("meter\n")

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//all the calculations are done in R scale T2=285+460 //R T1=32+460 //R P2=1.30 //atm P1=1 //atm V1dot=3.95*10^5 //ft^3/h

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r0=2*10^3 r1=1*10^3 nl=4//no. of large cells ns=(r0/r1)^2*nl-1//split cells within area=split cells within square-1 ncpl=120 n2=nl*ncpl//no. of channels without cell splitting ncps=120 n1=ns*ncps//no. of channels with cell splitting inc=n1/n2//increase in the number of cells disp(inc,'increase in the number of cells in times')

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testxlabel.sce

// generate a list of random values X=grand(100,1,'bin',10,0.6); m=tabul(X); // table of frequencies x=m(:,1); // values n=m(:,2); // bin counts clf();bar(x,n) // histogram A=gca(); A.x_label.text="grade over 10"; A.x_label.font_size=3; A.x_label.font_style=4; A.y_label.text="counts"; A.y_label.font_size=3; A.y_label.font_style=4;

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function [x]=stp(orbit,NbrIti,Dim,Delai, ResTemps, EtapTemp, EtapFarc) // Initialisation Commandline=''; NbrComp=size(orbit,2); if ~isdef('DoEstim','local')... then DoEstim=%F, end; if isdef('NbrIti','local')... then Commandline=Commandline+' -l'+string(NbrIti), end; if isdef('EtapTemp','local')... then Commandline=Commandline+' -t'+string(EtapTemp), end; if isdef('Dim','local')... then Commandline=Commandline+' -m'+string(Dim), end; if isdef('MinEps','local')... then Commandline=Commandline+' -r'+string(MinEps), end; if isdef('ResTemps','local')... then Commandline=Commandline+' -#'+string(ResTemps), end; if isdef('EtapFarc','local')... then Commandline=Commandline+' -%'+string(EtapFarc), end; if isdef('Delai','local')... then Commandline=Commandline+' -d'+string(Delai), end; // Utilisation de Lyap_K from TiSeAn if isdef('orbit','local')... then mdelete('tmp') write('tmp',string(orbit)), Commandline=' tmp'+Commandline+' -c'+string(NbrComp)+' -otmpout.dat', end; mdelete('tmpout.dat') Commandline='stp'+Commandline, // Reading the output x=host(Commandline); if x~=0... then disp('Erreur!!! Fichier ou Tisean manquant'); return; end; x=read('tmpout.dat',-1,1,'(a)'); x=evstr(x); endfunction

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3_3.sce

//example 3.3 clc; funcprot(0); // Initialization of Variable patm=14.7;//in lbf/in^2 mpiston=100; g=32.2; A=1;//area mair=0.6; delu=18; k=1.6;//V2-V1; P=mpiston*g/A/32.2/144+14.7; W=P*k*144/778; Q=W+mair*delu; disp(Q,"Heat transferred in Btu") W2=patm*k*144/778; disp(W2,"Work done in Btu"); delz=k/A; PE=mpiston*g*delz/32.2/778; Q2=W2+PE+mair*delu; disp(Q2,"Heat transferred in Btu") clear()

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clc;funcprot(0);//EXAMPLE 17.3 // Initialisation of Variables rho1=19.3;...........//Density of pure Tungsten in g/cm^3 rho2=10.49;............//Density of pure Silver in g/cm^3 f1=0.75;..............//Volume fraction of Tungsten f2=0.25;...........//Volume fraction of Silver and pores //Calculations per=((f2*rho2)/((f2*rho2)+(f1*rho1)))*100;.........//Percentage weight of silver disp(per,"Percentage Weight of Silver:")

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// ELECTRICAL MACHINES // R.K.Srivastava // First Impression 2011 // CENGAGE LEARNING INDIA PVT. LTD // CHAPTER : 6 : SYNCHRONOUS MACHINES // EXAMPLE : 6.9 clear ; clc ; close ; // Clear the work space and console // GIVEN DATA printf("\n EXAMPLE : 6.9 : \n\n Given Data \n"); printf("\n Voc(kV) 10 10.80 11.50 12.10 12.60 13 14 14.50 14.80 \n"); printf("\n If(A) 175 200 225 250 275 300 400 450 500 \n\n"); p = 6; // Total number of Poles of Alternator V = 11*10^3; // Operating voltage of the Alternator in Volts N = 1500; // speed of the Alternator in RPM Ia_scc = 2099; // SCC test Armature current in Amphere at If = 200 A If_scc = 200; // SCC test field Rated current in Amphere Ia_pt = 2099; // Pottier test Armature current in Amphere at If = 450 A If_pt = 450; // Pottier test field Rated current in Amphere VA = 40*10^6; // VA rating of the Alternator in Volts-Amphere f = 50; // Operating Frequency of the Alternator in Hertz pf = 0.8; // Power factor (lagging) // CALCULATIONS // Some of the data obtained from OCC and SCC test Graph or Pottier triangle in Figure6.24 & Page no:-407 v = V/sqrt(3); // Rated phase Voltage in Volts I = VA/(sqrt(3)*V); // Full-load phase current in Amphere Xl = 0.4481; // Leakage reactance in Ohms From OCC and SCC test Graph or Pottier triangle in Figure6.24 & Page no:-407 // For Case(a) General Method pfa_a = acosd(pf); // Power factor angle in degree Er_a = (V/sqrt(3))+(Ia_scc*(cosd(pfa_a)-%i*sind(pfa_a))*Xl); // Induced Voltage in Volts R_a = 208.4; A_a = 200; //From OCC the field current required for Er_a (Should be in Line-line Voltage) Er_a = 11043.66 V will get R_a & A_a value Respectively from SCC (Figure6.24 & Page no:-407) angle_a = 131.93; // Angle between R_a & A_a (Figure6.25(a) & Page no:-408) = 90'+5.06'+36.87' = 131.93' F_a = sqrt((R_a^2)+(A_a^2)-(2*R_a*A_a*cosd(angle_a))); // From phasor diagram in figure 6.25(a) & Page no:-408 the neccessary field excitation in Amphere Eo_a = 13720; // Corresponding to field current, F_a = 373 A the open circuit EMF from OCC is 560 V (Figure6.15 & Page no:-386) r_a = 100*((Eo_a-V)/V); // Percentage regulation // For Case (b) ASA Method pfa_b = acosd(pf); // Power factor angle in degree Er_b = (V/sqrt(3))+Ia_scc*(cosd(pfa_b)-%i*sind(pfa_b))*Xl; // Induced Voltage in Volts R_b = 160; A_b = 200; //From OCC the field current required for Er_b (Should be in Line-line Voltage) Er_b = 11043.66 V will get R_b & A_b value Respectively from SCC (Figure6.24 & Page no:-407) angle_b = 126.87; // Angle between R_b2 & A_b2 (Figure6.22b & Page no:-403) = 90'+36.87' = 126.87' F_b = sqrt((R_b^2)+(A_b^2)-(2*R_b*A_b*cosd(angle_b))); // From phasor diagram in figure 6.25(b) & Page no:-408 the neccessary field excitation in Amphere Eo_b = 13660; // Corresponding to field current ( OF'=OF+FF') F_b = 337.88+15.38=337.88 A the open circuit EMF from OCC is 13660 V (Figure6.15 & Page no:-386) r_b = 100*((Eo_b-V)/V); // Percentage regulation // DISPLAY RESULTS disp(" SOLUTION :-"); printf("\n For Case (a) General(ZPF) Method \n Induced EMF, EMF = %.f < %.2f V \n",abs(Er_a),atand(imag(Er_a),real(Er_a))) printf("\n Percenatge Regulation, R = %.2f Percenatge \n",r_a) printf("\n For Case (b) ASA Method \n Induced EMF, EMF = %.f < %.2f V \n",abs(Er_b),atand(imag(Er_b),real(Er_b))) printf("\n Percenatge Regulation, R = %.2f Percenatge \n",r_b) printf("\n\n [ TEXT BOOK SOLUTION IS PRINTED WRONGLY ( I verified by manual calculation )]\n" ); printf("\n WRONGLY PRINTED ANSWERS ARE :- For Case (a) General(ZPF) Method (a) Induced EMF = 6376<-5.07 degree instead of %.f < %.2f \n ",abs(Er_a),atand(imag(Er_a),real(Er_a))) printf("\n For Case (b) ASA Method (a) Induced EMF = 6376<-5.07 degree instead of %.f < %.2f \n\n ",abs(Er_b),atand(imag(Er_b),real(Er_b))) printf(" CALCULATION OF THE POWER ANGLE IS NOT CALCULATED IN THE TEXT BOOK FOR THIS PROBLEM\n ") printf("\n INDUCED EMF AND PERCENTAGE REGULATION IS APPROXIMATED VALUE BECACUSE IN THE TEXT BOOK, CALCULATED INDUCED EMF IS WRONGLY PRINTED")

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Ex5_5.sce

clear //given // //find the final pressure gage and convert absloute temperature to normal temprature a=210. t=160. t2=60. //absloute temperature to convert is 460 AT=160.+460. AT1=60.+460. IP=210.+14.7 FP=IP*(520./620.) printf("\n FP") FPg=(FP-14.7) printf("\n \n final pressue gage is %.2f ",FPg)

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Example7_14_page_250.sce

////Example 7.14 at page no. 250 clc; clear; close; format('v',6); //Given data : g=9.81;//gravity constant l=4;//km n=5000;//habitants Ch=200;//litres/day(habitant capacity) t=10;//hour(daiy supply time) hf=20;//meter(Head loss) f=0.008;//coeff. of friction Qty=n*Ch/2;//litres(Water supplied in 10 hours) Q=Qty/(t*60*60);//litres/sec Q=Q/1000;//m^3/sec d=(f*l*1000*Q^2/3.0257/hf)^(1/5);//meter disp(d*1000,"Diameter of pipe(mm) : ");

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HH_RG.sce

//**************************** HH_RG ********************************** if (blk_name.entries(bl) == "HH_RG") then mputl("#HH_RG",fd_w); for ss=1:scs_m.objs(bl).model.ipar(1) HH_RG_str= '.subckt HH_RG'+' in[0]=net'+string(blk(blk_objs(bl),2))+'_'+string(ss)+' in[1]=net'+string(blk(blk_objs(bl),3))+'_'+string(ss)+' in[2]=net'+string(blk(blk_objs(bl),4))+'_'+string(ss)+' in[3]=net'+string(blk(blk_objs(bl),5))+'_'+string(ss)+' in[4]=net'+string(blk(blk_objs(bl),6))+'_'+string(ss)+' out[0]=net'+string(blk(blk_objs(bl),2+numofip))+'_'+string(ss)+' out[1]=net'+string(blk(blk_objs(bl),3+numofip))+'_'+string(ss)+' #HH_RG_ls =0'+'&HH_RG_Nafb_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(1-1)+ss)))+'&HH_RG_in0_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(2-1)+ss)))+'&HH_RG_pfet_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(3-1)+ss)))+'&HH_RG_nmr_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(4-1)+ss)))+'&HH_RG_Na_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(5-1)+ss)))+'&HH_RG_Na_pbias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(6-1)+ss)))+'&HH_RG_Na_nbias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(7-1)+ss)))+'&HH_RG_K_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(8-1)+ss)))+'&HH_RG_K_pbias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(9-1)+ss)))+'&HH_RG_K_nbias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(10-1)+ss)))+'&HH_RG_buf_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(11-1)+ss)))+'&HH_RG_comp_ibias ='+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(12-1)+ss))) if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 1 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_1x_cs =0'; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 2 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_2x_cs =0'; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 3 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_1x_cs =0'+'&HH_RG_cap0_2x_cs =0'; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 4 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_4x_cs =0'; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 5 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_1x_cs =0'+'&HH_RG_cap0_4x_cs =0'; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 6 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_2x_cs =0'+'&HH_RG_cap0_4x_cs =0'; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss) == 7 then HH_RG_str=HH_RG_str+'&HH_RG_cap0_1x_cs =0'+'&HH_RG_cap0_2x_cs =0'+'&HH_RG_cap0_4x_cs =0'; end mputl(HH_RG_str,fd_w); mputl("",fd_w); if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(14-1)+1) == 1 then plcvpr = %t; plcloc=[plcloc;'net'+string(blk(blk_objs(bl),2+numofip))+'_'+string(ss),string(scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(14-1)+1+2*ss-1))+' '+string(scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(14-1)+1+2*ss))+' 0']; end end end

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// Scilab code Exa5.6.2: To calculate the kinetic energy of photoelectron and rate at which photoelectron emitted : P.no. 231 (2011) C = 3e+08; // Speed of light, m/s h = 6.626e-034; // Planck's constant, Js lambda = 250e-09; // Wavelength of light, m w = 2.30; // Work function, eV A = 2e-04; // Area of the surface, m^2 I = 2; // Intensity of light, W/m^2 e = 1.6e-019; // Charge of the electron, C E_p = h*C/(lambda*e); // Energy of photoelectron, eV E_max = E_p-w; // Maximum kinetic energy of photoelectron, eV n_p = I*A/(E_p*e); // Number of photons reaching the surface per second, photons/s R_p = 0.2/100*n_p; // Rate at which photoelectrons are emitted, photoelectrons/s printf("\n The maximum kinetic energy = %4.2f eV \n The rate at which photoelectrons are emitted = %4.2e photoelectrons/s ", E_max, R_p) // Result // The maximum kinetic energy = 2.67 eV // The rate at which photoelectrons are emitted = 1.01e+012 photoelectrons/s

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<?xml version="1.0" encoding="utf-8"?> <test> <description> NekMesh with Spherigons and variable Boundary Layer </description> <executable>NekMesh</executable> <parameters> -m spherigon:surf=10:surf=13 -m spherigon:surf=8:surf=9 -m bl:surf=3,10,13:layers=4:r="1.7*( 1-x/0.3 )+1":nq=7 -m bl:surf=2,8,9:layers=4:r="1.7*(1-(x-0.27)/0.078)+1":nq=7 -m jac:list spherigon_bl_straight_rw.dat spherigon_bl_straight_rw-out.xml:xml:test </parameters> <files> <file description="Input File">spherigon_bl_straight_rw.dat</file> </files> <metrics> <metric type="regex" id="1"> <regex>.*Total negative Jacobians: (\d+)</regex> <matches> <match> <field id="0">0</field> </match> </matches> </metric> </metrics> </test>

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COM_receive file enable testTemp\test_results.txt sleep 10000 COM_send string start sleep 100000 COM_receive file disable testTemp\test_results.txt

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2020-10-24T18:37:02

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result3s0.tst

@relation unknow @attribute height real[1.0,804.0] @attribute lenght real[1.0,553.0] @attribute area real[7.0,143993.0] @attribute eccen real[0.007,537.0] @attribute p_black real[0.052,1.0] @attribute p_and real[0.062,1.0] @attribute mean_tr real[1.0,4955.0] @attribute blackpix real[1.0,33017.0] @attribute blackand real[7.0,46133.0] @attribute wb_trans real[1.0,3212.0] @attribute class{1,2,4,5,3} @inputs height,lenght,area,eccen,p_black,p_and,mean_tr,blackpix,blackand,wb_trans @outputs class @data 1 1 1 1 1 1 2 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 2 2 1 1 2 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 5 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 5 1 1 1 1 1 5 1 1 1 1 1 1 1 1 1 2 2 2 1 1 1 4 4 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 2 1 1 1 1 1 1 2 1

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Ex4_1.sce

clc // initialization of variables clear P=170 //kN A=645 // (mm)^2 // part (a) E=211.4 // G Pa (from figure) Y=252.6 // M Pa (from figure) Beta=0.0799 // G Pa (from figure) Ey=Y/E // The stress strain law given is // Sigma= E*eps for eps< Ey // Sigma= (1-Beta)*Y + Beta*E*eps otherwise // part (b) th=atan(1.8/2.4)// radians F=P/(2*cos(th)) F=F*10^3 //N A=A*10^-6 //m^2 E=E*10^9 //Pa Y=Y*10^6 //Pa L=3.0 //m Sigma=F/A if(Sigma<Y) eps=Sigma/E else eps=(Sigma-(1-Beta)*Y )/(Beta*E) end u=eps*L/cos(th) u=u*10^3 //mm // results printf('part (b)\n') printf(' Deflection = %.3f mm',u) // part (c) P=270 //kN F=P/(2*cos(th)) F=F*10^3 //N Sigma=F/A if(Sigma<Y) eps=Sigma/E else eps=(Sigma-(1-Beta)*Y )/(Beta*E) end u=eps*L/cos(th) u=u*10^3 //mm // results printf('\n part (c)\n') printf(' Deflection = %.3f mm for P = %.d kN',u,P) P=300 //kN F=P/(2*cos(th)) F=F*10^3 //N Sigma=F/A if(Sigma<Y) eps=Sigma/E else eps=(Sigma-(1-Beta)*Y )/(Beta*E) end u=eps*L/cos(th) u=u*10^3 //mm // results printf('\n Deflection = %.3f mm for P = %.d kN',u,P)

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ex9_36.sce

// Exa 9.36 clc; clear; close; // Given data V_GSth= 2;// in V k= 2*10^-4;// in A/V^2 V_DD= 12;// in V R_D= 5*10^3;// in ohm I_D= poly(0,'I_D'); V_DS= V_DD-I_D*R_D;// in V I_D= I_D-k*(V_DS-V_GSth)^2; I_D= roots(I_D);// in A I_D= I_D(2);// in A V_DS= V_DD-I_D*R_D;// in V disp(I_D*10^3,"The value of I_D in mA is : ") disp(V_DS,"The value of V_DS in volts is : ")

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clc //initialization of varaibles T1=1050+460//R T2=90+460 //R //calculations eta=(T1-T2)/T1 //results printf("Max. possible efficiency = %d percent",eta*100)

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// Calculate apparent resistance, actual resistance and error clc; Et=100; It=5*10^-3; Rt=Et/It; disp(Rt,'apparent value of resistance (ohm)=') Rv=1000*150; Rx=Rt*Rv/(Rv-Rt); disp(Rx,'true value of resistance(ohm)') Er_percentage=[(Rt-Rx)/Rx]*100; disp(Er_percentage,'percentage error=')

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// This file is adapted from part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. load Mux4.hdl, output-file Mux4.out, compare-to Mux4.cmp, output-list a%B1.4.1 b%B1.4.1 sel%D2.1.2 out%B1.4.1; set a 0, set b 0, set sel 0, eval, output; set sel 1, eval, output; set a %B0000, set b %B0101, set sel 0, eval, output; set sel 1, eval, output; set a %B0000, set b %B0110, set sel 0, eval, output; set sel 1, eval, output; set a %B1010, set b %B0000, set sel 0, eval, output; set sel 1, eval, output; set a %B0101, set b %B0000, set sel 0, eval, output; set sel 1, eval, output; set a %B1010, set b %B0101, set sel 0, eval, output; set sel 1, eval, output;

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//Fluid Systems- By Shiv Kumar //Chapter 5- Francis Turbine //Example 5.1 //To Find (a)Discharge passing through the Runner and (b) Width of Runner at Outlet clc clear //Given Data:- Do=0.8; //External Diameter of the Runner, m Di=0.4; //Internal Diameter of the Runner, m Vfi=1.4; //Velocity of Flow at Inlet, m/s Vfo=Vfi; //Velocity of Flow at Outlet, m/s bo=210; //Width of Runner at Inlet, mm //Computations:- Q=%pi*Do*(bo/1000)*Vfi; //Discharge passing through the Runner, m^3/s bi=Do*bo/Di; //Width of Runner at Outlet, mm //Results printf("(a)Discharge passing through the Runner, Q=%.4f m^3/s\n",Q) //The Answer Vary due to Round off Error printf("(b)Width of Runner at Outlet, bi=%.f mm",bi)

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EX20_29.sce

clc;funcprot(0);//EXAMPLE 20.29 // Initialisation of Variables ns=3;........//No of stages N=200;.......//Compressor rpm p1=1;.......//Intake pressure in bar t1=20+273;....//Intake temperature in K D=0.35;......//Engine bore in m L=0.4;.......//Engine stroke in m p2=4;........//Discharge pressure from first stage in bar p6=16;........//Discharge pressure from second stage in bar p10=64;........//Discharge pressure from third stage in bar pd=0.2;........//Loss of pressure between intercoolers in bar R=0.287;......//Gas constant in kJ/kgK k=0.04;.......//Clearence volume in 4% of the stroke volume n1=1.2;.....//Compressor index for first stage n2=1.25;.....//Compressor index for second stage n3=1.3;.....//Compressor index for third stage cp=1.005;......//Specific heat at constant pressure in kJ/kgK etamech=0.8;.....//Mechanical efficiency //Calculations p5=p2-pd;p9=p6-pd;t5=t1;t9=t1; Vs=(%pi/4)*D*D*L*N*2;............//Swept volume of low pressure cylinder per min in m^3 etav1=(1+k)-(k*((p2/p1)^(1/n1)));.....//Volumetric efficiency in first stage etav2=(1+k)-(k*((p6/p5)^(1/n2)));.....//Volumetric efficiency in second stage etav3=(1+k)-(k*((p10/p9)^(1/n3)));.....//Volumetric efficiency in third stage vain1=Vs*etav1;.................//Volume of air taken in first stage in m^3/min m=(p1*10^5)*vain1/(R*t1*1000);...........//Mass of air intake in kg/min in first stage t2=round(t1*((p2/p1)^((n1-1)/n1))); t6=t5*((p6/p5)^((n2-1)/n2)); t10=t9*((p10/p9)^((n3-1)/n3)); Qr1=m*cp*(t2-t5);........//Heat rejected in intercooler after first stage in kJ/min Qr2=m*cp*(t6-t9);........//Heat rejected in intercooler after second stage in kJ/min Qr3=m*cp*(t10-t1);........//Heat rejected in intercooler after third stage in kJ/min disp(Qr1,"Heat rejected in intercooler after first stage in kJ/min:") disp(Qr2,"Heat rejected in intercooler after second stage in kJ/min:") disp(Qr3,"Heat rejected in intercooler after third stage in kJ/min:") vainip=m*R*t5*1000/(p5*10^5);.........//Volume drawn in intermediate pressure cylinder/min Vsip=vainip/etav2;.............//Swept volume of intermediate cylinder in m^3/min Dip=sqrt(Vsip/(2*N*L*(%pi/4)));............//Diameter of the intermediate cylinder in m disp(Dip*1000,"Diameter of the intermediate cylinder in mm:") vainhp=m*R*t9*1000/(p9*10^5);.........//Volume drawn in high pressure cylinder/min Vshp=vainhp/etav3;.............//Swept volume of high pressure cylinder in m^3/min Dhp=sqrt(Vshp/(2*N*L*(%pi/4)));............//Diameter of the intermediate cylinder in m disp(Dhp*1000,"Diameter of the intermediate cylinder in mm:") Ps=[{(n1/(n1-1))*m*R*(t2-t1)}+{(n2/(n2-1))*m*R*(t6-t5)}+{(n3/(n3-1))*m*R*(t10-t9)}]*(1/(60*etamech));...//Shaft power in kW disp(Ps,"Shaft power in kW:") cv=cp-R;..........//Specific heat at constant volume in kJ/kgK ga=cp/cv;...........//Ratio of specific heats Qt1=cv*((ga-n1)/(ga-1))*(t2-t1)*m;............//Heat transfer during first stage in kJ/min Qt2=cv*((ga-n2)/(ga-1))*(t6-t1)*m;............//Heat transfer during second stage in kJ/min Qt3=cv*((ga-n3)/(ga-1))*(t10-t1)*m;............//Heat transfer during third stage in kJ/min printf("\nHeat transferred during first stage in kJ/min: %f\n",Qt1) printf("\nHeat transferred during second stage in kJ/min: %f\n",Qt2) printf("\nHeat transferred during third stage in kJ/min: %f\n",Qt3)

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/2522/CH7/EX7.6/exm7_6.sce

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exm7_6.sce

//page no 228 //example no 7.6 // ARITHEMETIC OPERATIONS. clc; disp('A-->30H'); disp('2040H-->68H'); disp('2041H-->7FH'); disp('LXI H,2040H'); // loads HL register pair. disp('H=20H L=40H M=68H'); disp('ADD M'); A=hex2dec(['30']); M=hex2dec(['68']); S=A+M; // adds the contents of A and data at memory location 2040H. s=dec2hex(S); printf('\n Content of A after addition with 2040H= '); disp(s); disp('INX H'); // takes the program to the next memory location. disp('H=20H L=41H M=7FH'); disp('SUB M'); M=hex2dec(['7F']); D=S-M; // subtracts the contents of A from the data at memory location 2041H. d=dec2hex(D); printf('\n Content of A after subtraction with 2041H= '); disp(d);

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/45/CH14/EX14.1/example_14_1.sce

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example_14_1.sce

//example 14.1 clc; clear; close; vdc = input('Enter the value of DC voltage Vdc in volts :'); r = input('Enter the value of resistace in K ohms :'); v = input(' Enter the value of voltage across diode in volts :'); i = (vdc-v)/r ; format('v',4); if(i>0) // checking whether the diode is forward or reverse biased by checking current disp('The diode is in forward bias'); disp('The diode current in mA is :'); disp(i); else disp('The diode is in Reverse bias'); disp('The diode current in mA is : 0.0'); end;

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/3718/CH13/EX13.10/Ex13_10.sce

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Ex13_10.sce

//Chapter 13: Fuel and Combustions //Problem: 10 clc; //Declaration of Variables H = 0.30 // metre cube CO = 0.10 // metre cube CH4 = 0.04 // metre cube N2 = 0.56 // metre cube // Solution vol_o = H * 0.5 + CO * 0.5 + CH4 * 2 vol_a = vol_o * 100 / 21 mprintf("Volumer of air required for complete combustion of 1 metre cube of producer gas: %.3f metre cube",vol_a)

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/686/CH1/EX1.3/Ex1_3.sci

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Ex1_3.sci

clc(); clear; // To calculate the size of heating surface m1 = 100; // Flow rate of water in lb/hr ta1 = 50; // Initial temperature of water in F ta2 = 170; // Final temperature of water Cp1 = 1; // Heat capacity of water in Btu/lb-F te1 = 330; // Initial temperatutre in flue gases in F m2 = 400; // Mass flow rate of flue gases in lb/hr Cp2 = .25; // Heat capacity of flue gases in Btu/lb-F q = m1*Cp1*(ta2-ta1); // Heat absorbed by water in Btu te2 = te1-q/(m2*Cp2); // Final temperature of flue gases in F U = 20; // Overall heat transfer in Btu/hr-ft^2-F // For parallel flow delte = te1-ta1; // Flue tempearture difference in F delta = te2-ta2; // Water temperature difference in F // Seeing the value of delte/delta=7, we can attain the value of a a1 = 0.77; deltm = (delte + delta)/2; // Arithmetic mean in F LMTD1 = a1*deltm; // Log mean temperature diffference A1 = q/(U*LMTD1); // Area in ft^2 printf("The area of heat exchanger for parallel flow is %.2f ft^2 \n ",A1); // for counterflow delte = te1-te2; // Flue tempearture difference in F delta = ta1-ta2; // Water temperature difference in F // Seeing the value of delte/dela=1, a=1. a2 = 1; LMTD2 = a2*deltm; // Log mean temperature diffference A2 = q/(U*LMTD2); // Area in ft^2 printf("The area of heat exchanger for counterflow flow is %.2f ft^2 \n ",A2); // For cross flow delte = te1-ta1; // Flue tempearture difference in F delta = te2-ta2; // Water temperature difference in F // Seeing the value of delta/delte=0.143, we can attain the value of a=0.939 a3 = 0.939; deltm = (delte + delta)/2; // Arithmetic mean in F LMTD3 = a3*deltm; // Log mean temperature diffference A3 = q/(U*LMTD3); // Area in ft^2 printf("The area of heat exchanger for cross flow is %.2f ft^2 \n ",A3);

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/main/saturation.sce

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saturation.sce

vitesse = [1,2,3]; vmax = [0.5, 0.5, 0.1]; dv = 0.05*vmax; vinf = 0.95*vmax; vsup = 1.05*vmax; fac = 1; for i=1:3 absVel =abs(vitesse(i)); fac = min(abs(fac),vmax(i)/(absVel+%eps)); disp(fac); end // for i=1:3 vitesse=fac*vitesse; // end disp(vitesse);

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/3050/CH1/EX1.4/Ex1_4.sce

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Ex1_4.sce

//calculating hardness //Example 1.4 clc clear //For Ca(HCO3)2, q1=40.5//quantity wt1=162//molecular weight M1=100/wt1//multiplication factor Eq1=M1*q1//CaCO3 equivalents in mg/L //For Mg(HCO3)2, q2=46.5//quantity wt2=146//molecular weight M2=100/wt2//multiplication factor Eq2=M2*q2//CaCO3 equivalents in mg/L //For MgSO4, q3=27.6//quantity wt3=120//molecular weight M3=100/wt3//multiplication factor Eq3=M3*q3//CaCO3 equivalents in mg/L //For CaSO4, q4=32.1//quantity wt4=136//molecular weight M4=100/wt4//multiplication factor Eq4=M4*q4//CaCO3 equivalents in mg/L //For CaCl2 q5=22.45//quantity wt5=111//molecular weight M5=100/wt5//multiplication factor Eq5=M5*q5//CaCO3 equivalents in mg/L Th=Eq1+Eq2//Temperory hardness due to Mg(HCO3)2 and Ca(HCO3)2 Ph=Eq3+Eq4+Eq5//Permanent hardness due to CaSO4 and MgSO4 and CaCl2 T=Th+Ph//Total hardness printf('Thus in Temporary hardness = %2.2f mg/L',Th) printf('\n and permanent hardness = %2.2f mg/L',Ph) printf('\n and total hardness = %3.2f mg/L',T)

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/1055/CH21/EX21.1/ch21.sce

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ch21.sce

//Determine the load bus voltage clear clc; load1=10+%i*15;//load per phase(MVA) SCC=250/3; V=11/sqrt(3); P=30; Q=45; Z=(11/sqrt(3))^2/(250/3);//Equivalent short circuit impedence dsc=atand(5); R=.0949; X=.4746; //Using equation: V^2= (Vcosd+PR/V)^2 + (Vsind+QX/V)^2, we get y=poly([51.7 0 -27.5 0 1],'V','c'); disp(y,"we get equation :"); X=roots(y); disp(X,"Roots of above equation are "); V=5.046; mprintf("V=%.3f\n",V); dV=6.35-V; Ssc=250; //using expression ,a=dV/v=1(Pcos(dsc)+Qsin(dsc))/Ssc +j(Psin(dsc)-Qcos(dsc))/Ssc a=(P*cosd(dsc)+Q*sind(dsc))/Ssc +%i*(P*sind(dsc)-Q*cosd(dsc))/Ssc; disp(abs(a),"dV/V= ");

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/2837/CH22/EX22.3/Ex22_3.sce

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Ex22_3.sce

clc clear //Initalization of variables h1=24.973 //Btu/lb h2=81.436 //Btu/lb cfm=200 //cfm v2=0.77357 v3=3.8750 h4=72.913 //calculations mass=cfm/v2 ref=h2-h1 tonnage=mass*ref/cfm mass2=cfm/v3 ref2=h4-h1 tonnage2=mass2*ref2/cfm //results printf("In case 1,Tonnage = %.1f tons",tonnage) printf("\n In case 2,Tonnage = %.2f tons",tonnage2)

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/Lab09/sintry.sce

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sintry.sce

//xq(find(((q(i)-d/2)<= xq)&(xq<=(q(i)+d/2)))) = // q(i).*ones(1,length(find(((q(i)-d/2)<=xq)&(xq<=(q(i)+d/2))))); // en_code(find(xq == q(i)))= (i-1).*ones(1,length(find(xq == q(i)))); fs = 10000; fm = 100; time = [0: 1.0/fs : 2.0/fm]; //plot(sin(2*%pi*fm*time)); //plot(time); n = 8 ; del = 0.586; input = (3.5*del)*(sin(2*%pi*fm*time) function ql = quant8(x) xmax = max(abs(x)); xq = x / xmax; // d = 2/n q = del*[0,n-1]; q = q-((n-1)/2)*d; for i = 1:len(x) // end // q = q-((L-1)/2)*d; for i = 1:len(x) if (x(i)< ) then end end endfunction

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/1067/CH45/EX45.B.6/45_B_6.sce

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45_B_6.sce

clear; clc; n1=.89; h1=150; c1=.9; h2=200; n2=.9; c2=.8; h3=500; n3=.93; c3=.707; p4=100; p1=h1*.746/n1; p2=h2*.746/n2; p3=h3*.746/n3; rr1=p1*(tan(acos(c1))); rr2=p2*(tan(acos(c2))); rr3=p3*(tan(acos(c3))); rr4=0; rr=rr1+rr2-rr3+rr4; p=p1+p2+p3+p4; c=rr/p; j=cos(atan(c)); j=round(j*1000)/1000; printf("the Power Factor of the combined sub-station=%f leading",j);