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Example26_4.sce
clear; clc; // Example 26.4 printf('Example 26.4\n\n'); //page no. 815 // Solution Fig E26.4b // Given SO2_in = 2200 ;// Amount of SO2 entering reactor 2-[lb mol/hr] // Basis : 1 lb mol CO entering reactor 1,therefore R1_CO_in = 1 ;//CO entering reactor 1-[lb mol] air = .80 ;// Fraction of air used in burning // System- reactor 2 // Given R2_fSO2_in = 0.667 ;// Fraction of SO2 entering reactor 2 R2_fO2_in = 0.333 ;// Fraction of O2 entering reactor 2 R2_fSO3_out = 0.586 ;// Fraction of SO3 exiting reactor 2 R2_fSO2_out = 0.276 ;// Fraction of SO2 exiting reactor 2 R2_fO2_out = 0.138 ;// Fraction of O2 exiting reactor 2 // Main Reaction: CO , (1/2)*O2 ---> CO2 R1_O2_in = (1/2)*air ;// O2 entering reactor 1-[g mol] R1_N2_in = R1_O2_in*(79/21) ;// N2 entering reactor 1-[g mol] //Output of reactor 1 R1_CO_out = R1_CO_in*(1 - air) ;// [g mol] R1_CO2_out = 1*( air) ;// [g mol] R1_N2_out = R1_N2_in ;//[g mol] // By analysis DOF is zero. // Get eqn. to solve by species balance //Unknowns - P- exit stream of reactor 2 , F - entry stream of reactor 2 , ex - extent of reaction // P*(R2_fSO2_out) - F*0 = 1*ex ... eqn.(a)- By SO3 balance // P*(R2_fSO2_out) - F*(R2_fSO2_in) = -1*ex ...eqn.(b) - By SO2 balance // By O2 balance we will get eqn. equivalent to eqn. (b), so we need one more eqn. // Energy balance // For energy balance, get required data from software in the CD of book and sensible heat data from Appendix F // given data of outputs is taken in array in order CO(g),CO2(g), N2(g),SO2(g),SO3(g) and then O2(g) del_Hi_out = [ -109.054,-393.250,0,-296.855,-395.263,0] ; // Heat of formation - [kJ/g mol] del_Hf_out = [35.332,35.178,22.540,20.845,34.302,16.313] ;//Change in enthalpy during temperature change -[kJ/g mol] del_H_out =del_Hi_out + del_Hf_out ;//[-371.825,15.043,160.781,-449.650,-581.35]// Change in enthalpy final - [kJ/g mol] // given data of inputs is taken in array in order CO(g),CO2(g), N2(g),SO2(g) and then O2(g) del_Hi_in = [ -109.054,-393.250,0,-296.855,0] ;// // Heat of formation - [kJ/g mol] del_Hf_in = [17.177,17.753,11.981,0,0] ;//Change in enthalpy during temperature change -[kJ/g mol] del_H_in = del_Hi_in+ del_Hf_in ;// Change in enthalpy final - [kJ/g mol] // Now do energy balance , assume Q = 0 , // del_H_out(4)*P*R2_fSO2_out + del_H_out(5)*P*R2_fSO3_out - del_H_in(4)*F*R2_fSO2_in + del_Hi_out(6)*P*R2_fO2_out = 0 ... eqn. (c) // Solve eqn. (a), (b) and (c) to get F ,P , ex a = [(R2_fSO3_out) 0 -1;(R2_fSO2_out) -(R2_fSO2_in) 1;(del_H_out(4)*R2_fSO2_out + del_H_out(5)*R2_fSO3_out + del_Hi_out(6)*R2_fO2_out ) -(del_H_in(4)*R2_fSO2_in) 0] ;// Matrix of coefficients b = [0;0;(del_H_in(1)*R1_CO_out+del_H_in(2)*R1_CO2_out+del_H_in(3)*R1_N2_out-(del_H_out(1)*R1_CO_out+del_H_out(2)*R1_CO2_out+ del_H_out(3)*R1_N2_out))] ;// Matrix of constants x = a\b ;// Matrix of solutions, P = x(1), F = x(2) ,ex = x(3) F = x(2) ;//exit stream of reactor 2 - [lb mol] R2_SO2_in = R2_fSO2_in*F ;// Moles of SO2 required per lb mol of CO - [lb mol] CO = (R1_CO_in*SO2_in)/R2_SO2_in ;//Mole of CO burned in reactor 1 - [lb mol] printf('Mole of CO burned in reactor 1 is %.0f lb mol.\n',CO) ;
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//Example 5.19, page no-317 clear clc e=0.2*10^-3 B=0.08 l=10*10^-2 v=e/(B*l) printf("V = %.3f m/sec = %.2f cm/sec",v,v*100)
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//clear// //Caption:Program to Caculate Electric Field E at P due to 4 identical charges //Example2.2 //page 33 clc; P = [1,1,1]; P1 = [1,1,0]; P2 = [-1,1,0]; P3 = [-1,-1,0]; P4 = [1,-1,0]; R1 = norm(P-P1); aR1 = UnitVector(P-P1); R2 = norm(P-P2); aR2 = UnitVector(P-P2); R3 = norm(P-P3); aR3 = UnitVector(P-P3); R4 = norm(P-P4); aR4 = UnitVector(P-P4); disp(R1,'R1=') disp(aR1,'aR1=') disp(R2,'R2=') disp(aR2,'aR2=') disp(R3,'R3=') disp(aR3,'aR3=') disp(R4,'R4=') disp(aR4,'aR4=') Q = 3e-09; //charge in Coulombs Eps = 8.854e-12; //free space permittivity E1 = (Q/(4*%pi*Eps*R1^2))*aR1; E2 = (Q/(4*%pi*Eps*R2^2))*aR2; E3 = (Q/(4*%pi*Eps*R3^2))*aR3; E4 = (Q/(4*%pi*Eps*R4^2))*aR4; E = E1+E2+E3+E4; disp(E,'Electric Field Intesnity at any point P due to four identical Charges in V/m=') //Result //R1= 1. //aR1= 0. 0. 1. //R2= 2.236068 //aR2= 0.8944272 0. 0.4472136 //R3= 3. //aR3= 0.6666667 0.6666667 0.3333333 //R4= 2.236068 //aR4= 0. 0.8944272 0.4472136 //Electric Field Intesnity at any point P due to four identical Charges in V/m= // 6.8206048 6.8206048 32.785194 //
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clc clear //input data P01=7//Total initial pressure of gases at entry in bar T01=1100//Total initial temperature in K P02=1.5//Total final pressure of gases at exit in bar T02=830//Total final temperature in K C2=250//Exit velocity in m/s r=1.3//Ratio of specific heats of gases M=28.7//Molecular weight of gases R1=8.314//Gas constant of air in kJ/kg.K //calculations T02s=T01*(P02/P01)^((r-1)/r)//Final temperature in K ntt=((T01-T02)/(T01-T02s))//Total-to-total efficiency R=(R1/M)//Gas constant of given gas in kJ/kg.K Cp=((r*R)/(r-1))//Specific heat of given gas at constant pressure in kJ/kg.K T2s=(T02s-((C2^2)/(2*Cp*1000)))//Temperature in isentropic process at exit in K nts=((T01-T02)/(T01-T2s))//Total-to-static efficiency //output printf('The total-to-total efficiency of gases is %3.3f\nThe total-to-static efficiency of gases is %3.3f',ntt,nts)
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i = 0; i = double(i); arr= []; final_arr = []; row = 0; count=1; count = int(count); temp = get_random_gaussian(200000); while i<=20 val = [sin(i),cos(i),(i/4)] temp1 = [temp(1+count),temp(2+count),temp(3+count)]; count = count + 3; val = val + temp1/20; color = colormap_jet(i,0,20); arr = [val,color]; final_arr = cat(1,final_arr,arr); row = row + 1; i = i + 0.001; end perspective_window(row , final_arr)
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clc //Initialization of variables clear mass=4000 //kg/m^2 Patm=1.013*10^5 //pa g=9.807 M=28 R=8.3143*10^3 T=303 //K P1=800*10^3 //pa //calculations Ps=Patm+mass*g n=1/M V1=n*R*T/P1 W=Ps*(2*V1) //results printf("Work done on the surroundings = %d J",W)
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// scilab Code Exa 11.6 General Swirl Distribution axial compressor Rm=0.5; // Degree of reaction dm=36/100; // Mean Blade ring diameter in m rm=dm/2; N=18e3; // rotor Speed in RPM h=6/100; // blade height at entry in m dh=dm-h; dt=dm+h; cx=180; // Axial velocity in m/s alpha_1m=25; // air angle at rotor and stator exit alpha_2m=54.820124; um=%pi*dm*N/60; omega=um/rm; rh=dh/2; rt=dt/2; uh=omega*rh; ut=omega*rt; // part(a) rotor blade air angles c_theta1m=cx*tand(alpha_1m); c_theta2m=cx*tand(alpha_2m); a=0.5*(c_theta1m+c_theta2m) b=rm*(c_theta2m-c_theta1m)*0.5; c_theta1h=a-(b/rh); c_theta1t=a-(b/rt); K1=cx^2+(2*(a^2)*((b/(a*rm))+log(rm))); cx1h=sqrt(K1-(2*(a^2)*((b/(a*rh))+log(rh)))); cx1t=sqrt(K1-(2*(a^2)*((b/(a*rt))+log(rt)))); c_theta2h=a+(b/rh); c_theta2t=a+(b/rt); K2=cx^2+(2*(a^2)*(log(rm)-(b/(a*rm)))); cx2h=sqrt(K2-(2*(a^2)*(log(rh)-(b/(a*rh))))); cx2t=sqrt(K2-(2*(a^2)*(log(rt)-(b/(a*rt))))); disp("(a) the rotor blade air angles are") // for hub section alpha1h=atand(c_theta1h/cx1h); alpha2h=atand(c_theta2h/cx2h); disp("for hub section") beta1h=atand((uh/cx1h)-tand(alpha1h)); beta2h=atand((uh/cx2h)-tand(alpha2h)); disp("degree",beta1h,"beta1h=") disp("degree",beta2h,"beta2h=") // for tip section alpha1t=atand(c_theta1t/cx1t); alpha2t=atand(c_theta2t/cx2t); disp("for tip section") beta1t=atand((ut/cx1t)-tand(alpha1t)); beta2t=atand((ut/cx2t)-tand(alpha2t)); disp("degree",beta1t,"beta1t= ") disp("degree",beta2t,"beta2t= ") // part(b) specific work w=2*omega*b; disp("kJ/kg",w*1e-3,"(b)specific work is") // part(c) the loading coefficients disp("(c)the loading coefficients are") shi_h=w/(uh^2); disp(shi_h,"shi_h=") shi_m=w/(um^2); disp(shi_m,"shi_m=") shi_t=w/(ut^2); disp(shi_t,"shi_t=") // part(c) degrees of reaction disp("(d)Degrees of reaction are") Rh=((cx1h^2)*(secd(beta1h)^2)-(cx2h^2)*(secd(beta2h)^2))*100/(2*w); Rt=((cx1t^2)*(secd(beta1t)^2)-(cx2t^2)*(secd(beta2t)^2))*100/(2*w); disp("%",Rh,"Rh=") disp("%",Rm*100,"Rm=") disp("%",Rt,"Rt=") disp("Comment: book contains wrong calculation for Rt value")
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c1=50; v1=16; c2=40; v2=10; disp("Part a"); v=v2*(c1+c2)/c1; disp("the maximum working voltage (in V) is");disp(v); disp("Part b"); v1=v*c2/(c1+c2); v2=v*c1/(c1+c2); disp("the voltage (in V) across 50 μF capacitor is"); disp(v1); disp("the voltage (in V) across 40 μF capacitor is"); disp(v2); disp("Part c"); c=c1*c2/(c1+c2); disp("the total capacitance (in μF) is"); disp(c);
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//Problem 34.05: For the network shown in Figure 34.20, determine (a) the current flowing in the (0+i10) ohm impedance, and (b) the power dissipated in the (20 + i0) ohm impedance. //initializing the variables: rv = 120; // in volts thetav = 0; // in degrees ZA = 25 - %i*5; // in ohm ZB = 15 + %i*10; // in ohm ZC = 20 - %i*30; // in ohm ZD = 20 + %i*0; // in ohm ZE = 0 + %i*10; // in ohm ZF = 2.5 - %i*5; // in ohm //calculation: //voltage V = rv*cos(thetav*%pi/180) + %i*rv*sin(thetav*%pi/180) //The network may initially be simplified by transforming the delta PQR to its equivalent star connection as represented by impedances Z1, Z2 and Z3 in Figure 34.21. From equation (34.7), Z1 = ZA*ZB/(ZA + ZB + ZC) Z2 = ZC*ZB/(ZA + ZB + ZC) Z3 = ZA*ZC/(ZA + ZB + ZC) //The network is shown redrawn in Figure 34.22 and further simplified in Figure 34.23, from which, Zab = ((Z3 + ZE)*(ZD + Z2)/(Z2 + ZE + ZD + Z3)) + (Z1 + ZF) //Current I1 I1 = V/Zab //current I2 I2 = ((ZE + Z3)/(Z2 + ZE + ZD + Z3))*I1 //current I3 I3 = I1 - I2 //The power P dissipated in the ZD impedance of Figure 34.20 is given by Pzd = ZD*I2^2 printf("\n\n Result \n\n") printf("\n (a)the current flowing in the (0+i10) ohm impedance is %.2f A",I3) printf("\n (b) the power dissipated in the (20 + i0) ohm impedance is %.2f W",Pzd)
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function ACORDETOC = interpret_correlation(S2) acordetoc = find(S2==max(S2)); if (length(acordetoc) > 1) acordetoc = acordetoc(1); end //DECODIFICADOR if (acordetoc == 1) ACORDETOC = 'CM'; end if (acordetoc == 2) ACORDETOC = 'Cm'; end if (acordetoc == 3) ACORDETOC = 'Caum'; end if (acordetoc == 4) ACORDETOC = 'Cdim'; end if (acordetoc == 5) ACORDETOC = 'C#M'; end if (acordetoc == 6) ACORDETOC = 'C#m'; end if (acordetoc == 7) ACORDETOC = 'C#aum'; end if (acordetoc == 8) ACORDETOC = 'C#dim'; end if (acordetoc == 9) ACORDETOC = 'DM'; end if (acordetoc == 10) ACORDETOC = 'Dm'; end if (acordetoc == 11) ACORDETOC = 'Daum'; end if (acordetoc == 12) ACORDETOC = 'Ddim'; end if (acordetoc == 13) ACORDETOC = 'D#M ou EbM'; end if (acordetoc == 14) ACORDETOC = 'D#m ou Ebm'; end if (acordetoc == 15) ACORDETOC = 'D#aum ou Ebaum'; end if (acordetoc == 16) ACORDETOC = 'D#dim ou Ebdim'; end if (acordetoc == 17) ACORDETOC = 'EM'; end if (acordetoc == 18) ACORDETOC = 'Em'; end if (acordetoc == 19) ACORDETOC = 'Eaum'; end if (acordetoc == 20) ACORDETOC = 'Edim'; end if (acordetoc == 21) ACORDETOC = 'FM'; end if (acordetoc == 22) ACORDETOC = 'Fm'; end if (acordetoc == 23) ACORDETOC = 'Faum'; end if (acordetoc == 24) ACORDETOC = 'Fdim'; end if (acordetoc == 25) ACORDETOC = 'F#M'; end if (acordetoc == 26) ACORDETOC = 'F#m'; end if (acordetoc == 27) ACORDETOC = 'F#aum'; end if (acordetoc == 28) ACORDETOC = 'F#dim'; end if (acordetoc == 29) ACORDETOC = 'GM'; end if (acordetoc == 30) ACORDETOC = 'Gm'; end if (acordetoc == 31) ACORDETOC = 'Gaum'; end if (acordetoc == 32) ACORDETOC = 'Gdim'; end if (acordetoc == 33) ACORDETOC = 'G#M ou AbM'; end if (acordetoc == 34) ACORDETOC = 'G#m ou Abm'; end if (acordetoc == 35) ACORDETOC = 'G#aum ou Abaum'; end if (acordetoc == 36) ACORDETOC = 'G#dim ou Abdim'; end if (acordetoc == 37) ACORDETOC = 'AM'; end if (acordetoc == 38) ACORDETOC = 'Am'; end if (acordetoc == 39) ACORDETOC = 'Aaum'; end if (acordetoc == 40) ACORDETOC = 'Adim'; end if (acordetoc == 41) ACORDETOC = 'A#M ou BbM'; end if (acordetoc == 42) ACORDETOC = 'A#m ou Bbm'; end if (acordetoc == 43) ACORDETOC = 'A#aum ou Bbaum'; end if (acordetoc == 44) ACORDETOC = 'A#dim ou Bbdim'; end if (acordetoc == 45) ACORDETOC = 'BM'; end if (acordetoc == 46) ACORDETOC = 'Bm'; end if (acordetoc == 47) ACORDETOC = 'Baum'; end if (acordetoc == 48) ACORDETOC = 'Bdim'; end //select expr, //case expr1 then instructions1, //case expr2 then instructions2, //... //case exprn then instructionsn, //[else instructions], //end endfunction
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mode(2);errcatch(-1,"stop");driver("GIF");syms K H=syslin('c',(K*(s+4))/((s-1)*(s-2))) fmin=0.1; fmax=100; bode(H,fmin,fmax) show_margins(H) // for phase margin =30 printf("From bode plot it can be seen that gain should be reduced by 4db") xinit('/home/fossee/Downloads/tbc_graphs/Control_Systems_Engineering_I._J._Nagrath_And_M._Gopal__28/ex9_13_2');xend();exit();
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chdir('C:\Users\matve\Desktop\Code These\ResilienceClosure\'); sheets=readxls('donnees3.xls'); data=sheets(1); data_cli=sheets(3); data_param=sheets(2); data_eff=sheets(4); data_eco=sheets(5); data_bio=sheets(6); data_demo=sheets(7); data_trophi=sheets(8); data_cost=sheets(9); data_actu=sheets(10); data_prix=sheets(11); data_otsp=sheets(12); Horizont=48; N_species=4; N_fleet=3; NN_calib=N_species-1; Hort=Horizont-1; //T_proj=Horizont; //Pour 2050 //T_proj=Horizont+128; //Pour 2070 //T_s=208; //T_proj= Horizont+T_s; //Pour 2100 T_s=328; T_proj=Horizont+T_s; t_0=2006; t_donnees_final=t_0+(T_proj)/4; c=0; species=["Acoupa Weakfish";"Green Weakfish";"Crucifix Catfish";"14 eme espece"]; ///capture/////// historical_catch_CC_AR=data(4:Hort+4,4)./(1000*1000); historical_catch_CCA_AR=data(4:Hort+4,5)./(1000*1000); historical_catch_T_AR=data(4:Hort+4,7)./(1000*1000); historical_catch_CC_AA=data(102:Hort+102,4)./(1000*1000); historical_catch_CCA_AA=data(102:Hort+102,5)./(1000*1000); historical_catch_T_AA=data(102:Hort+102,7)./(1000*1000); historical_catch_CC_MB=data(53:Hort+53,4)./(1000*1000); historical_catch_CCA_MB=data(53:Hort+53,5)./(1000*1000); historical_catch_T_MB=data(53:Hort+53,7)./(1000*1000); historical_catch_CC=[historical_catch_CC_AR,historical_catch_CC_AA,historical_catch_CC_MB]; historical_catch_CCA=[historical_catch_CCA_AR,historical_catch_CCA_AA,historical_catch_CCA_MB]; historical_catch_T=[historical_catch_T_AR,historical_catch_T_AA,historical_catch_T_MB]; catch_hist_sum=historical_catch_CCA+historical_catch_CC+historical_catch_T; sum_capture_CC_h=[sum(historical_catch_CC,'c')]; sum_capture_CCA_h=[sum(historical_catch_CCA,'c')]; sum_capture_T_h=[sum(historical_catch_T,'c')]; sum_capture_h=[sum_capture_CC_h,sum_capture_CCA_h,sum_capture_T_h]; sum_capture_agg_h=sum(sum_capture_h,'c'); ////////////////////////////////////////////////////////////////////////////////////////////////////////////////////// //Pour RCP 8.5 //8.5 moy gam_AR_85=data_cli(4:395,3); gam_AA_85=data_cli(4:395,4); gam_MB_85=data_cli(4:395,5); //gam_AR_85=data_cli(16:T_proj+16,3); //gam_AA_85=data_cli(4:T_proj+4,4); //gam_MB_85=data_cli(20:T_proj+20,5); ////////////////////////////////////////////////////////////////////////////////////////////////////////////////////// //Pour RCP 2.6 //2.6 moy gam_AR_26=data_cli(4:395,7); gam_AA_26=data_cli(4:395,8); gam_MB_26=data_cli(4:395,9); gam_85=[gam_AR_85,gam_AA_85,gam_MB_85]; gam_26=[gam_AR_26,gam_AA_26,gam_MB_26]; //Pour temperature standard gam_AR_stand=data_cli(4:395,11); gam_AA_stand=data_cli(4:395,12); gam_MB_stand=data_cli(4:395,13); gam_stand=[gam_AR_stand,gam_AA_stand,gam_MB_stand]; //changement de parametre //PARAMETRE CALIB I=data_param(2:T_proj+1,1); aij=data_param(2:2+N_species-1,2:2+N_species-1); q_CC=data_param(2:2+N_species-1,6); q_CCA=data_param(2:2+N_species-1,7); q_P=data_param(2:2+N_species-1,8); q_T=data_param(2:2+N_species-1,9); M=data_param(2:2+N_species-1,10); gi=data_param(2:2+N_species-1,11); Bio_1=data_param(7,2:2+N_species-1); tho=data_param(9,2:2+N_species-2); //ECONOMIE OLD nb_boats=data_eco(4,6:8); Var_cost=data_eco(5,6:8); fix_cost=data_eco(6,6:8); //On a une valeur de couts fixes par année, on trimestrialise fix_cost_trim=fix_cost./4; //PRIX OLD pr_AW=data_eco(8,6:8); pr_GW=data_eco(9,6:8); pr_CrC=data_eco(10,6:8); pr=[pr_AW;pr_GW;pr_CrC]; //pr: stock sur lignes et flot sur colonnes==> on inverse P=pr'; //On recupère les prix par stock (sur des lignes) p_CC=P(1,1:3); p_CCA=P(2,1:3); p_T=P(3,1:3); nb_j_peche_per_boats_per_trim=data_eco(11,6:8); //nb_j_peche_per_boats_per_trim=nb_j_peche_per_boats_per_trim.*3; bet=[0,0.5,0.5]; r=0.03/4; alpha_add=data_eco(12,6:8); alpha_mul=data_eco(13,6:8); //INDICATEURS BIOLOGIQUES poids_moy=data_bio(2,2:4); poids_moy_kt=poids_moy.*(10^-6); T=data_bio(3,2:4); //POPULATION GUYANE PopGuy=round(data_demo(3:97,3)); PopGuyTrim=zeros(T_proj,1); //ligne decrivant le nombre de ligne initial du fichier for n=1:(T_proj/4); //ligne decrivant le nombre de ligne souhaite du fichier for t=1+n*4-4:(n+1)*4-4; PopGuyTrim(t)=PopGuy(n); //PopGuyTrim(t)=PopGuy(n) end end for i=1:N_fleet for t=1:T_proj // AE(t,i)=rand(); end end //save('C:\Users\matve\Desktop\Code These\ResilienceMEY\'+'AE','AE'); CoutVar=data_cost(2:95,2:7); PrixPet=CoutVar(:,1); CoutVarAnCC=(1403.84*PrixPet(:,1)+1946.51) CoutVarAnCCA=(7372.68*PrixPet(:,1)+2933.77) CoutVarAnT=(10978.63*PrixPet(:,1)+10416.4) Coutss=[]; Coutss=[Coutss,CoutVarAnCC]; Coutss=[Coutss,CoutVarAnCCA]; Coutss=[Coutss,CoutVarAnT]; /////////////////////////////////////////////////////////////////////////////// PrixPetDel=CoutVar(:,2); CoutVarAnCCDel=(1403.84*PrixPetDel(:,1)+1946.51) CoutVarAnCCADel=(7372.68*PrixPetDel(:,1)+2933.77) CoutVarAnTDel=(10978.63*PrixPetDel(:,1)+10416.4) CoutDel=[]; CoutDel=[CoutDel,CoutVarAnCCDel]; CoutDel=[CoutDel,CoutVarAnCCADel]; CoutDel=[CoutDel,CoutVarAnTDel]; /////////////////////////////////////////////////////////////////////////////// PrixPetSus=CoutVar(:,3); CoutVarAnCCSus=(1403.84*PrixPetSus(:,1)+1946.51) CoutVarAnCCASus=(7372.68*PrixPetSus(:,1)+2933.77) CoutVarAnTSus=(10978.63*PrixPetSus(:,1)+10416.4) CoutSus=[]; CoutSus=[CoutSus,CoutVarAnCCSus]; CoutSus=[CoutSus,CoutVarAnCCASus]; CoutSus=[CoutSus,CoutVarAnTSus]; CoutVarAgg(:,1)=CoutVarAnCC; CoutVarAgg(:,2)=CoutVarAnCCA; CoutVarAgg(:,3)=CoutVarAnT; for n=1:(T_proj/4); //ligne decrivant le nombre de ligne souhaite du fichier for t=1+n*4-4:(n+1)*4-4; CoutVarTrim(t,1:3)=CoutVarAgg(n,1:3)./4; CoutVarTrimDel(t,1:3)=CoutDel(n,1:3)./4; CoutVarTrimSus(t,1:3)=CoutSus(n,1:3)./4; CoutVarTrimTrad(t,1:3)=Coutss(n,1:3)./4; // CoutVarTrim(t,1:3)=CoutVar(1,1:3)./4; end end CoutVarTrim=CoutVarTrimSus; save('C:\Users\matve\Desktop\Code These\ResilienceBAU\CoutVarSus','CoutVarTrim'); save('C:\Users\matve\Desktop\Code These\ResilienceMEY2\CoutVarSus','CoutVarTrim'); save('C:\Users\matve\Desktop\Code These\ResilienceMSY\CoutVarSus','CoutVarTrim'); CoutVarTrim=CoutVarTrimTrad; save('C:\Users\matve\Desktop\Code These\ResilienceBAU\CoutVarTrad','CoutVarTrim'); save('C:\Users\matve\Desktop\Code These\ResilienceMEY2\CoutVarTrad','CoutVarTrim'); save('C:\Users\matve\Desktop\Code These\ResilienceMSY\CoutVarTrad','CoutVarTrim'); CoutVarTrim=CoutVarTrimDel; save('C:\Users\matve\Desktop\Code These\ResilienceBAU\CoutVarDel','CoutVarTrim'); save('C:\Users\matve\Desktop\Code These\ResilienceMEY2\CoutVarDel','CoutVarTrim'); save('C:\Users\matve\Desktop\Code These\ResilienceMSY\CoutVarDel','CoutVarTrim'); //LIEN TROPHIQUE Trophi=data_trophi(2:5,2); //DATE CHOC DateChoc=15 //ACTUALISATION Actu=data_actu(2:96,5); for n=1:(T_proj/4); //ligne decrivant le nombre de ligne souhaite du fichier for t=1+n*4-4:(n+1)*4-4; ActuTrim(t,1)=Actu(n,1); end end //PRIX AVEC INFLATION prix=data_prix(2:96,2:4); //ligne decrivant le nombre de ligne souhaite du fichier //Possibilite de lever l'evolution du prix base sur l inflation CE for n=1:(T_proj/4); for t=1+n*4-4:(n+1)*4-4; PrixTrim(t,1:3)=prix(n,1:3)*1000; end end //AE load('AE','AE'); Inflation=data_prix(2:96,5); ProfOtSP=data_otsp(1:3,16)'; ProfOtSPinf=[ProfOtSP(1)*Inflation,ProfOtSP(2)*Inflation,ProfOtSP(3)*Inflation]; for n=1:(T_proj/4); for t=1+n*4-4:(n+1)*4-4; ProOtSP(t,1:3)=ProfOtSPinf(n,1:3)./4; end end
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Chapter1_Example4.sce
//Chapter-1, Illustration 4, Page 17 //Title: Fuels and Combustion //============================================================================= clc clear //INPUT DATA C=0.84;//Percentage composition of Carbon H=0.09;//Percentage composition of Hydrogen CO2=0.0875;//Volumetric composition of CO2 CO=0.0225;//Volumetric composition of CO O2=0.08;//Volumetric composition of Oxygen N2=0.81;//Volumetric composition of Nitrogen M1=44;//Molecular mass of CO2 M2=28;//Molecular mass of CO M3=32;//Molecular mass of O2 M4=28;//Molecular mass of N2 //CALCULATIONS c1=CO2*M1;//Proportional mass of CO2 c2=CO*M2;//Proportional mass of CO c3=O2*M3;//Proportional mass of O2 c4=N2*M4;//Proportional mass of N2 c=c1+c2+c3+c4;//Total proportional mass of constituents m1=c1/c;//Mass of CO2 per kg of flue gas in kg m2=c2/c;//Mass of CO per kg of flue gas in kg m3=c3/c;//Mass of O2 per kg of flue gas in kg m4=c4/c;//Mass of N2 per kg of flue gas in kg d1=m1*100;//Mass analysis of CO2 d2=m2*100;//Mass analysis of CO d3=m3*100;//Mass analysis of O2 d4=m4*100;//Mass analysis of N2 m=((3*m1)/11)+((3*m2)/7);//Mass of carbon in kg md=C/m;//Mass of dry flue gas in kg //OUTPUT mprintf('Mass of dry flue gases per kg of coal burnt is %3.1f kg',md) //==============================END OF PROGRAM=================================
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//Least square approximation to continuous functions clc; clear; close(); format('v',8); funcprot(0); deff('[g]=f(x,y)','g= -y^2/(1+x)'); disp('approximation of e^x on [0,1] with a uniform weight w(x)=1') a11 = integrate('1','x',0,1); a12 = integrate('x','x',0,1); a13 = integrate('x*x','x',0,1); a14 = integrate('x^3','x',0,1); a21 = integrate('x','x',0,1); a22 = integrate('x^2','x',0,1); a23 = integrate('x^3','x',0,1); a24 = integrate('x^4','x',0,1); a31 = integrate('x^2','x',0,1); a32 = integrate('x^3','x',0,1); a33 = integrate('x^4','x',0,1); a34 = integrate('x^5','x',0,1); a41 = integrate('x^3','x',0,1); a42 = integrate('x^4','x',0,1); a43 = integrate('x^5','x',0,1); a44 = integrate('x^6','x',0,1); c1 = integrate('exp(x)','x',0,1); c2 = integrate('x*exp(x)','x',0,1); c3 = integrate('x^2*exp(x)','x',0,1); c4 = integrate('x^3*exp(x)','x',0,1); A = [a11 a12 a13 a14;a21 a22 a23 a24;a31 a32 a33 a34;a41 a42 a43 a44]; C = [c1;c2;c3;c4]; ann = inv(A)*C; disp(ann, 'The coefficients a0,a1,a2,a3 are respectively : ' ); deff('[px]=p3(x)','px=ann(4)*x.^3+ann(3)*x.^2+ann(2)*x+ann(1)'); x = [0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0]'; e = exp(x); p = p3(x); err = e-p; ann = [x e p err]; disp(ann,'Displaying the value of x exp(x) p3(x) exp(x)-p3(x) :'); plot(x,err); plot(x,zeros(length(x),1));
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errcatch(-1,"stop");mode(2);//Example 2.8.5 // limiting error ; ; //given data : del_A=2.5;// may be +ve or-ve in % As=400; FSD=600;// in volts del_A1=(del_A/100)*600; disp(del_A1,"del_A1 (V)=± ") e=(del_A1/As)*100; disp(e,"limiting error,e(%) = ") exit();
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clc //Chapter 1 Signals //Example 1.6, page no 21 //given t0=1,T=1,w0=2*3.14/T,P=1 t=0:0.1:1 f=P*t// function f(t)=P*t, 0<t<1 a=1 disp('The Exponential Fourier coeff(Fn) are:for n=-5 to 5') for n=-5:5// Calculating the fourier coeff fr=f.*cos(%pi*n*t/T) Fr(a)=inttrap(t,fr) fi=f.*sin(%pi*n*t/T) Fi(a)=inttrap(t,fi) if Fr(a)<0.01 then Fr(a)=0 end if Fi(a)<0.01 then Fi(a)=0 end disp(Fr(a)-%i*Fi(a)) a=a+1 end mprintf('The given function in Expo Fourier series can be represented as \n') mprintf('f(t)= %f+jP/2*pi* ∑1/n *exp(j2*pi*t)',P/2)
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//To determine the d.c. output voltage when delay anglw (a)0 (b)30 (c)45 clear clc; Vo=3*sqrt(2)*110/%pi; Vd=Vo*(cosd(0) + cosd(15))/2; Vd1=Vo*(cosd(30) + cosd(45))/2; Vd2=Vo*(cosd(45) + cosd(60))/2; mprintf("(a)For a=0, Vd=%.2f kV\n",Vd); mprintf("(b)For a=30,Vd=%.2f kV\n",Vd1); mprintf("(c)For a=45,Vd=%.2f kV\n",Vd2);
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; @Harness: simulator ; @Format: atmel ; @Arch: avr ; @Purpose: "Test the SUBI (subtract immediate from register) instruction" ; @Result: "flags.h=1, flags.s=0, flags.v=0, flags.n=0, flags.z=0, flags.c=0, r16 = 8" start: ldi r16, 0b00010000 subi r16, 0b00001000 end: break
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clc //For normally consolidated clay, c' = 0. a=30 T3=10 T1=T3*(tand(45+a/2))^2 Tf=T1-T3 printf('The deviator stress at failure = %f lb/in^2',Tf)
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<?xml version="1.0" encoding="utf-8"?> <test> <description>NavierStokes, restart from file, BCs from file, WeakDG, GLL</description> <executable>CompressibleFlowSolver</executable> <parameters> hump3D_GLL.xml </parameters> <files> <file description="Session File">hump3D_GLL.xml </file> <file description="Session File">hump3D_b1.bc</file> <file description="Session File">hump3D_b2.bc</file> <file description="Restart File">hump3D.rst</file> </files> <metrics> <metric type="L2" id="1"> <value variable="rho" tolerance="1e-12">1.95793e-05</value> <value variable="rhou" tolerance="1e-12">0.0161709</value> <value variable="rhov" tolerance="1e-12">1.02091e-07</value> <value variable="rhow" tolerance="1e-12">0.000238819</value> <value variable="E" tolerance="1e-12">45.8424</value> </metric> <metric type="Linf" id="2"> <value variable="rho" tolerance="1e-12">0.0608055</value> <value variable="rhou" tolerance="1e-12">55.621</value> <value variable="rhov" tolerance="1e-7">0.0616451</value> <value variable="rhow" tolerance="1e-12">0.444359</value> <value variable="E" tolerance="1e-12">60454.3</value> </metric> </metrics> </test>
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//Electric Drives:concepts and application by V.Subrahmanyam //Publisher:Tata McGraw-Hill //Edition:Second //Ex1_2 clc; clear; V1=400;//supply voltage is V I1=70;//Current in A N1=78.5;//speed in rad/sec R1=0.3;//resistance in ohm I2=90;//current in A N2=31.4;//Speed in rpm Eb1=V1-(I1*R1); T1=(Eb1*I1)/N1; V2=V1+Eb1; R2=(V2/I2)-R1; T2=(Eb1*I2)/N1; Eb2=(Eb1*N2)/N1; I=(V1+Eb2)/R2; T=(Eb2+I)/N2; disp(T,'The initial breaking torque in Nm is:') //Calculation error in the textbook
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errcatch(-1,"stop");mode(2);; ; disp(10^1.6,'ans for part a :- '); disp(%e^0.04,'ans for part b :- '); exit();
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//Example 6 Page 86 clc clear function s=S(t)//function for s(t) s=54*t+20 endfunction t=[0 0.5 1 1.5 2]//values of t given in question disp(t,'time(h)')//displaying the t values s=S(t);//function calling disp(s,'marker(mi)')//displaying the s values plot(t,s,'blue')//plotting the graph xtitle('','Time(hours)','Location(miles)')//naming the axes
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//Ex 3.16 page 128 clc; clear; close; n=3;// no. of phase Vs=400;// V f=50;// Hz Ls=5/1000;// H Io=20;// A Ri=1;// ohm Vdc=400;// V Vo=Vdc+Io*Ri;// V // Vo=3*Vm/%pi*cos(alpha*%pi/180)-3*2*%pi*f*Ls/%pi*Io Vm=sqrt(2)*Vs;// V alpha=acos((Vo+3*2*%pi*f*Ls/%pi*Io)/(3*Vm/%pi))*180/%pi;// degree // Vo=3*Vm/%pi*cos((alpha+mu)*%pi/180)-3*2*%pi*f*Ls/%pi*Io mu=acos((Vo-3*2*%pi*f*Ls/%pi*Io)/(3*Vm/%pi))*180/%pi-alpha;// degree printf('\n Firing angle = %.2f degree',alpha) printf('\n Overlap angle = %.2f degree',mu) // ans in the textbook is not accurate.
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r = read('/home/alisa/rosws/src/youbot_arm_kinematics/scripts/youbot_furier_goal.txt', -1, 2) plot(r(:,1), r(:,2)) scf r = read('/home/alisa/rosws/src/youbot_arm_kinematics/scripts/youbot_furier_mes.txt', -1, 4) plot(r(:,4), [r(:,1), r(:,2)])
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clear all; clc; disp("Scilab Code Ex 1.13 : ") //Given: shear_allow = 90; //MPa tensile_allow = 115; //MPa l_AP = 2; //m l_PB = 1; //m resultant_A = 5.68; //kN resultant_B = 6.67; //kN v_a = 2.84; //kN v_b = 6.67; //kN //Diameter of the Pins: A_A = (v_a*10^3)/(shear_allow*10^6); //Area of pin A da = (sqrt((4*A_A)/%pi))*10^3 // d = (square root of(area*4/pi)) in mm A_B = (v_b*10^3)/(shear_allow*10^6) ; //Area of pin B db = (sqrt((4*A_B)/%pi))*10^3 // Area = (%pi\4)d^2 in mm^2 chosen_da = ceil(da); chosen_db = ceil(db); //Diameter of Rod: A_bc = (resultant_B*10^3)/(tensile_allow*10^6); //Area of BC dbc = (sqrt((4*A_bc)/%pi)*10^3); // Area = %pi\4)d^2 chosen_dbc = ceil(dbc); //Displaying Results: printf ("\n\n The diameter of pin A = %.3f mm",da); printf ("\n The diameter of pin B = %.3f mm",db); printf ("\n The diameter of rod BC = %.2f mm",dbc); printf ("\n\n\nThe chosen diameters are: "); printf ("\n The diameter of pin A = %.3f mm",chosen_da); printf ("\n The diameter of pin B = %.3f mm",chosen_db); printf ("\n The diameter of rod BC = %.2f mm",chosen_dbc); //-----------------------------------------------------------------------END--------------------------------------------------------------------
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//Chapter-4, Illustration 11, Page 142 //Title: Gears and Gear Drivers //============================================================================= clc clear //Input data Ta=40// no of teeth on gear A Td=90// no of teeth on gear D //Calculations Tb=(Td-Ta)/2// no of teeth on gear B Tc=Tb// no of teeth on gear C // //x+y=-1 //-40x+90y=45 A=[1 1 -Ta Td]//Coefficient matrix B=[-1 (Td/2)]//Constant matrix X=inv(A)*B//Variable matrix // //x+y=-1 //-40x+90y=0 A1=[1 1 -Ta Td]//Coefficient matrix B1=[-1 0]//Constant matrix X1=inv(A1)*B1//Variable matrix disp(X(2)) printf('speed of the arm = %.3f revolution clockwise',X1(2))
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// Chapter9 // value of Rf // Page.No-313 // Example9_4 //Figure 9.15 // Given clear;clc; C=0.1*10^-6; //in F R=1000; //in Ohm Av=-29; Rf=-Av*R; printf("\n The value for Rf is = %.0f Ohm\n",Rf); // Result f=1/(2*%pi*6^0.5*R*C); printf("\n The frequency ,fo = %.0f Hz\n",f); // Result
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//Neural computation //basic functions function [VO]=VDIS(e,VI) TE=max(size(VI)); VO=zeros(1,TE); for elem=1:TE VO(elem)=e; end endfunction function [MO]=MDIS(e,MI) [TR,TC]=size(MI); MO=zeros(TR,TC); for r=1:TR for c=1:TC MO(r,c)=e; end end endfunction function s=SumM(M) [TR,TC]=size(M); s=0; for r=1:TR for c=1:TC s = s + M(r,c); end end endfunction function y=FGauss(x,cm,lambda) y=exp(-(x-cm)^2/lambda); endfunction function [MO]=EVFGauss(MI,cm,lambda) //Gaussian function for all the elements of the matrix [TR, TC]=size(MI); MO=zeros(TR,TC); for r=1:TR for c=1:TC MO(r,c)=FGauss(MI(r,c),cm,lambda); end end endfunction function [MO]=MADD(MI1,MI2) [TR, TC]=size(MI1); MO=zeros(TR,TC); for r=1:TR for c=1:TC MO(r,c)=MI1(r,c)+MI2(r,c); end end endfunction function [MO]=MSUB(MI1,MI2) [TR, TC]=size(MI1); MO=zeros(TR,TC); for r=1:TR for c=1:TC MO(r,c)=MI1(r,c)-MI2(r,c); end end endfunction function [MO]=MMUL(MI1,MI2) [TR, TC]=size(MI1); MO=zeros(TR,TC); for r=1:TR for c=1:TC MO(r,c)=MI1(r,c)*MI2(r,c); end end endfunction function [row,column]=CMC(MI) [TR, TC]=size(MI); //Rows s1=0;s2=0; for r=1:TR aux=0; for c=1:TC aux = MI(r,c) + aux; end s1 = s1 + aux*r; s2 = s2 + aux; end row = s1/s2; //Column s1=0;s2=0; for c=1:TC aux=0; for r=1:TR aux = MI(r,c) + aux; end s1 = s1 + aux*c; s2 = s2 + aux; end column=s1/s2; endfunction //*************** Artificial Neural System ****** function [sa]=NGauss(sa) lambda=0.14; cm=0.25; sa=FGauss(sa,cm,lambda); endfunction function [y,sa]=ANSV1(e,sa) W1=[0.1 0.2 0.3; 0.6 0.5 0.4; 0.7 0.8 0.9]; //W2=[0.1 0.2 0.3; 0.6 0.5 0.4; 0.7 0.8 0.9]; W2=[0 0.0182 0; 0.6814 0 0.2645; 0 0.9984 0]; //A1=[-0.3 -0.7 0.48; -0.7 -0.2 0.5; 0.2 0 0.9]; //A1=[0 0 0; 0.350 1 0; 0.350 0 0.550]; A1=[0 0 1;1 0 1; 0 1 0]; Maux=zeros(3,3); [MO]=MDIS(e,Maux); [MO1]=MSUB(MO,W1); [sa]=NGauss(sa); [MO]=MDIS(sa,Maux); [MO2]=MSUB(MO,W2); [Maux]=MADD(MO1,MO2); [MO]=EVFGauss(Maux,0.0,0.15); [MO1]=MMUL(MO,A1); s1=SumM(MO1); s2=SumM(MO); y=s1/(s2+0.00000052); endfunction function [Rep]=plotbehavior(e) sa=rand(); Rep=[]; for ti=1:250 [y,sa]=ANSV1(e,sa); Rep=[Rep; y]; end endfunction //Second experiment function [MO,sa]=ANSV2(e,sa) W1=[0.1 0.2 0.3; 0.6 0.5 0.4; 0.7 0.8 0.9]; W2=[0.1 0.2 0.3; 0.6 0.5 0.4; 0.7 0.8 0.9]; //A1=[-0.3 -0.7 0.48; -0.7 -0.2 0.5; 0.2 0 0.9]; //A1=[0 0 0; 0.350 1 0; 0.350 0 0.550]; A1=[0.1 0.1 0.1; 0.10 1 0.1; 0.1 0 0.1]; Maux=zeros(3,3); [MO]=MDIS(e,Maux); [MO1]=MSUB(MO,W1); [sa]=NGauss(sa); //Chaotic neuron [MO]=MDIS(sa,Maux); [MO2]=MSUB(MO,W2); [Maux]=MADD(MO1,MO2); [MO]=EVFGauss(Maux,0.0,0.15); [MO]=MMUL(MO,A1); //[row,column]=CMC(MO); //CM=[row column]; endfunction function [Rep]=plotbehavior2(e) //sa=rand(); sa=0; Rep=[]; for ti=1:500 [MO,sa]=ANSV2(e,sa); Rep=[Rep; MO(2,2)]; end //[Rep]=plotbehavior2(0.1); //plot(Rep(20:2500,1),Rep(20:2500,2),':*m') endfunction function [Rep]=plotbehavior3(e) //sa=rand(); sa=0; Rep=[]; for ti=1:450 [MO,sa]=ANSV2(e,sa); Rep=[Rep; MO(:,1:2)]; end for ti=1:50 [MO,sa]=ANSV2(e,sa); //Rep=[Rep; MO(:,1:2)]; Rep=[Rep; MO(2,1:2)]; end //[Rep]=plotbehavior2(0.1); //plot(Rep(20:2500,1),Rep(20:2500,2),':*m') endfunction function [Rep]=plotbehavior4(e) sa=rand(); Rep=[]; for ti=1:250 [y,sa]=ANSV1(e,sa); Rep=[Rep; y]; end //A perturbation is given sa=0; for ti=1:25 [y,sa]=ANSV1(e,sa); Rep=[Rep; y]; end endfunction function [Rep]=plotbehavior5() //Applying different stimulus sa=rand(); Rep=[]; for ti=1:100 [y,sa]=ANSV1(0.1,sa); Rep=[Rep; y]; end for ti=1:100 [y,sa]=ANSV1(0.5,sa); Rep=[Rep; y]; end for ti=1:100 [y,sa]=ANSV1(0.9,sa); Rep=[Rep; y]; end endfunction function Report3() [Rep]=plotbehavior(0.1); Xk=Rep(50:250); Xkmo=Rep(49:249); plot(Xkmo,Xk,':*b'); [Rep]=plotbehavior(0.5); Xk=Rep(50:250); Xkmo=Rep(49:249); plot(Xkmo,Xk,'-*g'); [Rep]=plotbehavior(0.9); Xk=Rep(50:250); Xkmo=Rep(49:249); plot(Xkmo,Xk,'.-*k'); legend('e=0.1','e=0.5','e=0.9') title('Performance of dynamic neural system with different stimmulus (e)') xlabel('X(k-1'); ylabel('Y(k-1'); endfunction function Report4() [Rep]=plotbehavior4(0.2); Xk=Rep(50:250); Xkmo=Rep(49:249); plot(Xkmo,Xk,':*b') Xk=Rep(250:275); Xkmo=Rep(249:274); plot(Xkmo,Xk,':*g') Xk=Rep(50:250); Xkmo=Rep(49:249); plot(Xkmo,Xk,':*b') title('Performance of dynamic neural system under perturbation (e=0.2)') xlabel('X(k)') ylabel('X(k+1)') endfunction function Report5() [Rep]=plotbehavior5(); Xk=Rep(2:300); Xkmo=Rep(1:299); plot(Xkmo,Xk,':*b') Xk=Rep(20:100); Xkmo=Rep(19:99); plot(Xkmo,Xk,':or') Xk=Rep(120:200); Xkmo=Rep(119:199); plot(Xkmo,Xk,':or') Xk=Rep(220:300); Xkmo=Rep(219:299); plot(Xkmo,Xk,':or') title('Performance of dynamic neural system considering continuous change of stimulus') xlabel('X(k)') ylabel('X(k+1)') endfunction
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//Net force// pathname=get_absolute_file_path('4.10.sce') filename=pathname+filesep()+'4.10-data.sci' exec(filename) u1=V-U u2=(V-U)*cosd(theta) v2=(V-U)*sind(theta) V1=V-U V2=V1 //X component of moment equation(in N): function y=f(A),y=u1*-(d*V1),endfunction function z=g(A),z=u2*d*V2,endfunction Rx=intg(0,A,f)+intg(0,A,g) //Y component of moment equation(in N): function a=h(A),a=v2*d*V1,endfunction Ry=intg(0,A,h) //This is after neglecting weight of vane and the water. printf("\n\nRESULTS\n\n") printf("\n\nNet force on the vane: %.3f i+%.2f j kN\n\n",Rx/1000,Ry/1000)
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//Discrete global uniKcD; uniKcD = 4.1; uniC = (s+0.1)/(s+2.1); uniGD = ss2tf(dscr(uniC,uni_Tc));
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sbci.instr.tst
; @Harness: disassembler ; @Result: PASS section .text size=0x00000054 vma=0x00000000 lma=0x00000000 offset=0x00000034 ;2**0 section .data size=0x00000000 vma=0x00000000 lma=0x00000000 offset=0x00000088 ;2**0 start .text: label 0x00000000 ".text": 0x0: 0x0f 0x47 sbci r16, 0x7F ; 127 0x2: 0x1f 0x47 sbci r17, 0x7F ; 127 0x4: 0x2f 0x47 sbci r18, 0x7F ; 127 0x6: 0x3f 0x47 sbci r19, 0x7F ; 127 0x8: 0x4f 0x47 sbci r20, 0x7F ; 127 0xa: 0x5f 0x47 sbci r21, 0x7F ; 127 0xc: 0x6f 0x47 sbci r22, 0x7F ; 127 0xe: 0x7f 0x47 sbci r23, 0x7F ; 127 0x10: 0x8f 0x47 sbci r24, 0x7F ; 127 0x12: 0x9f 0x47 sbci r25, 0x7F ; 127 0x14: 0xaf 0x47 sbci r26, 0x7F ; 127 0x16: 0xbf 0x47 sbci r27, 0x7F ; 127 0x18: 0xcf 0x47 sbci r28, 0x7F ; 127 0x1a: 0xdf 0x47 sbci r29, 0x7F ; 127 0x1c: 0xef 0x47 sbci r30, 0x7F ; 127 0x1e: 0xff 0x47 sbci r31, 0x7F ; 127 0x20: 0x0f 0x4f sbci r16, 0xFF ; 255 0x22: 0x00 0x40 sbci r16, 0x00 ; 0 0x24: 0x0f 0x47 sbci r16, 0x7F ; 127 0x26: 0x0f 0x43 sbci r16, 0x3F ; 0x63 0x28: 0x0f 0x41 sbci r16, 0x1F ; 0x31 0x2a: 0x0f 0x40 sbci r16, 0x0F ; 0x15 0x2c: 0x07 0x40 sbci r16, 0x07 ; 7 0x2e: 0x03 0x40 sbci r16, 0x03 ; 3 0x30: 0x01 0x40 sbci r16, 0x01 ; 1 0x32: 0x00 0x4f sbci r16, 0xF0 ; 240 0x34: 0x08 0x47 sbci r16, 0x78 ; 120 0x36: 0x0c 0x43 sbci r16, 0x3C ; 0x60 0x38: 0x0e 0x41 sbci r16, 0x1E ; 0x30 0x3a: 0x0c 0x4c sbci r16, 0xCC ; 204 0x3c: 0x06 0x46 sbci r16, 0x66 ; 102 0x3e: 0x03 0x43 sbci r16, 0x33 ; 0x51 0x40: 0x09 0x41 sbci r16, 0x19 ; 0x25 0x42: 0x0c 0x40 sbci r16, 0x0C ; 0x12 0x44: 0x06 0x40 sbci r16, 0x06 ; 6 0x46: 0x0a 0x4a sbci r16, 0xAA ; 170 0x48: 0x05 0x45 sbci r16, 0x55 ; 0x85 0x4a: 0x0a 0x42 sbci r16, 0x2A ; 0x42 0x4c: 0x05 0x41 sbci r16, 0x15 ; 0x21 0x4e: 0x0a 0x40 sbci r16, 0x0A ; 0x10 0x50: 0x05 0x40 sbci r16, 0x05 ; 5 0x52: 0x02 0x40 sbci r16, 0x02 ; 2 start .data:
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ch_3_eg_4.sce
a12=437.98*4.186, a21=1238*4.186, v1=76.92, v2=18.07 //calc of BPP clc disp("the soln of eg 3.4-->"); t=100 x1=.5, R=8.314 a1=16.678,b1=3640.2,c1=219.61 a2=16.2887,b2=3816.44,c2=227.02 x2=1-x1 p1sat=exp(a1-b1/(c1+t)) p2sat=exp(a2-b2/(c2+t)) h12=v2*exp(-a12/(R*(t+273.15)))/v1 h21=v1*exp(-a21/(R*(t+273.15)))/v2 m=h12/(x1+x2*h12)-h21/(x2+x1*h21) g1=exp(-log(x1+x2*h12)+x2*m) g2=exp(-log(x2+x1*h21)-x1*m) p=x1*g1*p1sat+x2*g2*p2sat disp(p,"boiling point pressure in kPa is"); //calc of BPT p=101.325,x1=.5, e=1 x2=1-x1 t1sat=b1/(a1-log(p))-c1 t2sat=b2/(a2-log(p))-c2 tnew=x1*t1sat+x2*t2sat while e>10^-4 do told=tnew, p1sat=exp(a1-b1/(c1+told)),p2sat=exp(a2-b2/(c2+told)), p1sat=p/(g1*x1+g2*x2*(p2sat/p1sat)) tnew=b1/(a1-log(p1sat))-c1, e=abs(tnew-told) end disp(tnew,"boiling point temperature in Celsius is"); //calc of dpp e1=1, e2=1, e3=1, pold=1 t=100,y1=.5 y2=1-y1 p1sat=exp(a1-b1/(c1+t)) p2sat=exp(a2-b2/(c2+t)) g1=1, g2=1, g11=1, g22=1 pnew=1/(y1/(g1*p1sat)+y2/(g2*p2sat)) while e1>.0001 do pold=pnew, while e2>.0001& e3>.0001 do g1=g11,g2=g22, x1=y1*pold/(g1*p1sat) x2=y2*pold/(g2*p2sat) x1=x1/(x1+x2) x2=1-x1 h12=v2*exp(-a12/(R*(t+273.15)))/v1 h21=v1*exp(-a21/(R*(t+273.15)))/v2 m=h12/(x1+x2*h12)-h21/(x2+x1*h21) g11=exp(-log(x1+x2*h12)+x2*m) g22=exp(-log(x2+x1*h21)-x1*m) e2=abs(g11-g1), e3=abs(g22-g2) end pnew=1/(y1/(g1*p1sat)+y2/(g2*p2sat)) e1=abs(pnew-pold) end disp(pnew,"dew point pressure in kPa is"); //calc dpt p=101.325,y1=.5, e4=1, e5=1,e6=1 y2=1-y1 t1sat=b1/(a1-log(p))-c1 t2sat=b2/(a2-log(p))-c2 tnew=y1*t1sat+y2*t2sat g11=1, g22=1 while e4>.0001 do told=tnew, p1sat=exp(a1-b1/(c1+told)) p2sat=exp(a2-b2/(c2+told)), while e5>.0001 & e6>.0001 do g1=g11, g2=g22, x1=y1*p/(g1*p1sat) x2=y2*p/(g2*p2sat) x1=x1/(x1+x2) x2=1-x1 h12=v2*exp(-a12/(R*(t+273.15)))/v1 h21=v1*exp(-a21/(R*(t+273.15)))/v2 m=h12/(x1+x2*h12)-h21/(x2+x1*h21) g11=exp(-log(x1+x2*h12)+x2*m) g22=exp(-log(x2+x1*h21)-x1*m) e5=abs(g11-g1), e6=abs(g22-g2) end p1sat=p*(y1/g1+y2*p1sat/(g2*p2sat)) tnew=b1/(a1-log(p1sat))-c1 e4=abs(tnew-told) end disp(tnew,"dew point temperature in Celsius is");
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Example35_2.sce
//Given that n1 = 1.6 n2 = 1.00 R = -3.0 //in mm i = -5.0 //in mm //Sample Problem 35-2 printf("**Sample Problem 35-2**\n") //n1/d + n2/i = (n2-n1)/R d = n1/(- n2/i + (n2-n1)/R) printf("The real depth of the mosquito is %1.2fmm", d)
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11_3.sce
//example 11.3 clc; funcprot(0); // Initialization of Variable b=2.0; a=4.0; gamm=9.8*10^3;//gamma pi=3.14; Fr=integrate('gamm*sin(pi*60/180)*b*y','y',6,10); yr=gamm*sin(pi*60/180)/Fr*b*integrate('y^2','y',6,10); disp(yr,"location of resultant weight in m"); //alternatively yr1=b*a^3/12/b/a/8+8; disp(yr1,"location of resultant weight in m"); clear()
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5_5.sce
clc //initialisation of variables clear T1= 25 //C T2= 100 //C dH1= -57.8 //kcal Cp1= 8.03 //cal deg^-1 Cp2= 6.92 //cal deg^-1 Cp3= 7.04 //cal deg^-1 //RESULTS Cp= Cp1-(Cp2+0.5*Cp3) dH2= Cp*10^-3*(T2-T1)+dH1 //RESULTS printf ('Stanadard heat of formation = %.2f kcal mole^-1',dH2)
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ising.sce
// importing all codes exec('ising.sci'); // running simulation for temperatures temperatures = [.5, 2.27, 5.] styles = ['b-', 'r-', 'g-'] for i=1:length(temperatures) do T = temperatures(i) // [lattice, energies, spins] = ising(n=200, nsteps=500000, H=0, J=1, T=1) [lattice, energies, spins] = ising(n=200, nsteps=50000, H=0, J=1, T=T) spins = spins ./ 200^2 // taking average spin per site plot(1:length(spins),spins,styles(i)) end legend(string(temperatures))
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ex_1_7.sce
//Ex 1.7 clc; clear; close; format('v',5); Iout=6;//micro A IREF=1.2;//mA VBE2=0.7;//V VT=26;//mV Beta=120;//unitless VCC=20;//V R=(VCC-VBE2)/IREF;//kohm disp(R,"Value of resistance R(kohm)") IC1=Iout;//micro A IC2=(IREF-IC1*10^-3/Beta)/(1+1/Beta);//mA RS=1/(IC1*10^-6)*VT*10^-3*log(IC2*1000/IC1);//ohm disp(RS/1000,"Value of resistance RS(kohm)");
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//Single-Sideband Communications : example 4-4 : (pg 187) a=455; x=2000+1; y=2000+3; c=2000+455; d=2455-2001; e=2455-2003; f=455-454; g=455-452; mprintf("\nRF and first mixer input: \n %.f kHz \n%.f kHz",x,y); printf("\nlocal oscillator = %.f kHz",c); mprintf("\nFirst mixer output: \n%.f kHz \n%.f kHz",d,e);//IF amp and second mixer input printf("\nBFO = %.f kHz",a); mprintf("\nSecond mixer output & audio amp: \n%.f kHZ \n%.f kHz",f,g);
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//Mission A4 //On récupère les deux images. pathname = "C:\Users\Jean-Guillaume P\Documents\Exia\A2\Projets\Imagerie\ExoLife\Images\Mission_A\Jupiter1.pbm"; pathname2 = "C:\Users\Jean-Guillaume P\Documents\Exia\A2\Projets\Imagerie\ExoLife\Images\Mission_A\Jupiter2.pbm"; jupiter1 = readpbm(pathname); jupiter2 = readpbm(pathname2); //On "extrait" le bruit des images. bruitJupiter = soustractionImage(jupiter1, jupiter2); //On soustrait le bruit obtenu précédemment de l'image de Jupiter. jupiterFinal1 = soustractionImage(jupiter1, bruitJupiter); //On "affine" l'image avec le filtre médian, faisant ainsi disparaître le bruit. jupiterFinal2 = filtreMedian(jupiterFinal1); // Affichage figure; display_gray(bruitJupiter); figure; display_gray(jupiterFinal1); figure; display_gray(jupiterFinal2); // Sauvegarde de l'image writepbm(jupiterFinal2, "C:\Users\Jean-Guillaume P\Documents\Exia\A2\Projets\Imagerie\ExoLife\Rendus\MissionA4.pbm");
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boardsize 4 play w g4 play b f5 play w e6 play b d7 play w c6 play b d6 play w e5 play b f4 play w g3 play b g2 play w f3 play b e4 play w d5 play b c5 play w b5 play b a4 play w b4 play b c4 play w d4 play b e3 play w f2 play b g1 play w f1 play b e2 play w d3 play b c3 play w b3 play b a3 play w a2 play b b2 play w c2 play b d2 play w e1 play b d1 play w c1 play b b1 1 havannah_winner #? [none] play w a1 2 havannah_winner #? [draw]
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25_6.sce
//clc() //f'(x,y) = -2*x^3 + 12*x^2 -20*x + 8.5 //f(x,y) = -x^4 / 2 + 4*x^3 - 10*x^2 + 8.5*x + 1 h = 0.5; x = 0:h:4; y1 = -x^4 / 2 + 4*x^3 - 10*x^2 + 8.5*x + 1; y(1) = 1; disp(x,"x =") disp(y1,"true value of y =") for i = 1:8 k1(i) = -2*x(i)^3 + 12*x(i)^2 -20*x(i) + 8.5; x1(i) = x(i) + h/2; k2(i) = -2*x1(i)^3 + 12*x1(i)^2 -20*x1(i) + 8.5; y(i+1) = y(i) + k2(i)*h; e(i) = (y1(i) - y(i))*100/y1(i); end disp(y(1:9),"y by midpoint method") disp(e,"error = ") for i = 1:8 k1(i) = -2*x(i)^3 + 12*x(i)^2 -20*x(i) + 8.5; x(i) = x(i) + 3*h/4; k2(i) = -2*x(i)^3 + 12*x(i)^2 -20*x(i) + 8.5; y(i+1) = y(i) + (k1(i)/3 + 2*k2(i)/3)*h; e(i) = (y1(i) - y(i))*100/y1(i); end disp(y(1:9),"y by second order Ralston RK") disp(e,"error = ")
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//Example 1.35// damping ration,damped natural frequency ,static sensivity and time constant clc; clear; close; k=1;//static sensivity wn=sqrt(30);//natural frequency in rad/s y=(0.1*wn)/2;//damping ratio wd=wn*sqrt(1-y^2);//damped natural frequency in rad/s t=(1/wn);//time constant in seconds disp(y,"damping ratio is") disp(wd,"damped natural frequency in rad/s is") disp(k,"static sensivity is") disp(t,"time constant in seconds is")
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// Electric Machinery and Transformers // Irving L kosow // Prentice Hall of India // 2nd editiom // Chapter 12: POWER,ENERGY,AND EFFICIENCY RELATIONS OF DC AND AC DYNAMOS // Example 12-10 clear; clc; close; // Clear the work space and console. // Given data V = 125 ; // Voltage rating of genrator in volt P_o = 12500 ; // Power rating of genrator in W P_hp = 20 ; // Power rating of motor in hp R_a = 0.1 ; // Armture resistance in ohm R_f = 62.5 ; // Field resistance in ohm P_var = 1040 ; // Rated variable electric loss in W // Calculations // case a P_in = P_hp * 746 ; // Power input to generator in W eta = P_o / P_in * 100 ; // Efficiency // case b V_f = V ; // Voltage across shunt field wdg in volt P_sh_loss = (V_f)^2 / R_f ; // Shunt field loss in W // case c V_L = V ; I_L = P_o / V_L ; // Line current in A I_f = V_f / R_f ; // Field current in A I_a = I_L + I_f ; // Armature current in A E_g = V_L + I_a*R_a ; // Generated EMF in volt P_d1 = E_g * I_a ; // Generated electric power in W P_f = V_f * I_f ; P_d2 = P_o + P_var + P_f ; // Generated electric power in W // case d P_d = P_d1; P_r = P_in - P_d ; // Rotational power losses in W // case e P_k = P_r + V_f*I_f ; // Constant losses in W Ia = sqrt(P_k/R_a); // Armature current in A for max.efficiency // case f I_a_rated = I_a ; // Rated armature current in A LF = Ia / I_a ; // Load fraction // case g rated_output = 12500 ; // Rated output in kW // Maximum efficiency eta_max = ( LF * rated_output ) / ( ( LF * rated_output ) + (2*P_k) ) * 100 ; // Display the results disp("Example 12-10 Solution : "); printf(" \n a: Efficiency :\n η = %f percent ≃ %.1f percent \n ",eta,eta); printf(" \n b: Shunt field loss :\n (V_f)^2/R_f = %d W \n ",P_sh_loss); printf(" \n c: Line current : I_L = %d A \n\n Field current : I_f = %d A",I_L,I_f); printf(" \n\n Armature current : I_a = %d A ",I_a); printf(" \n\n Generated EMF : E_g = %.1f V ",E_g); printf(" \n\n Generated electric power : "); printf(" \n 1. P_d = %d W \n\n 2. P_d = %d W \n ",P_d1,P_d2); printf(" \n d: Rotational power losses :\n P_r = %f W ≃ %.f W \n",P_r,P_r); printf(" \n e: Constant losses : P_k = %f W ≃ %.f W \n ", P_k ,P_k); printf(" \n Armature current for max.efficiency : I_a = %.1f A \n ",Ia); printf(" \n f: Load fraction : L.F. = %.2f \n ",LF); printf(" \n g: Maximum efficiency : η = %f percent ≃ %.2f percent",eta_max,eta_max);
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// Exa 2.7 clc; clear; close; // Given data miu_n= 3900;// in cm^2/Vs miu_p= 1900;// in cm^2/Vs ni= 2.5*10^10;// in /cm^3 Nge= 4.41*10^22;// in /cm^3 q=1.6*10^-19;// in C N_D= Nge/10^8;// in /cm^3 n=N_D;// approx p= ni^2/N_D;// in /cm^2 sigma= q*n*miu_n;// in (Ωcm)^-1 rho= 1/sigma;// in Ωcm disp(rho,"Resistivity of the doped germanium in Ωcm is : ")
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errcatch(-1,"stop");mode(2);//caption:find (a)system accuracy(b)system precision //Ex1.3 Tmin=100.3//minimum measured temperature at true value(in degree centigrate) Tmax=100.5//maximum measured temperature at true value(in degree centigrate) T1=100.4//measured temperature at true value(in degree centigrate) T2=100.3//measured temperature at true value(in degree centigrate) Tt=100//true value(in degree centigrate) A=((Tmax-Tt)/Tt)*100 disp(A,'(a)system accuracy(in %)=') M=(T1+Tmin+Tmax+T2)/4 Md=Tmax-M disp(Md,'(b)system precision(in %)=') exit();
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printf('K(ph)=2*pi/λph\n=ħ*ω/ħ*ν\n=Eg/ħ*ν'); //k-vector of a photon Eg=(1.5)*(1.6)*(10^-19); b=(1.05)*(10^-26); //say (ħ*ν)=b a=(Eg)/(b); printf('\nthe k-vector of photon for GaAs will be %f',a);
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clear close xdel(winsid()) // close all windows clc imOrigin = imread('images\finger.png'); [x,y] = size(imOrigin); for i = 1:x for j = 1:y im(i,j) = imOrigin(i,j,1); end end im2 = [cat(2, double(zeros(x,2)), double(im), double(zeros(x,2)))]; //adds 2 zeros columns to the right and left im2 = [cat(1, double(zeros(2, y+4)), double(im2), double(zeros(2, y+4)))]; //adds 2 lines of zeros to the right and left im2 = double(im2); im3 = im2; for i = 1:x+1 for j = 1:y+1 im3(i+1, j+1) = (im2(i,j)+ ... im2(i+1,j)+ ... im2(i+2,j)+ ... im2(i,j+1)+ ... im2(i+1,j+1)+ ... im2(i+2,j+1)+ ... im2(i,j+2)+ ... im2(i+1,j+2)+ ... im2(i+2,j+2))/9; end end mx = [-1 -2 -1; 0 0 0; 1 2 1]; //mask my = [-1 0 1; -2 0 2; -1 0 1]; imx = im3; imy = im3; for i=1:x+1 for j=1:y+1 imx(i+1, j+1) = im3(i, j) *mx(1, 1) + ... im3(i, j+1) *mx(1, 2) + ... im3(i, j+2) *mx(1, 3) + ... im3(i+1, j) *mx(2, 1) + ... im3(i+1, j+1)*mx(2, 2) + ... im3(i+1, j+2)*mx(2, 3) + ... im3(i+2, j) *mx(3, 1) + ... im3(i+2, j+1)*mx(3, 2) + ... im3(i+2, j+2)*mx(3, 3); imy(i+1, j+1) = im3(i, j) *my(1, 1) + ... im3(i, j+1) *my(1, 2) + ... im3(i, j+2) *my(1, 3) + ... im3(i+1, j) *my(2, 1) + ... im3(i+1, j+1)*my(2, 2) + ... im3(i+1, j+2)*my(2, 3) + ... im3(i+2, j) *my(3, 1) + ... im3(i+2, j+1)*my(3, 2) + ... im3(i+2, j+2)*my(3, 3); end end imMag = abs(imx)+abs(imy); imMag = imMag(3:$-2, 3:$-2); bigger = max(max(imMag)); [x,y] = size(imMag); for i = 1:x for j = 1:y if(imMag(i,j)) > 0.20*bigger; imMag(i,j) = 0; else imMag(i,j) = 255; end end end imshow(uint8(imMag));
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//ex1Q1 t = linspace(-1, 1, 100); x0 = linspace (-2, 2, 5); clf(); subplot(1, 2, 1); xtitle( 'cas a(x) = x','t','x') for i = 1 : 5 plot2d(t, x0(i) * exp(t) ,[i]); end; subplot(1,2,2); xtitle( 'cas a(x) = -x','t','x') for i = 1 : 5 plot2d(t, x0(i) * exp(-t), [i]); end; legends(['x0 = -2';'x0 = -1';'x0 = 0';'x0 = 1';'x0 = 2'],[1,2,3,4,5],opt="below"); //xs2pdf(gcf(),"Q1");
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errcatch(-1,"stop");mode(2);; ; // To calculate the relative permeability of ferromagnetic material H=220; //field in amp/m M=3300; //magnetisation in amp/m chi=M/H; mew_r=1+chi; printf("relative permeability is %f",mew_r); exit();
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// Data Reconciliation Benchmark Problems From Lietrature Review // Author: Edson Cordeiro do Valle // Contact - edsoncv@{gmail.com}{vrtech.com.br} // Skype: edson.cv // aux functions to sum of absolute errors // it is necessary to install the "diffcode" package using ATOMS in Scilab // smooth functions according to Gopal and Biegler // AICHE Journal 45(7) 1535-1547 - July 1999 // Quasi Weighted Robust function, according to Zhang et al. - Comp. & Chem. Eng. // 34, p. 154-162-402, (2010) function f = objfun ( x ) e1 = (xm(red)-x(red))./(var(red).^(0.5)); // smoothing functions // for sigmoidal function (Eq. 24 from paper) // abs_error = sum(sig1=1./alpha_smooth*log(2+exp(alpha_smooth*e1)+exp(-alpha_smooth*e1))); // for interior point function (Eq 25 from paper) abs_error = (e1.^2 + beta_smooth.^2).^0.5; // sigmoidal, but based in max operator property (Eq 28 from paper) // this one leads to a small error when e1 = 0 // abs_error = e1 + beta_smooth*log(1+exp(-2*alpha_smooth*e1)); f = sum( ((e1.^(2))./(2 + const_qw*abs_error)) ); endfunction // gradient of the objetive function function gf = gradf ( x ) // in the future we can express this function analytically // gf = diffcode_jacobian(objfun,x)'; gf = zeros(nv,1); sqrarg = const_qw.*sqrt(((xm(red)-x(red)).^2)./(var(red)) + beta_smooth.^2); sqrargdiv = sqrarg + 2; gf(red,1) = (sqrarg.*(xm(red)-x(red)))./(var(red).*sqrargdiv.^2) - (2*(xm(red)-x(red)))./(var(red).*sqrargdiv); endfunction function H = hessf ( x ) // For the robust functions, the lagrangean of the objective function is not constant // as in weigthed least squares. // in the future we can express this function analytically // H = diffcode_hessian(objfun,x); onesqw = ones(length(red),1); sqrarg = const_qw.*sqrt(((xm(red)-x(red)).^2)./(var(red)) + beta_smooth.^2); sqrarg2 = sqrarg./const_qw; sqrargdiv = sqrarg + 2; t1 = zeros (nv,1); t1(red,1) = -3.*const_qw.*((xm(red) - x(red)).^2)./((var(red).^2).*(sqrargdiv.^2).*sqrarg2) + 2*(const_qw.^2).*((xm(red) - x(red)).^2)./(var(red).*sqrargdiv.^3) - (sqrarg)./(var(red).*sqrargdiv.^2) + (2*onesqw)./(var(red).*sqrargdiv); H=diag(t1); endfunction
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syms G1 G2 G3 G4 H1 H2; T1=G1*G3*G2; T2=G4; L1=-G1*H1*G2; L2=-G3*H2*G2; L3=-G2*G1*G3; L4=-G4; L5=-G2*G4*H1*H2; delta=1-(L1+L2+L3+L4+L5) del1=1; del2=1 TF=(T1*del1 + T2*del2)/delta ; disp(TF,"C/R = ")
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function [X,dX] = steps(t,n,U,X0,dX0,start) dt=1/n; A=[ -1/dt, 0, 0; -1/dt^2,-1/dt, 0; -1/dt^3,-1/dt^2,-1/dt ]; B=[1/dt; 1/dt^2; 1/dt^3 ]; X = X0; dX = dX0; for i=[1+start:t+start] dX(i+1,1:3) = X(i,1:3)*A'+(B*U(i))' X(i+1,1) = X(i,1)+dX(i+1,1)*dt; X(i+1,2) = dX(i+1,1); X(i+1,3) = dX(i+1,2); end endfunction function [X,dX,P,U] = goals(amplitude, phase) m=100; T=[1:m+1]; P=sin((T-1)*2*%pi/20+phase)*amplitude; // Funzione di ingresso (sinusoidale con periodo 20 e max=amplitude (deg) ) // Stato iniziale e steps n=100; X=[0,0,0]; // Stato: Angolo, Velocità Angolare, Accelerazione Angolare dX=[0,0,0]; // Stato: Velocità Angolare, Accelerazione Angolare, Derivata Accelerazione Angolare for i=[1:m+1] U((i-1)*n+1:i*n)=X((i-1)*n+1) + (P(i)-X((i-1)*n+1))*([1:n]./n); // Funzione di ingresso (lineare a gradini) [X,dX]=steps(n,n,U,X,dX,(i-1)*n); end endfunction [X,dX,P,U]=goals(35, %pi/2); plot(X(1:size(X,1),1));
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//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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function [x,y,lam] = BVPeigen1(L,n) Dx = L/(n-1); x=[0:Dx:L]; a = 1/Dx^2; k = n-2; A = zeros(k,k); for j = 1:k A(j,j) = 2*a; end; for j = 1:k-1 A(j,j+1) = -a; A(j+1,j) = -a; end; exec eigenvectors.sce [yy,lam]=eigenvectors(A); //disp('yy');disp(yy); y = [zeros(1,k);yy;zeros(1,k)]; //disp('y');disp(y); xmin=min(x);xmax=max(x);ymin=min(y);ymax=max(y); rect = [xmin ymin xmax ymax]; if k>=5 then m = 5; else m = k; end endfunction
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clear; clc; close; function [tca,tcl]= prepara_arq() acha_arq= uigetfile("*.csv",pwd(),"ESCOLHA O ARQUIVO"); //achar arquivo ler_arq_matriz= csvRead(acha_arq); //ler arquivo como matriz [linha_arq,coluna_arq]=size(ler_arq_matriz); //recebe o número de linhas e colunas do arquivo tca=ler_arq_matriz; tcl=linha_arq; //recebe a matriz e a linha para h endfunction //usar a função que retorna a matriz e a quntidade de linhas [dados,h]= prepara_arq(); //separar x e y em 2 matrizes de uma coluna X= dados(:,1); y= dados(:,2); som1=0;som2=0;som3=0;som4=0; //SOMATÓRIO for i=1:1:h som1= som1+X(i,1)*y(i,1); som2= som2+X(i,1); som3= som3+y(i,1); som4= som4+(X(i,1)*X(i,1)); end //coef angular Ac=(som1-(1/h)*som2*som3)/(som4-(1/h)*som2*som2); //coef linear Al= (som3/h)-(Ac*som2/h); //DECLARAR Y2 y2= zeros(h,1); //servirá pra traçar a reta for i2=1:1:h y2(i2)=Ac*X(i2)+Al; end //EQUAÇÃO DA RELA LINEAR printf("\n\n\n EQUAÇÃO DA RETA LINEAR: \n"); printf("\n f(x)= %ix + %i",Ac,Al); //Plotagem e detalhes plot(X,y,'r+',X,y2); xtitle('GRÁFICO DA COTAÇÃO'); legend('Pontos-cotação','Reta linear que representa o conjunto de pontos'); xlabel('METRAGEM'); ylabel('VALOR COTADO');
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//=============================================================================== //Chapter 12 Example 6 clc;clear all; //variable declaration R2 = 400; //resistance of arm in Ω R3 = 400; //resistance of arm in Ω R4 = 400; //resistance of arm in Ω C4 = 2*10^-6; //capacitance in F r = 500; //resistance in Ω //calculations R1 = ((R2*R3)/(R4)); //resistance of coil in Ω x = (r*(R3+R4))+(R3*R4) L1 = (C4*R2*x)/(R3); //inductance of inductor in H //result mprintf("resistance of coil = %3.2f Ω",R1); mprintf("\ninductance of inductor = %3.2f Henry",L1);
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clear; clc Xd=.7 pf=.8 pfa=acos(pf) V=1 I0=1* exp( %i * pfa *-1) E0=V+ (%i * Xd * I0) E=round(abs(E0)*100)/100 d0=atand(imag(E0)/real(E0)) E0=E * exp(%i * d0 * %pi/180) Pe0=E*V*sind(d0)/Xd Qe0=(E*V*cosd(d0)/Xd)-(V*V/Xd) mprintf("\n(a)\nPe= %.1f Qe=%.1f E= %.2f load angle=%.1f",Pe0, Qe0, E, d0); e1=E0 E1=abs(e1) Pe1=1.2* Pe0; d1=asind(Pe1* Xd/ (V*E1)) Qe1=(E1*V*cosd(d1)/Xd)-(V*V/Xd) mprintf("\n(b)\nPe= %.2f Qe=%.2f E= %.2f load angle=%.1f",Pe1, Qe1, E1, d1); e2=1.2 * E0 E2=abs(e2) Pe2=Pe0; d2=asind(Pe2* Xd/ (V*E2)) Qe2=(E2*V*cosd(d2)/Xd)-(V*V/Xd) mprintf("\n(c)\nPe= %.1f Qe=%.2f E= %.2f load angle=%.1f",Pe2, Qe2, E2, d2);
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//To find exciting current and expess impedence in pu in both HV and LV sides clc; V_BHV=2000; I_BHV=10; Z_BHV=V_BHV/I_BHV; V_BLV=200; I_BLV=100; Z_BLV=V_BLV/I_BLV; I_o=3; a=V_BHV/V_BLV; I_oLV=I_o/100; disp(I_oLV,'I_o(LV)pu='); I_oHV=I_o/(a*10); disp(I_oHV,'I_o(HV)pu='); Z=complex(8.2,10.2); ZHV=Z/Z_BHV; disp(ZHV,'Z(HV)pu='); z=Z/a^2; ZLV=z/Z_BLV; disp(ZLV,'Z(LV)pu=');
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t = 486; mfull = 24500; mflow = 7; thrust = 280000; g = 9.81; a = thrust / ( mfull - mflow * t ) - g; a0 = thrust / ( mfull ) - g; s = a * t^2 / 2 * (1 + a/g ); s2 = a * t^2 / 2 * (1 + a/g ); a = thrust / ( mfull - mflow * t ) v = a* t t = mfull * v / ( thrust + mflow*v)
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//Example 24.6. perform the binary divisions clc x=bin2dec('110') x1=bin2dec('10') x2=x/x1 x3=dec2bin(x2) disp("(i) 110 / 10") disp(x3," = binary") disp(x2," = decimal") x=bin2dec('1111') x1=bin2dec('110') x2=x/x1 x3=dec2bin(int(x2)); disp("(ii) 1111 / 110") disp(x3," = binary") disp(x2," = decimal")
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//[s]=%pslss(d1,s2) //s=%pslss(s1,d2) ou s=p-s1 // s1 : systeme donne par sa representation d'etat // p : matrice de polynomes // //! // origine S Steer INRIA 1992 //! [a2,b2,c2,d2,x2,dom2]=s2(2:7), s=list('lss',a2,b2,c2,d1-d2,x2,dom2), //end
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mode(0) global Rc Sc Tc gamm u_old_old u_old r_old_old r_old y_old_old y_old u_new r_new y_new s=%s; z=%z; //TFcont = syslin('c',0.593/((47.21*s+1)*(1.373*s+1)));//second order //TFcont = syslin('c',0.594/(49.19*s+1))//first order TFcont = syslin('c',0.42/(35.61*s+1));//first order SScont = tf2ss(TFcont); Ts = 1; [B,A,k] = myc2d(SScont,Ts); //polynomials are returned [Ds,num,den] = ss2tf(SScont); num = clean(num); den = clean(den); // Transient specifications rise = 100; epsilon = 0.05; phi = desired(Ts,rise,epsilon); // Controller design Delta = [1 -1]; [Rc,Sc,Tc,gamm] = pp_im(B,A,k,phi,Delta);//with integral // initial values u_old_old = 0; u_old = 0; r_old_old = 0; r_old = 0; y_old_old = 0; y_old = 0;
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//Chapter 7_Operational Amplifier Characteristics //Caption : Temperature Coefficient //Example7.5: Determine the temperature coefficient of the input offset voltage for the bipolar differential amplifier having Vos=1.5 mV. What is the percentage change in the Vos per degree temperature change. //Solution: clear; clc; // temperature cofficient of the input offset voltage for the bipolar differential amplifier Vos is=dVos/dT=Vos/T; Vos=1.5*10^-3;//input offset voltage for bipolar differential transistor amplifier T=300;// assuming room temperature TC=Vos/T;// temperature cofficient of Vos //percentage change in the Vos per degree temperature change will be given by as follow: PC=(TC/Vos)*100;// percentage change(PC) in the Vos per degree temperature change disp('%per degree celcius',PC,'percentage change in the Vos per degree temperature change is:')
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// Scilab code Ex7.11: Pg:307 (2008) clc;clear; P = 3.2e+07/1.6e-013; // Power developed by the reactor, MeV E = 200; // Energy released by the reactor per fission, MeV n = P/E; // Number of fissions occuring in the reactor per second, per sec N = n*1000*3600; // Number of atoms or nuclei of Uranium 235 consumed in 1000 hours // Since the number of atoms in 235 g of Uranium is 6e+023 M = N/6e+023*235/1000; // Mass of Uranium 235 consumed in 1000 hours, kg printf("\nThe number of atoms of Uranium 235 undergoing fission per second = %4.1e ", N); printf("\nThe mass of Uranium 235 consumed in 1000 hours = %4.2f kg ", M); // Result // The number of atoms of Uranium 235 undergoing fission per second = 3.6e+024 // The mass of Uranium 235 consumed in 1000 hours = 1.41 kg
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exec('scilab-base-calculs-testexo3d.sce',-1)//to delete exec('scilab-base-calculs-testexo3a.sce',-1)//to delete exec('scilab-base-calculs-testexo3b.sce',-1)//to delete // set of values already taken D=union(union(A,B),C) // candidate values for element (i,j) E=[1:9];E(D)=[]
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## Test of strip blobs reduce command set echo read <roundup.fi strip --blobs --reduce write -
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//Integral de Monte Carlo //Integral de x^3dx em [0 1] clear n = 10; //numero de amostras u = rand(1,n); g = u.^3; I = mean(g)
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//Initialize possible constant values on users functions e = 2.718281; function index_menu = display_menu() disp("Select one of the following methods:"); disp("1) Roots Methods"); disp("2) Non Linear Methods"); disp("3) Linear Regression Method ") disp("4) Interpolation Direct Method") disp("5) Integration Trapezoidal") disp("6) Integration Roomberg") index_menu = input("Type the number of the numeric method you want to use: "); funcprot(0); endfunction; function index_sub_menu_roots = display_menu_roots() disp("Select one of the following methods:"); disp("1) Bisection Method"); disp("2) Secant Method"); disp("3) Newthon-Raphson Method"); disp("4) Bairstow Method"); disp("0) For going out of the program"); disp(""); index_sub_menu_roots = input("Type the number of the numeric method you want to use: "); endfunction; function index_submenu_non_linear = display_menu_non_linear() disp("Select one of the following methods:"); disp("1) Gauss Elimination With Partial Pivoting"); disp("2) Gauss Jordan"); disp("3) LU Decomposition"); disp("4) Gauss Seidel"); disp("0) For going out of the program"); disp(""); index_submenu_non_linear = input("Type the number of the numeric method you want to use: "); endfunction; function Index_Integration = display_menu_Integration() disp("Choose how do you want to type the Integration_Method"); disp("1) Enter the function to evaluate"); disp("2) Enther the values of the segments"); Index_Integration = input("Type how you want to enter the values for the Integration_Method: "); endfunction function Index_Romberg = display_menu_Romberg() disp("Choose how do you want to type the Romberg_Method"); disp("1) Enter the number of Iterations"); disp("2) Enther the minimum expected error"); Index_Romberg = input("Type how you want to enter the values for the Integration_Method: "); endfunction function bisection_method() // Ask for required data disp("Type the function to evaluate with the following format:"); disp(" y=a*x^n + b*x^(n-1) + c*x^(n-2) ..., where a, b, c are constants"); user_function = input("","string"); xl = input("xl value: "); xu = input("xu value: "); max_error = input("max error value in %")/100.0; //Initialize user function and required values deff('[y] = bisection(x)', user_function); output = ["iteration", "xl", "xu", "xm", "sign", "error"]; disp(output); _error = 1; //First iteration iteration = 1; xm = (xl + xu)/2; is_positive = bisection(xl)*bisection(xm) > 0; if(is_positive) then _sign = "+"; else _sign = "-"; end output = [" " + string(iteration), string(xl), string(xu), string(xm), _sign, "---"]; disp(output); //Next iterations while abs(_error) >= max_error then iteration = iteration + 1; prev_xm = xm; if(is_positive) then xl = prev_xm; else xu = prev_xm; end xm = (xl + xu)/2; is_positive = bisection(xl)*bisection(xm) > 0; if(is_positive) then _sign = "+"; else _sign = "-"; end _error = (xm - prev_xm)/xm; //Display values output = [" " + string(iteration), string(xl), string(xu), string(xm), _sign, string(abs(_error)*100) + "%"]; disp(output); end ri = xl-3:0.01:xu+3; plot(ri,bisection(ri)); plot(xm,bisection(xm),'o') endfunction function secant_method() // Ask for required data disp("Type the function to evaluate with the following format:"); disp(" y=a*x^n + b*x^(n-1) + c*x^(n-2) ..., where a, b, c are constants"); user_function = input("","string"); x0 = input("x0 value: ") x1 = input("x1 value: ") max_error = input("max error value in %")/100.0; //Initialize user function and required values deff('[y] = secant(x)', user_function); _error = 1; x2 = 0; iteration = 0; output = ["iteration", "xi-1", "xi", "f(xi-1)", "f(xi)", "xi+1", "error"]; disp(output); //Iterations while abs(_error) >= max_error then iteration = iteration + 1; f_x0 = secant(x0); f_x1 = secant(x1); x2 = x1 - f_x1*(x1-x0)/(f_x1-f_x0); _error = (x2 - x1)/x2; //Display values if(iteration <> 1) then output = [" " + string(iteration), string(x0), string(x1), string(f_x0), string(f_x1), string(x2), string(abs(_error)*100) + "%"]; else output = [" " + string(iteration), string(x0), string(x1), string(f_x0), string(f_x1), string(x2), " --- "]; end; disp(output); x0 = x1; x1 = x2; end ri = x0-3:0.01:x1+3; plot2d(ri,secant(ri)); plot(x1,0,'o'); endfunction function newton_method() // Ask for required data disp("Type the function to evaluate with the following format:"); disp(" y=a*x^n + b*x^(n-1) + c*x^(n-2) ..., where a, b, c are constants"); user_function = input("","string"); x0 = input("x0 value: ") max_error = input("max error value in % ")/100.0; //Initialize user function and required values deff('[y] = newton_raphson(x)', user_function); _error = 1; output = ["iteration", "xi", "f(xi)", "derivate f(xi)", "error"]; disp(output); //First interation iteration = 1; f_x0 = newton_raphson(x0); deriv_f_x0 = numderivative(newton_raphson, x0); x1 = x0 - f_x0/deriv_f_x0; output = [" " + string(iteration), string(x0), string(f_x0), string(deriv_f_x0), " --- "]; disp(output); //Next Iterations while abs(_error) >= max_error then iteration = iteration + 1; prev_x0 = x0; x0 = x1; f_x0 = newton_raphson(x0); deriv_f_x0 = numderivative(newton_raphson, x0); x1 = x0 - f_x0/deriv_f_x0; _error = (x0 - prev_x0)/x0; //Display values output = [" " + string(iteration), string(x0), string(f_x0), string(deriv_f_x0), string(abs(_error)*100) + "%"]; disp(output); end ri = x0-3:0.01:x0+3; plot(ri,newton_raphson(ri)); plot(x1,0,'o'); endfunction function bairstow_method() // Ask for required data disp("Type the coefficients of the polynomial in a decreasing order of the function degree :"); disp("[1, 2, 3, 4] means 1*x^3 + 2*x^2 + 3*x^1 + 4*x^0"); a_values = input(""); r0 = input("r0 value: "); s0 = input("s0 value: "); max_error = input("max error value in % ")/100.0; //Process data b_values = a_values; c_values = a_values; [matrix_x, matrix_y] = size(a_values); _error = 1; iteration = 1; r1 = r0; s1 = s0; while abs(_error) >= max_error then output = ["iteration", "initial r", "initial s"]; disp(output); output = [" ", string(iteration), string(r0), string(s0)]; disp(output); output = [" ", " a ", " b ", " c "]; disp(output); b_values(2) = a_values(2) + r0*b_values(1); c_values(2) = b_values(2) + r0*c_values(1); //Display n a,b, c values output = [" _1_ ", string(a_values(1)), string(b_values(1)), string(c_values(1))]; disp(output); //Display n-1 a,b,c values output = [" _2_ ", string(a_values(2)), string(b_values(2)), string(c_values(2))]; disp(output); for i = 3:matrix_y, b_values(i) = a_values(i) + r0*b_values(i-1) + s0*b_values(i-2); c_values(i) = b_values(i) + r0*c_values(i-1) + s0*c_values(i-2); output = [" _" + string(i) + "_ ", string(a_values(i)), string(b_values(i)), string(c_values(i))]; disp(output); end b0 = b_values(matrix_y); b1 = b_values(matrix_y - 1); c1 = c_values(matrix_y - 1); c2 = c_values(matrix_y - 2); c3 = c_values(matrix_y - 3); delta_r = (-b0/c1 + c2*b1/(c1*c3))/(1-(c2^2)/(c1*c3)) delta_s = (-b0-c1*delta_r)/c2; r1 = r0 + delta_r; s1 = s0 + delta_s; _error_r = (r1-r0)/r1; _error_s = (s1-s0)/s1; if(abs(_error_r) > abs(_error_s)) then _error = _error_r; else _error = _error_s; end output = [" ", " delta r ", " delta s ", " r ", " s ", "error r", "error s"]; disp(output); output = [" ", string(delta_r), string(delta_s), string(r1), string(s1), string(_error_r*100) + "%", string(_error_s*100) + "%"]; disp(output) iteration = iteration + 1; r0 = r1; s0 = s1; end root_1 = r1/2 + sqrt(r1^2+4*s1)/2; root_2 = r1/2 - sqrt(r1^2+4*s1)/2; output = "Root values"; disp(output); disp(root_1); disp(root_2); endfunction function Partial_Pivoting_Method() //Partial Pivoting Method disp("Partial_Pivoting_Method Function Executing"); matrix_A = input("Define matrix A"); matrix_B = input("Define matrix B"); n = size(matrix_A, "r"); for i=1: n actual_row_A = matrix_A(i,:); value_1_A = matrix_A(i,i); actual_row_B = matrix_B(i,:); for j=i+1: n next_row_A = matrix_A(j, :); value_2_A = matrix_A(j,i); matrix_A(j, :) = next_row_A - actual_row_A*value_2_A/value_1_A; next_row_B = matrix_B(j, :); matrix_B(j, :) = next_row_B - actual_row_B*value_2_A/value_1_A; end end //Now that we have the lower part with 0's, we must do the needed operations. starting from the bottom. for i = n : -1 : 1; for j = i+1 : n matrix_B(i) = matrix_B(i)-matrix_A(i,j)*matrix_B(j); end matrix_B(i) = matrix_B(i)/matrix_A(i,i); end disp("The solution for x is:") disp(matrix_B); //Partial_Pivotin_method endfunction function Gauss_Jordan_Method() //Gauss Jordan Method disp("Gauss_Jordan_Method Function Executing"); matrix_A = input("Define matrix A"); matrix_B = input("Define matrix B"); n = size(matrix_A, "r"); for i=1: n actual_row_A = matrix_A(i,:); value_1_A = matrix_A(i,i); actual_row_B = matrix_B(i,:); for j=i+1: n next_row_A = matrix_A(j, :); value_2_A = matrix_A(j,i); matrix_A(j, :) = next_row_A - actual_row_A*value_2_A/value_1_A; next_row_B = matrix_B(j, :); matrix_B(j, :) = next_row_B - actual_row_B*value_2_A/value_1_A; end matrix_A(i, :) = actual_row_A/actual_row_A(i); matrix_B(i, :) = actual_row_B/actual_row_A(i); end //Now that we have the lower part with zeros and the diagonal with 1s we must reduce the upper part and substract rows beginning from the bottom for i=n:-1:1 actual_row_A = matrix_A(i,:); value_1_A = matrix_A(i,i); actual_row_B = matrix_B(i,:); for j=i-1:-1:1 next_row_A = matrix_A(j, :); value_2_A = matrix_A(j,i); matrix_A(j, :) = next_row_A - actual_row_A*value_2_A/value_1_A; next_row_B = matrix_B(j, :); matrix_B(j, :) = next_row_B - actual_row_B*value_2_A/value_1_A; end end disp("La solución para x es:") disp(matrix_B); endfunction function LU_Decomposition() //LU Decomposition disp("LU_Decomposition Function Executing"); //Definir Matriz A matrix_A = input("Define matrix A "); //Definir Matriz B matrix_B = input("Define matrix B "); matrix_AO = matrix_A; matrix_BO = matrix_B; //n = Renglones n = size(matrix_A, "r"); [renglon,columna] = size(matrix_A); //Definir matriz L con 0 matrix_L = zeros(renglon,columna); //Definir matriz U con 0 matrix_U = zeros(renglon,columna); matrix_X = ones(n); matrix_Z = ones(n); matrix_Temp = ones(n); for i = 1 : n matrix_L(i,i) = 1; end for i=1: n //Sacar el i renglon de la matriz A actual_row_A = matrix_A(i,:); //Obtener el primer cada uno de los valores de la matriz value_1_A = matrix_A(i,i); //Sacar el i renglon de B actual_row_B = matrix_B(i,:); //Asigna los valores de la matriz U de la diagonal matrix_U(i,i) = value_1_A; for j = i+1 : n //Sacar el segundo renglon de A next_row_A = matrix_A(j, :); value_2_A = matrix_A(j,i); matrix_A(j, :) = next_row_A - actual_row_A*value_2_A/value_1_A; next_row_B = matrix_B(j, :); matrix_B(j, :) = next_row_B - actual_row_B*value_2_A/value_1_A; matrix_L(j,i) = value_2_A/value_1_A; end end matrix_U = matrix_A; for i=n :-1 : 1 actual_row_A = matrix_A(i,:); value_1_A = matrix_A(i,i); actual_row_B = matrix_B(i,:); for j=i-1:-1:1 next_row_A = matrix_A(j, :); value_2_A = matrix_A(j,i); matrix_A(j, :) = next_row_A - actual_row_A*value_2_A/value_1_A; next_row_B = matrix_B(j, :); matrix_B(j, :) = next_row_B - actual_row_B*value_2_A/value_1_A; end end matrix_Z(1) = matrix_BO(1); for i = 2 : n matrix_Z(i) = matrix_BO(i) for j = i-1 :-1 : 1 matrix_Z(i)=matrix_Z(i)-matrix_L(i,j)*matrix_Z(j); end end for i = n : -1 : 1 matrix_X(i) = matrix_Z(i); for j = i+1 : n matrix_X(i)=matrix_X(i)-matrix_U(i,j)*matrix_X(j); end matrix_X(i) = matrix_X(i)/matrix_U(i,i); end disp("A matrix"); disp(matrix_AO); disp("B matrix"); disp(matrix_BO); disp("L matrix"); disp(matrix_L); disp("Z values"); disp(matrix_Z); disp("U matrix"); disp(matrix_U); disp("X values"); disp(matrix_X); endfunction function Gauss_Seidel() disp("Gauss_Seidel Function Executing ..."); disp("In vector format {x1,x2,x3,x4,...,xn}") //ask for the initial values of the X values _new = input("Initial values for you X :") disp("introduce the constants of each equation in matrix style ") disp("For example: {A,B,C;D,E,F;G,H,I} representig a [3x3] matrix") matrixA = input("Matrix A : "); //get the size of the matrix _size = size (matrixA, "r") //ask for the equation in vector format disp("introduce the other side of the equaility") disp("For example: {A;B;C} for a matrix[1x3]") matrixB = input("Matrix B : "); _error = input("max error value in % ")/100.0; max_iterations = input("insert the max number of iterations"); //flag to detect that the error is less than the maxError maxError = _error + 1 actualError = zeros(_size,1) //flag to detect non Diagonal Dominant Matrix flagNonDiagonal = 0 //variable to save the sum of each row totalInLine = zeros(_size,1) //array of new and old values of all X variables i.e x1,x2..xn _old = zeros(_size, 1) iteration = 1 //verify that the matrix is Diagonally dominant for i = 1 : _size for j = 1 : _size if j <> i then totalInLine(i) = totalInLine(i) + matrixA(i,j) end end if matrixA(i,i) < totalInLine(i) then flagNonDiagonal = 1 end end //if its diagonal dominat proceed if flagNonDiagonal == 0 then //do the procedure until reaching a maxError value that is less than the set error while maxError > _error & iteration <= max_iterations then for i = 1 : _size //save the value of to get the error value _old(i) = _new(i) tmpX = 0 //sum of all values in row that are not in the main diagonal //and multiply each of them by their corresponding X value for j = 1 : _size if j <> i then tmpX = tmpX + _new(j) * matrixA(i,j) end end //get the newest value for the X that we are trying to find _new(i) = (matrixB(i) - tmpX) / matrixA(i,i) //get the error actualError(i) = abs((_new(i) - _old(i)) / _new(i)) if(i == 1) then maxError = actualError(i) end end //verify if this round got the maxError if(actualError(i) > maxError) then maxError = actualError(i) end //output setting sizeOfMatrixOutput = (_size + _size + 1) output = zeros(1,sizeOfMatrixOutput) output(1,1) = iteration for k = 2 : sizeOfMatrixOutput if k < (_size + 2) then //write the value of X output(1,k) = _new(k - 1) else //write the values of the errors posOfError = (k-_size-1) output(1,k) = actualError(posOfError) * 100 end end disp("| Iter | values of X {x1 .. xn} | Error {E1 .. En |}") disp(output) iteration = iteration + 1 end else disp("Could not proceed with the method, The main matrix is not Diagonally dominant"); end endfunction function Linear_Regression_Method() disp("Executing Linear_Regression_Method"); matrix_data = input("Insert a matrix of two columns, the first one for x values and the other one for y values. The number of rows is equal to the number of data points"); //Initialize the needed variables sum_xy = 0; sum_x = 0; sum_y = 0; sum_square_x = 0; n = size(matrix_data, "r"); a1 = 0; a0 = 0; for i = 1 : n sum_x = sum_x + matrix_data(i,1); sum_y = sum_y + matrix_data(i,2); sum_xy = sum_xy + matrix_data(i,1) * matrix_data(i,2); sum_square_x = sum_square_x + matrix_data(i,1) * matrix_data(i,1); plot(matrix_data(i,1), matrix_data(i,2), "ro"); end a1 = (n * sum_xy - sum_x * sum_y) / (n * sum_square_x - sum_x * sum_x); a0 = sum_y/n - a1 * sum_x/n; y_data = zeros(1,n); for i = 1 : n y_data(i) = matrix_data(i,1)*a1 + a0; end plot(matrix_data(:,1),y_data); disp("The result for a1 is "); disp(a1); disp("The result for a0 is "); disp(a0); endfunction function Interpolation_Direct_Method() disp("Executing Interpolation_DirectM"); disp("Type your table in matrix 2xN {1,2;3,4;5,6;7,8;9,10}") matrixA = input("insert you table : ") numOfRows = size (matrixA, "r") disp("MAX VALUE to chose " + string(matrixA(numOfRows,1)) + ", MIN VALUE to chose " + string(matrixA(1,1))) valueToFind = input("Introduce the value you want to find : ") order = input("Introduce the order you want to use, MAX ORDER = " + string(numOfRows - 1) + " : ") nearestValue = abs(matrixA(1,1) - valueToFind) nearestValuePos = 1 //extend 1 column matrix A to save wich are the neares values matrixA = cat(2, matrixA, zeros (numOfRows, 1)) matrixA(1,3) = nearestValue //finding the neareast values for i = 2 : numOfRows //get values from the x axis value = matrixA(i,1) - valueToFind matrixA(i,3) = value //compare them and try to find wich one is the closest to the value we want to find if abs(value) < nearestValue then nearestValue = abs(value) nearestValuePos = i end end //sort values in order to get the neareast values [sortedNeareastValues, originalPos] = gsort(abs(matrixA(:,3)),'g' ,'i') sizeOfsolveMatrix = order + 1 coefficients = zeros(sizeOfsolveMatrix, 1) b = zeros (sizeOfsolveMatrix, 1) solveMatrix = zeros (sizeOfsolveMatrix, sizeOfsolveMatrix) //get the coefficients of the polynomials for rowInCoefficients = 1 : sizeOfsolveMatrix coefficients(rowInCoefficients) = matrixA(originalPos(rowInCoefficients), 1) b(rowInCoefficients) = matrixA(originalPos(rowInCoefficients), 2) maxColumns = order + 1 for columns = 2 : maxColumns exponent = columns - 1 //coefficientes in column 1 will always be 1 solveMatrix(rowInCoefficients, 1) = 1 solveMatrix(rowInCoefficients, columns) = coefficients(rowInCoefficients)^(exponent) end end //solve the matrix x0 = inv(solveMatrix) * b //display value of the coefficientes of the polynomial disp("Coefficientes for the polynomial") for l = 1 : sizeOfsolveMatrix disp("a" + string(l) + " = " + string(x0(l))) end rowInx0 = rowInCoefficients total = 0 //get the value of the function after the substitution of the value that we want to find for rowInx0 = 1 : sizeOfsolveMatrix exponent = rowInx0 - 1 total = total + ( x0(rowInx0) * valueToFind^exponent) end //plot the equation x = matrixA(:,1) stringToDisplay = sprintf("X: %d, Y: %d", valueToFind, total); xstring( valueToFind, total, stringToDisplay ); plot(x, matrixA(:,2)) //plot the point we find where its X = valueToFind and Y = total plot(valueToFind, total, 'o') //display the value disp("value of the function evaluated ") disp(total) endfunction function Integration_Trapezoidal() disp("Executing Integration_Trapezoidal"); sel_menu = display_menu_Integration(); if sel_menu == 1 then disp("Type the function to evaluate with the following format:"); disp(" y=a*x^n + b*x^(n-1) + c*x^(n-2) ..., where a, b, c are constants"); user_function = input("","string"); deff('[y] = ffunction(x)', user_function); lower_lim = input("Insert the lower limit of the Integral : "); upper_lim = input("Insert the upper limit of the Integral : "); n_segments= input("Insert the number of segments :"); integral_range = upper_lim - lower_lim; h = integral_range/n_segments; // I = (b-a)/(2*n) {sumation functions} formula_h = h/2; //formula_h = (b-a)/(2*n) acum_function = 0; primerValorPol = 0; nValorPol = 0; sumation_functions = 0; for j = lower_lim : h : upper_lim acum_function = acum_function + ffunction(j); if j == lower_lim then primerValorPol = acum_function; //Guarda el valor de la funcion en el n valor elseif j == upper_lim then nValorPol = acum_function; //Guarda el valor de las funciones intermedias else sumation_functions = sumation_functions + acum_function; end acum_function = 0; end final_result = formula_h *(primerValorPol+(2*sumation_functions)+nValorPol); disp("Solution is"); disp(final_result); //plot x_values = lower_lim:.1:upper_lim x_values2 = lower_lim:h:upper_lim plot(x_values, ffunction) plot(x_values2, ffunction, '--') //Linea 44 elseif sel_menu == 2 then //n_segments= input("Insert the number of segments :"); x_values = input("Enter the X segments as following [1,2,3,...,n] : "); y_values = input("Enter the Y segments as following [1,2,3,...,n] : "); [x,n_segments] = size(x_values); if size(x_values) <> size(y_values) then disp("The segments of X are different that segments of Y Insert them again please"); elseif (size(x_values) == size(y_values)) then lower_X_lim = x_values(1,1); upper_X_lim = x_values(1,n_segments); lower_Y_lim = y_values(1,1); upper_Y_lim = y_values(1,n_segments); funct_h = (upper_X_lim - lower_X_lim)/(n_segments*2); sumation_middle_values = 0; for i = 2 : n_segments - 1 sumation_middle_values = sumation_middle_values + y_values(1,i); end final_result = funct_h * (lower_Y_lim + sumation_middle_values*2 + upper_Y_lim); disp("The result is"); disp(final_result); plot(x_values, y_values) //disp(upper_Y_lim,sumation_middle_values,lower_Y_lim); //disp(funct_h); else disp("Not a Correct Input"); end else disp("Not a Correct Input"); end endfunction function Integration_Romberg() //disp("Executing Integration_Trapezoidal"); //sel_menu = display_menu_Integration(); //if sel_menu == 1 then disp("Type the function to evaluate with the following format:"); disp(" y=a*x^n + b*x^(n-1) + c*x^(n-2) ..., where a, b, c are constants"); user_function = input("","string"); deff('[y] = ffunction(x)', user_function); lower_lim = input("Insert the lower limit of the Integral : "); upper_lim = input("Insert the upper limit of the Integral : "); iterations = input("Enter the number of Iterations : "); h_vector = zeros(iterations); i_matrix = zeros(iterations,iterations); prev_r_values = zeros(iterations); errors = zeros(iterations); for j = 1 : iterations cont_r_values = 0; h = upper_lim -lower_lim; if j == 1 then h_vector(1) = upper_lim - lower_lim; else h_vector(j) = h_vector(j-1)/2 end for i = 1 : iterations if i == 1 then acum_function = 0; primerValor = 0; nValor = 0; sumation_functions = 0; segments = 0; segments = (upper_lim - lower_lim) / h_vector(j); for r = lower_lim : h_vector(j) : upper_lim acum_function = acum_function + ffunction(r); if r == lower_lim then primerValor = acum_function; elseif r == upper_lim then nValor = acum_function; else sumation_functions = sumation_functions + acum_function; end acum_function = 0; cont_r_values = cont_r_values +1; end final_result = (h/(2*segments)) * (primerValor+(2*sumation_functions)+nValor); i_matrix(j,i) = final_result; i_results(j) = i_matrix(j,i); else if j <> 1 & i <= j then i_matrix(j,i) = (((4*(i-1))*(i_matrix(j,i-1))) - i_matrix(j-1,i-1))/ (4*(i-1)-1); i_results(j) = i_matrix(j,i); end end end if j > 1 then errors(j) = (i_results(j)-i_results(j-1))/i_results(j); end end x_values = lower_lim:.1:upper_lim plot(x_values, ffunction) for r = 1 :iterations x_values2 = lower_lim:h_vector(r):upper_lim plot(x_values2,ffunction,'--') end disp(i_matrix,"I Matrix :"); disp(i_matrix(iterations,iterations), "Final Result = ") disp(errors(iterations), "The error is : ") //elseif sel_menu == 2 then //disp("Type the function to evaluate with the following format:"); //disp(" y=a*x^n + b*x^(n-1) + c*x^(n-2) ..., where a, b, c are constants"); //user_function = input("","string"); //deff('[y] = ffunction(x)', user_function); //lower_lim = input("Insert the lower limit of the Integral : "); //upper_lim = input("Insert the upper limit of the Integral : "); //exp_error = input("Enter the expected error : "); //h_vector = zeros(iterations); //i_matrix = zeros(iterations,iterations); //prev_r_values = zeros(iterations); //errors = zeros(iterations); //cont = 0; //final_error = 100; //while final_error < exp_error , //End while //end //End if //end //End function endfunction function start() selected_menu = display_menu(); if selected_menu == 1 then disp("Roots Menu"); selected_method = display_menu_roots(); while selected_method <> 5 & selected_method <> 1 & selected_method <> 2 & selected_method <> 3 & selected_method <> 4 then disp("Invalid input, please try again"); selected_method = display_menu_roots(); end; if selected_method == 1 then disp("Executing Bisection Method"); bisection_method(); elseif selected_method == 2 then disp("Executing Secant Method"); secant_method(); elseif selected_method == 3 then disp("Executing Newthon-Raphson Method") newton_method(); elseif selected_method == 4 then disp('Executing Bairstow Method'); bairstow_method(); elseif selected_method == 5 then disp("Ending program"); end; elseif selected_menu == 2 then disp("Non Linear Menu"); selected_method = display_menu_non_linear(); while selected_method <> 5 & selected_method <> 1 & selected_method <> 2 & selected_method <> 3 & selected_method <> 4 then disp("Invalid input, please try again"); selected_method = display_menu_non_linear(); end; if selected_method == 1 then disp("Gauss Elimination With Partial Pivoting Method"); Partial_Pivoting_Method(); elseif selected_method == 2 then disp("Gauss Jordan Method"); Gauss_Jordan_Method(); elseif selected_method == 3 then disp("LU Decomposition Method") LU_Decomposition(); elseif selected_method == 4 then disp("Gauss Seidel Method"); Gauss_Seidel(); elseif selected_method == 0 then disp("Ending program"); end; //Funciones del ultimo parcial, no se agregaron en subMenu debido a las instrucciones elseif selected_menu == 3 then disp("Linear_Regression_Method"); Linear_Regression_Method(); elseif selected_menu == 4 then disp("Interpolation_Direct_Method"); Interpolation_Direct_Method(); elseif selected_menu == 5 then disp("Integration_Trapezoidal"); Integration_Trapezoidal(); elseif selected_menu == 6 then disp("Integration_Romberg"); Integration_Romberg(); //elseif selected_menu == 7 then // linear_regression(); end; endfunction;
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// Example 9.4 // Calculation of the maximum reach up to which the carrier orthogonality is preserved. // Page no 408 clc; clear; close; //Given data b=22*10^-27; // Power launched in port 1 T=1.28*10^-9; // Guard interval N=128; // Subcarriers f=78.125*10^6; // Frequency spacing between subcarriers // Bit rate of communication system I=T/(b*2*%pi*N*f); I=I*10^-3; //Displaying results in the command window printf("\n The maximum reach up to which the carrier orthogonality is preserved = %0.0f km ",I); // The answers vary due to round off error
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// Example 9.6 // Determine (a) System kilowatts (b) System frequency (c) kilowatt loads // carried by each machine // Page 361 clc; clear; close; // Given data Pres=440; // Resistive load PF=0.8; // Power factor Pind=200; // Induction motor power Palt=210; // Alternator bus load deltaPa=70; // Change in load for machine A f=60; // Frequency deltaPb=70; // Change in load for machine B deltaPc=70; // Change in load for machine C // (a) System kilowatts deltaPbus=Pres+PF*Pind; // Increase in bus load Psys=Palt+deltaPbus; // (b) System frequency GDa=(60.2-f)/deltaPa; // Governor droop for machine A GDb=(60.4-f)/deltaPb; // Governor droop for machine B GDc=(60.6-f)/deltaPc; // Governor droop for machine C // From the figure 9.18(b) deltaF=600/(350+175+116.6667) ; f2=f-deltaF; // (c) Kilowatt loads carried by each machine Pa2=deltaPa+350*deltaF; Pb2=deltaPb+175*deltaF; Pc2=deltaPc+116.6667*deltaF; // Display result on command window printf("\n System kilowatts = %0.0f kW ",Psys); printf("\n System frequency = %0.2f Hz",f2); printf("\n Kilowatt loads carried by machine A = %0.1f kW",Pa2); printf("\n Kilowatt loads carried by machine B = %0.1f kW",Pb2); printf("\n Kilowatt loads carried by machine C = %0.1f kW",Pc2);
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function []=affichage(C,ville1,ville2,d) RGB = ReadImage('C:\Program Files\scilab-5.2.1\contrib\france1.jpg'); [image, ColorMap] = RGB2Ind(RGB); FigureHandle = ShowImage(image, 'Example', ColorMap); coordIm=transform(C) if d>=100 then xstring(coordIm(1,2),coordIm(1,1),ville1) xstring(coordIm(2,2),coordIm(2,1),ville2) xpoly([coordIm(1,2),coordIm(2,2)],[coordIm(1,1),coordIm(2,1)],"lines",1); d=round(d); d=string(d)+" Km"; xstring((coordIm(1,2)+coordIm(2,2))/2,(coordIm(1,1)+coordIm(2,1))/2,d); else yhaut=max(coordIm(1,1),coordIm(2,1)); if yhaut=coordIm(1,1) then xhaut=coordIm(1,2);yhaut=yhaut+5;ybas=coordIm(2,1)-5;xbas=coordIm(2,2); villehaut=ville1;villebas=ville2; else yhaut=yhaut+5; xhaut=coordIm(2,2); ybas=coordIm(1,1)-5;xbas=coordIm(1,2); villehaut=ville2;villebas=ville1; end xstring(xhaut,yhaut,villehaut); xstring(xbas,ybas,villebas); xpoly([coordIm(1,2),coordIm(2,2)],[coordIm(1,1),coordIm(2,1)],"lines",1); d=round(d); d=string(d)+" Km"; xstring((xhaut+xbas)/2,(yhaut+ybas)/2,d); end endfunction
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Ch2_2_46.sce
clc disp("Example 2.46") printf("\n") disp("Find the capacitor value for full wave rectifier") printf("Given\n") Vdc=20 f=60 RL=500 r=0.1/(2*sqrt(3)) c=1/(4*sqrt(3)*r*f*RL) printf("Capacitor value =\t%e farad\n",c)
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# Simple distilation column test units SI $thermo = VirtualMaterials.Advanced_Peng-Robinson / -> $thermo thermo + PROPANE n-BUTANE ISOBUTANE n-PENTANE col = Tower.Tower() col.Stage_0 + 20 # twenty two stages` cd col.Stage_10 f = Tower.Feed() f.Port.T = 30 f.Port.P = 720 f.Port.MoleFlow = 10 f.Port.Fraction = .4 .05 .4 .15 f.Port cd ../Stage_0 l = Tower.LiquidDraw() l.Port.P = 700 l.Port.MoleFlow = 5 cond = Tower.EnergyFeed(0) reflux = Tower.StageSpecification('Reflux') reflux.Value = 1 cd ../Stage_21 l = Tower.LiquidDraw() l.Port.P = 730 reb = Tower.EnergyFeed(1) cd .. TryToSolve = 1 # start calculation # since there was little output here, I will put some profile stuff here L_MassFraction.PROPANE V_MoleFraction.ISOBUTANE L_MassFlow L_Viscosity L_StdVolFraction.PROPANE V_StdVolFraction.PROPANE L_VolumeFlow L_StdLiqVolumeFlow V_StdLiqVolumeFlow #Now lets test efficiencies Efficiencies #Make sure it works for zero flow in vap /col.Stage_0.v = Tower.VapourDraw() /col.Stage_0.v.Port.MoleFlow = 0.0 Efficiencies = 0.9 V_MoleFraction.PROPANE Efficiencies = 0.5 V_MoleFraction.PROPANE Efficiencies = :0 .3 1 .5 2 .7 3-19 .5 20-21 .8 V_MoleFraction.PROPANE #Per compound Efficiencies = :-2 .32 4 .18 8 .91 @PROPANE 0 .2 1 .4 2 .6 3-7 .7 @n-BUTANE 1 .3 4-5 .8 6- .4 @CARBON_DIOXIDE -3 .2 4 .6 V_MoleFraction.PROPANE #Switching compounds should not affect $thermo.PROPANE >> n-PENTANE Efficiencies = :-2 .32 4 .18 8 .91 @PROPANE 0 .2 1 .4 2 .6 3-7 .7 @n-BUTANE 1 .3 4-5 .8 6- .4 @CARBON_DIOXIDE -3 .2 4 .6 V_MoleFraction.PROPANE #Get rid of the generic efficiencies Efficiencies = :@PROPANE 0 .2 1 .4 2 .6 3-7 .7 17 .9 18 .9 @n-BUTANE 1 .3 4-5 .8 6- .4 @CARBON_DIOXIDE -3 .2 4 .6 V_MoleFraction.PROPANE #Delete a compound $thermo - ISOBUTANE V_MoleFraction.PROPANE #Now play with removing and adding stages Efficiencies = 1.0 /col.Stage_10 - 2 Efficiencies Efficiencies = :0 .9 1 .8 2 .9 3 .87 4 .98 5 .76 6 .9 7-14 .93 15- 1.0 /col.Stage_13 - 2 Efficiencies /col.Stage_3 - 2 Efficiencies #/col.Stage_3 + 2 #Efficiencies Efficiencies = :-2 .32 4 .18 8 .91 @PROPANE 0 .2 1 .4 2 .6 3-7 .7 @n-BUTANE 1 .3 4-5 .8 6- .4 @CARBON_DIOXIDE -3 .2 4 .6 /col.Stage_4 - 2 Efficiencies /col.Stage_0 - 2 Efficiencies #Now lets play with the P_Profile object Efficiencies = 1.0 TryToSolve = 0 /col.P_Profile.Values /col.LiquidDraw_0_l.P = /col.P_Profile.Values /col.P_Profile.Item0 = 700 /col.LiquidDraw_0_l.P /col.P_Profile.Values TryToSolve = 1 /col.LiquidDraw_0_l.P /col.P_Profile.Values TryToSolve = 0 /col.P_Profile.Item4 = 701 TryToSolve = 1 /col.LiquidDraw_0_l.P /col.P_Profile.Values /col.P_Profile.Item0 = cd /col.Stage_2 . + 2 cd /col /col.LiquidDraw_0_l.P /col.P_Profile.Values /col.LiquidDraw_13_l.P = /col.P_Profile.Item6 = /col.LiquidDraw_0_l.P /col.LiquidDraw_13_l.P /col.P_Profile.Values TryToSolve = 0 /col.P_Profile.Item0 = 700 /col.P_Profile.Item13 = 720 TryToSolve = 1 /col.LiquidDraw_0_l.P /col.LiquidDraw_13_l.P /col.P_Profile.Values #Degrees of subcooling /col.Stage_0.dsc = Tower.DegSubCooling() /col.Stage_0.l.Port /col.Stage_0.dsc.Port = 3 /col.Stage_0.l.Port /col.Stage_0.v = Tower.VapourDraw() /col.Stage_0.v.MoleFlow = 0.0 /col.Stage_0.v.Port /col.Stage_0.dsc.Port = 0 /col.Stage_0.v.Port /col.Stage_0.l.Port /col.Stage_0.dsc.Port = 2 /col.Stage_0.v.Port /col.Stage_0.l.Port copy /col paste / /col.LiquidDraw_0_l /colClone.LiquidDraw_0_l delete /col.Stage_0.dsc /col.Stage_0.v.Port /col.Stage_0.l.Port
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//Problem 1 //Calculate the wavelength of X-rays clear clc V=12400// Potential difference in V e=1.6*10^(-19)//charge on an electron in C h=6.626*10^(-34)//planck's constant in J-s c=3*10^(8)//velocity of light in m/s w=((h*c)/(e*V))*10^(10)// wavelength of X-rays in A printf('wavelength of X-rays = %.1f A',w)
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clc //Example 7.3 //Let wc be the energy stored in capacitor C=20*10^-6; R=10^6; t=0:0.001:0.5 v=100*sin(2*%pi*t) wc=0.5*C*v^2 plot(t,wc) xtitle('wC vs t','t in sec','wC in J') //Let iR be the current in the resistor iR=v/R //Let pR be the power dissipated in the resistor pR=iR^2*R //If wR is the energy dissipated in the resistor syms s wR=integ(100*(sin(2*%pi*s))^2,s,0,0.5) disp(wR,'wR=')
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//Example 5.15 clc;clear;close; format('v',6); G=100;//MVA f=50;//Hz delL=50;//MW Tc=0.4;//sec H=5;///kWs/kVA KE=G*1000*H;//kWs delKE=delL*1000*Tc;////kWs///due to decrease in load fnew=sqrt((KE+delKE)/KE) *f;//Hz fdev=(fnew-f)/f*100;//% disp(fnew,"New frequency(Hz)"); disp(fdev,"Frequency deviation(%)");
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//Début Q9* clear stacksize('max') T= 60 h = 1/1000 n = 21 N = T/h m = 0.5 for k = 1:n if modulo(k, 2) == 0 SM(k,:) = m else SM(k,:) = 1 end end M = diag(SM) X_0 = zeros(n,1) X_m1 = zeros(n, 1) X_m1(1,1) = -h function[S_M] = secondmembre(Y) S_M = zeros(n,1) S_M(1) = -max(Y(1) - Y(2), 0)**(1.5) for i= 2 : (n-1) S_M(i) = max(Y(i-1) - Y(i),0)**(1.5) - max(Y(i) - Y(i+1),0)**(1.5) end S_M(n) = max(Y(n-1) - Y(n), 0)**(1.5) endfunction function[F_y] = feulerimp(Y) F_y = M*(Y - 2*X_k + X_km1) - (h**2)*secondmembre(Y) endfunction function[X_kp1] = eulerimp(M, h) X_k = X_0 X_km1 = X_m1 X_kp1(:, 1) = X_k for k = 2 : N X_k1 = fsolve(X_k, feulerimp) X_kp1(:, k) = X_k1 X_km1 = X_k X_k = X_k1 end endfunction X= eulerimp(M,h) function[FC]= force_contact() for i = 1:n-1 FC(i,1) = max(X(i,1) - X_m1(i,1), 0)**(1.5) for k = 2 : N FC(i,k) = max(X(i,k) - X(i+1,k), 0)**(1.5) end end endfunction contc = force_contact() t = [0:h:(N-1)*h]' u = 0:1:n-2 Sgrayplot(u,t,contc) clear
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fir_design.sce
// code to design the FIR filters // ideal_BPF = ideal_LPF1 - ideal_LPF_2 with appropriate cutoff frequencies // get the impulse response of ideal_BPF and then use window (rectangular) // use functions defined to get all results // first, common parameters for both filters M = 37; // my filter design number delta = 0.15; // tolerance in passband and stopband B_tran = 4e3; // transition bandwidth in Hz //................................................... // parameters specific to the two filters // Filter 1: A Bandpass filter B_signal_analog_1 = 160e3; // bw of analog signal, inconsequential F_sampling_1 = 330e3; // sampling frequency in Hz for filter 1 filter_type_1 = 'bpf'; filter_nature_2 = 'bu'; //................................................... // Filter 2: Band Stop filter B_signal_analog_2 = 120e3; //analog signal BW in Hz F_sampling_2 = 260e3; // Sampling frequency in Hz filter_type_2 = 'bsf'; filter_nature_2 = 'ch'; //.................................................. // Normalized filter specifications criticalf_1 = un_norm_filter_edges(M, B_tran, filter_type_1); criticalf_2 = un_norm_filter_edges(M, B_tran, filter_type_2); //disp("Un-normalized Filter_1 (BPF) Specifications [fs1, fp1, fp2, fs2]:"); //disp(criticalf_1); //disp("Un-normalized Filter_2 (BSF) Specifications [fp1, fs1, fs2, fp2]:"); //disp(criticalf_2); criticalw_1 = get_critical_w(M, filter_type_1, B_tran, F_sampling_1); criticalw_2 = get_critical_w(M, filter_type_2, B_tran, F_sampling_2); //disp("Normalized Filter_1 (BPF) Specifications [ws1, wp1, wp2, ws2]:"); //disp(criticalw_1); //disp("Normalized Filter_2 (BSF) Specifications [wp1, ws1, ws2, wp2]:"); //disp(criticalw_2); //...................................................... A = -20*log10(delta); //disp("The value of A") //disp(A) del_wt_1 = criticalw_1(2)-criticalw_1(1); del_wt_2 = criticalw_2(2)-criticalw_2(1); //disp("Transition BW Filter 1:") //disp(del_wt_1) //disp("Transition BW Filter 2:") //disp(del_wt_2) l_min_1 = 1 + (A-8)/(2.285*del_wt_1); //=49.7 l_min_2 = 1 + (A-8)/(2.285*del_wt_2);//=39.4 addi_1 = 15; addi_2 = 13; len_trial_1 = ceil(l_min_1)+addi_1; // =50+addi_1 =65 for satisfying criteria len_trial_2 = ceil(l_min_2)+addi_2; // =40+addi_2 = 53 for satisfying criteria N_1 = (len_trial_1-1)/2; // 32 N_2 = (len_trial_2-1)/2; //26 //disp("Minimum length for Filter 1:") //disp(l_min_1) //disp("Minimum length for Filter 2:") //disp(l_min_2) n_max = 1000; // max time points (on each side of 0, ie num points =2n+1) to be working with, even for ideal filters n_axis = -n_max:n_max; w_axis = -3.14:0.001:3.14; // FILTER1: BPF w_cutoff_low_filter1 = (criticalw_1(2) + criticalw_1(1))/2 ; w_cutoff_high_filter1 = (criticalw_1(3) + criticalw_1(4))/2; // middle of transition band w_cutoff_low_filter2 = (criticalw_2(2) + criticalw_2(1))/2; w_cutoff_high_filter2 = (criticalw_2(3) + criticalw_2(4))/2; // obtain ideal LPF response for LPF with wp=wp2, wp1 and subtract h_ideal_wp2_filter1 = impulse_response_ideal_lpf(w_cutoff_high_filter1, n_max); h_ideal_wp1_filter1 = impulse_response_ideal_lpf(w_cutoff_low_filter1, n_max); h_ideal_bpf_filter1 = h_ideal_wp2_filter1 - h_ideal_wp1_filter1; h_ideal_wp2_filter2 = impulse_response_ideal_lpf(w_cutoff_high_filter2, n_max); h_ideal_wp1_filter2 = impulse_response_ideal_lpf(w_cutoff_low_filter2, n_max); h_ideal_delta_filter2 = impulse_response_ideal_lpf(%pi, n_max); h_ideal_bsf_filter2 = h_ideal_delta_filter2-(h_ideal_wp2_filter2 - h_ideal_wp1_filter2); // constant - bpf = bsf //plot(n_axis, h_ideal_bpf_filter1); //xlabel("n"); //ylabel("h[n] for ideal BPF") //title("Ideal BPF impulse response Filter 1") H_bpf_ideal = freq_transform(n_axis, w_axis, h_ideal_bpf_filter1); //plot(w_axis, abs(H_bpf_ideal)); H_bsf_ideal = freq_transform(n_axis, w_axis, h_ideal_bsf_filter2); //plot(w_axis, abs(H_bsf_ideal)); //............................................ // obtain the windowed Finite impulse response h_bpf_windowed = apply_window_h_ideal(h_ideal_bpf_filter1, N_1); //plot(n_axis(n_max-80:n_max+80),h_bpf_windowed(n_max-80:n_max+80)); //xlabel("n"); //ylabel("h_windowed[n]"); //title("Filter 1 (BPF) Impulse response after windowing "); //disp("Impulse response after applying window Filter1: BPF"); nonzero_indices_h_bpf_win = find(h_bpf_windowed); samples_h_bpf = h_bpf_windowed(nonzero_indices_h_bpf_win); //disp(samples_h_bpf); n_axis_reduced = -N_1:N_1; z = poly(0,'z'); assert_checkequal(length(n_axis_reduced), length(samples_h_bpf)); H_z_bpf = sum( samples_h_bpf.*(z^(-n_axis_reduced))); //disp("H(z) for Filter 1 BPF :"); //disp(H_z_bpf); name_1 = "FIR Bandpass Filter: Kaiser-Window "; //plot_H_z(H_z_bpf, criticalw_1, delta,name_1); h_bsf_windowed = apply_window_h_ideal(h_ideal_bsf_filter2, N_2); //plot(n_axis(n_max-80:n_max+80),h_bsf_windowed(n_max-80:n_max+80)); //xlabel("n"); //ylabel("h_windowed[n]"); //title("Filter 2 (BSF) Impulse response after windowing "); //title("Impulse response - windowed Filter 2 BSF"); //disp("Impulse response after applying window Filter2: BSF"); nonzero_indices_h_bsf_win = find(h_bsf_windowed); samples_h_bsf = h_bsf_windowed(nonzero_indices_h_bsf_win); //disp(samples_h_bsf); n_axis_reduced_bsf = -N_2:N_2; //z = poly(0,'z'); assert_checkequal(length(n_axis_reduced_bsf), length(samples_h_bsf)); H_z_bsf = sum( samples_h_bsf.*(z^(-n_axis_reduced_bsf))); name_2 = "FIR Bandstop Filter: Kaiser Window "; //plot_H_z(H_z_bsf, criticalw_2, delta, name_2); //disp("H(z) for Filter 2 BSF :"); //disp(H_z_bsf); // look at freq spectrum of windowed function //H_bpf_windowed = freq_transform(n_axis, w_axis, h_bpf_windowed); //plot(w_axis, abs(H_bpf_windowed)); // //set(gca(),"auto_clear","off"); //plot(w_axis,(1+delta)*ones(1,length(w_axis)),':'); // horizontal line at 1 //plot(w_axis,(1-delta)*ones(1,length(w_axis)),':'); // horizontal line at 1 //plot(w_axis,(delta)*ones(1,length(w_axis)),':'); // horizontal line at 1 //plot(criticalw_1(1)*ones(1, length(w_axis)), abs(H_bpf_windowed),':'); //plot(criticalw_1(2)*ones(1, length(w_axis)), abs(H_bpf_windowed),':'); //plot(criticalw_1(3)*ones(1, length(w_axis)), abs(H_bpf_windowed),':'); //plot(criticalw_1(4)*ones(1, length(w_axis)), abs(H_bpf_windowed),':'); w_axis_new = 0.001:0.001:3.14; H_bpf_windowed = freq_transform(n_axis, w_axis_new, h_bpf_windowed); //bode(w_axis_new, H_bpf_windowed); mag_bpf = abs(H_bpf_windowed); phase_bpf = abs(atan(imag(H_bpf_windowed), real(H_bpf_windowed))); // tan-1(y/x) //h1 = gca(); //plot(w_axis_new, mag_bpf, 'r'); ////legend(["|H(w)|"]); //xlabel("w (normalized frequency)"); //ylabel("|H(w)|", "color",'r'); //h2 = newaxes(); //plot(w_axis_new, phase_bpf); //h2.filled="off"; //h2.y_location="right"; //ylabel("argH(w)", "color",'b') //set(gca(),"auto_clear","off"); ////legends(["|H(w)|";"arg(H(w))"]); //title("FIR Filter-1 (BPF) Frequency Response") H_bsf_windowed = freq_transform(n_axis, w_axis_new, h_bsf_windowed); mag_bsf = abs(H_bsf_windowed); phase_bsf = abs(atan(imag(H_bsf_windowed), real(H_bsf_windowed))); // tan-1(y/x) h1 = gca(); plot(w_axis_new, mag_bsf, 'r'); //legend(["|H(w)|"]); xlabel("w (normalized frequency)"); ylabel("|H(w)|", "color",'r'); h2 = newaxes(); plot(w_axis_new, phase_bsf); h2.filled="off"; h2.y_location="right"; ylabel("argH(w)", "color",'b') set(gca(),"auto_clear","off"); //legends(["|H(w)|";"arg(H(w))"]); title("FIR Filter-2 (BSF) Frequency Response"); //plot(w_axis, abs(H_bsf_windowed)); // //set(gca(),"auto_clear","off"); //plot(w_axis,(1+delta)*ones(1,length(w_axis)),':'); // horizontal line at 1 //plot(w_axis,(1-delta)*ones(1,length(w_axis)),':'); // horizontal line at 1 //plot(w_axis,(delta)*ones(1,length(w_axis)),':'); // horizontal line at 1 //plot(criticalw_2(1)*ones(1, length(w_axis)), abs(H_bsf_windowed),':'); //plot(criticalw_2(2)*ones(1, length(w_axis)), abs(H_bsf_windowed),':'); //plot(criticalw_2(3)*ones(1, length(w_axis)), abs(H_bsf_windowed),':'); //plot(criticalw_2(4)*ones(1, length(w_axis)), abs(H_bsf_windowed),':');
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n=1000; a=ones(n,n)+1000*eye(n,n); b=1000*ones(n,1); x=a\b; print(%io(2),max(abs(x-0.5))); quit;
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clc //initialisation of variables m= 5 //kg g= 9.8 //m/sec^2 k= 500 //N/m //CALCULATIONS x= m*g/k W= -m*g*x //RESULTS printf ('work interaction of spring = %.2f J',W)
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function[k]=fact(a) k=-1; if(a<0|a>200) disp("Invalid"); break; else if(a==1|a==0) k=1; else k=a*fact(a-1); end end endfunction a=4; p=fact(a); disp(p,'the value of 4! is')
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ex1.sce
//example 1 //maximum power generation by wind turbine clear clc V=10 //Average velocity of wind in m/s ke=(V^2/2)/1000 //exegy of the blowing air in kJ/kg D=12 //diameter of wind turbine in m d=1.18 //density of air in kg/m^3 M=d*%pi*D^2*V/4 //mass flow rate in kg/s p=M*ke //maximum power generated by wind turbine in kW printf("\n Hence, the maximum power generated by wind turbine is = %.1f kW. \n",p);
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latcfilt14.sce
//i/p arg x contains complex valued elements k=[0.2 0.3 0.4 1]; x=[1 2 3 4 5+5*%i 6 7]; [f,g] = latcfilt(k,x); disp(f); disp(g); //output // //!--error 10000 //dimension mis-match between k and v //at line 46 of function latcfilt called by : //[f,g] = latcfilt(k,x); // //matlab //Columns 1 through 3 // // 1.0000 + 0.0000i 2.7800 + 0.0000i 5.3680 + 0.0000i // // Columns 4 through 6 // // 8.7360 + 0.0000i 13.1040 + 5.0000i 17.4720 + 3.9000i // // Column 7 // // 21.8400 + 4.0400i // // Columns 1 through 3 // // 1.0000 + 0.0000i 2.7800 + 0.0000i 5.3680 + 0.0000i // // Columns 4 through 6 // // 8.7360 + 0.0000i 13.1040 + 5.0000i 17.4720 + 3.9000i // // Column 7 // // 21.8400 + 4.0400i
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Giza.sce
Name=Giza PlayerCharacters=King Tut BotCharacters=Sphynx.bot IsChallenge=true Timelimit=120.0 PlayerProfile=King Tut AddedBots=Sphynx.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=1 BotTeams=2 MapName=b4.map MapScale=5.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=true TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Tracking, Strafing WeaponHeroTag=Laser Beam DifficultyTag=2 AuthorsTag=faiNt` BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=true Description=HEADSHOTS ONLY // STRAFING ADDS TO SCORE GameVersion=1.0.7.2 ScorePerDistance=0.02 [Aim Profile] Name=At Feet 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=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill At Feet MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Bot Profile] Name=Sphynx DodgeProfileNames=Long Strafe FB DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=2.0 DodgeProfileMinChangeTime=1.5 WeaponProfileWeights=1.0;1.0;2.0;1.0;0.0;0.0;0.0;0.0 AimingProfileNames=At Feet;Low Skill At Feet;Low Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Watcher SeeThroughWalls=false NoDodging=false NoAiming=false [Character Profile] Name=King Tut MaxHealth=300.0 WeaponProfileNames=steezy shooter;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=700.0 MaxCrouchSpeed=500.0 Acceleration=5000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=320.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 [Character Profile] Name=Watcher MaxHealth=200.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=45.0 CrouchHeightModifier=0.69 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=20.000 HeadshotOnly=true DamageKnockbackFactor=3.0 MovementType=Base MaxSpeed=250.0 MaxCrouchSpeed=270.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=100.0 BrakingFrictionFactor=0.0 JumpVelocity=300.0 Gravity=1.0 AirControl=0.16 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=1.000 Z=1.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=1.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=100.0 MainBBRadius=26.0 MainBBHasHead=true MainBBHeadRadius=20.0 MainBBHeadOffset=40.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=160.0 ProjBBRadius=26.0 ProjBBHasHead=false ProjBBHeadRadius=20.0 ProjBBHeadOffset=15.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 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 [Dodge Profile] Name=Long Strafe FB MaxTargetDistance=100000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=1.0 MaxLRTimeChange=3.0 MinFBTimeChange=0.25 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.8 DamageReactionMinimumDelay=0.15 DamageReactionMaximumDelay=0.18 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.9 BlockedMovementReactionMin=0.05 BlockedMovementReactionMax=0.1 [Weapon Profile] Name=steezy shooter Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.046 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=1.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=7.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.05 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=1.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.1 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=Clamped Horizontal ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices 240.000000 54.000000 96.000000 614.000000 54.000000 96.000000 614.000000 54.000000 90.000000 240.000000 54.000000 90.000000 240.000000 -6.000000 96.000000 614.000000 -6.000000 96.000000 614.000000 -6.000000 90.000000 240.000000 -6.000000 90.000000 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//Example 8.1 clear; clc; //Given Kp=0.10;//equillibrium constant at 300K Pa=20;// Partial pressure of A in atm Pm=1.0;///partial pressure of M in atm T=300;//Temperature in K R=8.314;// gas constant in J K^-1 mol^-1 //To determine the free energy Qp=Pm/Pa;//reaction quotient delG=R*T*log(Qp/Kp);//free energy change mprintf('(a) delG = %f J mol^-1',delG); delG0=-R*T*log(Kp);//standard free energy in J mol^-1 mprintf('\n (b) standard free energy = %f J mol^-1',delG0); mprintf('\n (c) Since delG is negetive,the reaction proceeds spontaneously in forward direction') //end
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//A Textbook of Chemical Engineering Thermodynamics //Chapter 9 //Chemical Reaction Equilibria //Example 16 clear; clc; //Given: //Reaction: CO(g) + H2O(g) --> CO2(g) + H2(g) P = 1; //pressure in bar K = 1; //equilibrium constant of reaction //To calculate the fractional dissociation of steam //Basis: 1 mole water vapour present in reactant stream //Let e be the extent of reaction //(a). CO supplied is 100% in excess of the stoichiometric requirement //Mole fraction of components: //CO: (2-e)/3 //H20: (1-e)/3 //CO2: e/3 //H2: e/3 //e^2/{(1-e)(2-e)] = K = 1, so //3e-2 = 0; e = 2/3; mprintf('(a). The conversion of steam is %f percent',e*100); //(b). CO supplied is only 50% of the theoretical requirement //Mole fraction of components //CO: (0.5-e)/1.5 //H20: (1-e)/1.5 //CO2: e/1.5 //H2: e/1.5 //e^2/[(0.5-e)(1-e)] = K = 1 //1.5e-0.5 = 1 e = 0.5/1.5; mprintf('\n\n (b). Percentage conversion of steam is %f percent',e*100); //end
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//Caption: probability of symbol error //Example 8.11 //page no 383 //Find probability of symbol error //assuming coherent detection clc; clear; rb=2.5*10^6//binary data rate N0=2*10^-20;//power spectral density of noise FSK system A=1*10^-6;//amplitude of received signal T=1/rb; Eb=(A^2*T)/2;// Eb=bit energy z=sqrt(Eb/(2*N0)) Pe=1/2*erfc(z);//probability of symbol error disp(Pe,"probability of symbol error");//
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// Scripts Q10, résoud numériquement l'équation (2) et montre la convergence vers la solution du problème stationnaire. // On fixe u0(t)=1 qqsoit t, u^(0)(x)=0 qqsoit x dans ]-l,l[ // téta = 1/2 Cranck-Nicholson clc; exec("Q7pbstationnaire.sce") //initialisation des variables l = 10 nbrPoints = 500 deltax = 2*l/(nbrPoints-1) deltat = 0.02 mu = deltat/deltax^2 function MembreDroit = calculMembreDroit(U, Ndiag, Ninf, B) // NU^(k) + B MembreDroit = Ndiag.* U + [0,Ninf.*U(1:size(U,"c")-1)] + [Ninf .* U(2:size(U,"c")),0] + mu*B endfunction function affiche(i,abscisse, ordonnee) //fonction d'affichage pour les solutions numériques et stationnaires ordonneeReel = (1/(exp(-1)-exp(1)))*(exp(abscisse/l)-exp(1)) subplot(2,2,i) //affichage de la solution numérique en bleu plot(abscisse, ordonnee) //affichage de la solution stationnaire en rouge plot(abscisse, ordonneeReel, 'r') title("Approximation de U au temps t = " + string((10^i)*deltat)) xlabel("x") ylabel("température") endfunction function U=iter(i, Ndiag, Ninf, B, MdiagFact, MinfFact) // fonction qui retourne U^(k) U = zeros(1,nbrPoints-2) U(1,1) = 1 for k=1:10^i // MembreDroite = NU^(k) + B MembreDroit = calculMembreDroit(U, Ndiag, Ninf, B) Z = descente(MdiagFact, MinfFact, MembreDroit) // U^(k+1) = M^-1 N U^(k) + M^-1 B U = remonte(MdiagFact, MinfFact, Z) end endfunction function main() // On initialise les matrices M, N et B [Adiag, Ainf, B] = genereMatricesAB(nbrPoints, l)//NbrPoints prend en compte les bornes!! Donc n = nbrPoints-2 Mdiag = 1 + (1/2)*mu*Adiag Minf = (1/2)*mu*Ainf Ndiag = 1 - (1/2)*mu*Adiag Ninf = -(1/2)*mu*Ainf [MdiagFact,MinfFact] = factorise(Mdiag, Minf) abscisse = linspace(-l,l,nbrPoints-2) // On calcul itérativement les U^(k) pour différent tk for i=1:4 U=iter(i, Ndiag, Ninf, B, MdiagFact, MinfFact) affiche(i, abscisse, U) end endfunction
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function [txx, txy, txz, tyy, tyz, tzz]=enmomt_parts(nx,ny,nz,dx,dy,dz,nparts, x, y, z,ppx, ppy, ppz, vx, vy, vz, m) txx=zeros(nx,ny,nz); txy=zeros(nx,ny,nz); txz=zeros(nx,ny,nz); tyy=zeros(nx,ny,nz); tyz=zeros(nx,ny,nz); tzz=zeros(nx,ny,nz); tpxx=m*vx*vx; tpxy=m*vx*vy; tpxz=m*vx*vz; tpyy=m*vy*vy; tpyz=m*vy*vz; tpzz=m*vz*vz; ipx=int8(1+ppx+(nx/2)); ipy=int8(1+ppy+(ny/2)); ipz=int8(ppz); if ipx > nx ipx=ipx-nx; end if ipx < 1 ipx=ipx+nx; end if ipy > ny ipy=ipy-ny; end if ipy < 1 ipy=ipy+ny; end if ipz > nz ipz=ipz-nz; end if ipz < 1 ipz=ipz+nz; end txx(ipx,ipy,ipz)=tpxx; txy(ipx,ipy,ipz)=tpxy; txz(ipx,ipy,ipz)=tpxz; tyy(ipx,ipy,ipz)=tpyy; tyz(ipx,ipy,ipz)=tpyz; tzz(ipx,ipy,ipz)=tpzz;
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//Section-14,Example-1,Page no.-PC.21 //To calculate collision number,collision frequency and mean free path for oxygen at 298K and 1 atm pressure. clc; M_w=32*10^-3 //(kg/mol) molecular weight of oxygen N_A=6.023*10^23 // Avogadro no.(mol^-1) M=((M_w)/(N_A)) disp(M,'Mass of one oxygen molecule(kg)') //N=P/(R*T) P=1 //atm R=0.0821 //litreatmK^-1mol^-1 T=298 //K N=(P*N_A*10^3)/(R*T) disp(N,'No.of O_2 molecules per m^3') R_1=8.314 //kgm^2K^-1mol^-1 m=32*10^-3 //kgmol^-1 v_avg=sqrt((8*R_1*T)/(%pi*m)) //ms^-1 disp(v_avg,'Average velocity of O2 molecule(ms^-1)') sig=3.6*10^-10 //m Z_1=sqrt(2)*%pi*(sig)^2*v_avg*N disp(Z_1,'Collision number(collisions per sec)') Z_11=(1/2)*(Z_1*N) disp(Z_11,'Collision frequency(collisions s^-1 m^-3)') lm=v_avg/Z_1 disp(lm,'Mean free path(m)')
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clc //Initialization of variables x1=0.0200 Kx=812 //calculations disp("Neglecting 2x in comparision with x1,") x=x1/Kx //results printf("Moles of Iodine present = %.2e mole",x)
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/* PROGRAM 3 : //HLL int i = 1 ; int sum = 0 ; while (i < 100) { sum = sum + i ; i = i + 1 ; } //endHLL i : RAM16K[16] sum : RAM16K[17] */ load HackComputer.hdl, //loading hdl file output-file loop.out, //declaring output file output-list RAM64[16]%D1.10.1 RAM64[17]%D1.10.1 ; //output list format ROM32K load loop.hack ; set reset 1, //reset is set to 1 tick, tock , output ; set reset 0, //reset is now set to 0 repeat 1420 { //min clock cycles required=1400 (divided into 100 iterations of 14 clock cycles each) n>1400 will do tick, tock, } output;
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// Example 19_4 clc;funcprot(0); // Given data mu=1.50*10^-5;// The viscosity of the CO_2 in kg/(m.s) T_1=300;// K T_2=305;// K k_p=1.00*10^-6;// m^2 k_o=2.00*10^4;// The osmotic heat conductivity in m^2/s // Solution dp=-((mu*k_o)/k_p)*log(T_2/T_1);// N/m^2 printf('\nThe steady state thermomolecular pressure difference across the membrane,p_2-p_1=%4.0f N/m^2',dp);
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//ques-35.1 //Calculating frequency of radiations clc w=500;//wavelength (in nm) c=2.996*10^10;//speed of light (in cm/s) f=c/(w*10^-7); printf("The frequency of the radiations is %.0f*10^14 Hz.",f*10^-14);
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//Example 2.12(b) clear; clc; R0=100;//Data taken from Example 2.11 alpha=0.00392;//Data taken from Example 2.11 Vref=15; Prtd=0.2*10^(-3); i=(Prtd/R0)^(0.5)-(0.41*10^(-3)); R1=(Vref/i); delta=alpha*1;//Fractional Deviation for 1 degree celsius change in temperature s=0.1;//Output Voltage for 1 degree Celsius temperature change A1=s*(2+(R1/R0)+(R0/R1)); A2=Vref*delta; A=A1/A2; dT=100; d2=alpha*dT; vO1num=A*Vref*d2; vO1den=1+(R1/R0)+((1+(R0/R1))*(1+d2)); vO1=vO1num/vO1den; vO2num=A*Vref*d2; vO2den=(2+(R1/R0)+(R0/R1)); vO2=vO2num/vO2den; vOchange=vO2-vO1; printf("vO(100 deg Celsius)=%.3f V",vO1); Tchange=vOchange/s; printf("\nEquivalent Temperature Error=%.2f deg Celsius",Tchange);
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optimizecode 1 maxversions 0 units Field /LiquidPhases = 2 /StdLiqVolRefT = 288.15 /StdLiqVolRefT = 60 F /RecycleDetails = 1 displayproperties displayproperties VapFrac T P MoleFlow MassFlow VolumeFlow StdLiqVolumeFlow StdGasVolumeFlow Energy H S MolecularWeight MassDensity Cp ThermalConductivity Viscosity molarV ZFactor commonproperties commonproperties + ZFactor P T MolecularWeight MassDensity StdLiqMolarVolVapFrac T P MoleFlow MassFlow VolumeFlow StdLiqVolumeFlow StdGasVolumeFlow Energy H S MolecularWeight MassDensity Cp ThermalConductivity Viscosity molarV ZFactor units SI $thermo = VirtualMaterials.Peng-Robinson / -> $thermo thermo + METHANE ETHANE PROPANE n-BUTANE realcomp = Compressor.CompressorWithCurve() cd realcomp NumberTables = 1 CompressorSpeed0 = 1800.0 FlowCurve0 = 0.0 1000.0 2000.0 3000.0 4000.0 5000.0 6000.0 7000.0 HeadCurve0 = 700.0 600.0 500.0 400.0 300.0 200.0 100.0 0.0 EfficiencyCurve0 = 0.0 0.5 0.7 0.8 0.8 0.7 0.5 0.0 CompressorSpeed = 1800 In.Fraction = .4 .3 .2 .1 In.P = 101.325 In.T = 30 Out.P = 106 Out InQ /realcomp.EfficiencyCurveType = Polytropic Out AdiabaticEff PolytropicEff /realcomp.EfficiencyCurveType = Adiabatic AdiabaticEff PolytropicEff '/realcomp.Out.P' = '/realcomp.In.VolumeFlow' = 2500 AdiabaticEff PolytropicEff cd / copy / paste / /RootClone.realcomp.Out
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kiks_calibrate.sci
function [] = kiks_calibrate(port,baud,forceul) // Number of arguments in function call [%nargout,%nargin] = argn(0) // Display mode mode(0); // Display warning for floating point exception ieee(1); // ----------------------------------------------- // (c) 2000 Theodor Storm (theodor@tstorm.se) // http://www.tstorm.se // ----------------------------------------------- // kiks_calibrate(port,baud): Calibrate KiKS // // Measures how many flops/second this computer can handle and, // optionally, calculates how much execution time each KSEND call to a // real robot requires. You need a robot connected to a serial port // in order to perform this operation. // // If you have a robot connected to your computer, // port is the # of the serial port a real robot is connected to. // baud is the baud rate to run the calibration process at - choose the baud // rate that you will usually run the real robot at for best results. // // If you do not have a robot connected to the computer, // do not specify port and baud rate and only computer speed will be measured. // // NOTE: kiks_calibrate will restart KiKS. global("KIKS_GUI_HDL","KIKS_COMPUTER_SPEED","KIKS_VISUALIZE","KIKS_KSEND_CONSTANT","KIKS_MAX_SPEED","KIKS_WALL_TIME","KIKS_CALIBRATE_BAUD","KIKS_KSEND_VARIATION"); getksend = 1; if %nargin<3 then forceul = []; end; if %nargin<2 then baud = 9600; end; if %nargin<1 then port = -1; end; if mtlb_logic(mtlb_double(port),"==",-1) then getksend = 0; end; arena = zeros(100,100); arena(50,50) = -360; kiks_arena(arena); // !! L.43: Unknown function kiks_gui_setstatlistbox not converted, original calling sequence used kiks_gui_setstatlistbox(7); xpause(1000*0.25); if mtlb_logic(mtlb_double(KIKS_VISUALIZE),">",0) then kiks_arena_window_close; end; xpause(1000*0.25); // !! L.51: Matlab function sprintf not yet converted, original calling sequence used // !! L.51: Unknown function kiks_status not converted, original calling sequence used kiks_status(sprintf("Calibrating KiKS, please wait. This will take a few moments.\n"),1); KIKS_COMPUTER_SPEED = 0; if getksend==1 then KIKS_KSEND_CONSTANT = 0; KIKS_KSEND_VARIATION = 0; // !! L.57: Unknown function kiks_settimescale not converted, original calling sequence used kiks_settimescale(KIKS_MAX_SPEED); maxksend = mtlb_double(baud)/64; KIKS_CALIBRATE_BAUD = baud; constarray = []; flops_total = 0; flops_time = 0; %v0_1(3:5) = []; %v1_1(3:5) = []; for i = 1:10 // loops=0; // !! L.66: Unknown function kiks_kopen not converted, original calling sequence used ref = kiks_kopen([port,baud,0]); nrksend = 0; while mtlb_logic(nrksend,"<",maxksend) // !! L.69: Matlab function sprintf not yet converted, original calling sequence used // !! L.69: Unknown function kiks_ksend not converted, original calling sequence used kiks_ksend([sprintf("G,%d,%d",nrksend,nrksend),10],ref); nrksend = nrksend+1; // !! L.71: Unknown function kiks_ksend not converted, original calling sequence used kiks_ksend("H"+10,ref); nrksend = nrksend+1; // !! L.73: Unknown function kiks_ksend not converted, original calling sequence used kiks_ksend("D,0,0"+10,ref); nrksend = nrksend+1; end; // !! L.76: Unknown function kiks_ktime not converted, original calling sequence used realruntime = kiks_ktime(port); // !! L.77: Unknown function kiks_kclose not converted, original calling sequence used kiks_kclose(ref); realksend = nrksend; // loops=0; // !! L.81: Unknown function kiks_kopen not converted, original calling sequence used ref = kiks_kopen([-1,baud,0]); // !! L.82: Matlab function flops not yet converted flops_before = mtlb(flops); %v0_1 = getdate(); %v0_1(6) = %v0_1(6)+%v0_1(7)/1000; t0 = %v0_1(1:6); nrksend = 0; while mtlb_logic(nrksend,"<",maxksend) // !! L.86: Matlab function sprintf not yet converted, original calling sequence used // !! L.86: Unknown function kiks_ksend not converted, original calling sequence used kiks_ksend([sprintf("G,%d,%d",nrksend,nrksend),10],ref); nrksend = nrksend+1; // !! L.88: Unknown function kiks_ksend not converted, original calling sequence used kiks_ksend("H"+10,ref); nrksend = nrksend+1; // !! L.90: Unknown function kiks_ksend not converted, original calling sequence used kiks_ksend("D,0,0"+10,ref); nrksend = nrksend+1; end; // !! L.93: Unknown function kiks_ktime not converted, original calling sequence used simruntime = kiks_ktime(-1); // !! L.94: Matlab function flops not yet converted flops_total = mtlb_a(flops_total,mtlb_s(mtlb_double(mtlb(flops)),mtlb_double(flops_before))); %v1_1 = getdate(); %v1_1(6) = %v1_1(6)+%v1_1(7)/1000; flops_time = flops_time+etime(%v1_1(1:6),t0); // !! L.96: Unknown function kiks_kclose not converted, original calling sequence used kiks_kclose(ref); simksend = nrksend; constarray(1,i) = matrix((mtlb_s(mtlb_double(realruntime),mtlb_double(simruntime))/nrksend)*mtlb_double(baud),1,-1); // !! L.100: Matlab function sprintf not yet converted, original calling sequence used calibration_progress = sprintf("%d%%",i*10); // !! L.101: Matlab function sprintf not yet converted, original calling sequence used // !! L.101: Unknown function kiks_status not converted, original calling sequence used kiks_status(sprintf("%s...",calibration_progress),1); end; constarray = mtlb_sort(constarray); KIKS_KSEND_CONSTANT = mean(constarray(2:9),"m"); // ignore lowest and highest values KIKS_KSEND_VARIATION = constarray(9)-constarray(2); end; //KIKS_COMPUTER_SPEED=flops_total/flops_time; //KIKS_COMPUTER_SPEED=flops_time; // !! L.111: Unknown function kiks_speedtest not converted, original calling sequence used KIKS_COMPUTER_SPEED = kiks_speedtest(3); // !! L.112: Matlab function sprintf not yet converted, original calling sequence used // !! L.112: Unknown function kiks_status not converted, original calling sequence used kiks_status(sprintf("Computer speed index: %1.2f\n",KIKS_COMPUTER_SPEED),1); // !! L.113: Unknown function kiks_save_settings not converted, original calling sequence used kiks_save_settings; // !! L.114: Unknown function kiks_status not converted, original calling sequence used kiks_status("Calibration finished."); // !! L.115: Unknown function kiks_quit not converted, original calling sequence used kiks_quit(1); endfunction
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# ************************************************************* # # Licensed to the Apache Software Foundation (ASF) under one # or more contributor license agreements. See the NOTICE file # distributed with this work for additional information # regarding copyright ownership. The ASF licenses this file # to you under the Apache License, Version 2.0 (the # "License"); you may not use this file except in compliance # with the License. You may obtain a copy of the License at # # http://www.apache.org/licenses/LICENSE-2.0 # # Unless required by applicable law or agreed to in writing, # software distributed under the License is distributed on an # "AS IS" BASIS, WITHOUT WARRANTIES OR CONDITIONS OF ANY # KIND, either express or implied. See the License for the # specific language governing permissions and limitations # under the License. # # ************************************************************* job=fileacc.SimpleFileAccess job=sc.ScCellFieldObj job=sc.ScCellFieldsObj job=sc.XMLImporter job=sc.XMLMetaExporter job=sd.SdDocLinkTargets job=sd.SdDrawPage job=sd.SdMasterPagesAccess job=sd.SdXCustomPresentation job=sd.SdXPresentation job=servicemgr.uno.OServiceManager job=sfx.SfxMacroLoader job=simplereg.uno.SimpleRegistry job=sm.XMLSettingsExporter job=sm.XMLSettingsImporter job=srtrs.SortedDynamicResultSetFactory job=svx.SvxShapeCollection job=svx.SvxUnoTextRangeEnumeration job=sw.SwXBodyText job=sw.XMLExporter job=sw.XMLImporter job=sw.XMLMetaExporter job=sw.XMLSettingsExporter job=sw.XMLSettingsImporter job=sw.XMLStylesExporter job=sysdtrans.SystemClipboard job=syssh.SystemShellExecute job=text.DefaultNumberingProvider job=toolkit.TabControllerModel job=toolkit.UnoControlCheckBox job=toolkit.UnoControlTimeField job=toolkit.UnoControlTimeFieldModel job=typeconverter.uno.TypeConverter job=typemgr.uno.TypeDescriptionManager job=ucb.UcbContentProviderProxyFactory job=ucb.UcbPropertiesManager job=ucb.UcbStore
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//Caption: peak Amplitude //Example 8.2 //page no 374 //Find peak Transmission pulseAmplitude clc; clear; NO=1.338*10^-5; Pe=2.055*10^-5; T=100*10^-6; //Pe=erfc(sqrt(Eb/(2*N0))); Eb=(2*2.9^2*NO); A=sqrt((Eb*2)/T); disp("Volts",A,"Transmission pulse Amplitude");