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//Single-Sideband Communications : example 4-1 : (pg 172 & 173) x=1*10^6; y=10^(80/20); z=sqrt(y); df=200; Q=(x*z)/(4*df); a=100*10^3; Q1=(a*z)/(4*df); disp(Q1); //part(a) : Q when 1-MHz & 80-dB sideband suppression printf("\nQ1 = fc.(log^-1(dB/20)^1/2)/4*delta(f) = %.f",Q); //part(b) : Q when 100-kHz & 80-dB sideband suppression printf("\nQ2 = fc.(log^-1(dB/20)^1/2)/4*delta(f) = %.f",Q1);
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clc// // // //Variable declaration M=3300; //magnetic field(amp/m) H=220; //magnetic field(amp/m) //Calculation chi=M/H; mew_r=1+chi; //relative permeability //Result printf("\n relative permeability is %0.3f ",mew_r)
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clc cv_N2=0.745; //kJ/kg K cv_CO2=0.653; //kJ/kg K cp_N2=1.041; //kJ/kg K cp_CO2=0.842; //kJ/kg K m_N2=4; //kg m_CO2=6; //kg pmix=4; //bar m=m_N2+m_CO2; T1=298; //K T2=323; //K cv_mix=(m_N2*cv_N2 + m_CO2*cv_CO2)/(m_N2+m_CO2); disp("cv_mix=") disp(cv_mix) disp("kJ/kg K") cp_mix=(m_N2*cp_N2 + m_CO2*cp_CO2)/(m_N2+m_CO2); disp("cp_mix=") disp(cp_mix) disp("kJ/kg K") dU=m*cv_mix*(T2-T1); disp("Change in internal energy=") disp(dU) disp("kJ") dH=m*cp_mix*(T2-T1); disp("Change in enthalpy=") disp(dH) disp("kJ") dS=m_N2*cv_N2*log(T2/T1) + m_CO2*cv_CO2*log(T2/T1); disp("Change in entropy=") disp(dS) disp("kJ/K")
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clc clear //INPUT DATA t1=300;//temperature in Degree C t2=700;//temperature in Degree C p1=1;//pressure in bar p3=12;//pressure in bar R=0.287;//gas constant //CALCULATIONS ns=(1-(t1/t2))*100;//Thermal efficiency in percentage Rc=((p3/p1)*(t1/t2));//compression ratio wn=R*log(Rc)*(t2-t1);//net work done in kJ/kg vs=(R*t1*(1-(1/Rc)))/(p1);//swept volume in m^3/kg pm=wn/vs;//mean effective pressure in bar //OUTPUT printf('(i)Thermal efficiency is %3.2f percentage \n (ii)The mean effective pressure is %3.2f bar',ns,pm)
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clc,clear //Example 4.1 //To convert a degree measure to radians deg=18 //degree measure radian=deg*(%pi/180) //radian measure printf('Radian measure is %f rad\n(or)\n',radian) printf('Radian measure is (pi/%.0f)rad',1/(radian/%pi))
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scenario = "Visual Oddball Instructions (Spanish Version)"; scenario_type = trials; # sets the default text font default_font = "Arial"; default_font_size = 14; default_text_color = 0,0,0; # sets text to black # sets the background colour to white (default is black) default_background_color = 255,255,255; #center the text default_text_align = align_center; begin; bitmap { filename = "SleepLookCircle.bmp";} NoSleep; bitmap { filename = "SleepLook.bmp";} Sleep; bitmap { filename = "IncorrectLookCircle.bmp";} NoLookAway; bitmap { filename = "IncorrectLook.bmp";} LookAway; bitmap { filename = "CorrectLookCircle.bmp";} YesLook; bitmap { filename = "CorrectLook.bmp";} Look; bitmap { filename = "BlankSubject.bmp";} sub; bitmap { filename = "F.pcx";} F; bitmap { filename = "T.pcx";} T; bitmap { filename = "default.pcx";} blankPCX; wavefile { filename = "nvmmn_instructionsES.wav"; } visInstruct; sound { wavefile visInstruct; attenuation = 0.2; } visualInstruction; picture { bitmap blankPCX; x = 0; y = 0; } default; trial { trial_duration = 50000; sound visualInstruction; time = 0; picture {bitmap sub; x = 0; y = 0; }; time = 1000; duration = 7000; picture {bitmap F; x = 0; y = 0; }; time= 10590; # 10.59 secs duration = 6000; picture {bitmap T; x = 0; y = 0; }; time = 18800; # 18.80 secs duration = 6000; picture {bitmap T; x = 0; y = 0; }; time = 30850; # 30.85 secs duration = 2000; picture {bitmap sub; x = 0; y = 0; }; time = 47000; # 47 secs duration = next_picture; picture {bitmap Look; x = 0; y = 0; }; time = 47200; #47.2 secs duration = next_picture; picture {bitmap YesLook; x = 0; y = 0; }; time = 47400; #47.4 secs duration = next_picture; picture {bitmap Look; x = 0; y = 0; }; time = 47600; #47.6 secs duration = next_picture; picture {bitmap YesLook; x = 0; y = 0; }; time = 47800; duration = next_picture; picture {bitmap Look; x = 0; y = 0; }; time = 48000; duration = next_picture; picture {bitmap YesLook; x = 0; y = 0; }; time = 48200; duration = next_picture; picture {bitmap sub; x = 0; y = 0; }; time = 50200; duration = next_picture; picture {bitmap LookAway; x = 0; y = 0; }; time = 50600; duration = next_picture; picture {bitmap NoLookAway; x = 0; y = 0; }; time = 50800; duration = next_picture; picture {bitmap LookAway; x = 0; y = 0; }; time = 51000; duration = next_picture; picture {bitmap NoLookAway; x = 0; y = 0; }; time = 51200; duration = next_picture; picture {bitmap LookAway; x = 0; y = 0; }; time = 51400; duration = next_picture; picture {bitmap NoLookAway; x = 0; y = 0; }; time = 51600; duration = next_picture; picture {bitmap sub; x = 0; y = 0; }; time = 52000; duration = next_picture; picture {bitmap Sleep; x = 0; y = 0; }; time = 56200; duration = next_picture; picture {bitmap NoSleep; x = 0; y = 0; }; time = 56400; duration = next_picture; picture {bitmap Sleep; x = 0; y = 0; }; time = 56600; duration = next_picture; picture {bitmap NoSleep; x = 0; y = 0; }; time = 56800; duration = next_picture; picture {bitmap Sleep; x = 0; y = 0; }; time = 57000; duration = next_picture; picture {bitmap NoSleep; x = 0; y = 0; }; time = 57200; duration = next_picture; picture {bitmap sub; x = 0; y = 0; }; time = 57600; duration = next_picture; };
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//*************************************************** // Displays the DC gain, poles, and zeros (see note) // of a linear system. Similar to Matlab function zpk // // Inputs: Linear system as state space model // or transfer function // // Outputs: None (prints results) // // NOTE: Any part of the zeros polynomial with a // coeffeicient < (10^-9 * DC coeffecient) // is removed. That is because SciLab tends // to have many rounding errors in the // numerator when going from state space // to transfer function //*************************************************** function kpz (G) // Make sure we're dealing with transfer function if typeof (G) == 'state-space' then G = ss2tf (G); end P = roots (denom (G)); K = coeff (numer (G), 0) / coeff (denom (G), 0); // Strip off any rounding errors in the zeros. These are easy to get when working with state space temp = coeff (numer (G)); temp2 = coeff (numer (G), 0); for i = 1:length (temp) if temp(i) / temp2 < 10^-9 then temp(i) = 0; end end Z = roots (poly (temp, varn (denom (G)), "coeff")); mprintf ("Gain:") disp (K) mprintf ("Poles:") disp (P) mprintf ("Zeros:") disp (Z) endfunction
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function [stk,txt,top]=sci_eye() // Copyright INRIA txt=[] if rhs==0 then stk=list(':','0','-1','-1','?') top=top+1 elseif rhs==1 then if stk(top)(3)=='1'&stk(top)(4)=='1' then stk=list('eye('+stk(top)(1)+','+stk(top)(1)+')','0',stk(top)(1),stk(top)(1),'?') elseif (stk(top)(3)=='1'&stk(top)(4)=='2')|(stk(top)(3)=='2'&stk(top)(4)=='1') then temp=gettempvar() txt=temp+'='+stk(top)(1) stk=list('eye('+temp+'(1),'+temp+'(2))','0','?','?','1','?') else set_infos('Not enough information using mtlb_eye instead of eye',1) stk=list('mtlb_eye('+stk(top)(1)+')','0','?','?','?') end else stk=list('eye('+stk(top-1)(1)+','+stk(top)(1)+')','0',stk(top-1)(1),stk(top)(1),'?') top=top-1 end
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// Example 11_12 clc;funcprot(0); // Given data T=60.0;// °F p_1=14.7;// psia r_c=19.2:1;// Compression ratio // Solution // From Table C.16a in Thermodynamic Tables to accompany Modern Engineering Thermodynamics,we find that, at 60.0°F = 520.R, u_1=88.62;// Btu/lbm p_r1=1.2147; v_r1=158.58; v_2byv_1=1/19.2; v_r2=v_r1*v_2byv_1; // Scanning down the v_r column in Table C.16a, we find that vr = 8.26 at about T_2=1600-459.67;// °F u_2=286.06;// Btu/lbm p_r2=71.73; p_2=p_1*(p_r2/p_r1);// psia W_12bym=u_1-u_2;// Btu/lbm printf("\nThe final temperature and pressure of the air at the end of the compression stroke,T_2=%4.0f°F and p_2=%3.1f psia. \nThe work required per lbm of air present,1W2/m=%3.2f Btu/lbm",T_2,p_2,W_12bym);
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 18.4w //calculation of image distance and focal length of concave mirror //given data h1=2; //height of object(in cm) h2=-5; //height of image(in cm) u=-12; //object distance in cm //calculation v=-(h2/h1)*u //image distance(in cm) using formula of lateral magnification if(v<0) disp(-v,'image is formed on same side of object at a distance(in cm)'); else disp(v,'image is formed on opposite side of mirror at a distance(in cm)'); end f=(u*v)/(u+v); //mirror formula disp(abs(f),'focal length(in cm) of the given concave mirror is');
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clc // //Variable declaration D=7.5 // Diameter of the bigger shaft(in) d=3.75 // Diameter of the smaller shaft(in) r=0.5625 // Inner radius(in) k=1.33 // Stress concentration factor //Calculation temp1=(D/d) temp2=(r/d) T=((1/2)*(%pi)*((1.875)**3)*(8/1.33)) // Maximum torque(ksi) //Power f=(900/60) // Frequency(Hz) Pa=(2*(%pi)*15*62.3*(10**3)) // Power(lb/s) Pa=(Pa/6600) // Power(hp) //Final Design r=15/16 // Radius(in) temp2=(0.9375/3.75) k=1.20 // Stress concentration factor T=(10.35*(8/1.20)) // Torque(kip.in) Pb=(2)*(%pi)*(15)*(69)*((10**3)) // Power(lb/s) Pb=(Pb/6600) // Power(hp) //Percent Change in Power PC=(((Pb-Pa)/Pa)*100) //Result printf("\n Case(a): Maximum power that can be transmitted = %1f hp' ,Pa) printf("\n Case(b): Percentage in power = %1f ' ,PC)
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//=========================================================================== //chapter 3 example 10 clc;clear all; //variable declaration R = 100; //resistance in Ω dR = 0.2; //resistancce error in Ω(ranging + to -) I = 2; //current in A dI = 0.01; //error in current in A(ranging + to -) //calaculatons eR = (dR/(R))*100; //percentage limiting error to resistance in %(ranging + to -) eI = (dI/(I))*100; //percentage limiting error to current in %(ranging + to -) P = (I^2)*R; //power dissioation in W eP = (2*eI)+eR; //worst ossible combination of errors the limiting error in the power dissipation in % p = (eP*10^-2)*P; //error in power in watts P1 = P+p; //power dissipation in W P2 =P-p; //power dissipation in W //result mprintf("limiting error = %3.2f percentage',eP); mprintf("\npower dissipation %3.2f W %3.2f W",P2,P1);
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//page 155 clear; close; clc; b=[1;2;3]; disp(b,'b='); a=[1;1;1]; disp(a,'a=') x=(a'*b)/(a'*a) disp(x*a,'Projection p of b onto the line through a is x^*a='); disp((a'*b)/(sqrt(a'*a)*sqrt(b'*b)),'cos(thetha)='); //end
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2023-02-25T08:33:08
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renamereset.tst
## test rename of a reset read <testrepo.fi reset master rename mistress write -
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ch7_10.sce
clc; clear; printf("\t\t\tChapter7_example10\n\n\n"); // Calculation of the pressure drop for the air passing over the tubes and the heat transferred to the air. // properties of air at 70 + 460 = 530 degree R = 540 degree R from appendix table D1 rou= 0.0735; // density in Ibm/cu.ft cp=0.240; // specific heat BTU/(lbm-degree Rankine) v= 16.88e-5; // viscosity in sq.ft/s kf = 0.01516 ; // thermal conductivity in BTU/(hr.ft.degree Rankine) a = 0.859; // diffusivity in sq.ft/hr Pr = 0.708; // Prandtl Number // specifications of 3/4 standard type K copper tubing from appendix table F2 OD=0.875/12; // outer diameter in ft ID=0.06208; // inner diameter in ft A=0.003027; // cross sectional area in sq.ft L=2; sL=1.5/12; sT=1.3/12; V_inf=12; // velocity of air in ft/s V1=(sT*V_inf)/(sT-OD); // velocity at area A1 in ft/s printf("\nVelocity at area A1 is %.1f ft/s",V1); sD=((sL)^2+(sT/2)^2)^0.5; // diagonal pitch in inch printf("\nThe diagonal pitch is %.2f in",sD*12); V2=(sT*V_inf)/(2*(sD-OD)); printf("\nVelocity at area A2 is %.1f ft/s",V2); if V1>V2 then Vmax=V1; else Vmax=V2; end Re_D=Vmax*OD/v; // Reynolds Number printf("\nThe Reynolds number is %.2e ",Re_D); sT_OD=1.3/0.875; sT_sL=1.3/1.5; printf("\nThe values of parameters are sT/Do=%.2f and sT/sL=%.2f",sT_OD,sT_sL); f1=0.35; //value of f1 for above values of sT/Do and Re f2=1.05; //Corresponding value of f2 for above values of sT/sL and Re gc=32.2; N=7; dP=N*f1*f2*(rou*Vmax^2/(2*gc)); printf("\nThe pressure drop is %.2f lbf/ft^2 = %.4f psi",dP, dP/147); sL_Do=sL/OD; C1=0.438; //value of C1 for above values of sT/Do and sL/Do C2=0.97; //value of C2 for above values of sT/Do and sL/Do m=0.565; //value of m for above values of sT/Do and sL/Do hc=kf*1.13*C1*C2*(Re_D)^m*(Pr)^(1/3)/OD; // The convection coefficient printf("\nThe convection coefficient is %.1f BTU/(hr.sq.ft.degree Rankine)",hc); As=70*%pi*OD*L; // outside surface area of 70 tubes printf("\nThe outside surface area of 70 tubes is %.1f sq.ft",As); Tw=200; // outside surface temeperature in degree F T_inf=70; // air temperature in degree F q=hc*As*(Tw-T_inf);// heat transferred printf("\nThe heat transferred is %.2e BTU/hr",q);
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//Exa 8.1 clc; clear; close; // Given data Q = 16;// in MJ Q = Q * 10^3;// in kJ T_H = 227;// in °C T_H = T_H + 273;// in K T_L = 15;// in °C T_L = T_L + 273;// in K del_S = Q/T_H;// in kJ/K A = Q - (T_L * del_S);// in kJ disp(A,"The available part of heat in kJ is "); U_P_ofHeat = T_L * del_S;// unavailable part of heat in kJ disp(U_P_ofHeat,"The unavailable part of heat in kJ is :");
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proba_q.3den.sce
clear; lines(0); np=100; q=3; //rang=190/300 msig = 1 // номер строки, отвечающая нужной нам плотности прививки, с которой мы будем считывать msig1 =2 msig2 =3 msig3 =4 msig4 =5 msig5 =6 msig6 =7 msig7 =8 msig8 =9 msig9 =10 msig10 =11 msig11 =12 msig12 =13 msig13 =14 msig14 =15 msig15 =16 msig16 =17 msig17 =18 msig18 =19 msig19 =20 msig20 =21 msig21 =22 msig22 =23 msig23 =24 msig24 =25 msig25 =26 msig26 =27 msig27 =28 msig28 =29 msig29 =30 msig30 =31 msig31 =32 msig32 =33 msig33 =34 msig34 =35 msig35 =36 msig36 =37 msig37 =38 msig38 =39 msig39 =40 msig40 =41 msig41 =42 msig42 =43 msig43 =44 msig44 =45 msig45 =46 msig46 =47 msig47 =48 msig48 =49 msig49 =50 msig50 =51 msig51 =52 msig52 =53 msig53 =54 msig54 =55 msig55 =56 msig56 =57 msig57 =58 msig58 =59 msig59 =60 msig60 =61 msig61 =62 msig62 =63 msig63 =64 msig64 =65 msig65 =66 msig66 =67 msig67 =68 msig68 =69 msig69 =70 msig70 =71 msig71 =72 msig72 =73 msig73 =74 msig74 =75 msig75 =76 msig76 =77 msig77 =78 msig78 =79 msig79 =80 msig80 =81 msig81 =82 msig82 =83 msig83 =84 msig84 =85 msig85 =86 msig86 =87 msig87 =88 msig88 =89 msig89 =90 msig90 =91 msig91 =92 msig92 =93 msig93 =94 msig94 =95 msig95 =96 msig96 =97 msig97 =98 msig98 =99 msig99 =100 msig100 =101 msig101 =102 msig102 =103 msig103 =104 msig104 =105 msig105 =106 msig106 =107 msig107 =108 msig108 =109 msig109 =110 msig110 =111 msig111 =112 msig112 =113 msig113 =114 msig114 =115 msig115 =116 msig116 =117 msig117 =118 msig118 =119 msig119 =120 msig120 =121 msig121 =122 msig122 =123 msig123 =124 msig124 =125 msig125 =126 msig126 =127 msig127 =128 msig128 =129 msig129 =130 msig130 =131 msig131 =132 msig132 =133 msig133 =134 msig134 =135 msig135 =136 msig136 =137 msig137 =138 msig138 =139 msig139 =140 msig140 =141 msig141 =142 msig142 =143 msig143 =144 msig144 =145 msig145 =146 msig146 =147 msig147 =148 msig148 =149 msig149 =150 msig150 =151 msig151 =152 msig152 =153 msig153 =154 msig154 =155 msig155 =156 msig156 =157 msig157 =158 msig158 =159 msig159 =160 msig160 =161 msig161 =162 msig162 =163 msig163 =164 msig164 =165 msig165 =166 msig166 =167 msig167 =168 msig168 =169 msig169 =170 msig170 =171 msig171 =172 msig172 =173 msig173 =174 msig174 =175 msig175 =176 msig176 =177 msig177 =178 msig178 =179 msig179 =180 msig180 =181 msig181 =182 msig182 =183 msig183 =184 msig184 =185 msig185 =186 msig186 =187 msig187 =188 msig188 =189 msig189 =190 msig190 =191 msig191 =192 msig192 =193 msig193 =194 msig194 =195 msig195 =196 msig196 =197 msig197 =198 msig198 =199 msig199 =200 msig200 =201 msig201 =202 msig202 =203 msig203 =204 msig204 =205 msig205 =206 msig206 =207 msig207 =208 msig208 =209 msig209 =210 msig210 =211 msig211 =212 msig212 =213 msig213 =214 msig214 =215 msig215 =216 msig216 =217 msig217 =218 msig218 =219 msig219 =220 msig220 =221 msig221 =222 msig222 =223 msig223 =224 msig224 =225 msig225 =226 msig226 =227 msig227 =228 msig228 =229 msig229 =230 msig230 =231 msig231 =232 msig232 =233 msig233 =234 msig234 =235 msig235 =236 msig236 =237 msig237 =238 msig238 =239 msig239 =240 msig240 =241 msig241 =242 msig242 =243 msig243 =244 msig244 =245 msig245 =246 msig246 =247 msig247 =248 msig248 =249 msig249 =250 msig250 =251 msig251 =252 msig252 =253 msig253 =254 msig254 =255 msig255 =256 msig256 =257 msig257 =258 msig258 =259 msig259 =260 msig260 =261 msig261 =262 msig262 =263 msig263 =264 msig264 =265 msig265 =266 msig266 =267 msig267 =268 msig268 =269 msig269 =270 msig270 =271 msig271 =272 msig272 =273 msig273 =274 msig274 =275 msig275 =276 msig276 =277 msig277 =278 msig278 =279 msig279 =280 msig280 =281 msig281 =282 msig282 =283 msig283 =284 msig284 =285 msig285 =286 msig286 =287 msig287 =288 msig288 =289 msig289 =290 msig290 =291 msig291 =292 msig292 =293 msig293 =294 msig294 =295 msig295 =296 msig296 =297 msig297 =298 msig298 =299 msig299 =300 msig300 =301 msig301 =302 msig302 =303 msig303 =304 msig304 =305 msig305 =306 msig306 =307 msig307 =308 msig308 =309 msig309 =310 msig310 =311 msig311 =312 msig312 =313 msig313 =314 msig314 =315 msig315 =316 msig316 =317 msig317 =318 msig318 =319 msig319 =320 msig320 =321 msig321 =322 msig322 =323 msig323 =324 msig324 =325 msig325 =326 msig326 =327 msig327 =328 msig328 =329 msig329 =330 msig330 =331 msig331 =332 msig332 =333 msig333 =334 msig334 =335 msig335 =336 msig336 =337 msig337 =338 msig338 =339 msig339 =340 msig340 =341 msig341 =342 msig342 =343 msig343 =344 msig344 =345 msig345 =346 msig346 =347 msig347 =348 msig348 =349 msig349 =350 msig350 =351 msig351 =352 msig352 =353 msig353 =354 msig354 =355 msig355 =356 msig356 =357 msig357 =358 msig358 =359 msig359 =360 msig360 =361 msig361 =362 msig362 =363 msig363 =364 msig364 =365 msig365 =366 msig366 =367 msig367 =368 msig368 =369 msig369 =370 msig370 =371 msig371 =372 msig372 =373 msig373 =374 msig374 =375 msig375 =376 msig376 =377 msig377 =378 msig378 =379 msig379 =380 msig380 =381 msig381 =382 msig382 =383 msig383 =384 msig384 =385 msig385 =386 msig386 =387 msig387 =388 msig388 =389 msig389 =390 msig390 =391 msig391 =392 msig392 =393 msig393 =394 msig394 =395 msig395 =396 msig396 =397 msig397 =398 msig398 =399 msig399 =400 msig400 =401 msig401 =402 msig402 =403 msig403 =404 msig404 =405 msig405 =406 msig406 =407 msig407 =408 msig408 =409 msig409 =410 msig410 =411 msig411 =412 msig412 =413 msig413 =414 msig414 =415 msig415 =416 msig416 =417 msig417 =418 msig418 =419 msig419 =420 msig420 =421 msig421 =422 msig422 =423 msig423 =424 msig424 =425 msig425 =426 msig426 =427 msig427 =428 msig428 =429 msig429 =430 msig430 =431 msig431 =432 msig432 =433 msig433 =434 msig434 =435 msig435 =436 msig436 =437 msig437 =438 msig438 =439 msig439 =440 msig440 =441 msig441 =442 msig442 =443 msig443 =444 msig444 =445 msig445 =446 msig446 =447 msig447 =448 msig448 =449 msig449 =450 msig450 =451 msig451 =452 msig452 =453 msig453 =454 msig454 =455 msig455 =456 msig456 =457 msig457 =458 msig458 =459 msig459 =460 msig460 =461 msig461 =462 msig462 =463 msig463 =464 msig464 =465 msig465 =466 msig466 =467 msig467 =468 msig468 =469 msig469 =470 msig470 =471 msig471 =472 msig472 =473 msig473 =474 msig474 =475 msig475 =476 msig476 =477 msig477 =478 msig478 =479 msig479 =480 msig480 =481 msig481 =482 msig482 =483 msig483 =484 msig484 =485 msig485 =486 msig486 =487 msig487 =488 msig488 =489 msig489 =490 msig490 =491 msig491 =492 msig492 =493 msig493 =494 msig494 =495 msig495 =496 msig496 =497 msig497 =498 msig498 =499 msig499 =500 msig500 =501 j=1; for w=190:10:300 s0 = '../n=' + string(np) + '/q=' + string(q) + 'den' +'/m=' + string(w) + '/zav_q/' ; s = s0 + 'zav_q=' + string(q) + '_' +'m='+ string(w) +'_np=' + string(np) + '.dat'; s1 = '../n=' + string(np) + '/Result/'; a=fscanfMat(s); [m,n]=size(a); j=j+1; b(1,j)=w; // w b(2,j)=a(msig,10) b(3,j)=a(msig1,10) b(4,j)=a(msig2,10) b(5,j)=a(msig3,10) b(6,j)=a(msig4,10) b(7,j)=a(msig5,10) b(8,j)=a(msig6,10) b(9,j)=a(msig7,10) b(10,j)=a(msig8,10) b(11,j)=a(msig9,10) b(12,j)=a(msig10,10) b(13,j)=a(msig11,10) b(14,j)=a(msig12,10) b(15,j)=a(msig13,10) b(16,j)=a(msig14,10) b(17,j)=a(msig15,10) b(18,j)=a(msig16,10) b(19,j)=a(msig17,10) b(20,j)=a(msig18,10) b(21,j)=a(msig19,10) b(22,j)=a(msig20,10) b(23,j)=a(msig21,10) b(24,j)=a(msig22,10) b(25,j)=a(msig23,10) b(26,j)=a(msig24,10) b(27,j)=a(msig25,10) b(28,j)=a(msig26,10) b(29,j)=a(msig27,10) b(30,j)=a(msig28,10) b(31,j)=a(msig29,10) b(32,j)=a(msig30,10) b(33,j)=a(msig31,10) b(34,j)=a(msig32,10) b(35,j)=a(msig33,10) b(36,j)=a(msig34,10) b(37,j)=a(msig35,10) b(38,j)=a(msig36,10) b(39,j)=a(msig37,10) b(40,j)=a(msig38,10) b(41,j)=a(msig39,10) b(42,j)=a(msig40,10) b(43,j)=a(msig41,10) b(44,j)=a(msig42,10) b(45,j)=a(msig43,10) b(46,j)=a(msig44,10) b(47,j)=a(msig45,10) b(48,j)=a(msig46,10) b(49,j)=a(msig47,10) b(50,j)=a(msig48,10) b(51,j)=a(msig49,10) b(52,j)=a(msig50,10) b(53,j)=a(msig51,10) b(54,j)=a(msig52,10) b(55,j)=a(msig53,10) b(56,j)=a(msig54,10) b(57,j)=a(msig55,10) b(58,j)=a(msig56,10) b(59,j)=a(msig57,10) b(60,j)=a(msig58,10) b(61,j)=a(msig59,10) b(62,j)=a(msig60,10) b(63,j)=a(msig61,10) b(64,j)=a(msig62,10) b(65,j)=a(msig63,10) b(66,j)=a(msig64,10) b(67,j)=a(msig65,10) b(68,j)=a(msig66,10) b(69,j)=a(msig67,10) b(70,j)=a(msig68,10) b(71,j)=a(msig69,10) b(72,j)=a(msig70,10) b(73,j)=a(msig71,10) b(74,j)=a(msig72,10) b(75,j)=a(msig73,10) b(76,j)=a(msig74,10) b(77,j)=a(msig75,10) b(78,j)=a(msig76,10) b(79,j)=a(msig77,10) b(80,j)=a(msig78,10) b(81,j)=a(msig79,10) b(82,j)=a(msig80,10) b(83,j)=a(msig81,10) b(84,j)=a(msig82,10) b(85,j)=a(msig83,10) b(86,j)=a(msig84,10) b(87,j)=a(msig85,10) b(88,j)=a(msig86,10) b(89,j)=a(msig87,10) b(90,j)=a(msig88,10) b(91,j)=a(msig89,10) b(92,j)=a(msig90,10) b(93,j)=a(msig91,10) b(94,j)=a(msig92,10) b(95,j)=a(msig93,10) b(96,j)=a(msig94,10) b(97,j)=a(msig95,10) b(98,j)=a(msig96,10) b(99,j)=a(msig97,10) b(100,j)=a(msig98,10) b(101,j)=a(msig99,10) b(102,j)=a(msig100,10) b(103,j)=a(msig101,10) b(104,j)=a(msig102,10) b(105,j)=a(msig103,10) b(106,j)=a(msig104,10) b(107,j)=a(msig105,10) b(108,j)=a(msig106,10) b(109,j)=a(msig107,10) b(110,j)=a(msig108,10) b(111,j)=a(msig109,10) b(112,j)=a(msig110,10) b(113,j)=a(msig111,10) b(114,j)=a(msig112,10) b(115,j)=a(msig113,10) b(116,j)=a(msig114,10) b(117,j)=a(msig115,10) b(118,j)=a(msig116,10) b(119,j)=a(msig117,10) b(120,j)=a(msig118,10) b(121,j)=a(msig119,10) b(122,j)=a(msig120,10) b(123,j)=a(msig121,10) b(124,j)=a(msig122,10) b(125,j)=a(msig123,10) b(126,j)=a(msig124,10) b(127,j)=a(msig125,10) b(128,j)=a(msig126,10) b(129,j)=a(msig127,10) b(130,j)=a(msig128,10) b(131,j)=a(msig129,10) b(132,j)=a(msig130,10) b(133,j)=a(msig131,10) b(134,j)=a(msig132,10) b(135,j)=a(msig133,10) b(136,j)=a(msig134,10) b(137,j)=a(msig135,10) b(138,j)=a(msig136,10) b(139,j)=a(msig137,10) b(140,j)=a(msig138,10) b(141,j)=a(msig139,10) b(142,j)=a(msig140,10) b(143,j)=a(msig141,10) b(144,j)=a(msig142,10) b(145,j)=a(msig143,10) b(146,j)=a(msig144,10) b(147,j)=a(msig145,10) b(148,j)=a(msig146,10) b(149,j)=a(msig147,10) b(150,j)=a(msig148,10) b(151,j)=a(msig149,10) b(152,j)=a(msig150,10) b(153,j)=a(msig151,10) b(154,j)=a(msig152,10) b(155,j)=a(msig153,10) b(156,j)=a(msig154,10) b(157,j)=a(msig155,10) b(158,j)=a(msig156,10) b(159,j)=a(msig157,10) b(160,j)=a(msig158,10) b(161,j)=a(msig159,10) b(162,j)=a(msig160,10) b(163,j)=a(msig161,10) b(164,j)=a(msig162,10) b(165,j)=a(msig163,10) b(166,j)=a(msig164,10) b(167,j)=a(msig165,10) b(168,j)=a(msig166,10) b(169,j)=a(msig167,10) b(170,j)=a(msig168,10) b(171,j)=a(msig169,10) b(172,j)=a(msig170,10) b(173,j)=a(msig171,10) b(174,j)=a(msig172,10) b(175,j)=a(msig173,10) b(176,j)=a(msig174,10) b(177,j)=a(msig175,10) b(178,j)=a(msig176,10) b(179,j)=a(msig177,10) b(180,j)=a(msig178,10) b(181,j)=a(msig179,10) b(182,j)=a(msig180,10) b(183,j)=a(msig181,10) b(184,j)=a(msig182,10) b(185,j)=a(msig183,10) b(186,j)=a(msig184,10) b(187,j)=a(msig185,10) b(188,j)=a(msig186,10) b(189,j)=a(msig187,10) b(190,j)=a(msig188,10) b(191,j)=a(msig189,10) b(192,j)=a(msig190,10) b(193,j)=a(msig191,10) b(194,j)=a(msig192,10) b(195,j)=a(msig193,10) b(196,j)=a(msig194,10) b(197,j)=a(msig195,10) b(198,j)=a(msig196,10) b(199,j)=a(msig197,10) b(200,j)=a(msig198,10) b(201,j)=a(msig199,10) b(202,j)=a(msig200,10) b(203,j)=a(msig201,10) b(204,j)=a(msig202,10) b(205,j)=a(msig203,10) b(206,j)=a(msig204,10) b(207,j)=a(msig205,10) b(208,j)=a(msig206,10) b(209,j)=a(msig207,10) b(210,j)=a(msig208,10) b(211,j)=a(msig209,10) b(212,j)=a(msig210,10) b(213,j)=a(msig211,10) b(214,j)=a(msig212,10) b(215,j)=a(msig213,10) b(216,j)=a(msig214,10) b(217,j)=a(msig215,10) b(218,j)=a(msig216,10) b(219,j)=a(msig217,10) b(220,j)=a(msig218,10) b(221,j)=a(msig219,10) b(222,j)=a(msig220,10) b(223,j)=a(msig221,10) b(224,j)=a(msig222,10) b(225,j)=a(msig223,10) b(226,j)=a(msig224,10) b(227,j)=a(msig225,10) b(228,j)=a(msig226,10) b(229,j)=a(msig227,10) b(230,j)=a(msig228,10) b(231,j)=a(msig229,10) b(232,j)=a(msig230,10) b(233,j)=a(msig231,10) b(234,j)=a(msig232,10) b(235,j)=a(msig233,10) b(236,j)=a(msig234,10) b(237,j)=a(msig235,10) b(238,j)=a(msig236,10) b(239,j)=a(msig237,10) b(240,j)=a(msig238,10) b(241,j)=a(msig239,10) b(242,j)=a(msig240,10) b(243,j)=a(msig241,10) b(244,j)=a(msig242,10) b(245,j)=a(msig243,10) b(246,j)=a(msig244,10) b(247,j)=a(msig245,10) b(248,j)=a(msig246,10) b(249,j)=a(msig247,10) b(250,j)=a(msig248,10) b(251,j)=a(msig249,10) b(252,j)=a(msig250,10) b(253,j)=a(msig251,10) b(254,j)=a(msig252,10) b(255,j)=a(msig253,10) b(256,j)=a(msig254,10) b(257,j)=a(msig255,10) b(258,j)=a(msig256,10) b(259,j)=a(msig257,10) b(260,j)=a(msig258,10) b(261,j)=a(msig259,10) b(262,j)=a(msig260,10) b(263,j)=a(msig261,10) b(264,j)=a(msig262,10) b(265,j)=a(msig263,10) b(266,j)=a(msig264,10) b(267,j)=a(msig265,10) b(268,j)=a(msig266,10) b(269,j)=a(msig267,10) b(270,j)=a(msig268,10) b(271,j)=a(msig269,10) b(272,j)=a(msig270,10) b(273,j)=a(msig271,10) b(274,j)=a(msig272,10) b(275,j)=a(msig273,10) b(276,j)=a(msig274,10) b(277,j)=a(msig275,10) b(278,j)=a(msig276,10) b(279,j)=a(msig277,10) b(280,j)=a(msig278,10) b(281,j)=a(msig279,10) b(282,j)=a(msig280,10) b(283,j)=a(msig281,10) b(284,j)=a(msig282,10) b(285,j)=a(msig283,10) b(286,j)=a(msig284,10) b(287,j)=a(msig285,10) b(288,j)=a(msig286,10) b(289,j)=a(msig287,10) b(290,j)=a(msig288,10) b(291,j)=a(msig289,10) b(292,j)=a(msig290,10) b(293,j)=a(msig291,10) b(294,j)=a(msig292,10) b(295,j)=a(msig293,10) b(296,j)=a(msig294,10) b(297,j)=a(msig295,10) b(298,j)=a(msig296,10) b(299,j)=a(msig297,10) b(300,j)=a(msig298,10) b(301,j)=a(msig299,10) b(302,j)=a(msig300,10) b(303,j)=a(msig301,10) b(304,j)=a(msig302,10) b(305,j)=a(msig303,10) b(306,j)=a(msig304,10) b(307,j)=a(msig305,10) b(308,j)=a(msig306,10) b(309,j)=a(msig307,10) b(310,j)=a(msig308,10) b(311,j)=a(msig309,10) b(312,j)=a(msig310,10) b(313,j)=a(msig311,10) b(314,j)=a(msig312,10) b(315,j)=a(msig313,10) b(316,j)=a(msig314,10) b(317,j)=a(msig315,10) b(318,j)=a(msig316,10) b(319,j)=a(msig317,10) b(320,j)=a(msig318,10) b(321,j)=a(msig319,10) b(322,j)=a(msig320,10) b(323,j)=a(msig321,10) b(324,j)=a(msig322,10) b(325,j)=a(msig323,10) b(326,j)=a(msig324,10) b(327,j)=a(msig325,10) b(328,j)=a(msig326,10) b(329,j)=a(msig327,10) b(330,j)=a(msig328,10) b(331,j)=a(msig329,10) b(332,j)=a(msig330,10) b(333,j)=a(msig331,10) b(334,j)=a(msig332,10) b(335,j)=a(msig333,10) b(336,j)=a(msig334,10) b(337,j)=a(msig335,10) b(338,j)=a(msig336,10) b(339,j)=a(msig337,10) b(340,j)=a(msig338,10) b(341,j)=a(msig339,10) b(342,j)=a(msig340,10) b(343,j)=a(msig341,10) b(344,j)=a(msig342,10) b(345,j)=a(msig343,10) b(346,j)=a(msig344,10) b(347,j)=a(msig345,10) b(348,j)=a(msig346,10) b(349,j)=a(msig347,10) b(350,j)=a(msig348,10) b(351,j)=a(msig349,10) b(352,j)=a(msig350,10) b(353,j)=a(msig351,10) b(354,j)=a(msig352,10) b(355,j)=a(msig353,10) b(356,j)=a(msig354,10) b(357,j)=a(msig355,10) b(358,j)=a(msig356,10) b(359,j)=a(msig357,10) b(360,j)=a(msig358,10) b(361,j)=a(msig359,10) b(362,j)=a(msig360,10) b(363,j)=a(msig361,10) b(364,j)=a(msig362,10) b(365,j)=a(msig363,10) b(366,j)=a(msig364,10) b(367,j)=a(msig365,10) b(368,j)=a(msig366,10) b(369,j)=a(msig367,10) b(370,j)=a(msig368,10) b(371,j)=a(msig369,10) b(372,j)=a(msig370,10) b(373,j)=a(msig371,10) b(374,j)=a(msig372,10) b(375,j)=a(msig373,10) b(376,j)=a(msig374,10) b(377,j)=a(msig375,10) b(378,j)=a(msig376,10) b(379,j)=a(msig377,10) b(380,j)=a(msig378,10) b(381,j)=a(msig379,10) b(382,j)=a(msig380,10) b(383,j)=a(msig381,10) b(384,j)=a(msig382,10) b(385,j)=a(msig383,10) b(386,j)=a(msig384,10) b(387,j)=a(msig385,10) b(388,j)=a(msig386,10) b(389,j)=a(msig387,10) b(390,j)=a(msig388,10) b(391,j)=a(msig389,10) b(392,j)=a(msig390,10) b(393,j)=a(msig391,10) b(394,j)=a(msig392,10) b(395,j)=a(msig393,10) b(396,j)=a(msig394,10) b(397,j)=a(msig395,10) b(398,j)=a(msig396,10) b(399,j)=a(msig397,10) b(400,j)=a(msig398,10) b(401,j)=a(msig399,10) b(402,j)=a(msig400,10) b(403,j)=a(msig401,10) b(404,j)=a(msig402,10) b(405,j)=a(msig403,10) b(406,j)=a(msig404,10) b(407,j)=a(msig405,10) b(408,j)=a(msig406,10) b(409,j)=a(msig407,10) b(410,j)=a(msig408,10) b(411,j)=a(msig409,10) b(412,j)=a(msig410,10) b(413,j)=a(msig411,10) b(414,j)=a(msig412,10) b(415,j)=a(msig413,10) b(416,j)=a(msig414,10) b(417,j)=a(msig415,10) b(418,j)=a(msig416,10) b(419,j)=a(msig417,10) b(420,j)=a(msig418,10) b(421,j)=a(msig419,10) b(422,j)=a(msig420,10) b(423,j)=a(msig421,10) b(424,j)=a(msig422,10) b(425,j)=a(msig423,10) b(426,j)=a(msig424,10) b(427,j)=a(msig425,10) b(428,j)=a(msig426,10) b(429,j)=a(msig427,10) b(430,j)=a(msig428,10) b(431,j)=a(msig429,10) b(432,j)=a(msig430,10) b(433,j)=a(msig431,10) b(434,j)=a(msig432,10) b(435,j)=a(msig433,10) b(436,j)=a(msig434,10) b(437,j)=a(msig435,10) b(438,j)=a(msig436,10) b(439,j)=a(msig437,10) b(440,j)=a(msig438,10) b(441,j)=a(msig439,10) b(442,j)=a(msig440,10) b(443,j)=a(msig441,10) b(444,j)=a(msig442,10) b(445,j)=a(msig443,10) b(446,j)=a(msig444,10) b(447,j)=a(msig445,10) b(448,j)=a(msig446,10) b(449,j)=a(msig447,10) b(450,j)=a(msig448,10) b(451,j)=a(msig449,10) b(452,j)=a(msig450,10) b(453,j)=a(msig451,10) b(454,j)=a(msig452,10) b(455,j)=a(msig453,10) b(456,j)=a(msig454,10) b(457,j)=a(msig455,10) b(458,j)=a(msig456,10) b(459,j)=a(msig457,10) b(460,j)=a(msig458,10) b(461,j)=a(msig459,10) b(462,j)=a(msig460,10) b(463,j)=a(msig461,10) b(464,j)=a(msig462,10) b(465,j)=a(msig463,10) b(466,j)=a(msig464,10) b(467,j)=a(msig465,10) b(468,j)=a(msig466,10) b(469,j)=a(msig467,10) b(470,j)=a(msig468,10) b(471,j)=a(msig469,10) b(472,j)=a(msig470,10) b(473,j)=a(msig471,10) b(474,j)=a(msig472,10) b(475,j)=a(msig473,10) b(476,j)=a(msig474,10) b(477,j)=a(msig475,10) b(478,j)=a(msig476,10) b(479,j)=a(msig477,10) b(480,j)=a(msig478,10) b(481,j)=a(msig479,10) b(482,j)=a(msig480,10) b(483,j)=a(msig481,10) b(484,j)=a(msig482,10) b(485,j)=a(msig483,10) b(486,j)=a(msig484,10) b(487,j)=a(msig485,10) b(488,j)=a(msig486,10) b(489,j)=a(msig487,10) b(490,j)=a(msig488,10) b(491,j)=a(msig489,10) b(492,j)=a(msig490,10) b(493,j)=a(msig491,10) b(494,j)=a(msig492,10) b(495,j)=a(msig493,10) b(496,j)=a(msig494,10) b(497,j)=a(msig495,10) b(498,j)=a(msig496,10) b(499,j)=a(msig497,10) b(500,j)=a(msig498,10) b(501,j)=a(msig499,10) b(502,j)=a(msig500,10) end sig = msig*0.001; // плотность прививки, соответствующая номеру строки msig sout = s1 + 'zav_q=' + string(q) + '_np=' + string(np) + '_range=190_300_min_sigma=0.001_fluctuation' + '.dat'; u=file('open',sout,'unknown'); write(u, b, '(f12.6,32(e16.6))'); file('close',u);
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//Ex 4.2 page 158 clc; clear; close; R=10;// ohm Vs=230;// V f=50;// Hz nc=18;// conducting cycles noff=32;// off cycles k=nc/(nc+noff);// duty ratio Vor=Vs*sqrt(k);// V Po=Vor**2/R;// W Pi=Po;// W (losses are negligble) Ior=Vor/R;//A pf=Po/Vs/Ior;//W Im=Vs*sqrt(2)/R;//A Irms=Im*sqrt(k)/2;//A Iav=k*Im/%pi;//A printf('\n (a) rms output voltage = %.0f V', Vor) printf('\n (b) Power output to load = %.1f W', Po) printf('\n (c) Power input to regulator = %.1f W', Pi) printf('\n (d) input power factor = %.1f ',pf) printf('\n (e) average scr current = %.3f A', Iav) printf('\n rms scr current = %.3f A', Irms)
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// Scilab code Ex2.9: Pg.86 (2008) clc; clear; E = 4.5e+17; // Energy of an object, J c = 3e+08; // Velocity of light ,m/s p_x = 3.8e+08; // X-component of Momentum of object, kg-m/s p_y = 3.0e+08; // Y-component of Momentum of object, kg-m/s p_z = 3.0e+08; // Z-component of Momentum of object, kg-m/s p = (p_x*c)^2+(p_y*c)^2+(p_z*c)^2; // Total momentum of object; kg-m/s m = sqrt((E^2)-(p))/(c^2); // Rest mass of moving object, kg printf("\nThe rest mass of the object = %3.1f kg",m); // Result // The rest mass of the object = 4.6 kg
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example11_2.sce
//clc() PE = 1.5*10^3;//J m = 10;//kg g = 9.81;//m/s^2 v = 50;//m/s //PE = mgz z = PE / (m*g); KE = m* (v^2) / 2; disp("m",z,"Height of the body from the ground = ") disp("kJ",KE/1000,"Kinetic energy of the body = ")
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//chapter 22 Ex 2 clc; clear; close; p=8000; n=2; r=15; amount=p*((1+r/100)^n)*((1+(1/3)*r/100)); CI=amount-p; printf("The Compound Interest is Rs. %3.0f",CI);
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// Premier oracle (fonction + gradient) function [F,G,ind] = OracleDG(lmb, ind) u = (-Ar'*pr-Ad'*lmb)./r; qsharp = sign(u) .* sqrt(abs(u)); if ind == 2 then F = -((1/3)*qsharp'*(r.*qsharp.*abs(qsharp)) + pr'*(Ar*qsharp) + lmb'*(Ad*qsharp-fd)); G = zeros(md,1); elseif ind == 3 then F = 0; G = -(Ad*qsharp-fd); else F = -((1/3)*qsharp'*(r.*qsharp.*abs(qsharp)) + pr'*(Ar*qsharp) + lmb'*(Ad*qsharp-fd)); G = -(Ad*qsharp-fd); end endfunction // Second oracle (fonction + gradient + hessienne) function [F,G,H,ind] = OracleDH(lmb, ind) u = (-Ar'*pr-Ad'*lmb)./r; qsharp = sign(u) .* sqrt(abs(u)); if ind == 2 then F = -(1./3.*qsharp'*(r.*qsharp.*abs(qsharp)) + pr'*(Ar*qsharp) + lmb'*(Ad*qsharp-fd)); G = zeros(md,1); H = zeros(md,md); elseif ind == 3 then F = 0; G = -(Ad*qsharp-fd); H = zeros(md,md); elseif ind == 4 then F = -(1./3.*qsharp'*(r.*qsharp.*abs(qsharp)) + pr'*(Ar*qsharp) + lmb'*(Ad*qsharp-fd)); G = -(Ad*qsharp-fd); H = zeros(md,md); elseif ind == 5 then F = 0; G = zeros(md,1); H = (1./2.)*Ad*diag(1. ./ (r.*sqrt(abs(u))))*Ad'; elseif ind == 6 then F = 0; G = -(Ad*qsharp-fd); H = (1./2.)*Ad*diag(1. ./ (r.*sqrt(abs(u))))*Ad'; elseif ind == 7 then F = -(1./3.*qsharp'*(r.*qsharp.*abs(qsharp)) + pr'*(Ar*qsharp) + lmb'*(Ad*qsharp-fd)); G = -(Ad*qsharp-fd); H = (1./2.)*Ad*diag(1. ./ (r.*sqrt(abs(u))))*Ad'; end endfunction
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R1=1; //voltage gain of an inverting amplifier Av Av=-100; printf("Av=(-R2/R1)\nTherefore R2=-Av*R1"); R2=-Av*R1; printf("\nRESULTS:\n"); printf("The design values are R1=%d Kohms and R2=%d Kohms",R1,R2);
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example_3_7.sce
clear; clc; clf(); xname("--------------Example 3.7----------------"); //display the figure subplot(121) // time domain plot a1=gca(); a1.y_label.text="Amplitude"; // y-axis a1.y_label.font_style = 3; a1.y_label.font_size = 4; a1.y_label.foreground = 3; a1.y_location = "left"; a1.x_label.text="Time"; // x-axis a1.x_label.font_style = 3; a1.x_label.font_size = 4; a1.x_label.foreground = 3; a1.x_location = "middle"; a1.data_bounds=[0,-15;1,15]; x=[0:.000125:1]; // sine waves to be plotted plot2d(x,10*sin(8*x)); plot2d(x,5*sin(16*x)); plot2d(x,15*sin(%pi/2 - 0*x)); xarrows([.5 .01],[-12 -12],5); xarrows([.5 .99],[-12 -12],5); xpoly([1 1],[-3 -12.5]); xset("font size",3) xstring(.5,-11,"1s") xset("font size",2) xstring(.02,-13.5,"a. Time-domain representation of three sine waves with frequencies 0, 8, and 16") subplot(122) // frequency domain plot a1=gca(); xarrows([0 1],[.5 .5],.5) xarrows([0 0],[.5 1],.5) xset("font size",3) xstring(-.01,1,"Amplitude") // y-axis xstring(1,.45,"Frequency") // x-axis xstring(.02,.4,"b. Frequency-domain representation of the same three signals") xstring(0,.45,"0 8 16") xstring(-.05,.7,"5") xstring(-.05,.8,"10") xstring(-.05,.9,"15") xset("thickness",2.5) xpoly([0 0],[.5 .9]) xpoly([.4 .4],[.5 .8]) xpoly([.8 .8],[.5 .7]) xpoly([0 -.01],[.7 .7]) xpoly([0 -.01],[.8 .8]) xpoly([0 -.01],[.9 .9])
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//Caption:transfer_function_using_mason's_gain_formula // example 4.4.4 //page 67 syms G1 G2 G3 H1; // forward path denoted by P1,P2 and so on and loop by L1,L2 and so on //path factor by D1,D2 and so on and graph determinant by D P1=G1*G2*1; P2=G1*G3; L1=G2*(-1); L2=G3*(-1); L3=-G1*G2*H1 D1=1; D2=1; D=1-(L1+L2+L3); Y=(P1*D1+P2*D2)/D; Y=simple(Y); disp(Y,"C(s)/R(s)=")
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DsServer=VK-TEST Object=CN=DhcpRoot OptName=Option#1 OptComment=Optcomment#1 ClassName= OptId=30 OptData=01020304 CreateOptionDef=
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example5_6.sce
//example 5.6 //calculate yield from well clc; //given b=30; //thickness of acquifer s=4; //drawdown r=0.1; //well radius k=36; //permeability coefficient R=3000*s*(k/(24*3600))^0.5; Q=2.72*b*k*s/(log10(R/r)*24*3.6); Q=round(Q*10)/10; mprintf("yield from well=%f lit/sec.",Q);
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//Calculations on turbocharged CI engine clc,clear //Given: Py=896 //Brake power at test in kW py=96 //Test ambient pressure in kPa Ty=302 //Test ambient temperature in K phiy=0.2 //Relative humidity at test px=98 //Site ambient air pressure in kPa Tx=315 //Site ambient temperature in K phix=0.4 //Relative humidity at site N=1800 //Engine speed in rpm V_s=51.8 //Swept volume in litres m_f=54.5 //Fuel delivery in gm/s pi=2.6 //Pressure ratio //Solution: //Refer table 27.1, 27.3 psy=4.8 //Saturation vapour pressure at test in kPa psx=8.2 //Saturation vapour pressure at site in kPa q=m_f*1000/(N/(2*60)*V_s) //Fuel delivery in mg/litrecycle qc=round(q/pi) //Corrected fuel delivery inmg/litrecycle //Applying condition given in fig 27.2 for value of engine factor (fm) if (qc <= 40) then fm=0.3; elseif (qc >= 65) then fm=1.2; else fm=0.036*qc-1.14; end fa=((px-phix*psx)/(py-phiy*psy))^0.7*(Ty/Tx)^1.5 //Atmospheric factor alpha_d=fa^fm //Correction factor for CI engine Px=alpha_d*Py //Brake power at site in kW //Results: printf("\n Power at site ambient conditions, Px = %d kW",Px)
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// Example 3.24, page no-153 clear clc Vbe=0.6 Ibmax=500*10^-9 fL=50 RL=3.3*10^3 R1max=0.1*Vbe/Ibmax R1=R1max/2 R2=R1 C3=1/(2*%pi*fL*RL) C3=C3*10^6 printf('\nC3=%.2f uF',C3) C2=1/(2*%pi*fL*R2/10) C2=C2*10^6 printf('\nC2=%.2f uF',C2) // answer in textbook is wrong Mmin=50000 Zinmin=(1+Mmin)*56*10^3 Zinmin=Zinmin/10^6 printf('\nZin(min)= %d Mohm',Zinmin)
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<scriptConfig name="disable" script="Disable_Functions"> <params> <param name="global.inverter.slave_id" type="int">5</param> <param name="global.inverter.baudrate" type="int">9600</param> <param name="global.inverter.ifc_name" type="string">COM7</param> <param name="global.inverter.parity" type="string">N</param> <param name="global.inverter.ifc_type" type="string">RTU</param> <param name="resets.inv2" type="string">yes</param> <param name="resets.inv3" type="string">yes</param> <param name="resets.inv1" type="string">yes</param> <param name="resets.vv" type="string">yes</param> </params> </scriptConfig>
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clear; clc; close; disp(10^1.6,'ans for part a :- '); disp(%e^0.04,'ans for part b :- ');
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clc //Given that r = 1e-14 // radius of nucleus of atom in meter h = 6.626e-34 // Plank's constant //Sample Problem 12 page No. 140 printf("\n\n\n # Problem 12 # \n") printf("\n Standard formula Used \n delta_p * delta_x >= h /(2*pi)") del_x = 2 * r //calculation of Uncertainty in position del_p = h / (2 * %pi * del_x) //calculation of Uncertainty in momentum printf ("\n Uncertainty in momentum is %e Kg-m/s. ", del_p )
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2_6.sce
//To Find the Angular Acceleration clc //Given: N0=0,N=2000 //rpm t=20 //seconds //Solution: //Calculating the angular velocities omega0=0, omega=2*%pi*N/60 //rad/s //Calculating the angular acceleration alpha=(omega-omega0)/t //rad/s^2 //Calculating the angular distance moved by the wheel during 2000 rpm theta=(omega0+omega)*t/2 //rad //Calculating the number of revolutions made by the wheel n=theta/(2*%pi) //Results: printf("\n\n The angular acceleration of the wheel, alpha = %.3f rad/s^2.\n",alpha) printf(" The wheel makes n = %.1f revolutions.\n\n",n)
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Chapter15_example5.sce
clc clear //Input data Vs=0.0045;//Swept volume in m^3 N=4000;//The speed of the engine in rpm nv=150;//Overall volumetric efficiency in percent ni=90;//Isentropic efficiency of the compressor in percent nm=85;//Mechanical efficiency in percent T=330;//The temperature of compressed air after cooler in K p2=1.8;//The pressure of the compressed air in bar T1=290;//The ambient temperature of air in K p1=1;//The pressure of the ambient condition in bar R=287;//The real gas constant in J/kgK g=1.4;//Adiabatic index Cp=1.005;//The specific heat of gas in kJ/kgK //Calculations T21=T1*(p2/p1)^((g-1)/g);//The temperature at 2' in K T2=T1+[(T21-T1)/(ni/100)];//The temperature of air after compressor in K Vs1=Vs*(N/(2*60));//Rate of swept volume in m^3/s Va=(nv/100)*Vs1;//Volume of air induced in m^3/s d=(p1*10^5)/(R*T1);//The density of air at ambient condition in kg/m^3 ma=d*Va;//Mass of air induced in kg/s Q=ma*Cp*(T2-T);//Heat rejected from after cooler in kJ/s P=ma*Cp*(T2-T1);//Power needed to run the compressor in kW Pa=P/(nm/100);//Power absorbed from the engine in kW //Output printf( '(a) The rate of heat rejected from the after cooler = %3.3f kJ/s \n (b) The power absorbed by the supercharger from the engine = %3.2f kW ',Q,Pa)
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//Exa 9.3 clc; clear; close; //Given data : V=66;//kV //Part(i) n=5;//no. of uniits K=1/5;//shunt to mutual capacitance ratio V1=V/(5+20*K+21*K^2+8*K^3+K^4);//kV V5=V1*(1+10*K+15*K^2+7*K^3+K^4);//kV Strinf_eff=V/n/V5; disp(Strinf_eff*100,"Part(i) Percentage String Efficiency(%)"); //Part(ii) n=5;//no. of uniits K=1/6;//shunt to mutual capacitance ratio V1=V/(5+20*K+21*K^2+8*K^3+K^4);//kV V5=V1*(1+10*K+15*K^2+7*K^3+K^4);//kV Strinf_eff=V/n/V5; disp(Strinf_eff*100,"Part(ii) Percentage String Efficiency(%)");
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#************************************************************ # Scenario of ADREAM # # date : Wed Nov 28 17:50:10 2012 #************************************************************ p3d_sel_desc_name P3D_ENV ADREAM p3d_sel_desc_name P3D_ROBOT HERAKLES_HUMAN1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.143000 6.521000 0.987000 0.000000 0.000000 33.732000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 79.416000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -69.156000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 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0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT WALLE_TAPE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT GREY_TAPE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_RED p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_BLUE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_GREEN p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT ACCESSKIT p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PINK_TRASHBIN p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PR2_GRIPPER p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 3 1 2 2 1.000000 0.000000 0 p3d_sel_desc_name P3D_ROBOT PR2_GRIPPER_LEFT p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 3 1 2 2 1.000000 0.000000 0 p3d_sel_desc_name P3D_ROBOT VISBALL_MIGHTABILITY p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT HUM_BAR p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SAHandRight p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 6 1 5 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 10 1 9 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 14 1 13 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 18 1 17 2 1.000000 0.000000 0 p3d_sel_desc_name P3D_ROBOT SAHandRight2 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 6 1 5 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 10 1 9 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 14 1 13 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 18 1 17 2 1.000000 0.000000 0 p3d_sel_desc_name P3D_ROBOT SIMPLECHAIR p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PR_2CYLINDER p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT HUMCYLINDER p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT TABLE_1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT CARPET p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.580000 7.020000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT FAUTEUIL_1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.350000 5.730000 0.000000 0.000000 0.000000 -164.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT FAUTEUIL_2 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.370000 8.150000 0.000000 0.000000 0.000000 48.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT LOW_TABLE_LARGE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 1.553000 6.760000 0.000000 0.000000 0.000000 16.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SOFA p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.100000 6.600000 0.000000 0.000000 0.000000 109.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT IKEA_SHELF_DARK p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.733000 4.835000 0.791000 0.000000 0.000000 90.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT IKEA_SHELF_LIGHT_1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.733000 4.835000 0.000000 0.000000 0.000000 90.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT IKEA_SHELF_LIGHT_2 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.523000 4.835000 0.000000 0.000000 0.000000 90.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PR2_ROBOT p3d_set_robot_steering_method Multi-Localpath p3d_set_robot_radius 1.000000 p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 5.934000 5.629000 0.000000 0.000000 0.000000 81.036000 0.192000 0.000000 0.000000 0.000000 -61.254000 55.426000 -68.284000 -74.959000 0.000000 0.000000 0.000000 0.000000 0.000000 53.566000 67.152000 97.737000 -119.288000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 5.741000 7.580000 0.000000 0.000000 0.000000 180.000000 0.192000 0.000000 0.000000 0.000000 -61.254000 55.426000 -68.284000 -74.959000 0.000000 0.000000 0.000000 0.000000 0.000000 53.566000 67.152000 97.737000 -119.288000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 15 1 14 2 1.000000 0.000000 0 p3d_constraint p3d_lin_rel_dofs 1 25 1 24 2 1.000000 0.000000 0 p3d_constraint p3d_pr2_arm_ik 7 6 7 9 10 11 12 13 1 32 0 1 8 p3d_set_cntrt_Tatt 2 1.000000 0.000000 0.000000 -0.180000 0.000000 1.000000 0.000000 0.000000 0.000000 0.000000 1.000000 0.000000 p3d_set_cntrt_Tatt2 2 0.000000 1.000000 0.000000 0.000000 0.000000 0.000000 1.000000 0.000000 1.000000 0.000000 0.000000 -0.180000 p3d_constraint p3d_pr2_arm_ik 7 16 17 19 20 21 22 23 1 33 0 1 18 p3d_set_cntrt_Tatt 3 1.000000 0.000000 0.000000 -0.180000 0.000000 1.000000 0.000000 0.000000 0.000000 0.000000 1.000000 0.000000 p3d_set_cntrt_Tatt2 3 0.000000 1.000000 0.000000 0.000000 0.000000 0.000000 1.000000 0.000000 1.000000 0.000000 0.000000 -0.180000 p3d_set_object_base_and_arm_constraints 32 1 0 2 2 3 p3d_set_arm_data 2 3 32 p3d_set_arm_data 3 3 33 p3d_sel_desc_name P3D_ROBOT PR2_SIMUL p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_camera_pos 4.909815 6.629659 0.584054 4.799191 5.971935 0.786875 0.000000 0.000000 1.000000 0.000000
21728d9407f120645c3094bb8569b06493dc781d
348b83f2cd32e6616b86e704a374661890d58cda
/cummulative average.sce
abc04f7520efa33615c8765069cae8e609b3fb08
[]
no_license
YashGandhi17/Scilab
012b35caad56d0c7600b9a207956e25774339c66
6d509dc17afe2ca32376df795693c84f94e3f360
refs/heads/master
2020-04-07T03:13:24.046967
2018-11-17T17:24:44
2018-11-17T17:24:44
157,837,866
0
0
null
null
null
null
UTF-8
Scilab
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false
398
sce
cummulative average.sce
Xn=input("enter the wave form Xn="); N=input("enter ending index N"); n=0:N; sum=0; for i =1:N+1 sum=sum+Xn(i); Yn(i)=sum/i; end disp("cummulative average Yn= "); disp(Yn); figure(1); clf(1); subplot(2,1,1); plot2d3(n,Xn); xlabel("n"); ylabel("Xn") title("input signal"); subplot(2,1,2); plot2d3(n,Yn); xlabel("n"); ylabel("Yn") title("cummulative avarage signal");
478b5fd0f00347d77c5fc4ac72460bb7c0f136f5
449d555969bfd7befe906877abab098c6e63a0e8
/1067/CH3/EX3.3/3_3.sce
15bfcde4cb7f0714b6eb45ce32c881374c26ed8c
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
12
null
null
null
null
UTF-8
Scilab
false
false
445
sce
3_3.sce
clear; close; clc; C=.003e-6 L=1.6e-3 y=sqrt(L*C); y=round(y*1e7)/1e7; f=(2*3.14*y)^-1; f=round(f/100)*100; i=7500; E=i*2*3.15*L*50; Em=1.414*E; Em=round(Em/10)*10 t=y*%pi/2; t=t*1e6; t=round(t*100)/100; e=Em/y; e=round((e)/1e6)*1e6; e=fix(e/1e7)*1e7 mprintf("frequency of oscillations=%fc/s",f); mprintf("\ntime of maximum restriking voltage=%fmicrosec",t); mprintf("\nmaximum restriking voltage=%dV/microsecs",e/1e6);
be1013786c4e62e7fb53b02c87cfdbf9dfbad5c2
089894a36ef33cb3d0f697541716c9b6cd8dcc43
/NLP_Project/test/tweet/bow/bow.16_12.tst
c4257b32c23e200dc943fb203c080d5c1b8182f1
[]
no_license
mandar15/NLP_Project
3142cda82d49ba0ea30b580c46bdd0e0348fe3ec
1dcb70a199a0f7ab8c72825bfd5b8146e75b7ec2
refs/heads/master
2020-05-20T13:36:05.842840
2013-07-31T06:53:59
2013-07-31T06:53:59
6,534,406
0
1
null
null
null
null
UTF-8
Scilab
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false
34,633
tst
bow.16_12.tst
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/2102/CH4/EX4.28/exa_4_28.sce
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[]
no_license
FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
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37,975,407
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sce
exa_4_28.sce
// Exa 4.28 clc; clear; close; kT= 0.025;// in eV (Let as take T=300 K) E= 1.42/2;// in ev (Let E = E_C-E_F) FE= %e^(-E/kT); disp(FE,"The probability of exciting electrons at conduction band will be ")
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/1670/CH11/EX11.10/11_10.sce
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no_license
FOSSEE/Scilab-TBC-Uploads
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37,975,407
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11_10.sce
//Example 11.10 //Gauss Seidel Method //Page no. 382 clc;clear;close; O=0.5; A=[-8,8,0;2,-8,4;0,4,-8]; //equation matrix B=[-1;-1;-1]; //solution matrix Ov=inv(A)*B; disp(Ov,'Values = ') Ox=Ov(1)+(Ov(1)-O)/3 disp(Ox,'O* = ')
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/Loop.tst
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[]
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Dragon-S1/Hack-Computer
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refs/heads/main
2023-06-15T20:10:55.473866
2021-07-21T07:41:33
2021-07-21T07:41:33
387,541,861
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tst
Loop.tst
load HackComputer.hdl, output-file Loop.out, output-list RAM16K[16]%D1.10.1 RAM16K[17]%D1.10.1; ROM32K load Loop.hack, repeat 1500{ tick,tock, } output;
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/1595/CH1/EX1.10/ex1_10.sce
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[]
no_license
FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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37,975,407
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sce
ex1_10.sce
//Introductory Topics :example 1-10 : (pg no. 26) i= 14*10^-3;//dc current R=50; x=(20*i*R); y=10*log10(x); printf("\nNR = 20.Idc.R = %.f",x);//noise ratio printf("\nNF = 10log(NR) = %.2f dB",y);//noise figure
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/2606/CH5/EX5.25/ex5_25.sce
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[]
no_license
FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
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sce
ex5_25.sce
//Page Number: 5.37 //Example 5.25 clc; //Given, fs=32D+3; //Hz fm=1000; //Hz fM=4D+3; //Hz //As SNR=(3*(fs^3))/(8*pi*pi*(fm^2)*fM) SNR=(3*(fs^3))/(8*%pi*%pi*(fm^2)*fM); SNRdb=(log10(SNR)); disp('dB',SNRdb,'Output SNR');
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/yukuva week-3/q1 signed/me.tst
0ec2baf506cd1da0e873e6c2d50f4df2aac1213a
[]
no_license
yuva-a/CS2310-week-3-yukuva-
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refs/heads/main
2023-07-16T22:05:24.735456
2021-09-05T07:58:23
2021-09-05T07:58:23
403,234,870
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tst
me.tst
// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/01/And.tst load me.hdl, output-file me.out, //compare-to And.cmp, output-list x%B3.16.3 y%B3.16.3 as%B3.1.3 s%B3.16.3 overflow%B3.1.3; set x %B0000000000001000, set y %B0000000000000101, set as 0, eval, output; set x %B0100010010001000, set y %B0101000010100000, set as 0, eval, output; set x %B1111111111111101, set y %B1111111111110101, set as 0, eval, output; set x %B1100010000100000, set y %B1000000100000100, set as 0, eval, output; set x %B0000100010000000, set y %B1111111111100100, set as 0, eval, output; set x %B0000001001000100, set y %B1111111111100100, set as 1, eval, output; set x %B00000100010010011, set y %B1000000100001000, set as 1, eval, output;
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/TP2/inverse.sci
b81bfc9bce446eb82760bf240d30dbc88061b80b
[]
no_license
BenFradet/MT09
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2020-04-14T02:47:55.441807
2014-12-22T17:34:50
2014-12-22T17:34:50
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function[b] = inverse(a) exec('resolG.sci', -1); [m n] = size(a); id = eye(n, n); b = zeros(n, n); for i = 1:n b(:, i) = resolG(a, id(:, i)); end endfunction
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mode(-1); warning('off'); // correct opgeloste sudokus S1 = [8 7 1 2 3 5 6 9 4; 2 9 6 1 8 4 5 7 3; 5 3 4 6 9 7 1 2 8; 9 4 5 8 2 3 7 1 6; 3 6 2 7 1 9 8 4 5; 7 1 8 5 4 6 9 3 2; 1 2 7 3 6 8 4 5 9; 6 5 9 4 7 2 3 8 1; 4 8 3 9 5 1 2 6 7] S2 = [1 2 3 4 5 6 7 8 9; 4 5 6 7 8 9 1 2 3; 7 8 9 1 2 3 4 5 6; 2 3 4 5 6 7 8 9 1; 5 6 7 8 9 1 2 3 4; 8 9 1 2 3 4 5 6 7; 3 4 5 6 7 8 9 1 2; 6 7 8 9 1 2 3 4 5; 9 1 2 3 4 5 6 7 8] // niet correct opgeloste sudokus T1 = [8 7 1 2 3 5 6 9 4; 2 9 6 1 8 4 5 7 3; 5 3 4 6 9 7 1 2 8; 9 4 5 8 2 3 7 1 6; 3 6 2 7 1 9 8 4 5; 7 1 8 5 4 6 9 3 2; 1 2 7 3 6 8 4 1 9; 6 5 9 4 7 2 3 8 1; 4 8 3 9 5 1 2 6 7] T2 = [8 7 1 2 3 5 6 9 4; 2 9 6 1 8 4 5 7 3; 5 3 4 6 9 7 1 2 8; 9 4 5 8 2 3 7 1 6; 3 6 2 7 1 9 8 4 5; 7 1 8 5 4 6 9 3 2; 1 2 7 3 6 8 4 5 9; 6 5 9 4 7 2 3 8 1; 4 8 3 9 5 1 2 0 7] T3 = [8 7 1 2 3 5 6 9 4; 2 9 6 1 8 4 5 7 3; 5 3 4 6 9 7 1 2 8; 9 4 5 8 2 3 7 1 6; 3 6 2 7 1 9 8 6 5; 7 1 8 5 4 6 9 3 2; 1 2 7 3 6 8 4 5 9; 4 5 9 4 7 2 3 8 1; 6 8 3 9 5 1 2 4 7] T4 = [1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9; 1 2 3 4 5 6 7 8 9] T5 = [1 1 1 1 1 1 1 1 1; 2 2 2 2 2 2 2 2 2; 3 3 3 3 3 3 3 3 3; 4 4 4 4 4 4 4 4 4; 5 5 5 5 5 5 5 5 5; 6 6 6 6 6 6 6 6 6; 7 7 7 7 7 7 7 7 7; 8 8 8 8 8 8 8 8 8; 9 9 9 9 9 9 9 9 9] T6 = [1 2 3 4 5 6 7 8 9; 2 3 4 5 6 7 8 9 1; 3 4 5 6 7 8 9 1 2; 4 5 6 7 8 9 1 2 3; 5 6 7 8 9 1 2 3 4; 6 7 8 9 1 2 3 4 5; 7 8 9 1 2 3 4 5 6; 8 9 1 2 3 4 5 6 7; 9 1 2 3 4 5 6 7 8] T7 = [1 2 3 4 5 6 7 8 9; 4 5 6 7 8 9 1 2 3; 7 8 9 1 2 3 4 5 6; 2 3 4 5 6 7 8 9 1; 5 6 7 8 9 1 2 3 4; 8 9 1 2 3 4 5 6 7; 3 4 5 6 7 8 9 1 2; 6 7 8 10 1 2 3 4 5; 9 1 2 3 4 5 6 7 8] T8 = [2 1 3 4 5 6 7 8 9; 5 4 6 7 8 9 1 2 3; 4 3 5 6 7 8 9 1 2; 8 7 9 1 2 3 4 5 6; 3 2 4 5 6 7 8 9 1; 6 5 7 8 9 1 2 3 4; 9 8 1 2 3 4 5 6 7; 7 6 8 9 1 2 3 4 5; 1 9 2 3 4 5 6 7 8] function testControleSudoku() nJuist = 0; nFout = 0; if(controleSudoku(S1)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(controleSudoku(S2)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T1)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T2)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T3)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T4)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T5)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T6)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T7)) then nJuist = nJuist +1; else nFout = nFout + 1; end if(~controleSudoku(T8)) then nJuist = nJuist +1; else nFout = nFout + 1; end disp("Aantal correct gecontroleerde sudoku puzzels = ");disp(nJuist); disp("Aantal niet correct gecontroleerde sudoku puzzels = ");disp(nFout); endfunction testControleSudoku()
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//Solutions to Problems In applied mechanics //A N Gobby clear all; clc //initialisation of variables w=20//cwt q=3//ft d=30//ft/ss w1=4//ft w2=6//in h=2240//ft/s g=32.2//ft s=15//ft f=4.5//ft c=2.25//ft //CALCULATIONS T=(h*(d)^2/(g*s*q))//lbf G=T*q//lbf ft W=h*f/2//lbf ft R=186.5//lbf D=h-R//lbf r=(q*h*d^2/(c*h)/g)//ft //RESULTS printf('the equal moment of the centrifugal force=% f ft',r)
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// this is a implement of a kalman filter function kf = kalman_filter_init(A, B, C, X0, P0, u, Q, R) // A, the system matrix // B, the control matrix // C, the transfer matrix // X0, the initial state of the system // P0, the coinvariance matrix of the initial state, default 0. // u, the control vector of the system // Q, the coinvariant of the predict, there might be some disturbance or errors // R, the coinvariant of the measured value // H, the scale matrix between the state and the measured value // kf, the struct of the kalman filter kf = struct('A', A, 'B', B, 'C', C, 'X', X0, 'u', u, 'P', P0, 'Q', Q, 'R', R); endfunction function kf = kalman_filter_predict(kf) // kf, the struct of the kalman filter kf.X = kf.A * kf.X + kf.B * kf.u; kf.P = A * kf.P * A' + kf.Q; endfunction function kf = kalman_filter_update(kf, Z) // kf, the struct of the kalman filter // K, the kalman gain // Z, the measured vector K = kf.P * kf.C' * inv( kf.C * kf.P * kf.C' + kf.R); kf.X = kf.X + K * (Z - kf.C * kf.X); kf.P = kf.P - K * kf.C * kf.P; endfunction
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// part - I // Dsa = GMR of phase a in section - I // (r'Da1a2)(Da1a2r')^(1/4) = sqrt(r'Da1a2) // Da1a2 = sqrt(D^2 + 4d^2) printf(" Dsa = sqrt(r * sqrt(D^2 + 4*d^2))") // Dsb = GMR of phase b in section - II // Dsb = sqrt(r * Db1b2) // Db1b2 = D printf(" Dsb = sqrt(rD) ") // Dsc = GMR of phase c in section - I // = sqrt(r'Dc1c2) // Dc1c2 = sqrt(D^2 + rd^2) printf(" Dsc = sqrt(r * sqrt(D^2 + 4*d^2))") // part - II // Dab = Mutual GMD between phase a and b in section I of the trasportation cycle. printf(" Dab = sqrt(d * sqrt(d^2 + D^2))") printf(" Dbc = sqrt(d * sqrt(d^2 + D^2))") printf(" Dca = sqrt(2d * D)") // part - III // GMD for fictitious equilateral spacing printf ( " Ds = (r)^(1/2) * (D^2 * 4d^2)^(1/6)*D^(1/6)") // so the inductance per phase is, printf(" L = 2 * 10^-4 * log((2^(1/6)*(D^2+d^2)^(1/6) * d^(1/2))/(r^(1/2) * (D^2 + 4d^2)^(1/6))) H/km" )
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//clear// clear; clc; //Example 18.7 //Given xF = 0.40; P = 1; //[atm] D = 5800; //[kg/h] R = 3.5; LbyV = R/(1+R); //Solution //Physical properties of methanol M = 32; Tnb = 65; //[C] rho_v = M*273/(22.4*338); //[kg/^3] rho_l_0 = 810; //[kg/m^3], At 0C, from Perry, Chemical Engineers' Handbook rho_l_20 = 792; //[kg/m^3], At 20C, from Perry, Chemical Engineers' Handbook rho_l = 750; //[kg/m^3], At 65C sigma = 19; //[dyn/cm], from Lange's Handbook of Chemistry //(a) //Vapor velocity and column diameter //Using Fig. 18.28, the abscissa is abscissa = LbyV*(rho_v/rho_l)^(1/2); //for 18-in. plate spacing Kv = 0.29; //Allowable vapor velocity uc = Kv*((rho_l-rho_v)/rho_v)^(1/2)*(sigma/20)^(0.2)/(3.2825112); //[ft/s] //From Eq.(18.71), the F factor is F = uc*sqrt(rho_v); disp(F,'the value of F factor is')
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// Exa 6.19 clc; clear; close; // Given data V_GS = 10;// in V I_G = 0.001;// in µA R_GS = V_GS/I_G;// in MΩ disp(R_GS,"The gate source resistance in MΩ is");
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// Método da Bisseção // // encontra uma raiz no intervalo [xa,xb] da função f(x)=x^3-9*x+3 // deff('y=f(x)','y=x^3-9*x+3'); // função f(x) xa= 2.0; // valor inicial de xa xb= 3.0; // valor inicial de xb epsilon=0.0000001; // tolerância Nmax=100; // número máximo de iterações i=0; // contador while (abs(xb-xa)>epsilon) & (i<Nmax) i=i+1; xm=(xa+xb)/2; if f(xa)*f(xm)<0 then xb=xm; else xa=xm; end; end; disp(xm) // exibe o último valor de xm calculado disp(i) // exibe o número de iterações executadas
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//Example 26_5 clc(); clear; //To find the energy difference between the n is 1 and n is 2 level e1=1 //Units in eV lamda2=1240 //Units in eV lamda3=0.07 //Units in eV e2=lamda2/lamda3 //Units in eV e=e2-e1 //Units in eV printf("The energy difference between n=1 and n=2 level is E=%d eV",e) //In textbook answer is prinred wrong as E=18000 eV the correct answer is E=17713 eV
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// sum 14-5 clc; clear; P=16*10^3; N=1000; w=2*%pi*N/60; T=P/w; Ks=1.4; Td=T*Ks; Tas=40; d=16*T*10^3/(%pi*Tas); d=d^(1/3); d=32; d1=2*d; l=1.5*d; ds=1.5*d; Tak=40; sigack=70; Ftk=Td*2/d; b=Ftk*10^3/(l*Tak); t=2*Ftk*10^3/(sigack*l); Taf=10; tf=Td*10^3*2/(%pi*Taf*d1^2); Ftb=Td*10^3/(1.5*d*4); Tab=40; db=sqrt(Ftb*4/(Tab*%pi)); D=4*d; trp=d/6; Ftb1=Td*10^3/(45*4); db1=sqrt(Ftb1*4/(Tab*%pi)); // printing data in scilab o/p window printf("d is %0.0f mm ",d); printf("\n b is %0.0f mm ",b); printf("\n t is %0.0f mm ",t); printf("\n db is %0.2f mm ",db); printf("\n db1 is %0.2f mm ",db1); //The answer to Key thickness 't' is calculated incorrectly in the book.
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(unwatch all) (clear) (progn (bind ?old (set-sequence-operator-recognition TRUE)) (load "gnrcexe.clp") (set-sequence-operator-recognition ?old)) (dribble-on "gnrcexe.out") (testit) (dribble-off) (clear) (open "gnrcexe.rsl" gnrcexe "w") (load "compline.clp") (printout gnrcexe "gnrcexe.clp differences are as follows:" crlf) (compare-files gnrcexe.exp gnrcexe.out gnrcexe) (close gnrcexe)
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clc; //e.g 3.18 RH=160; rho=0.16; mun=(1/rho)*RH; disp('cm^2/volt-sec',mun*1,"mu=");
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clc; funcprot(0); //Example 10.6 Induced drag of tappered wings // Initialisation of variables b = 46; w = 4; c = 8; r = 2; //data from figure 10.9 CO = sqrt(6^2+19^2); CH = sqrt(19.93^2 - 2^2); EOH = atand(6/19); COH = acosd(2/19.93); GOH = 270 - EOH - COH; Area_ABCD = 2*c; Area_BGOC = 19*(2+8)*0.5; Area_COH = 0.5*r*CH; Area_GOH = GOH/360*(%pi*r^2); // Calculations Area_half_wing = Area_ABCD + Area_BGOC + Area_COH + Area_GOH; S = 2*Area_half_wing; AR = b^2/S; //Results disp(AR,"Required aspect ratio :" );
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function y = f(x) y = x^2 - 6; endfunction function [p,it] = falsa_posicion(p0,p1,tol,maxit) it = maxit; p = zeros(maxit,1); q0 = f(p0); q1 = f(p1); for i=1:maxit p(i) = p1 - q1*(p1 - p0)/(q1 - q0); if(abs(p(i)-p1)<tol) it = i; return; end q = f(p(i)); if(q*q1 < 0) p0 = p1; q0 = q1; end p1 = p(i); q1 = q; end endfunction
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// Calculate the output of successive approximation A/D clc; disp('Set d3=1') Output=5/2^1; disp('since 3.217>2.5 so d3=1') disp('Set d2=1') Output=(5/2^1)+(5/2^2); disp('since 3.217< 3.75 so d2=0') disp('Set d1=1') Output=(5/2^1)+(5/2^3); disp('since 3.217>3.125 so d1=1') disp('Set d0=1') Output=(5/2^1)+(5/2^3)+(5/2^4); disp('since 3.217<3.4375 so d0=0') disp('Output of successive approximation A/D = 1010')
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//chapter 4 //example 4.10 //page 118 clear all; clc ; //given Ic=2;//collector current mA Vce=5;//collector to emitter voltage V Vcc=9;//supply voltage +-V hfe=70; Vbe=0.7; Ie=Ic; VR3=Vcc-Vbe; R3=VR3/Ic; printf("\nR3=%.2f kohm,standard value 3.9 kohm",R3);R3=3.9; Ic=VR3/R3; Ie=Ic; VR2=Vcc-Vce+Vbe; R2=VR2/Ic; printf("\nR2=%.1f kohm,standard value 2.2 kohm",R2);R2=2.2; Ibmax=1000*Ic/hfe; //VR1<<Vbe VR1=1000*Vbe/10; R1=VR1/Ibmax; printf("\nR1=%.1f kohm,standard value 2.2 kohm",R1);
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@relation relation @attribute sepalLength real [4.3, 7.9] @attribute sepalWidth real [2.0, 4.4] @attribute petalLength real [1.0, 6.9] @attribute petalWidth real [0.1, 2.5] @attribute class {Iris-setosa, Iris-versicolor, Iris-virginica} @data Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-setosa Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-virginica Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-versicolor Iris-virginica Iris-virginica Iris-virginica Iris-versicolor Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-versicolor Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica Iris-virginica
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@relation tae @attribute Native integer[1,2] @attribute Instructor integer[1,25] @attribute Course integer[1,26] @attribute Semester integer[1,2] @attribute Size integer[3,66] @attribute Class{1,2,3} @inputs Native,Instructor,Course,Semester,Size @outputs Class @data 3 3 2 2 2 1 2 2 2 1 1 1 1 2 3 3 3 3 3 3 3 3 2 2 2 2 1 1 1 1 3 3 3 3 3 3 3 2 3 2 2 3 2 1 1 1 1 3 1 3 1 1 1 1 1 1 2 1 2 2
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// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/01/Mux.tst load Exercise1.hdl, output-file Exercise1.out, compare-to Exercise1.cmp, output-list Studied%B7.1.7 hadBreakfast%B7.1.7 isFailed%B7.1.7; set Studied 0, set hadBreakfast 0, eval, output; set Studied 0, set hadBreakfast 1, eval, output; set Studied 1, set hadBreakfast 0, eval, output; set Studied 1, set hadBreakfast 1, eval, output;
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//SimpleAddVME.tst load SImpleAdd.vm, output-file SimpleAdd.out, compare-to SimpleAdd.cmp, output-list RAM[0]%D2.6.2 RAM[256]%D2.6.2; set RAM[0] 256; repeat 3 { vmstep; } output;
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// Scilab Code Ex12.6: Page-444 (2014) clc; clear; Z = 92; // Atomic number of U-238 A = 238; // Mass number of U-238 E_Coul = 0.72*Z*(Z-1)*A^(-1/3); // Total Coulomb energy of U-238, MeV printf("\nThe total Coulomb energy of U-238 = %3d MeV", E_Coul); // Result // The total Coulomb energy of U-238 = 972 MeV
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//fiber optic communications by joseph c. palais //example 5.4 //OS=Windows XP sp3 //Scilab version 5.4.1 clc clear all //given led_output_power=2//led output power in dBm fiber_loss=0.5//fiber loss /dB receiver_sensitivity=30//receiver sensitivity in dBm coupling_loss=16//coupling loss in dB connector_and_splices=6//connector and splices loss in dB power_margin=4//power margin in dB //to find loss_budget=led_output_power+receiver_sensitivity;//loss budget in dB total_losses=coupling_loss+connector_and_splices+power_margin;//total losses in dB available_fibre_loss=loss_budget-total_losses;//available fibre loss in dB maximum_allowable_fibre =available_fibre_loss/fiber_loss;//maximum allowable fibre length in Km mprintf(' Maximum allowable fibre length=%fKm',maximum_allowable_fibre)
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Chap4_Ex12_R1.sce
// Y.V.C.Rao ,1997.Chemical Engineering Thermodynamics.Universities Press,Hyderabad,India. //Chapter-4,Example 12,Page 110 //Title:Final temperature Pressure work done and heat interaction in polytropic process //================================================================================================================ clear clc //INPUT volume_ratio=1/15;//final volume to the initial volume of ideal gas at the end of compression (no unit) T1=300;//initial temperature of ideal gas in K P1=0.1;//initial pressure of ideal gas in MPa R=8.314;//universal gas constant in J/molK n=1.2;//index of expansion (no unit) gaamma=1.4;//ratio of the molar heat capacities at constant pressure and constant volume for ideal gas (no unit) //CALCULATION P2=P1*((1/volume_ratio)^n);//calculation of final pressure in MPa using Eq.(4.37) T2=T1*(P2/P1)*(volume_ratio);//calculation of final temperature in K (since the gas is taken to be ideal, (P1*V1)/T1=(P2*V2)/T2)) W=(R*(T1-T2)*10^-3)/(n-1);//calculation of work to be done on the system in kJ/mol using Eq.(4.38) del_u=(R*(T2-T1)*10^-3)/(gaamma-1);//calculation of the change in the internal energy in kJ/mol using Eq.(4.28 and 4.29) (del_u=Cv*(T2-T1) and Cv=R/(gaamma-1)) q=del_u+W;//calculation of the heat interaction during the process in kJ/mol using the first law of thermodynamics //OUTPUT mprintf('\n The final pressure= %0.3f MPa\n',P2); mprintf('\n The final temperature= %0.1f K\n',T2); mprintf('\n Work done on the gas= %f kJ/mol\n',W); mprintf('\n Heat interaction during the process= %f kJ/mol\n',q); //===============================================END OF PROGRAM===================================================
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clear; clc; // Stoichiometry // Chapter 2 // Basic Chemical Calculations // Example 2.25 // Page 40 printf("Example 2.25, Page 40 \n \n"); // solution p = 4 //[bar] T = 773.15 //[K] R = .083145 V = R*T/p // [l/mol] molar volume printf("Molar volume = "+string(V)+" l/mol.\n \n \n") // using appendix III // calculating Tc and Pc of different gases according to their mass fractions Tc1 = .352*32.20 // H2 Tc2 = .148*190.56 // methane Tc3 = .128*282.34 //ethylene Tc4 = .339*132.91 // CO Tc5 = .015*304.10 // CO2 Tc6 = .018*126.09 // N2 Tc = Tc1+Tc2+Tc3+Tc4+Tc5+Tc6 // Tc of gas // similarly finding Pc Pc1=.352*12.97 Pc2=.148*45.99 Pc3=.128*50.41 Pc4=.339*34.99 Pc5=.015*73.75 Pc6=.018*33.94 Pc=Pc1+Pc2+Pc3+Pc4+Pc5+Pc6 // Pc of gas a = (27*R^2*Tc^2)/(64*Pc) // [bar/mol^2] b = (R*Tc)/(8*Pc) // l/mol // substituting these values in vanderwall eq and solving by Newton Rhapson method we get V = 15.74 // [l/mol] printf("by Vanderwall eq molar volume = "+string(V)+" l/mol")
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//Engineering and Chemical Thermodynamics //Example 8.5 //Page no :378 clear ; clc; //Given P1_sat = 0.72 ; //[bar] P2_sat = 0.31 ; //[bar] A = 3590 ; B = -1180 ; R = 8.314 ; T = 70 + 273 ;//[K] function y85 = f85(x1) , y85 = -.48 + ( x1 * exp((A + 3*B) * (1 - x1)^2 / (R * T) - 4 * B * (1 - x1)^3 / (R * T)) * P1_sat) / ( x1 * exp((A + 3*B) * (1 - x1)^2 / (R * T) -4 * B * (1 - x1)^3 / (R * T)) * P1_sat +(1 - x1) * exp((A - 3*B) * x1^2 / (R * T) -4 * B * x1^3 / (R * T)) * P2_sat ) ; endfunction y = fsolve([0.1],f85); x1 = y ; P = ( x1 * exp((A + 3*B) * (1 - x1)^2 / (R * T) - 4 * B * (1 - x1)^3 / (R * T)) * P1_sat) + (1 - x1) * exp((A - 3*B) * x1^2 / (R * T) -4 * B * x1^3 / (R * T)) * P2_sat ; disp(" Example: 8.5 Page no : 378") ; printf("\n The value of x1 = %.3f\n\n",y) ; printf(" Pressure = %.2f bar",P) ;
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//Author: Parthasarathi Panda //parthasarathipanda314@gmail.com //ss2sos converts a state-space representation of a given digital filter to an equivalent second-order section representation. ////Example: //a =[0.5095,0,0,0,0; //0.3007, 0.2260, -0.3984, 0, 0; //0.0977, 0.3984, 0.8706, 0, 0; //0.0243, 0.0991, 0.4652, 0.5309, -0.4974; //0.0079, 0.0322, 0.1512, 0.4974, 0.8384]; // // //b =[0.6936 0.1382 0.0449 0.0112 0.0036]' // // //c =[0.0028 0.0114 0.0534 0.1759 0.6500] // // //d =0.0013 //[sos,g]=ss2sos(a,b,c,d) //Expected output: //g = // 0.0013 // sos = // 1. 1.2679417 0.6443293 1. - 1.0966 0.3554782 // 1. 3.1480112 3.2063892 1. - 1.3693 0.6925133 // 1. 0.4742625 0. 1. - 0.5095 0. // function [sos,g]=ss2sos(A,B,C,D) //not taking if, order and scale as input since they do not seem useful if (type(A)~=1 | type(B)~=1 | type(C)~=1 | type(D)~=1) then error('check input types'); end if (length(size(A))~=2 | length(size(B))~=2 | length(size(C))~=2 | length(size(D))~=2) then error('input must be 2d matrices'); end if (norm(imag(A))~=0 | norm(imag(B))~=0 | norm(imag(C))~=0 | norm(imag(D))~=0) then error('input must be real matrices'); end //cross checking dimensions of matrix if size(D)~=[1,1] then error('for single input single output, D must be 1 by 1'); end [n,k]=size(B); if k~=1 then error('for single input single output, B must be column matrix'); end [n,k]=size(C); if n~=1 then error('for single input single output, C must be row matrix'); end if size(A)==[1,1] then error('A must be square matrix'); end //obtaining the transfer function(continuous) tf=ss2tf(syslin('c',A,B,C,D)); //factorising the numerator and the denominator into second order systems [zero,gn]=sosbreak(numer(tf));//function is defined in the same folder [pole,gd]=sosbreak(denom(tf)); //reducing each pair of second order in the necessary form sos=[]; for i=[1:length(pole)] den=pole(i); // if no polynomial is left in the numerator if i>length(zero) then //z^(-1) is in the numerator if the denominator in linear if degree(den)==1 then b=[0,1,0]; //z^(-2) is in the numerator if the denominator is quadratic else b=[0,0,1]; end //if polynomial is left else b=coeff(zero(i));//obtain coefficient of the polynomial b=[b,zeros(1,degree(den)+1-length(b))];//add a zero in the end if the numerator is linear and denominator is quadratic b=b($:-1:1);//reverse the coefficients b=[b,zeros(1,3-length(b))];//add a zero if both numerator and denominator are linear end a=coeff(den);//coefficient of the denominator a=a($:-1:1);//reversing the coefficients a=[a,zeros(1,3-length(a))];//adding zeros if the denominator is linear v=[b,a]; sos=[sos;v]//adding the second order sub-system end g=gn/gd;//computing the gain endfunction
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pathname=get_absolute_file_path('5_20.sce') filename=pathname+filesep()+'5_20data.sci' exec(filename) V1=sqrt(2*Wt/(D*S*Clm));disp(V1,"V1=","V1=sqrt(2*Wt/(D*S*Clm))","stalling speed for full fuel tank V1:") V2=sqrt(2*Wf/(D*S*Clm));disp(V2,"V2=","V2=sqrt(2*Wf/(D*S*Clm))","stalling speed for empty fuel tank V1:") printf("\Answer:\n") printf("\n\stalling speed for full fuel tank : %f m/s\n\n",V1) printf("\n\stalling speed for empty fuel tank : %f m/s\n\n",V2)
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2016-08-01T14:45:40
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KalmanFilter.sci~
// Object Tracking using Kalman Filter // // Calling Sequence // KalmanFilterKalmanFilter("FileName",<value>,"dynamParams",<value>,"measureParams",<value>,"controlParams",<value>, // "type",<value>,"colour",<value>,"drawpath",<value> // "delay",<value>) // // Parameters // int dynamparams- This specifies the state dimensionality. // int measureparams- This specifies the measurement dimensionality // int controlparams- This specifies the control vector values // int type- This specifies the datatype of frames in the video // string colour- This specifies the colour of the object to be tracked // bool drawpath- This specifies whether you want the path of the moving object to be drawn // bool delay - This specifies whether video playback show be slower or not. // // Description // The function tracks the object using Kalman Filter. The red box is the object being // detected using Kalman Filter method wheras the green box is the same except the method used // here are basic image processing techniques to detect the object in the video frame. // // Examples // //Performing Object Tracking on green ball // KalmanFilter("FileName","singleball.avi","colour","green","delay","true","drawpath","true") // //Performing Object Tracking on red juggling ball // KalmanFilter("FileName","juggling.mp4","colour","red","drawpath","false"); // // Author // Kevin George //
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e133f6a9b73e66f8c6879c47278fc5723f459785
36c5f94ce0d09d8d1cc8d0f9d79ecccaa78036bd
/1x1 SMG Duel Gauntlet v2.sce
f98157c380ce40814768a8aa2f0627b30ef1adbe
[]
no_license
Ahmad6543/Scenarios
cef76bf19d46e86249a6099c01928e4e33db5f20
6a4563d241e61a62020f76796762df5ae8817cc8
refs/heads/master
2023-03-18T23:30:49.653812
2020-09-23T06:26:05
2020-09-23T06:26:05
null
0
0
null
null
null
null
UTF-8
Scilab
false
false
24,345
sce
1x1 SMG Duel Gauntlet v2.sce
Name=1x1 SMG Duel Gauntlet v2 PlayerCharacters=Quaker BotCharacters=ROT.rot IsChallenge=true Timelimit=120.0 PlayerProfile=Quaker AddedBots=ROT.rot PlayerMaxLives=1 BotMaxLives=6 PlayerTeam=0 BotTeams=0 MapName=1x1_cone.map MapScale=3.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=0.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=1.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag= WeaponHeroTag=SMG DifficultyTag=5 AuthorsTag=Tropycs, kidded BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=An improved 1x1 SMG Duel Gauntlet featuring aim profile tweaks, endomorphic viewmodels, ands revised scoring. GameVersion=2.0.2.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.1 MBSTime2=0.25 MBSTime3=100.0 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=true LockedFOVMin=103.0 LockedFOVMax=103.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=LVL1 MinReactionTime=0.275 MaxReactionTime=0.3 MinSelfMovementCorrectionTime=0.005 MaxSelfMovementCorrectionTime=0.08 FlickFOV=40.0 FlickSpeed=1.0 FlickError=0.0 TrackSpeed=1.0 TrackError=0.0 MaxTurnAngleFromPadCenter=60.0 MinRecenterTime=0.375 MaxRecenterTime=0.425 OptimalAimFOV=40.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=50.0 VerticalAimOffset=0.0 MaxTolerableSpread=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [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=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Aim Profile] Name=LVL2 MinReactionTime=0.25 MaxReactionTime=0.275 MinSelfMovementCorrectionTime=0.004 MaxSelfMovementCorrectionTime=0.07 FlickFOV=37.0 FlickSpeed=1.1 FlickError=10.0 TrackSpeed=1.3 TrackError=0.0 MaxTurnAngleFromPadCenter=63.0 MinRecenterTime=0.35 MaxRecenterTime=0.4 OptimalAimFOV=37.0 OuterAimPenalty=1.0 MaxError=57.0 ShootFOV=47.0 VerticalAimOffset=0.0 MaxTolerableSpread=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Aim Profile] Name=LVL3 MinReactionTime=0.225 MaxReactionTime=0.25 MinSelfMovementCorrectionTime=0.003 MaxSelfMovementCorrectionTime=0.06 FlickFOV=34.0 FlickSpeed=1.2 FlickError=0.0 TrackSpeed=1.6 TrackError=0.0 MaxTurnAngleFromPadCenter=66.0 MinRecenterTime=0.35 MaxRecenterTime=0.375 OptimalAimFOV=34.0 OuterAimPenalty=1.0 MaxError=54.0 ShootFOV=44.0 VerticalAimOffset=0.0 MaxTolerableSpread=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Aim Profile] Name=LVL4 MinReactionTime=0.225 MaxReactionTime=0.25 MinSelfMovementCorrectionTime=0.002 MaxSelfMovementCorrectionTime=0.06 FlickFOV=31.0 FlickSpeed=1.3 FlickError=0.0 TrackSpeed=1.9 TrackError=0.0 MaxTurnAngleFromPadCenter=69.0 MinRecenterTime=0.325 MaxRecenterTime=0.375 OptimalAimFOV=31.0 OuterAimPenalty=1.0 MaxError=51.0 ShootFOV=41.0 VerticalAimOffset=0.0 MaxTolerableSpread=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Aim Profile] Name=LVL5 MinReactionTime=0.175 MaxReactionTime=0.2 MinSelfMovementCorrectionTime=0.002 MaxSelfMovementCorrectionTime=0.05 FlickFOV=29.0 FlickSpeed=1.4 FlickError=0.0 TrackSpeed=2.1 TrackError=0.0 MaxTurnAngleFromPadCenter=71.0 MinRecenterTime=0.3 MaxRecenterTime=0.35 OptimalAimFOV=29.0 OuterAimPenalty=1.0 MaxError=49.0 ShootFOV=39.0 VerticalAimOffset=0.0 MaxTolerableSpread=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Aim Profile] Name=LVL6 MinReactionTime=0.175 MaxReactionTime=0.2 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.04 FlickFOV=36.0 FlickSpeed=1.5 FlickError=0.0 TrackSpeed=2.4 TrackError=0.0 MaxTurnAngleFromPadCenter=74.0 MinRecenterTime=0.3 MaxRecenterTime=0.325 OptimalAimFOV=26.0 OuterAimPenalty=1.0 MaxError=46.0 ShootFOV=36.0 VerticalAimOffset=0.0 MaxTolerableSpread=0.0 MinTolerableSpread=0.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=1.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=LVL1 DodgeProfileNames=Long Strafes;Short Strafes DodgeProfileWeights=1.8;1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=LVL1;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=1.0 UseWeapons=true CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.000 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=LVL2 DodgeProfileNames=Long Strafes;Short Strafes DodgeProfileWeights=1.6;1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=LVL2;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=1.0 UseWeapons=true CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.000 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=LVL3 DodgeProfileNames=Long Strafes;Short Strafes DodgeProfileWeights=1.4;1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=LVL3;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=1.0 UseWeapons=true CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.000 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=LVL4 DodgeProfileNames=Long Strafes;Short Strafes DodgeProfileWeights=1.2;1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=LVL4;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=1.0 UseWeapons=true CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.000 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=LVL5 DodgeProfileNames=Long Strafes;Short Strafes DodgeProfileWeights=1.0;1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=LVL5;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=1.0 UseWeapons=true CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.000 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=LVL6 DodgeProfileNames=Long Strafes;Short Strafes DodgeProfileWeights=1.0;1.2 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=LVL6;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=1.0 UseWeapons=true CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.000 Z=0.000 LaserAlpha=1.0 [Bot Rotation Profile] Name=ROT ProfileNames=LVL1;LVL2;LVL3;LVL4;LVL5;LVL6 ProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0 Randomized=false [Character Profile] Name=Quaker MaxHealth=300.0 WeaponProfileNames=SMG;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.7 CrouchAnimationSpeed=1.8 CameraOffset=X=0.000 Y=0.000 Z=100.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=300.0 MaxCrouchSpeed=150.0 Acceleration=3000.0 AirAcceleration=16000.0 Friction=0.0 BrakingFrictionFactor=0.0 JumpVelocity=0.0 Gravity=100.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false 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=140.0 MainBBRadius=25.0 MainBBHasHead=true MainBBHeadRadius=18.0 MainBBHeadOffset=-18.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=150.0 ProjBBRadius=30.0 ProjBBHasHead=true ProjBBHeadRadius=18.0 ProjBBHeadOffset=-18.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.1 StrafeSpeedMult=0.8 BackSpeedMult=0.75 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=0.8 HealthRegainedonkill=300.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=true TPSArmLength=180.0 TPSOffset=X=0.000 Y=60.000 Z=-100.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=Endo CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Quaker Bot MaxHealth=300.0 WeaponProfileNames=SMG;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.7 CrouchAnimationSpeed=1.8 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=300.0 MaxCrouchSpeed=150.0 Acceleration=3000.0 AirAcceleration=16000.0 Friction=0.0 BrakingFrictionFactor=0.0 JumpVelocity=0.0 Gravity=100.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false 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=140.0 MainBBRadius=25.0 MainBBHasHead=true MainBBHeadRadius=18.0 MainBBHeadOffset=-18.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=150.0 ProjBBRadius=30.0 ProjBBHasHead=true ProjBBHeadRadius=18.0 ProjBBHeadOffset=-18.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.1 StrafeSpeedMult=0.8 BackSpeedMult=0.75 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=true LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=0.8 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=200.0 TPSOffset=X=0.000 Y=60.000 Z=-100.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=Endo CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Long Strafes MaxTargetDistance=300.0 MinTargetDistance=150.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=1.0 MaxLRTimeChange=1.5 MinFBTimeChange=1.0 MaxFBTimeChange=1.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.1 TargetStrafeOverride=Oppose TargetStrafeMinDelay=0.14 TargetStrafeMaxDelay=0.3 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=1.0 BlockedMovementReactionMin=0.1 BlockedMovementReactionMax=0.15 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Dodge Profile] Name=Short Strafes MaxTargetDistance=150.0 MinTargetDistance=75.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=0.8 MinFBTimeChange=0.5 MaxFBTimeChange=0.8 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Mimic TargetStrafeMinDelay=0.13 TargetStrafeMaxDelay=0.2 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.4 MaxCrouchTime=0.5 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=1.0 BlockedMovementReactionMin=0.1 BlockedMovementReactionMax=0.15 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=SMG 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 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//Example 2_3 clc(); clear; //To calculate the minimum number of lines lemda=5890 //units in angstrom lemda=5890*10^-8 //units in centimeters dlemda=6*10^-8 //units in centimeters k=2 width=2.5 //units in centimeters n=(lemda/(k*dlemda))/width printf("no of lines per cm is %.1f",n)
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N=10; resAbs=zeros(N); resOrd=zeros(N); function [y]= f(x) y= cos(x); endfunction function y=Trapeze(resAbs,resOrd,a,b,N) for i=a:(b-a)/(N-1):b resAbs(i )= i; resOrd(i) = f(i); end y=1 endfunction y=Trapeze(resAbs,resOrd,0,2,N); //v = inttrap(resAbs, resOrd)
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//Example 11.1 (a) //Program to Calculate Resonant Frequency of the given Circuit clear; clc ; close ; //Given Circuit Data C=300*10^(-12); //F L=220*10^(-6); //H R=20; //Ohms //Calculation fr=1/(2*%pi*sqrt(L*C)); //Displaying The Results in Command Window printf("\n\t The Resonant Frequency, fr = %f kHz .",fr/10^3);
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// Exa 3.14 clc; clear; close; // Given data bita=100; hFE= 100; VCEsat= 0.2;// in V VBEsat= 0.8;// in V VBEactive= 0.7;// in V VBB= 5;// in V VCC= 10;// in V R_C= 3;// in kΩ R_C=R_C*10^3;// in Ω R_B= 50;// in kΩ R_B=R_B*10^3;// in Ω // Formula VCC= ICsat*R_C+VCEsat ICsat= (VCC-VCEsat)/R_C;//A disp(ICsat*10^3,"The value of IC(sat) in mA is : ") IBmin= ICsat/bita;// in A // Apply KVL to input circuit, VBB= IB*R_B+VBEsat IB= (VBB-VBEsat)/R_B;// in A disp(IB*10^6,"Actual base current in µA is : ")
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//Chapter 24 Ex5 clc; clear; close; //consider breadht=x and length=2x as given. Thus solving statement we get following equation. //(2*x-5)(x+5)-2*x*x=75 and solving it we get x=(75+25)/5; mprintf("The length of rectangle is %d cm.",x);
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//page 187 //Example 6.3 clc; clear; close; disp('Standard ordered matrix for Linear operator T on R^3 is:'); A = [5 -6 -6; -1 4 2; 3 -6 -4]; disp(A,'A = '); disp('xI - A = '); B = eye(3,3); x = poly(0,"x"); P = x*B - A; disp(P); disp('Applying row and column transformations:'); disp('C2 = C2 - C3'); P(:,2) = P(:,2) - P(:,3); disp('=>'); disp(P); disp('Taking (x-2) common from C2'); c = x-2; P(:,2) = P(:,2) / (x-2); disp('=>'); disp(' * ', c); disp(P); disp('R3 = R3 + R2'); P(3,:) = P(3,:) + P(2,:); disp('=>'); disp(' * ', c); disp(P); P = [P(1,1) P(1,3); P(3,1) P(3,3)]; disp('=>'); disp(' * ', c); disp(P); disp('=>'); disp(' * ',c); disp(det(P)); disp('This is the characteristic polynomial'); disp(A-B,'Now, A - I = '); disp(A-2*B,'And, A- 2I = '); disp(rank(A-B),'rank(A-I) = '); disp(rank(A-2*B),'rank(A-2I) = '); disp('W1,W2 be the spaces of characteristic vectors associated with values 1,2'); disp('So by theorem 2, T is diagonalizable'); a1 = [3 -1 3]; a2 = [2 1 0]; a3 = [2 0 1]; disp(a1,'Null space of (T- I) i.e basis of W1 is spanned by a1 = '); disp('Null space of (T- 2I) i.e. basis of W2 is spanned by vectors x1,x2,x3 such that x1 = 2x1 + 2x3'); disp('One example are;'); disp(a2,'a2 = '); disp(a3,'a3 = '); disp('The diagonal matrix is:'); D = [1 0 0 ;0 2 0;0 0 2]; disp(D,'D = '); disp('The standard basis matrix is denoted as:'); P = [a1;a2;a3]'; disp(P,'P = '); disp(A*P,'AP = '); disp(P*D,'PD = '); disp('That is, AP = PD'); disp('=> inverse(P)*A*P = D'); //end
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//Problem 13.04: //initializing the variables: DG0fH2O = -54635; // cal/gmol DG0fHCl = -22778; // cal/gmol //calculation: DG0298 = 1*DG0fH2O - 2*DG0fHCl printf("\n\nResult\n\n") printf("\n DG0298 of reaction is %.0f cal/gmol",DG0298)
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//Ex6_11 clc ic = 3*10^-3 ib = 3.08*10^-3 disp("ib = "+string(ib)+"A")//base current disp("ic = "+string(ic)+"A")//collector current alpha = ic/ib disp("alpha = ie/ib = ic/ib = "+string(alpha))//current gain, assuming ie = ic
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// Chapter 11_ Metal-Oxide-Semiconductor Field Effect Transistor:Additional Concepts //Caption_Narrow channel effects //Ex_3//page 520 Na=3*10^16 tox=450*10^-8 //oxide thickness fi=%pi/2 //fitting parameter delVt=0.2 Cox=7.67*10^-8 //oxide capacitance xdt=0.18*10^-4 W=10^4*e*Na*(fi*xdt^2)/(Cox*delVt) printf('The channel width that will limit the threshold voltage is %1.2f micrometer',W)
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// Chapter 5 Example 3 //============================================================================== clc; clear; //input data //α-Iron solidifies to BCC structure r = 1.273; // Atomic radius in angstrom N = 6.023*10^26; // Avagadros number in atoms/kilomole A = 55.85; // Atomic weight of α-Iron in kilograms n = 2; // No. of atoms per unit cell for BCC p = 7860; // density in kg/m^-3 //Calculations // p = (n*A)/(N*a^3); density a = ((n*A)/(N*p))^(1/3); // lattice constant a1 = a*10^10; // m to angstrom conversion r = (a1*sqrt(3))/4 // atomic radius for BCC //Output mprintf('The Radius of the atom = %3.5f Å\n',r); mprintf(' Note : atomic wt taken as 55.58*10^-3 instead of 55.85 in calculation') //==============================================================================
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path=sci+'/demos/bike/' // compile if necessary host("cd "+path+"; make simul"); // link if necessary deff('[]=linkif(fname)',['if ~c_link(fname) then'; 'link(''/tmp/''+fname+''.o'',fname);end']); linkif('gjx'); linkif('constr'); linkif('ii'); linkif('h'); // Macros made by Maple getf(path+'gjx.sci','c'); getf(path+'constr.sci','c'); getf(path+'ii.sci','c'); getf(path+'h.sci','c'); getf(path+'iihs.sci','c'); // Other macros getf(path+'show.sci','c'); getf(path+'macros.sci','c'); getf(path+'qinit.sci','c') iiww=read(path+'iiww.dat',222,2,"(e24.18)"); getf(path+'simulation.sci','c'); getf(path+'bike.sci','c'); exec(path+'param.sci'); getf(path+'velo1.sci','c'); getf(path+'velo2.sci','c'); getf(path+'velo3.sci','c'); getf(path+'velo4.sci','c');
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//Example No. 4.7 clc; clear; close; format('v',6); //Given Data : t_on=15;//min t_off=25;//min T=100;//min Tdash=140;//min theta_f=55;//degree C //theta=theta_f-(theta_f-theta1)*exp(-t/T) //theta1=theta*exp(-tdash/Tdash); theta_max=theta_f*[1-exp(-t_on/T)]/(1-exp(-(t_off/Tdash+t_on/T)));//degreeC disp(theta_max,"Maximum temperature rise in degree C : ");
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Turbomachinery Design and Theory,Rama S. R. Gorla and Aijaz A. Khan, Chapter 4, Example 5") disp("Impeller tip speed is given by") D = 0.914; N = 9000; U2 = %pi*D*N/60 disp("Since the exit is radial and no slip, Cw2 = U2 = 431 m/s") disp("From the velocity triangle,") alpha2 = 20; Cw2 = U2; Cr2 = U2*tan(alpha2 *%pi/180) disp("For radial exit, relative velocity is exactly perpendicular to rotational velocity U2. Thus the angle beta2 is 90degrees for radial exit.") disp("Using the velocity triangle") C2 = (U2^2 + Cr2^2)^0.5
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// Example 8.18.1 page 8.48 clc; clear; Cd=7d-12; B=9d6; Ca=7d-12; R=(2*3.14*Cd*B)^-1; B1=(2*3.14*R*(Cd+Ca))^-1; R=R/1000; B1=B1/10^6; printf("\nThus for 9MHz bandwidth maximum load resistance is %.2f Kohm\nNow if we consider input capacitance of following amplifier Ca then Bandwidth is %.2fMHz\nMaximum post detection bandwidth is half.",R,B1); //answer for resistance in the book is 4.51Kohm, deviation of 0.01Kohm, while for bandwidth it is 4.51 MHz, deviation of 0.01MHz
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clear; clc; // Stoichiometry // Chapter 4 // Material Balances involving Chemical Reaction // Example 4.13 // Page 138 printf("Example 4.13, Page 138 \n \n"); // solution m1 = 1200*1.2 //[kg] mass of reactants pOH1 = 14-6 //pOH of reactants pOH = 14-9 //pOH of final mass // ROWs = 1/sigma(Wi/ROWsi) //Ms = mass of .5% NaOH required //ROWs = density of final solution //ROWs = 1/{((m1*10^3*1)/(((m1*10^3+Ms)*1.2)+(Ms/((m1*10^3+Ms)*1.005))} (i) //balance of OH- ions //1200*10^-8 +Ms*10^-1.15/(1.005*10^-5) = (1200*1.2*10^3+Ms)*10^-5/ROWs*10^-5 (ii) //solving (i) and (ii) Ms = 170.21 //g ROWs = 1.2016 //[kg/l] printf("Mass of 0.5 percnt NaOH required to be added to raise the pH = "+string(Ms)+"g.")
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function [y,t]=modulate(x,fc,fs,method,opt) //Modulates signal according to the modulation method //Calling Sequence //y=modulate(x,fc,fs,method,opt) //[y,t]=modulate(x,fc,fs,method,opt) //Parameters //x //A vector or a matrix //fc //Carrier frequency //fs //Sampling frequency //method //Modulation Method //opt //An optional parameter required by certain modulation methods //Description //[y,t]=modulate(x,fc,fs,method,opt) //Returns the modulated vector y and the time vector 't' //Modulation is performed according to the following table // METHOD MODULATION SCHEME // 'am', Amplitude modulation, double side-band, suppressed carrier // 'amdsb-sc' opt not used. This is the default method. // 'amdsb-tc' Amplitude modulation, double side-band, transmitted carrier // opt is a scalar subtracted from x before multiplying x // with the carrier wave. It defaults to min(min(x)) so that // the input signal after offset is always non-negative // 'amssb' Amplitude modulation, single side-band // OPT not used. // 'fm' Frequency modulation // opt is the constant of frequency modulation. // opt = (fc/fs)*2*pi/max(max(abs(x))) by default // 'pm' Phase modulation // OPT is the constant of phase modulation. // opt = pi/max(max(abs(x))) by default // Phase lies between -pi and +pi // 'pwm' Pulse width modulation // opt='left' corresponds to left justified pulses. // opt='centered' correspondes to centered pulses. // The default value of opt is 'left'. // 'ppm' Pulse position modulation // opt is a scalar between 0 and 1 which specifies the pulse // width in fractions of the carrier period with default value 0.1. // 'qam' Quadrature amplitude modulation // opt is a matrix of the same size as X which is modulated in // quadrature with x. // // If x is a matrix, its columns are modulated. //Example //y = // // 1. 1. 0. 0. //Author //Ankur Mallick funcprot(0); if (argn(2)<3|argn(2)>5) then error('Incorrect number of input arguments.'); elseif (isreal(fc)&isreal(fs)&fc>fs/2) error('The career frequency must be less than half the sampling frequency.') else flag1=0; flag2=0; if (argn(2)<4) method='am'; end [M,N]=size(x); if(M==1) flag1=1; x=x(:); [M,N]=size(x); end t=((0:M-1)/fs)'; t=t*ones(1,N); if(method=='am'|method=='amdsb-sc') y=x.*cos(2*%pi*fc*t); elseif(method=='amdsb-tc') if(argn(2)<5) opt=min(min(x)); end y=(x-opt).*cos(2*%pi*fc*t); elseif(method=='amssb') y=x.*cos(2*%pi*fc*t)+imag(hilbert(x)).*sin(2*%pi*fc*t); elseif(method=='fm') if(argn(2)<5) opt=max(abs(x(:))); //if all elements of x are zero if(opt>0) opt=(fc/fs)*2*%pi/opt; end end y=cos(2*%pi*fc*t + opt*cumsum(x,1)); elseif(method=='pm') if(argn(2)<5) opt=%pi/(max(abs(x(:)))); end y=cos(2*%pi*fc*t + opt*x); elseif(method=='qam') if(argn(2)<5) error('For qam, a 5th input parameter is required.') else if(size(opt,1)==1) opt=opt(:); end S=sum(abs(size(opt)-size(x))); //S=0 only if opt and x have the same size if(S==0) y = x.*cos(2*%pi*fc*t) + opt.*sin(2*%pi*fc*t) else error('For qam input signals must be the same size') end end elseif(method=='pwm') if(argn(2)<5) opt='left' end if(max(x(:))>1|min(x(:))<0) error('x must lie between 0 and 1'); else t=(0:(M*fs/fc-1))'; t=t*ones(1,N); T=fs/fc; y=zeros(t); if(opt~='left'&opt~='centered') error('5th input parameter not recognized'); else if(opt=='left') compar=(pmodulo(t,T))/T; pos=floor(t/T)+1; elseif(opt=='centered') compar1=2*pmodulo(t,T)/T; compar=min(compar1,2-compar1); x(M+1,:)=zeros(1,N); pos=floor(t/T)+1; r1=ceil(T/2); r2=floor(T/2); pos=[pos(r1+1:length(pos));(M+1)*ones(r2,1)]; end for i=1:N //x1=matrix(ones(T,1)*x(:,i)',size(t,1),1); x1=x(pos,i) y(compar<x1,i)=1; end end end elseif(method=='ppm'|method=='ptm') if(argn(2)<5) opt=0.1 end t=(0:(M*fs/fc-1))'; t=t*ones(1,N); T=fs/fc; y=zeros(t); if(max(x(:))>1|min(x(:))<0) error('x must lie between 0 and 1'); elseif(~isscalar(opt)|opt<0|opt>1) error('opt must be a scalar between 0 and 1') else if (max(x) > 1-opt) warning('Overlapping pulses') end for i=1:N x1=x(:,i)' start=1+ceil((x1+(0:M-1))*T); //y(1) corresponds to t=0 L=floor(opt*T); v=(0:1:L-1)'; p1=matrix(ones(L,1)*start,1,M*L) p2=matrix(v*ones(1,M),1,M*L); pos=p1+p2; y(pos,i)=1; end y(length(t)+1:length(y),:)=[]; //Truncating vector end else error('Method not recognised'); flag2=1; end if(flag2==0) t=t(:,1); //only first column required if(flag1==1) //x is a row vector y=conj(y'); t=t'; end end end endfunction
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clc // initialization of variables clear // Loads and stresses and dimensions P=10 //kN Q=30 //kN S0=70 //MPa eps0=0.001 b1=400 //mm h=400 //mm b2=300 //mm A1=300 //mm^2 A2=300 //mm^2 // calculations // Units convertion P=P*10^3 Q=Q*10^3 S0=S0*10^6 b1=b1*10^-3 b2=b2*10^-3 h=h*10^-3 A1=A1*10^-6 A2=A2*10^-6 L1=sqrt(b1^2+h^2) L2=sqrt(b2^2+h^2) a=L1*(Q*b2+P*h)/(A1*S0*h*(b1+b2)) b=L2*(Q*b1-P*h)/(A2*S0*h*(b1+b2)) c=L1^2*eps0/(b1+b2) d=L2^2*eps0/(b1+b2) u=c*sinh(a)-d*sinh(b) v=b2/h*c*sinh(a)+b1/h*d*sinh(b) // results printf('u = %.4f mm',u*10^3) printf('\n v = %.4f mm',v*10^3)
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// Determine current through branch AB using loop and nodal analysis clc; clear; Is=4; // Current Source //Resistances Rab=2; R1=4;// After point B towards the right R2=1; V=10; // Voltage source //Using Simple Logic i1=Is; // Current source connected in series with resistor i2=10/(R1+R2); printf('The Current through branch AB: \n') printf('i) Simple Logic = %g A\n',i1) //Using Loop Analysis //Conversion of Current source into voltage source, R tends to infinity R=poly(0,'R'); Rmat=[R+2 0; 0 5]; Vmat=[(4*R)-V;V]; Imat=inv(Rmat)*Vmat; printf('\nii) Loop Analysis\n') disp(Imat(1,1),'The current through AB is') printf('\nWhere R tends to infinity\n') R=%inf; i1=(4-(V/R))/(1+(Rab/R)); printf('\n = %g A\n',i1) // Using Nodal Analysis // Conversion of voltage source into current source, R then tends to zero R=poly(0,'R'); // Nodal Eqaution //0.5V1-0.5V2+0V3 = 4 //-0.5V1+(0.75+(1/R))V2-0.25V3 = 10/R //0V1-0.25V2+1.25V3=0 Y=[0.5 -0.5 0;-0.5 (0.75+(1/R)) -0.25;0 -0.25 1.25]; // Admittance Matrix Im=[4; (10/R); 0] ; // Current Matrix Vm=inv(Y)*Im; // Voltage Matrix V1=Vm(1,1); V2=Vm(2,1); V3=Vm(3,1); DiffV=V1-V2; printf('\niii) Nodal Analysis:\n') disp(V2,'V2:',V1,'V1:') Vdiff=roots(DiffV(2)-R); // To change data type disp(DiffV,'V1-V2 :') In=Vdiff/Rab; // Current due to nodal analysis printf('\n The Current Through 2 ohm resistor = %g A\n',In )
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clc // Given that S_I1 = 5 // Surface irregulation in micro meter S_I2 = 8 // Surface irregulation in micro meter V = 12 // DC supply voltage in Volt k = 0.2 // Conductivity of electrolyte in ohm^-1-cm^-1 Vo = 1.5 // Total overvoltage in Volt F = 96500 // Faraday constant in coulombs per mole // Sample Problem 6 on page no. 353 printf("\n # PROBLEM 6.6 # \n") Y_min = (S_I1+S_I2)*(10^(-4)) A = 55.85 // Atomic gram weight of iron in gm Z = 2 // Valency of dissolation of iron D = 7.86 // Density of iron in gm/cm^3 f_max = (k*A*(V-Vo)/(Z*D*F*Y_min))*60 printf("\n Largest passible feed rate = %f mm/min",f_max*10)
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clc clear //Input data r=6//Compression ratio It=0.6//Indicated thermal efficiency ratio CV=10000//Calorific value in kcal/kg g=1.4//Ratio of specific heats //Calculations an=(1-(1/r)^(g-1))*100//Air standard efficiency in percent In=(It*(an/100))//Indicated thermal efficiency SFC=((4500*60)/(427*CV*In))//Specific fuel consumption in kg/I.H.P.hr //Output printf('Specific fuel consumption is %3.3f kg/I.H.P. hr',SFC)
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//chapter 6 //page no182 //Ex6_17 //given clear; clc; dV=50; //in mV di=4; //in Amp Cbypas=200; //in microF Lbypas=0.2; //in nH fL=di/(dV*10^-3*2*%pi*Cbypas*10^-6); printf("\n fLnoise = %0.0f kHz\n ",fL/1000); //Result misprinted fH=dV*10^-3/di/2/%pi/Lbypas/10^-9; printf("\n fHnoise = %0.0f MHz\n ",fH/10^6); Bw=fH-fL; printf("\n Bwnoise = %0.2f MHZ",Bw/10^6); //Result miscalculated
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Ex5_20.sce
clear // // // //Variable declaration n1=1.55 //Core refractive index n2=1.6 //Cladding refractive index theta1=60*%pi/180 //angle of incidence(radian) //Calculation x=n1*sin(theta1)/n2 theta2=asin(x)*180/%pi //angle of reflection(degrees) //Result printf("\n angle of reflection is %0.2f degrees",theta2)
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ex_3_10.sce
//Example 3.10 // Strength of solution clc; clear; //given data : l=2;//length of solution in decimeter theta=12;// angle of rotation in degree S=60;//specific rotation in degree C=theta/(S*l);// concentration in gm/cc disp(C,"strength of solution in gm/cc")