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printf("\texample 14.5\n"); printf("\tapproximate values are mentioned in the book \n"); st1=280; //°F vt6=125; //°F odT=st1-vt6; //°F printf("\tOverall temperature difference = %.0f °F\n",odT); //corresponding to 35 psig and 26 in. Hg bpr(1)=10; //°F bpr(2)=8; //°F bpr(3)=7; //°F bpr(4)=6; //°F bpr(5)=5; //°F bpr(6)=5; //°F i=1; tbpr=0; while(i<7) tbpr=tbpr+bpr(i); i=i+1; end printf("\tThe estimated total BPR = %.0f °F\n",tbpr); //from fig. 14.36a edT=odT-tbpr; printf("\tEffective temperature difference = %.0f °F\n",edT); printf("\n\t\t\t\tEVAPORATOR SUMMARY\n\tAll bodies will consist of 300 2 in. OD, 10 BWG tubes 24 long\n"); printf("\t------------------------------------------------------------------------------------------------------------------------------\n"); printf("\tItem\t\t\t\t\t\t\t\t\tEffects\n\t\t\t\t\t----------------------------------------------------------------------------------------------\n\t\t\t\t\t1A\t\t1B\t\t2\t\t3\t\t4\t\t5\n"); printf("\t------------------------------------------------------------------------------------------------------------------------------\n"); printf("\t1.Steam flow, lb/hr\t\t20000\n\t2.Steam pressure, psi/in.Hg\t35\t\t14.5\t\t4\t\t7\t\t16.5\t\t22\n\t3.Steam temp,°F\t\t\t280\t\t249\t\t224\t\t199\t\t174\t\t151\n\t4.delT,°F\t\t\t21\t\t17\t\t18\t\t19\t\t18\t\t21\n\t5.Liquor temp, °F\t\t259\t\t232\t\t206\t\t180\t\t156\t\t130\n\t6.BPR, °F\t\t\t10\t\t8\t\t7\t\t6\t\t5\t\t5\n\t7.Vapor temp, °F\t\t259\t\t232\t\t206\t\t180\t\t156\t\t130\n\t8.Vapor pressure, pis/in.Hg\t14.5\t\t4\t\t7\t\t6\t\t5\t\t5\n\t9.Lambda, Btu/lb\t\t946\t\t962\t\t978\t\t994\t\t1008\t\t1022\n\t10.Liquor in, lb/hr\t\t73400\t\t88300\t\t101000\t\t113000\t\t72000\t\t72000\n\t11.Liqour out, lb/hr\t\t56200\t\t73400\t\t88300\t\t101100\t\t58300\t\t54700\n\t12.Evaporation,lb/hr\t\t17200\t\t14900\t\t12800\t\t11900\t\t13700\t\t17300\n\t13.Total solids, \t\t38.9\t\t29.8\t\t24.7\t\t21.6\t\t18.7\t\t20.0\n\t14.A,ft^2\t\t\t3250\t\t3250\t\t3250\t\t3250\t\t3250\t\t3250\n\t15.UD,Btu/(hr)*(ft^2)*(°F)\t262\t\t295\t\t252\t\t251\t\t221\t\t221\n\t16.UD delT,Btu/(hr)*(ft^2)\t5510\t\t5000\t\t4530t\t\t4770\t\t3980\t\t4650\n");//BPR values from fig 14.36a //Specific-heat data are given in Fig. 14.36b ev(1)=17200; //lb/hr ev(2)=14900; //lb/hr ev(3)=12800; //lb/hr ev(4)=11900; //lb/hr ev(5)=13700; //lb/hr ev(6)=17300; //lb/hr i=1; tev =0; while(i<7) tev = tev+ev(i); i=i+1; end printf("\n\tTotal amount of water evaporated = %.0f lb/hr\n",tev); ttev=tev/6;//lb/hr printf("\tTheoretical amount of steam for a six-effect evaporator = %.0f lb/hr\n",ttev); tev2=tev/(6*0.75); //lb/hr . order of 75 percent of theoretical printf("\tSteam used for trail balance = %.0f lb/hr\n",tev2); lq=(tev/6); lq=lq+(lq*0.15); printf("\tEstimate of the amount of evaporation in the first effect = %.0f lb/hr\n",lq); lout6=54000;//lb/hr lq2=lout6+lq+2200;//lb/hr printf("\tEstimated discharge from second effect = %.0f lb/hr\n",lq2); printf("\n\t\t\t\tHEAT BALANCE\n"); cw = 17750000/(500*(125-15-60)); //gpm, values from table 14.6 printf("\t\tCooling water at 60 °F = %.0f gpm\n",cw); printf("\t--------------------------------------------------------\n"); printf("\tEffect\t\t\tBtu/hr\t\tEvaporation,l/hr\n"); printf("\t--------------------------------------------------------\n"); sf=20000;//lb/hr lqi=73400;//lb/hr lqi2=88300 lt1=259;//°F lt2=232;//°F lt3=206;//°F ev=17200;//lb/hr his=sf*924*0.97;//Btu/hr printf("\t1.a.Heat in steam \t%.2e\n",his); hl=lqi*(lt1-lt2)*0.82;//Btu/hr printf("\t b.Heating liquor \t%.2e\n",hl); hh=his-hl; ev1=(hh)/946;//lb/hr printf("\t c.Evaporation\t\t\t\t%.0f\n",ev1); dif=lqi-ev1; tft=(dif)*(lt1-209)*0.78; printf("\t d.To flash tank\t%.1e",tft); ev2=tft/978;//lb/hr printf("\t\t%.0f\n",ev2); printf("\t e.Flashed vapor=%.0f\n",ev2); p=dif-ev2; printf("\t f.product %.1e\n",p); printf("\n\t2.a.Heat in 1st vapors\t%.3e\n",hh); hl2=lqi2*(lt2-lt3)*0.85; printf("\t b.Heating liqour\t%.2e\n",hl2); ev3=(hh-hl2)/962; printf("\t c.Evaporation=%.0f",ev3); printf("\t\t\t%.0f\n",ev3); lto1=lqi2-ev3; printf("\t d.Liquor to 1b=%.0f\n",lto1); //end
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// Initilization of variables m=5 // kg // mass of the block theta=30 // degree // inclination of the plane x=0.5 // m // distance travelled by the block k=1500 // N/m // stiffness of the spring mu=0.2 // coefficient of friction between the block and the surface g=9.81 // m/s^2 // acc due to gravity // Calculations // Consider the F.B.D of the block // Applying the principle of work and energy between the positions 1 & 2 and on further simplification we get the generic eq'n for delta as, 750*delta^2-16.03*delta-8.015=0. From this eq'n e have values of a.b & c as, a=750 b=-16.03 c=-8.015 // Thus the roots of the eq'n are given as, delta=(-b+(sqrt(b^2-(4*a*c))))/(2*a) // m // Results clc printf('The maximum compression of the spring is %f m \n',delta)
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disp("PREGUNTA A") fase=[-120 -110 -80 -40 -10 30 80 110 120] magnitud= [7.92 7.98 8.95 10.71 11.7 10.01 8.23 7.86 7.92] h=[] ;fy=[] ;B=[] ; dl=[] n=length(fase) for i=1:n-1 h(i)=fase(i+1)-fase(i) fy(i)=(magnitud(i+1)-magnitud(i))/h(i) end for i=1:n if i<9 & i>1 then dl(i)=2*(h(i)+h(i-1)) B(i)=6*(fy(i)-fy(i-1)) elseif i==1 dl(i)=2*(h(i)) B(i)=6*fy(i) elseif i==9 dl(i)=2*(h(i-1)) B(i)=6*fy(i-1) end end mt=zeros(n,n) for i=1:n for j=1:n if i==j mt(i,j)=dl(i) ; end if i==j+1 mt(i,j)=h(i-1) ; end if i==j-1 mt(i,j)=h(i) end end end disp(mt) M=inv(mt)*B //derivadas a=[] ; b=[] ; c=[] ; d=[]; pol=[] for i=1:n-1 a(i)=(M(i+1)-M(i))/(6*h(i)) b(i)=M(i)/2 c(i)=fy(i)-(M(i+1)+2*M(i))*h(i)/6 d(i)= magnitud(i) pol(i)= poly([d(i) c(i) b(i) a(i)], "x", "coeff") end fase=fase' mxl=[fase(1:n-1,:) pol] disp("PREGUNTA B") disp(mxl) fn = [] deff('y=F1(x)','y=7.92 +0.0004355*(x+120)^2 +0.0000165*(x+120)^3') x=-120 res=F1(x) fn(1) = res disp('-120',res) deff('y=F2(x)','y=7.98+0.0136453*(x+110) +0.0009291*(x+110)^2 -0.0000102*(x+110)^3') x=-110 res=F2(x) fn(2) = res disp('-110',res) deff('y=F3(x)','y=8.95 +0.0418377*(x+80) +0.0000107*(x+80)^2 +0.0000011*(x+80)^3') x=-80 res=F3(x) fn(3) = res disp('-80',res) deff('y=F4(x)','y=10.71+0.0478971*(x+40) +0.0001408*(x+40)^2 -0.0000212*(x+40)^3') x=-40 res=F4(x) fn(4) = res disp('-40',res) deff('y=F5(x)','y=11.7-0.0010182*(x+10) -0.0017713*(x+10)^2 +0.0000185*(x+10)^3') x=-10 res=F5(x) fn(5) = res disp('-10',res) deff('y=F6(x)','y=10.01-0.0538611*(x-30) +0.0004502*(x-30)^2 -0.0000017*(x-30)^3') x=30 res=F6(x) fn(6) = res disp('30',res) deff('y=F7(x)','y=8.23 -0.0215897*(x-80) +0.0001952*(x-80)^2 +0.0000038*(x-80)^3') x=80 res=F7(x) fn(7) = res disp('80',res) deff('y=F8(x)','y= 7.86 +0.0003237*(x-110) +0.0005353*(x-110)^2 +0.0000032*(x-110)^3') x=110 res=F8(x) fn(8) = res disp('110',res) x=120 res=F8(x) fn(9) = res disp('120',res) scf(1) plot(fase,fn) leg=legend(['Periodic Spline']) xlabel('Fase (ø)') ; ylabel('Magnitud') title("Pregunta C - Osa Mayor") gca().grid=[1 1 1] // fn2 = [] disp("PREGUNTA C") x=-100 res=F1(x) fn2(1) = res disp('-100',res) x=-60 res=F3(x) fn2(2) = res disp('-60',res) x=-20 res=F4(x) fn2(3) = res disp('-20',res) x=20 res=F5(x) fn2(4) = res disp('20',res) x=60 res=F6(x) fn2(5) = res disp('60',res) x=100 res=F7(x) fn2(6) = res disp('100',res) scf(2) col1=[-100 -60 -20 -20 60 100] f1=[8.37 9.40 11.39 10.84 8.53 7.89] error = abs(f1'-fn2) disp("M Real Approx Error") fn2=[col1' f1' fn2 error] disp(fn2) disp("PREGUNTA D (ver la gráfica)") plot(fn2(:,1),fn2(:,2),'b',fn2(:,1),fn2(:,3),'r') ; xlabel('Fase (ø)') ; ylabel('Magnitud') leg=legend(['Real points';'Periodic Spline']); title("Pregunta D - Osa Mayor") gca().grid=[1 1 1]
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// 08.06.18 function P=Paramark(varargin) Nargs=length(varargin); PA=varargin(1); PB=varargin(2); PC=varargin(3); R=0.5; if Nargs>=4 R=varargin(4)*R; end U=R*(PA-PB)/Vecnagasa(PA,PB); V=R*(PC-PB)/Vecnagasa(PC,PB); if Gaiseki(PA-PB,PC-PB)~=0 P=Listplot([PB+U,PB+U+V,PB+V]); else P=[]; end endfunction
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clc d = 150 // diameter in mm h = 10 // thickness in mm R = d/2 // radius in mm mu = 0.2 // coefficient of friction sigma_0 = 200 // N/mm^2 Rs = R - (h/(2*mu))*log(1/(sqrt(3)*mu)) // sticking radius in mm Ps = sigma_0*exp(2*mu*(R-Rs)/h) // pressure at sticking radius in N/mm^2 function y=f(r) y=2*%pi*r*sigma_0*exp(2*mu/h*(R-r)) endfunction L_sld = intg(48.5,75,f) L_sld = L_sld/1000 // load on sliding portion in kN Pc = Ps + (2*sigma_0*Rs)/(h*sqrt(3)) // pressure at centre in N/mm^2 L_sp = (Pc+Ps)*%pi*(Rs)^2/(2*1000) // load on sticking portion in kN F_l = L_sld + L_sp // total forging load in kN printf("\n Sticking radius = %0.1f mm \n Total forging load = %0.3f MN",Rs ,F_l/1000) // 'Answers vary due to round off error'
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// Shrinkage in sintering clc L = 1 // let del_l = 5/100*L // linear shrinkage rho_sint = 90 // sintered density in% printf("\n Example 11.4") rho_green = rho_sint*(1-(del_l/L))^3 printf("\n Density of green compact becomes %d%%.",rho_green)
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# I love comments... # [a] [a] #aws_access_key_id=wrong-key aws_access_key_id=a # More comments... aws_secret_access_key=a unsupported_property=foo # More comments... [b] # More comments... aws_access_key_id=b aws_secret_access_key=b [c] aws_access_key_id=c # More comments... aws_secret_access_key=c aws_session_token=c [d] aws_access_key_id=d aws_secret_access_key=d # More comments... aws_session_token=d # More comments...
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printf('IT software problem')
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Ax = 18.75; A_ = 12.50; // A_= A* AA_ = 1.5; // A/A* Mx = 1.86; Pxox = 0.159; R = 0.287; Pox = 0.21e03; // in kPa Px = Pxox*Pox; // from the gas table on normal shock Mx = 1.86; My = 0.604; Pyx = 3.87; Poyx = 4.95; Poyox = 0.786; Py = Pyx*Px; Poy = Poyx*Px; My = 0.604; Ay_ = 1.183; A2 = 25; Ay = 18.75; A2_ = (A2/Ay)*Ay_; // From isentropic table M2 = 0.402; P2oy = 0.895; P2 = P2oy*Poy; syx = -R*log(Poy/Pox); // sy-sx disp(M2,"Exit mach number is M2") disp("kPa",P2,"Exit pressure is") disp("kPa",Pox-Poy,"Exit Stagnation pressure is") disp("kJ/kg K",syx,"Entropy increase is")
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// Test # 1 : No Input Arguments exec('./tf2cl.sci',-1); [k1,k2,b]=tf2cl(); //!--error 10000 //Only 2 input arguments allowed //at line 38 of function tf2cl called by : //[d1,d2,b]=tf2cl();
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//Finding of Shear Stress //Given //du/dy = vg vg=.25; //Velocity gradient in m/sec/meter nu=6.30*10^-4; //Kinematic viscosity in m^2/sec rho=1268.4; //Mass density in Kg/m^3 mu=rho*nu; //Dynamic Viscosity //To Find tau=mu*vg; //Shear stress in N/m^2 disp("Shear Stress ="+string(tau)+" N/m^2");
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check_mysql_running: module_and_function: service.status args: - mysql assertion: assertTrue
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V=440 I=25 pf=0.85 Pin=sqrt(3)*V*I*pf ns=1500 Pcore=750 Pcus=950 Pcur=450 Pwfl=250 Pg=Pin-Pcore-Pcus disp(Pg) Pm=Pg-Pcur disp(Pm) Pmout=Pm-Pwfl disp(Pmout) effi=Pmout/Pin disp(effi) s=Pcur/Pg n=(1-s)*ns disp(n) w=2*%pi*n/60 Tdev=Pm/w disp(Tdev) Tnet=Pmout/w disp(Tnet)
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//Electric machines and power systems by Syed A Nasar //Publisher:Tata McGraw Hill //Year: 2002 ; Edition - 7 //Example 6.8 //Scilab Version : 6.0.0 ; OS : Windows clc; clear; V=230; //supply voltage in v Ra=.05; //armature resistance in ohms Rf1=75; //field resistance in no load in ohms Rf2=100; //field resistance in on load condition in ohms I1=7;N1=1120; //no load current and speed I2=46; //on load current in A Ra2=0.15 //armature resistance at on load condition in ohms If=V/Rf1; Ia1=I1-If; K=(V-Ia1*Ra)/(N1*If); Ia2=I2-If; N=(V-Ia2*Ra)/(If*K); If1=V/Rf1; Ia0=I2-If1; n=(V-Ia2*Ra2)/(If1*K); pl=(Ia0^2)*0.1; printf('speed of the motor is %d rpm\n',n) printf('power dissipated in 0.1 ohm resistor is %f W',pl)
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clc(); clear; // To calculate the resultant voltage across the capacitors Q=2*10^-10; //charge in coulomb d=4; //plate seperation in mm d=d*10^-3; //plate seperation in m epsilon_r=3.5; epsilon_0=8.85*10^-12; //f/m A=650; //area in mm^2 A=A*10^-6; //area in m^2 V=(Q*d)/(epsilon_0*epsilon_r*A); printf("voltage across the capacitor is %f Volts",V);
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clear;lines(0); n=5; for i = 1:n, for j = 1:n, a(i,j) = 1/(i+j-1);end;end for j = 2:n-1, a(j,j) = j; end; a for e=eye(3,3),e,end for v=a, write(6,v),end for j=1:n,v=a(:,j), write(6,v),end for l=list(1,2,'example'); l,end
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Ch02Ex25.sce
// Scilab Code Ex2.25:: Page-2.19 (2009) clc; clear; lambda = 5890e-008; // Wavelength of light used, cm mu = 1.5; // Refractive index of material sheet // As shift = 9*lambda*D/d = D/d*(mu - 1)*t, solving for t t = 9*lambda/(mu - 1); // Thickness of the glass sheet, cm printf("\nThe thickness of the glass sheet = %4.2e cm", t); // Result // The thickness of the glass sheet = 1.06e-003 cm
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/*poly2lsf.sci * *Prediction polynomial to line spectral frequencies * *Converts the prediction polynomial specified by 'a' *into the corressponding line spectral frequencies, LSF. *Normalizes the prediction polynomial by a(1) * *Syntax: *lsf = poly2lsf(a) *Description: *lsf = poly2lsf(a) returns a vector, lsf, of line spectral frequencies from *a vector,'a', of prediction filter coefficient * *Example: *Given a vector, a, of prediction filter coefficient, generate the corressponding *line spectral frequencies * *Input: *a = [1.0000 0.6149 0.9899 0.0000 0.0031 -0.0082]; *lsf = poly2lsf(a) * *Output: *lsf = * 0.7842 * 1.5605 * 1.8776 * 1.8984 * 2.3593 * * *Author: Vrishabh Lakhani * *References: *Deller, John R., John G. Proakis, and John H. L. Hansen. Discrete-Time Processing of Speech Signals. New York: Macmillan, 1993. *Rabiner, Lawrence R., and Ronald W. Schafer. Digital Processing of Speech Signals. Englewood Cliffs, NJ: Prentice-Hall, 1978. * */ function lsf = poly2lsf(a) //Line spectral frequencies are not defined for complex polynomials //Therefore, we need to normalise them if a(1)<>1 then a=a/a(1) end if max(abs(roots(a))) >= 1.0 then error('The polynomial must have all the roots inside of the unit circle.') end //Create the sum and the difference filters p=length(a)-1 //The first element '1' is not used x=[0] a1=cat(2,a,x) a2=flipdim(a1,2,1) P1 = a1 - a2 //Difference filter Q1 = a1 + a2 //Sum filter P2=P1(1) Q2=P2(1) z=poly(0,"z") for i=2:length(P1) P2=P2+P1(i)*z^(i) end for i=2:length(Q1) Q2=Q2+Q1(i)*z^(i) end divisorOdd=-1*z^2+0*z^1+1 divisorEven1=-1*z^1+1 divisorEven2=1*z^1+1 //If order is even, we have to remove the known roots at z=1 for P1 and z=-1 for Q1 //If odd, remove both the roots from P1 if modulo(p,2) then //Odd order [r,P]= pdiv(P2,divisorOdd) Q=Q1 else //Even order [r, P] = pdiv(P2, divisorEven1) [r, Q] = pdiv(P2, divisorEven2) end P=coeff(P) rP = roots(coeff(P)) rQ = roots(coeff(Q)) aP = atan(imag(rP), real(rP)) aQ = atan(imag(rQ), real(rQ)) lsf = gsort(cat(1,-aP, -aQ),'r','i') lsf = lsf(find(lsf>0)) return lsf endfunction
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Overhead Jumps FN.sce
Name=Overhead Jumps FN PlayerCharacters=A BotCharacters=Shinji Bot.bot IsChallenge=true Timelimit=60.0 PlayerProfile=A AddedBots=Shinji Bot.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=1 BotTeams=2 MapName=Flick_Audio_Hard.map MapScale=1.0 BlockProjectilePredictors=false BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Overwatch,OW,Track,Flick,Genji,ddtv WeaponHeroTag=Tracer,Soldier,McCree DifficultyTag=3 AuthorsTag=DevinDTV BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=A bot jumps over your head GameVersion=2.0.1.2 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Default MinReactionTime=0.1 MaxReactionTime=0.11 MinSelfMovementCorrectionTime=0.1 MaxSelfMovementCorrectionTime=0.11 FlickFOV=90.0 FlickSpeed=1.0 FlickError=0.1 TrackSpeed=1.0 TrackError=0.1 MaxTurnAngleFromPadCenter=360.0 MinRecenterTime=0.1 MaxRecenterTime=0.1 OptimalAimFOV=1.0 OuterAimPenalty=1.0 MaxError=0.1 ShootFOV=10.0 VerticalAimOffset=0.1 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=Shinji Bot DodgeProfileNames=Long Strafes Close DodgeProfileWeights=2.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Shinji SeeThroughWalls=true NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=A MaxHealth=100.0 WeaponProfileNames=Track Master 100;Six Shooter;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=50.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=20.0 MainBBRadius=1.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Shinji MaxHealth=200.0 WeaponProfileNames=Shinji Stars;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=30.0 CrouchHeightModifier=0.69 CrouchAnimationSpeed=5.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=500.0 MaxCrouchSpeed=270.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=100.0 BrakingFrictionFactor=10000.0 JumpVelocity=500.0 Gravity=1.0 AirControl=0.025 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=true EnemyBodyColor=X=0.774 Y=0.000 Z=0.000 EnemyHeadColor=X=0.163 Y=0.167 Z=0.166 TeamBodyColor=X=0.000 Y=0.000 Z=0.771 TeamHeadColor=X=0.163 Y=0.167 Z=0.166 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=true BlockTeamDamage=true AirJumpCount=1 AirJumpVelocity=300.0 MainBBType=Cylindrical MainBBHeight=80.0 MainBBRadius=15.0 MainBBHasHead=true MainBBHeadRadius=10.0 MainBBHeadOffset=-5.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=101.0 ProjBBRadius=20.0 ProjBBHasHead=true ProjBBHeadRadius=12.5 ProjBBHeadOffset=-12.5 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.0 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=100.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=Movement Ability.abilmov;out of range.abilmov;; HideWeapon=false AerialFriction=0.3 StrafeSpeedMult=0.75 BackSpeedMult=0.5 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Long Strafes Close MaxTargetDistance=400.0 MinTargetDistance=200.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.5 MaxFBTimeChange=1.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.2 MaxJumpTime=0.3 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] 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ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.05 HitSoundCooldown=0.05 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=0.0 TaggingHitFactor=0.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=None ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=1000.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=Six Shooter Type=Hitscan ShotsPerClick=1 DamagePerShot=5.0 KnockbackFactor=0.1 TimeBetweenShots=0.5 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=2200.0 DamageFalloffStopDistance=4500.0 DamageAtMaxRange=20.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.5 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=4.0 MinRecoilUp=4.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.44 AAMode=2 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=0.5 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=Shinji Stars Type=Projectile ShotsPerClick=1 DamagePerShot=28.0 KnockbackFactor=0.1 TimeBetweenShots=1.0 Pierces=false Category=FullyAuto BurstShotCount=3 TimeBetweenBursts=0.1 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=5333.333 Y=0.000 Z=0.000 MuzzleVelocityMax=X=5333.333 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=0.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=24 AmmoPerShot=1 ReloadTimeFromEmpty=1.0 ReloadTimeFromPartial=1.0 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=28.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=false DecalType=1 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=true ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.1,0.1,0.0,0.0 SpreadSCA=0.1,0.1,0.0,0.0 SpreadMSA=0.1,0.1,0.0,0.0 SpreadMCA=0.1,0.1,0.0,0.0 SpreadSSH=0.1,0.1,0.0,0.0 SpreadSCH=0.1,0.1,0.0,0.0 SpreadMSH=0.1,0.1,0.0,0.0 SpreadMCH=0.1,0.1,0.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.2 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=Movement Ability MaxCharges=1.0 ChargeTimer=1.5 ChargesRefundedOnKill=0.0 DelayAfterUse=1.5 FullyAuto=false AbilityDuration=0.005 LockDirectionForDuration=true NegateGravityForDuration=false MainVelocity=400.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=false UpVelocity=200.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=true AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=false AIUseInAir=true AIReuseTimer=0.1 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=250.0 AIMaxTargDist=400.0 AIMaxTargFOV=15.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.95 AIDamageReactionMinDelay=0.01 AIDamageReactionMaxDelay=0.2 AIDamageReactionCooldown=0.1 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Movement Ability Profile] Name=out of range MaxCharges=1.0 ChargeTimer=1.0 ChargesRefundedOnKill=0.0 DelayAfterUse=0.5 FullyAuto=false AbilityDuration=0.25 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=150.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=false UpVelocity=0.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=true AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=400.0 AIMaxTargDist=12000.0 AIMaxTargFOV=90.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -1008.000000 -1088.000000 1488.000000 1216.000000 -1088.000000 1488.000000 1216.000000 -1088.000000 -936.000000 -1008.000000 -1088.000000 -936.000000 -1008.000000 -1152.000000 1488.000000 1216.000000 -1152.000000 1488.000000 1216.000000 -1152.000000 -936.000000 -1008.000000 -1152.000000 -936.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 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vertices 664.000000 912.000000 1216.000000 816.000000 912.000000 1216.000000 816.000000 912.000000 -856.000000 664.000000 912.000000 -856.000000 664.000000 -1088.000000 1216.000000 816.000000 -1088.000000 1216.000000 816.000000 -1088.000000 -856.000000 664.000000 -1088.000000 -856.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 5 4 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 2 1 5 6 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 0 3 7 4 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 3 2 6 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 1 0 4 5 0x00000000 brush vertices -952.000000 920.000000 1120.000000 1216.000000 920.000000 1120.000000 1216.000000 920.000000 816.000000 -952.000000 920.000000 816.000000 -952.000000 -1088.000000 1120.000000 1216.000000 -1088.000000 1120.000000 1216.000000 -1088.000000 816.000000 -952.000000 -1088.000000 816.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 5 4 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 2 1 5 6 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 0 3 7 4 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 3 2 6 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 1 0 4 5 0x00000000 brush vertices -720.000000 912.000000 1320.000000 -536.000000 912.000000 1320.000000 -536.000000 912.000000 -784.000000 -720.000000 912.000000 -784.000000 -720.000000 -1088.000000 1320.000000 -536.000000 -1088.000000 1320.000000 -536.000000 -1088.000000 -784.000000 -720.000000 -1088.000000 -784.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 5 4 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 2 1 5 6 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 0 3 7 4 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 3 2 6 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 1 0 4 5 0x00000000 brush vertices -960.000000 1032.000000 1240.000000 1136.000000 1032.000000 1240.000000 1136.000000 1032.000000 -856.000000 -960.000000 1032.000000 -856.000000 -960.000000 112.000000 1240.000000 1136.000000 112.000000 1240.000000 1136.000000 112.000000 -856.000000 -960.000000 112.000000 -856.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 2 3 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 5 4 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 2 1 5 6 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 0 3 7 4 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 3 2 6 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 1 0 4 5 0x00000000 entity type PlayerSpawn Vector3 position 72.000000 -1098.000000 232.000000 Bool8 teamB 0 Bool8 modeCTF 0 Bool8 modeFFA 0 Bool8 modeTDM 0 Bool8 mode1v1 0 Bool8 modeRace 0 Bool8 mode2v2 0 entity type CameraPath UInt32 entityIdAttachedTo 132 UInt8 posLerp 2 UInt8 angleLerp 2 entity type Effect Vector3 position 0.000000 256.000000 0.000000 String64 effectName internal/misc/reflectionprobe entity type PlayerSpawn Vector3 position 72.000000 -995.000000 732.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position 422.000000 -995.000000 582.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position -428.000000 -995.000000 232.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position -278.000000 -995.000000 582.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position 572.000000 -995.000000 232.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position 422.000000 -995.000000 -118.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position 72.000000 -995.000000 -268.000000 Bool8 teamA 0 entity type PlayerSpawn Vector3 position -278.000000 -995.000000 -118.000000 Bool8 teamA 0
621a9a8e516474a75d4b9c942768b29c560c9d81
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/2579/CH4/EX4.49/Ex4_49.sce
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FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
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Ex4_49.sce
//Ex:4.49 clc; clear; close; f=10*10^3;// frequency in MHz y=300/f;// wavelength in m a=5.2/100;// height in m b=3.8/100;// width in m A=a*b;// area in m^2 G=(4*%pi*A)/y^2;// the gain of the horn G1=10*log(G)/log(10);// the gain of the horn in dB he=(51*y)/b;// the half power point beam width in E-plane in degree hh=(67*y)/a;// the half power point beam width in H-plane in degree printf("The gain of the horn = %f", G); printf("\n The the gain of the horn in dB = %f dB", G1); printf("\n The half power point beam width in E-plane = %f degree", he); printf("\n The half power point beam width in H-plane = %f degree", hh);
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
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2018-02-03T05:31:52
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clc m_s=50; //kg m_w=1.5; //kg x=m_s/(m_s+m_w); disp("dryness fraction=") disp(x)
fa69fb0f4b4a458470a431ee860f51dd84821e31
80c4f32677abf57e118950a28c918a042269200c
/UI_Edit/Scenes/PPPP.sce
9bafbd38eea60e92f7d94916d799e3c1bb137a5a
[ "MIT" ]
permissive
ggcrunchy/ui-edit-v1
ab31697a8db0387e71edd1e61f3bcc3cd0bcbc7e
e5b1b1867f5f9bca941e3638a0274f8133711759
refs/heads/master
2021-01-19T14:24:13.514011
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// Leyes de Newton de Enfriamiento con Temperatura del Ambiente Constante // function [T, t] = cambioTemperatura(Tambiente, Tinicial, k, stepsize, tfinal) // Entrada: // Tambiente : Temperatura del ambiente en °C // Tinicial : Temperatura inicial del objeto de interes en °C // k : constante de proporcionalidad en 0.019/min // Salida: // t : tiempo en minutos // T : temperatura del objeto de interes function [T, t] = cambioTemperatura(Tambiente, Tinicial, k, stepsize, tfinal) T(1) = Tinicial; t = 0:stepsize:tfinal; for i=1:length(t)-1; T(i+1) = T(i) - k*(T(i)-Tambiente)*(t(i+1)-t(i)); end // plot(t,T,'color','red','marker','>'); // xlabel("t, seg"); // ylabel("T, °C"); // set(gca(),"grid",[1 1]); endfunction
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clear; lines(0); np=100; q=7; //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 j=1; i=1; w=190 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); k=1 j=j+1; b(1,j)=w; // w b(2,j)=a(msig,11) b(3,j)=a(msig1,11) b(4,j)=a(msig2,11) b(5,j)=a(msig3,11) b(6,j)=a(msig4,11) b(7,j)=a(msig5,11) b(8,j)=a(msig6,11) b(9,j)=a(msig7,11) b(10,j)=a(msig8,11) b(11,j)=a(msig9,11) b(12,j)=a(msig10,11) b(13,j)=a(msig11,11) b(14,j)=a(msig12,11) b(15,j)=a(msig13,11) b(16,j)=a(msig14,11) b(17,j)=a(msig15,11) b(18,j)=a(msig16,11) b(19,j)=a(msig17,11) b(20,j)=a(msig18,11) b(21,j)=a(msig19,11) b(22,j)=a(msig20,11) b(23,j)=a(msig21,11) b(24,j)=a(msig22,11) b(25,j)=a(msig23,11) b(26,j)=a(msig24,11) b(27,j)=a(msig25,11) b(28,j)=a(msig26,11) b(29,j)=a(msig27,11) b(30,j)=a(msig28,11) b(31,j)=a(msig29,11) b(32,j)=a(msig30,11) b(33,j)=a(msig31,11) b(34,j)=a(msig32,11) b(35,j)=a(msig33,11) b(36,j)=a(msig34,11) b(37,j)=a(msig35,11) b(38,j)=a(msig36,11) b(39,j)=a(msig37,11) b(40,j)=a(msig38,11) b(41,j)=a(msig39,11) b(42,j)=a(msig40,11) b(43,j)=a(msig41,11) b(44,j)=a(msig42,11) b(45,j)=a(msig43,11) b(46,j)=a(msig44,11) b(47,j)=a(msig45,11) b(48,j)=a(msig46,11) b(49,j)=a(msig47,11) b(50,j)=a(msig48,11) b(51,j)=a(msig49,11) b(52,j)=a(msig50,11) b(53,j)=a(msig51,11) b(54,j)=a(msig52,11) b(55,j)=a(msig53,11) b(56,j)=a(msig54,11) b(57,j)=a(msig55,11) b(58,j)=a(msig56,11) b(59,j)=a(msig57,11) b(60,j)=a(msig58,11) b(61,j)=a(msig59,11) b(62,j)=a(msig60,11) b(63,j)=a(msig61,11) b(64,j)=a(msig62,11) b(65,j)=a(msig63,11) b(66,j)=a(msig64,11) b(67,j)=a(msig65,11) b(68,j)=a(msig66,11) b(69,j)=a(msig67,11) b(70,j)=a(msig68,11) b(71,j)=a(msig69,11) b(72,j)=a(msig70,11) b(73,j)=a(msig71,11) b(74,j)=a(msig72,11) b(75,j)=a(msig73,11) b(76,j)=a(msig74,11) b(77,j)=a(msig75,11) b(78,j)=a(msig76,11) b(79,j)=a(msig77,11) b(80,j)=a(msig78,11) b(81,j)=a(msig79,11) b(82,j)=a(msig80,11) b(83,j)=a(msig81,11) b(84,j)=a(msig82,11) b(85,j)=a(msig83,11) b(86,j)=a(msig84,11) b(87,j)=a(msig85,11) b(88,j)=a(msig86,11) b(89,j)=a(msig87,11) b(90,j)=a(msig88,11) b(91,j)=a(msig89,11) b(92,j)=a(msig90,11) b(93,j)=a(msig91,11) b(94,j)=a(msig92,11) b(95,j)=a(msig93,11) b(96,j)=a(msig94,11) b(97,j)=a(msig95,11) b(98,j)=a(msig96,11) b(99,j)=a(msig97,11) b(100,j)=a(msig98,11) b(101,j)=a(msig99,11) b(102,j)=a(msig100,11) b(103,j)=a(msig101,11) b(104,j)=a(msig102,11) b(105,j)=a(msig103,11) b(106,j)=a(msig104,11) b(107,j)=a(msig105,11) b(108,j)=a(msig106,11) b(109,j)=a(msig107,11) b(110,j)=a(msig108,11) b(111,j)=a(msig109,11) b(112,j)=a(msig110,11) b(113,j)=a(msig111,11) b(114,j)=a(msig112,11) b(115,j)=a(msig113,11) b(116,j)=a(msig114,11) b(117,j)=a(msig115,11) b(118,j)=a(msig116,11) b(119,j)=a(msig117,11) b(120,j)=a(msig118,11) b(121,j)=a(msig119,11) b(122,j)=a(msig120,11) b(123,j)=a(msig121,11) b(124,j)=a(msig122,11) b(125,j)=a(msig123,11) b(126,j)=a(msig124,11) b(127,j)=a(msig125,11) b(128,j)=a(msig126,11) b(129,j)=a(msig127,11) b(130,j)=a(msig128,11) b(131,j)=a(msig129,11) b(132,j)=a(msig130,11) b(133,j)=a(msig131,11) b(134,j)=a(msig132,11) b(135,j)=a(msig133,11) b(136,j)=a(msig134,11) b(137,j)=a(msig135,11) b(138,j)=a(msig136,11) b(139,j)=a(msig137,11) b(140,j)=a(msig138,11) b(141,j)=a(msig139,11) b(142,j)=a(msig140,11) b(143,j)=a(msig141,11) b(144,j)=a(msig142,11) b(145,j)=a(msig143,11) b(146,j)=a(msig144,11) b(147,j)=a(msig145,11) b(148,j)=a(msig146,11) b(149,j)=a(msig147,11) b(150,j)=a(msig148,11) b(151,j)=a(msig149,11) b(152,j)=a(msig150,11) b(153,j)=a(msig151,11) b(154,j)=a(msig152,11) b(155,j)=a(msig153,11) b(156,j)=a(msig154,11) b(157,j)=a(msig155,11) b(158,j)=a(msig156,11) b(159,j)=a(msig157,11) b(160,j)=a(msig158,11) b(161,j)=a(msig159,11) b(162,j)=a(msig160,11) b(163,j)=a(msig161,11) b(164,j)=a(msig162,11) b(165,j)=a(msig163,11) b(166,j)=a(msig164,11) b(167,j)=a(msig165,11) b(168,j)=a(msig166,11) b(169,j)=a(msig167,11) b(170,j)=a(msig168,11) b(171,j)=a(msig169,11) b(172,j)=a(msig170,11) b(173,j)=a(msig171,11) b(174,j)=a(msig172,11) b(175,j)=a(msig173,11) b(176,j)=a(msig174,11) b(177,j)=a(msig175,11) b(178,j)=a(msig176,11) b(179,j)=a(msig177,11) b(180,j)=a(msig178,11) b(181,j)=a(msig179,11) b(182,j)=a(msig180,11) b(183,j)=a(msig181,11) b(184,j)=a(msig182,11) b(185,j)=a(msig183,11) b(186,j)=a(msig184,11) b(187,j)=a(msig185,11) b(188,j)=a(msig186,11) b(189,j)=a(msig187,11) b(190,j)=a(msig188,11) b(191,j)=a(msig189,11) b(192,j)=a(msig190,11) b(193,j)=a(msig191,11) b(194,j)=a(msig192,11) b(195,j)=a(msig193,11) b(196,j)=a(msig194,11) b(197,j)=a(msig195,11) b(198,j)=a(msig196,11) b(199,j)=a(msig197,11) b(200,j)=a(msig198,11) b(201,j)=a(msig199,11) b(202,j)=a(msig200,11) b(203,j)=a(msig201,11) b(204,j)=a(msig202,11) b(205,j)=a(msig203,11) b(206,j)=a(msig204,11) b(207,j)=a(msig205,11) b(208,j)=a(msig206,11) b(209,j)=a(msig207,11) b(210,j)=a(msig208,11) b(211,j)=a(msig209,11) b(212,j)=a(msig210,11) b(213,j)=a(msig211,11) b(214,j)=a(msig212,11) b(215,j)=a(msig213,11) b(216,j)=a(msig214,11) b(217,j)=a(msig215,11) b(218,j)=a(msig216,11) b(219,j)=a(msig217,11) b(220,j)=a(msig218,11) b(221,j)=a(msig219,11) b(222,j)=a(msig220,11) b(223,j)=a(msig221,11) b(224,j)=a(msig222,11) b(225,j)=a(msig223,11) b(226,j)=a(msig224,11) b(227,j)=a(msig225,11) b(228,j)=a(msig226,11) b(229,j)=a(msig227,11) b(230,j)=a(msig228,11) b(231,j)=a(msig229,11) b(232,j)=a(msig230,11) b(233,j)=a(msig231,11) b(234,j)=a(msig232,11) b(235,j)=a(msig233,11) b(236,j)=a(msig234,11) b(237,j)=a(msig235,11) b(238,j)=a(msig236,11) b(239,j)=a(msig237,11) b(240,j)=a(msig238,11) b(241,j)=a(msig239,11) b(242,j)=a(msig240,11) b(243,j)=a(msig241,11) b(244,j)=a(msig242,11) b(245,j)=a(msig243,11) b(246,j)=a(msig244,11) b(247,j)=a(msig245,11) b(248,j)=a(msig246,11) b(249,j)=a(msig247,11) b(250,j)=a(msig248,11) b(251,j)=a(msig249,11) // b(1,j)=a(k,10) // b(j,1)=a(k,1)// sigma // b(2,j)=a(msig,10); // zeL_av // b(3,j)=a(k,10) // b(4,j)=a(k,1) // b(j,k)=a(k,10) // end //end end //i=i+1; 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' + '.dat'; u=file('open',sout,'unknown'); write(u, b, '(f12.6,32(e16.6))'); file('close',u);
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// Exa Misc. 6.13 clc; clear; close; format('v',6) // Given data R1 = 20;// in k ohm R3 = 10;// in k ohm R2 = R3;// in k ohm R_F = 20;// in k ohm Vin1 = 2;// in V Vin2 = 2.1;// in V // The input voltage at non-inverting terminal, V_A = (R2*Vin2)/R1;// in V // The output voltage, by using super position theorm, Vo = ((-R_F/R1)*Vin1) + ((1+(R_F/R1))*(R1/(R2+R3))*V_A);// in V disp(Vo,"The output voltage in V is");
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//Example 6.7 // Equilibrium position time clc; clear; //given data : r=exp(2);//ratio of amplitude Q=2D3;//quality factor v=240;// frequency of fork in cycles/s w=2*%pi*v;//angular frequency in rad/sec T=Q/w;// relaxation time in sec t=2*T*log(r);//time for ne amplitude disp(t,"time to become for new amplitude in sec")
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//Example 1.6<g>// //draw the waveform of the signal x7(t)=u(t)-2*u(t-1)+u(t-2)// clc ; clear all; t=-10:.001:10 for i=1:length(t) if t(i)>=0 & t(i)<=1 then x(i)=1; end if t(i)>=1 & t(i)<=2 then x(i)=-1 end end //figure plot2d(t,x); xtitle('Required figure','t','x(t)')
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errcatch(-1,"stop");mode(2);// Example 3.6 all; ; // Given data sigmas_H_1 = 3; // Scattering cross section of Hydrogen in barn at 1 MeV sigmas_O_1 = 8; // Scattering cross section of Oxygen in barn at 1 MeV sigmas_H_th = 21; // Scattering cross section of Hydrogen in barn at 0.0253 eV sigmas_O_th = 4; // Scattering cross section of Oxygen in barn at 0.0253 eV // Calculation sigmas_H20_1 = (2*sigmas_H_1)+(1*sigmas_O_1); // Result printf('\n Scattering cross section of Water at 1 MeV = %d b \n',sigmas_H20_1); // The equation used to calculate the scattering cross section at 1 MeV cannot be used at thermal energy. printf(' Experimental value of scattering cross section of Water at 0.0253 eV = %d b \n',103); exit();
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//Variable Declaration n=24 //Number of channels g=13.57 //Peak/rms factor(dB) b=3.1 //Channel Bandwidth(kHz) P=4 //Emphasis improvement (dB) W=2.5 //Noise weighting improvement(dB) CNR=25 //Carrier to noise ratio (dB) delFrms=35 //rms value of Peak Deviation(kHz) fm=108 //Baseband frequency (kHz) //Calculation L=10**((-1+4*log10(n))/20) g=10**(g/20) //Converting process gain to ratio delF=g*delFrms*L //Peak Deviation(Hz) BIF=2*(delF+fm) //Signal Bandwidth(kHz) by Carson's rule Gp=(BIF/b)*((delFrms/fm)**2) //Processing Gain Gp=10*log10(Gp) //Converting Gp to dB SNR=CNR+Gp+P+W //Signal to noise ratio for top channel in 24-channel FDM basseband signal //Results printf("Signal to noise ratio for top channel in 24-channel FDM Baseband signal is %.1f db", SNR)
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// ==================================================================== // Allan CORNET // Simon LIPP // INRIA 2008 // This file is released into the public domain // ==================================================================== src_c_path = get_absolute_file_path('builder_c.sce'); CFLAGS = "-I" + src_c_path; tbx_build_src(['err_codes'], ['err_codes.c'], 'c', .. src_c_path, '', '', CFLAGS); tbx_build_src(['read_tchstn'], ['read_tchstn.c'], 'c', .. src_c_path, 'liberr_codes', '', CFLAGS); tbx_build_src(['write_tchstn'], ['write_tchstn.c'], 'c', .. src_c_path, 'liberr_codes', '', CFLAGS); clear tbx_build_src; clear src_c_path; clear CFLAGS;
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////Chapter 13 Steam Engines ////Example 13.13 Page No 293 ///Find Brake Power //Input data clc; clear; Db=900*10^-3; //Diameter of break drum in mm dr=50*10^-3; //Diameter of rope in mm W=105*9.81; //dead weight on the tight side of the rope in Kg S=7*9.81; //Spring balance of the rope in N N=240; //Speed of the engine in rpm pi=3.142; //Calculation T=(W-S)*((Db+dr)/2); //Torque Nm Bp=2*pi*N*T/60000; //Brake Power in Kw //Output printf('Torque= %f Nm \n',T); printf('Brake Power= %f Kw \n',Bp);
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clear; clc; close; Cs = 10*10^(-6); Ce = 20*10^(-6); Cc = 1*10^(-6); Rs = 1*10^(3); R1 = 40*10^(3); R2 = 10*10^(3); Re = 1.2*10^(3); Rc = 4*10^(3); Rl = 10*10^(3); Beta = 100; ro = %inf; re = 24.01; Vcc = 10; Ve = 2-0.7; Cwo = 8*10^(-12); Cwi = 6*10^(-12); Cce = 1*10^(-12); Cbc = 4*10^(-12); Cbe = 36*10^(-12); fls = 6.86; Ri = 1.85*10^(3); Avmid = -119; Rthi = Rs*R1*R2*Ri/(Rs*R1*R2+R1*R2*Ri+R2*Ri*Rs+Ri*Rs*R1); Ci = Cwi+Cbe+(1-Avmid)*Cbc; fhi = 1/(2*%pi*Rthi*Ci); Rtho = Rc*Rl/(Rc+Rl); Co = Cwo+Cce+(1-(1/Avmid))*Cbc; fho = 1/(2*%pi*Rtho*Co); fpie = 1/(2*%pi*Beta*re*(Cbe+Cbc)); ft = Beta*fpie; disp(fhi,'fhi = '); disp(fho,'fho = '); disp(fpie,'fbeta = '); disp(ft,'ft = '); fle = 500; flc = 1/(2*%pi*(Rl+Rtho)*Cc); f1 = fle; f = 0.1*f1:100:10*f1; av = (1+(f1./f)^2)^(-1/2); av1 = -20*log10(f1/f1); f2 = f1/10; av2 = -20*log10(f1/f2); f3 = f1/4; av3 = -20*log10(f1/f3); f4 = f1/2; av4 = -20*log10(f1/f4); x = [f2 f3 f4 f1]; y = [av2 av3 av4 av1]; gainplot(f,av); a = gca(); a.y_location = 'left'; a.x_location = 'top'; a.x_label.text = 'frequency'; a.y_label.text = 'Av'; a.title.text = 'Bode'; plot2d(x,y); f1 = fls; //f = .1*f1:10:10*f1; av = -10*log10(1+(f1./f)^2); av1 = -20*log10(f1/f1); f2 = f1/10; av2 = -20*log10(f1/f2); f3 = f1/4; av3 = -20*log10(f1/f3); f4 = f1/2; av4 = -20*log10(f1/f4); x = [f2 f3 f4 f1]; y = [av2 av3 av4 av1]; plot2d(x,y); f1 = flc; //f = .1*f1:10:10*f1; av = -10*log10(1+(f1./f)^2); av1 = -20*log10(f1/f1); f2 = f1/10; av2 = -20*log10(f1/f2); f3 = f1/4; av3 = -20*log10(f1/f3); f4 = f1/2; av4 = -20*log10(f1/f4); x = [f2 f3 f4 f1]; y = [av2 av3 av4 av1]; plot2d(x,y); f1 = fhi; f = 0.1*f1:100:10*f1; av = (1+(f/f1)^2)^(-1/2); av1 = -20*log10(f1/f1); f2 = f1*10; av2 = -20*log10(f2/f1); f3 = f1*4; av3 = -20*log10(f3/f1); f4 = f1*2; av4 = -20*log10(f4/f1); x = [f1 f4 f3 f2]; y = [av1 av4 av3 av2]; gainplot(f,av); plot2d(x,y); f1 = fpie; av1 = -20*log10(f1/f1); f2 = f1*10; av2 = -20*log10(f2/f1); f3 = f1*4; av3 = -20*log10(f3/f1); f4 = f1*2; av4 = -20*log10(f4/f1); x = [f1 f4 f3 f2]; y = [av1 av4 av3 av2]; plot2d(x,y); f1 = fho; av1 = -20*log10(f1/f1); f2 = f1*10; av2 = -20*log10(f2/f1); f3 = f1*4; av3 = -20*log10(f3/f1); f4 = f1*2; av4 = -20*log10(f4/f1); x = [f1 f4 f3 f2]; y = [av1 av4 av3 av2]; plot2d(x,y);
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clear // l=1 b=1.5 i=50 u=5 //case a f=b*i*l printf("\n f= %0.1f N",f) //case b p=f*u printf("\n p= %0.1f W",p) //case c e=b*l*u printf("\n e= %0.1f V",e)
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//Reading grayscale image I1 = imread("left.jpg"); //Extracting HOG feature values from image values = extractHOGFeatures(I1,"CellSize",[8,8]); //Correct output is given //Reading image I2 = imread("lena.jpeg"); //Extracting HOG feature values from image values2 = extractHOGFeatures(I2,"CellSize",[8,8]); //Correct output is given //Reading image I3 = imread("clc1.jpg"); //Extracting HOG feature values from image values3 = extractHOGFeatures(I3,"CellSize",[8,8]); //Correct output is given //Reading image I4 = imread("board1.jpg"); //Extra cting HOG feature values from image values4 = extractHOGFeatures(I4,"CellSize",[8,8]); //Correct output is given
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//Chapter-12, Example 12.18, Page 365 //============================================================================= clc clear //During the positive half of the input signal,the diode conducts and acts like a short circuit.Now,the output voltage,V0=0V.The capacitor is charged to 12V with polarities and it behaves like a battery. //during the negative half of the input signal,the diode does not conduct and acts like an open circuit.Hence the output voltage ,V0=-24V.This gives negatively clamped voltage. mprintf("V0=0V\n") mprintf("output voltage V0=-24V") //=================================END OF PROGRAM=======================================================================================================
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//Problem 20.09: A single-phase, 50 Hz transformer has 25 primary turns and 300 secondary turns. The cross-sectional area of the core is 300 cm2. When the primary winding is connected to a 250 V supply, determine (a) the maximum value of the flux density in the core, and (b) the voltage induced in the secondary winding. //initializing the variables: V1 = 250; // in Volts A = 0.03; // in m2 N2 = 300; // sec turns N1 = 25; // prim turns f = 50; // in Hz //calculation: //e.m.f. E1 = 4.44*f*Phim*N1 //maximum flux density, Phim = V1/(4.44*f*N1) //Phim = Bm*A, where Bm = maximum core flux density and A = cross-sectional area of the core //maximum core flux density Bm = Phim/A //voltage induced in the secondary winding, V2 = V1*N2/N1 printf("\n\n Result \n\n") printf("\n (a)maximum core flux density %.2f T", Bm) printf("\n (b)voltage induced in the secondary winding is %.0f V", V2)
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//Ex:8.13 clc; clear; close; tr=3.5;// relative life time in ms tnr=50;// nonrelative life time in ms ni=tnr/(tr+tnr);// internal quantam efficiency printf("The internal quantam efficiency =%f %%", ni*100);
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//clear// //Example 1.16:Classification of system:Time Invariance Property //Page 52 //To check whether the given system is a Time variant (or) Time In-variant // The given discrete signal is y(t) = x(2t) clear; clc; to = 2; //Assume the amount of time shift =2 T = 10; //Length of given signal x = [1,2,3,4,5,6,7,8,9,10]; y = zeros(1,length(x)); for t = 1:length(x)/2 y(t) = x(2*t); end //First shift the input signal only Input_shift = x(T-to); Output_shift = y(T-to); if(Input_shift == Output_shift) disp('The given discrete system is a Time In-variant system'); else disp('The given discrete system is a Time Variant system'); end
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// 08.08.16 // 08.10.10 // 13.10.21 ( __ added to varibles ) function PL__=Sf3data(varargin) Nargs__=length(varargin); FdL__=Fullformfunc(varargin(1)); F__=Mixop(1,FdL__); Xf__=Mixop(2,FdL__); Yf__=Mixop(3,FdL__); Zf__=Mixop(4,FdL__); Urg__=Mixop(5,FdL__); Vrg__=Mixop(6,FdL__); K__=mtlb_findstr(Urg__,'='); U__=part(Urg__,1:K__-1); Tmp__=part(Urg__,K__+1:length(Urg__)); Tmp__=evstr(Tmp__); Umin__=Tmp__(1); Umax__=Tmp__(2); K__=mtlb_findstr(Vrg__,'='); V__=part(Vrg__,1:K__-1); Tmp__=part(Vrg__,K__+1:length(Vrg__)); Tmp__=evstr(Tmp__); Vmin__=Tmp__(1); Vmax__=Tmp__(2); Ndu__=25 ; Ndv__=25; Np__=[50,50]; if Nargs__>=3 Ndu__=varargin(2); Ndv__=varargin(3); end; if Nargs__>=4 Np__=varargin(4); if type(Np__)==1 & length(Np__)==1 Np__=[Np__,Np__]; end; end; Du__=(Umax__-Umin__)/Ndu__; Dv__=(Vmax__-Vmin__)/Ndv__; PL__ = []; for I__=0:Ndu__ U0__ ='('+string(Umin__+I__*Du__)+')'; Tmp__=strsubst(Xf__,U__,U0__); Tmp1__=strsubst(Tmp__,V__,'t'); Tmp__=strsubst(Yf__,U__,U0__); Tmp2__=strsubst(Tmp__,V__,'t'); Tmp__=strsubst(Zf__,U__,U0__); Tmp3__=strsubst(Tmp__,V__,'t'); Tmp__='['+Tmp1__+','+Tmp2__+','+Tmp3__+']'; PD__=Spacecurve(Tmp__,'t=[Vmin__,Vmax__]','N='+string(Np__(2))); PL__=Mixadd(PL__,PD__); end; for J__=0:Ndv__ V0__='('+string(Vmin__+J__*Dv__)+')'; Tmp__=strsubst(Xf__,V__,V0__); Tmp1__=strsubst(Tmp__,U__,'t'); Tmp__=strsubst(Yf__,V__,V0__); Tmp2__=strsubst(Tmp__,U__,'t'); Tmp__=strsubst(Zf__,V__,V0__); Tmp3__=strsubst(Tmp__,U__,'t'); Tmp__='['+Tmp1__+','+Tmp2__+','+Tmp3__+']'; PD__=Spacecurve(Tmp__,'t=[Umin__,Umax__]','N='+string(Np__(1))); PL__=Mixadd(PL__,PD__); end; endfunction;
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clc; function output = add(vec1,vec2,pos1,pos2) if pos1 > pos2 then vec2 = [zeros(1,pos1-pos2) vec2] elseif pos2 > pos1 then vec1 = [zeros(1, pos2-pos1) vec1] end aft = length(vec1)-pos1 aft2 = length(vec2) - pos2 if aft > aft2 then vec2 = [vec2 zeros(1,aft-aft2)] elseif aft2 > aft then vec1 = [vec1 zeros(1,aft2-aft)] end output = vec1 + vec2 endfunction v3 = [1,2,3,4,3,-2,-1] v4 = [4,-2,2,1.2,3,4,5,6] out = add(v3,v4,4,4) disp(out)
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function [A,b]=Gauss(A,b) n=size(A,1); m=eye(n,n); for k=1:n-1 for i=k+1:n m(i,k)=A(i,k)/A(k,k); b(i)=b(i)-m(i,k)*b(k); for j=k+1:n A(i,j)=A(i,j)-m(i,k)*A(k,j); end end end endfunction function x=Usolve(U,b) n=size(U,1); x=zeros(n,1); x(n)=b(n)/U(n,n); for i=n-1:-1:1 x(i)=(b(i)-U(i,(i+1):n)*x(i+1:n))/U(i,i); end endfunction
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//<f>=%rdp(f,p) // %rdp(r,p) calcule la division element par element de la matrice de // fractions rationnelles r par la matrice de polynomes p //! f(3)=f(3).*p //end
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#test # TEST SUITE 2: TABLES ############################################ with(TestTools): kernelopts(opaquemodules=false): #libname := libname, "/home/mike/thesis/trunk/maple/pe/current/lib": libname := libname, "../lib": # TEST 1 ########################################################### # very basic p := proc() local x, t; x := 99; t[5] := x; t[5]; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 99 end proc); Test(100, got, expected); # TEST 1 ########################################################### # same thing but with symbols p := proc() local x, t; x := 99; t[C] := x; t[C]; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 99 end proc); Test(200, got, expected); #################################################################### p := proc(d) local t; t[1] :=88; if d then t[1] := 99; end if; t[1]; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc(d) if d then 99 else 88 end if end proc); Test(300, got, expected); #################################################################### p := proc(x, y, d) local t; t["x"] := d; t["y"] := d; if x = y then t["compare"] := "equals"; else t["compare"] := "ne"; end if; return t; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc (x, y, d) local t; t["x"] := d; t["y"] := d; if x = y then t["compare"] := "equals"; return t else t["compare"] := "ne"; return t end if end proc); Test(400, got, expected); goal := proc(d) p(1,1,d) end proc; ped := OnPE(goal); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc (d) local t1; t1["x"] := d; t1["y"] := d; t1["compare"] := "equals"; t1 end proc); Test(401, got, expected); #################################################################### p := proc() local t,s; t := table(); t[1] := 99; s := t; s[2] := 100; t[1], t[2]; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 99, 100 end proc); Test(501, got, expected); p := proc() t := table(); l := [t]; q := l[1]; q[1] := 99; t[1]; end proc: ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 99 end proc); Test(502, got, expected); #################################################################### # in this case x is not a table, it should still work p := proc () local x; x := [1, 2, 3, 4]; x[3] end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 3 end proc); Test(601, got, expected); #################################################################### p := proc() local t; t["a"] := 1; t["b"] := 2; g(t); t["a"], t["b"], t["c"]; end proc; g := proc(t) t["c"] := 3; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 1,2,3 end proc); Test(701, got, expected); #################################################################### p := proc() local t; t := table(); t["a"] := 66; g(t); t["a"], t["b"] end proc; g := proc() h(args); end proc; h := proc(t) t["b"] := 77; end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 66,77 end proc); Test(801, got, expected); #################################################################### p := proc() t := table(); s := table(); s[1] := 100; t["s"] := s; b := t["s"]; b[2] := 200; op(s); end proc; ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() 100, 200 end proc); Test(901, got, expected); g := proc(S, operation, x) S[operation] := x; S[Const][operation] := x*x; end proc; p := proc() local s; s := table(); g(s, Plus, 5); g(s, Minus, 10); op(s); end proc: ped := OnPE(p); got := ToInert(eval(ped:-ModuleApply)); expected := ToInert(proc() table([(Plus)=5,(Minus)=10,(Const)=(table([(Plus)=25,(Minus)=100]))]) end proc); Test(902, got, expected); #################################################################### opts := PEOptions(); opts:-setInlineAssigns(); f := proc(A) local i, B; B := table(); B[1] := A[1,1]; B[2] := A[1,2]; B; end; goal1 := proc() local A; A := table([ (1,1) = 4, (1, 2)=5 ]); f(A); end proc: res1 := OnPE(goal1, opts); # the easy one got := ToInert(eval(res1:-ModuleApply)); expected := ToInert(proc() table([(1)=4, (2)=5]) end proc); Test(1001, got, expected); goal2 := proc(x) local A; A := table([ (1,1) = 1, (1, 2)=x ]); f(A); end proc: res2 := OnPE(goal2, opts); # the one we really care about got := ToInert(eval(res2:-ModuleApply)); expected := ToInert(proc(x) local B1; B1[2] := x; B1[1] := 1; B1 end proc); Test(1002, got, expected); f := proc(t) t[1,2] end; goal3 := proc() local A; A := [table([(1,1)=1, (1,2)=2, (2,1)=-5, (2,2)=6])]; f(A[1]); end proc: res1 := OnPE(goal3, opts); # the easy one got := ToInert(eval(res1:-ModuleApply)); expected := ToInert(proc() 2 end); Test(1003, got, expected); ####################################################################### #end test ####################################################################### #end test #################################################################### #end test
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function [x, At] = gauss(A,b) [l, c] = size(A); At = [A b] for i = 1:l-1 //linha e coluna do pivo pivo = At(i,i); for j = i + 1: l //linha do elemento que vamos zerar m = At(j,i)/pivo; At(j,:) = At(j,:) - m*At(i,:); end end x = resoRetro(At(:,1:c), At(:,c+1)); endfunction
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clear; clc; //Example - 4.16 //Page number - 169 printf("Example - 4.16 and Page number - 169\n\n"); //Given P_1 = 300;//[kPa] - Initial pressure T_1 = 450;//[K] - Initial temperature Vel_1 = 90;//[m/s] - Initial velocity P_2 = 180;//[kPa] - Final pressure eff = 0.95;// Adiabatic effciciency of the nozzle R = 8.314;//[J/mol*-] - Universal gas constant Cp = 5.19;//[kJ/kg-K] - Specific heat capacity at constant pressure //(a) // Exit velocity is highest when drop in enthalpy is highest or when isentropic conditions are maintained Mol_wt_He = 4;//[g/mol] - Molecular weight of helium R_He = R/Mol_wt_He;// 'R' for helium Y = Cp/(Cp - R_He); // Now temperature at exit to be determined T_2s = T_1*(P_1/P_2)^((1-Y)/Y);//[K] delta_H_2s = Cp*(T_2s - T_1);//[kJ/kg] // Since no work is done and heat exchange is zero,from first law we get // delta_H + delta_Vel^(2)/2 = 0 delta_Vel_square = 2*(-delta_H_2s)*1000;//[m^(2)/s^(2)] Vel_2 = (delta_Vel_square)^(1/2);//[m/s] - ( as Vel_1 << Vel_2) printf(" (a).The maximum exit velocity is %f m/s\n\n",Vel_2); //(b) T_2a = 373;//[K] - Measured temperature of helium delta_H_a = Cp*(T_2a - T_1);//[kJ/kg] delta_Vel_square_a = 2*(-delta_H_a)*1000;//[m^(2)/s^(2)] Vel_2a = (delta_Vel_square_a)^(1/2);//[m/s] - ( as Vel_1 << Vel_2a) printf(" (b).The actual exit velocity is %f m/s\n\n",Vel_2a); //(c) delta_S_sys = Cp*log(T_2a/T_1) - R_He*log(P_2/P_1); // we know that delta_S_sys = q/T_b + S_gen and since q = 0, therfore S_gen = delta_S_sys;//[kJ/kg-K] printf(" (c).The increasse in entropy per unit mass is %f kJ/kg-K",S_gen); // The source of irreversibility is friction in the nozzle.
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clc //initialisation of variables d1= 8 //in d2= 4 //in h= 10 //in of mercury Cd= 0.98 g= 32.2 //ft/sec^2 sm= 13.56 //CALCULATIONS a1= %pi*(d1/12)^2/4 a2= %pi*(d2/12)^2/4 h1= h*(sm-1)/12 Q= a1*a2*sqrt(2*g)*sqrt(h1)/sqrt(a1^2-a2^2) Qactual= Cd*Q //RESULTS printf ('Actual discharge = %.2f cuses ',Qactual)
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 10.19w //calculation of the moment of inertia of the system about the axis perpendicular to the rod passing through its middle point //given data m=1.2//mass(in kg) of the sphere R=10*10^-2//radius(in cm) of the sphere sep=50*10^-2//separation(in m) between the two spheres //calculation d=sep/2//distance of each sphere from centre Icm=(2*m*R*R)/5//moment of inertia about diameter I=Icm+(m*d*d)//by parallel axis theorem,moment of inertia about given axis //since second sphere has same moment of inertia Isys=2*I//moment of inertia of the system printf('the moment of inertia of the system about the axis perpendicular to the rod passing through its middle point is %3.3f kg-m^2',Isys)
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//chapter 2 Ex 14 clc; clear; close; n1=62; n2=132; n3=237; V=int32([n2-n1 n3-n2 n3-n1]); //since it leaves same reminder Hcf=gcd(V); mprintf("The largest such number is %d.",Hcf);
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//chapter13 //example13.8 //page282 del_Ib=10d-3 // mA del_Ic=1 // mA del_Vbe=0.02 // V Rc=5 // kilo ohm Rl=10 // kilo ohm Ai=del_Ic/del_Ib Rin=del_Vbe/del_Ib R_AC=Rc*Rl/(Rc+Rl) Av=Ai*R_AC/Rin Ap=Av*Ai printf("current gain = %.3f \n",Ai) printf("input impedence = %.3f kilo ohm \n",Rin) printf("ac load = %.3f kilo ohm \n",R_AC) printf("voltage gain = %.3f \n",Av) printf("power gain = %.3f \n",Ap) // the accurate answer for voltage gain = 166.667 and for power gain = 16666.667 but in book they are given as 165 and 16500 respectively.
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// lege kernel voor opslag van geluidssignaal storage = zeros(1,4000); storage(4000) = 0.5; convolutie = convol(y2, storage); resize = resize_matrix(convolutie,[1 y2_size]); echo = y2 + resize; figure; plot(echo); playsnd(echo,16000);
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// Example 14_8 clc;clear;funcprot(0); //Given data V_in=47.1; //Velocity at the inlet in m/s beta_sl=0.0;// The leading edge angle of each stator blade in degree beta_st=60;// The trailing edge angle in degrees n=1750;//Speed of the impeller in rpm r=0.40;//Radius in // Calculation V_st=(V_in/(cosd((beta_st))));// The velocity leaving the trailing edge of the stator in m/s u_theta=(n*2*%pi*r)/(60);// The tangential velocity of the rotor blades in m/s beta_rl=atand(((u_theta)+(V_in*tand(beta_st)))/(V_in));// The angle of the leading edge of the rotor in degree beta_rt=atand((u_theta)/(V_in));// The angle of the trailing edge of the rotor in degree printf('\nThe rotor blade at this radius has a leading edge anle of about %0.2f degree and a trailing edge angle of about %0.2f degree \nWe pick a number like 13, 15, or 17 rotor blades.',beta_rl,beta_rt);
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//exapple 1.13 clc; funcprot(0); // Initialization of Variable pi=3.14159; alpha=21+30/60;//altitude of star A=140//azimuth angle delta=48;//latitude of observer //in triangle ZPM(figure in book) PZ=(90-delta)*pi/180; A=A*pi/180; ZM=(90-alpha)*pi/180; PM=(cos(PZ)*cos(ZM)+sin(ZM)*sin(PZ)*cos(A)); if PM<0 then PM=-PM; PM=acos(PM); PM=180-PM*180/pi; disp(PM-90,"declination of star in (degrees) southwards:"); end H=acos((cos(ZM)-cos(PZ)*cos(PM*pi/180))/sin(PZ)/sin(PM*pi/180)); H=2*pi-H; disp(H*180/pi,"hour angle of star in (degrees)");
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ok=open_serial(1,2,115200); if ok~=0 then error('Unable to open serial port, please check'); end for i=1:10000 //input pins; 2,3,4,5,6,7,8 representing decimal numbers from 1 to 7 resp. d1=cmd_digital_in(1,2) //decimal number 1 d2=cmd_digital_in(1,3) d3=cmd_digital_in(1,4) d4=cmd_digital_in(1,5) d5=cmd_digital_in(1,6) d6=cmd_digital_in(1,7) d7=cmd_digital_in(1,8) //decimal number 7 //output pins: LSB 10,11,12 MSB representing binary //decimal input 0, binary output 000 if d1==0 & d2==0 & d3==0 & d4==0 & d5==0 & d6==0 & d7==0 cmd_digital_out(1,10,0) cmd_digital_out(1,11,0) cmd_digital_out(1,12,0) //decimal input 1, binary output 001 else if d1==1 & d2==0 & d3==0 & d4==0 & d5==0 & d6==0 & d7==0 cmd_digital_out(1,10,0) cmd_digital_out(1,11,0) cmd_digital_out(1,12,1) //decimal input 2, binary output 010 else if d2==1 & d3==0 & d4==0 & d5==0 & d6==0 & d7==0 //since it is a PRIORITY encoder, the input d1 does not matter cmd_digital_out(1,10,0) cmd_digital_out(1,11,1) cmd_digital_out(1,12,0) //decimal input 3, binary output 011 else if d3==1 & d4==0 & d5==0 & d6==0 & d7==0 cmd_digital_out(1,10,0) cmd_digital_out(1,11,1) cmd_digital_out(1,12,1) //decimal input 4, binary output 100 else if d4==1 & d5==0 & d6==0 & d7==0 cmd_digital_out(1,10,1) cmd_digital_out(1,11,0) cmd_digital_out(1,12,0) //decimal input 5, binary output 101 else if d5==1 & d6==0 & d7==0 cmd_digital_out(1,10,1) cmd_digital_out(1,11,0) cmd_digital_out(1,12,1) //decimal input 6, binary output 110 else if d6==1 & d7==0 cmd_digital_out(1,10,1) cmd_digital_out(1,11,1) cmd_digital_out(1,12,0) //decimal input 7, binary output 111 else if d7==1 cmd_digital_out(1,10,1) cmd_digital_out(1,11,1) cmd_digital_out(1,12,1) end end end end end end end end end close_serial(1)
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//(Springs) Example 10.17 //Maximum force on the composite spring P (N) P = 6000 //Deflection in both the springs delta (mm) delta = 50 //Maximum torsional shear stress in each spring tau (N/mm2) tau = 800 //Spring index of each spring C C = 6 //Modulus of rigidity of each spring G (N/mm2) G = 81370 //For plain ends, endtype = 1 //For plain ends(ground), endtype = 2 //For square ends, endtype = 3 //For square ends(ground), endtype = 4 endtype = 4
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clear// //Variables VCC = 3.0 //Source voltage (in volts) RB = 33.0 //Base Resistance (in kilo-ohm) RC = 1.8 //Collector Resistance (in kilo-ohm) VBE = 0.7 //Emitter-to-Base Voltage (in volts) beta = 90.0 //Common emitter current gain //Calculation IB = (VCC - VBE) / (RB + beta * RC) //Base current (in milli-Ampere) IC = beta * IB //Collector current (in milli-Ampere) VCE = VCC -IC * RC //Collector-to-emitter voltage (in volts) S = (1 + beta)/(1 + beta*RC/(RC + RB)) //Stability factor //Result printf("\n DC bias current is %0.2f mA.\nDC bias voltage is %0.1f V.\nStability factor is %0.1f .",IC,VCE,S)
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//5.2 clc; V_per_cm=1.0186/60; //When S is replaced by a dry cell we get PK=85 cm for null deflection Dpk=85; V_dry_cell=Dpk*V_per_cm; printf("Voltage of dry cell=%.2f V",V_dry_cell)
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//Exa 6.1 clc; clear; close; // given data epsilon_r=2.5; epsilon_o=8.854*10^-12; d=.2*10^-3;// in m A=20*10^-4;// in m^2 omega=2*%pi*10^6;// in radians/s f=10^6; tan_delta=4*10^-4; C=epsilon_o*epsilon_r*A/d;// in F disp("Capicitance is : "+string(C*10^12)+" miu miu F"); // Formula P=V^2/R, so // R=V^2/P and P= V^2*2*%pi* f * C * tan delta, putting the value of P, we get R=1/(2*%pi*f*C*tan_delta);// in ohm disp("The element of parallel R-C circuit is : "+string(R*10^-6)+" M ohm");
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function diff() //First discrete difference of element. // Syntax //df.isna() // // Parameters // periods: int, default 1 //axis: {0 or ‘index’, 1 or ‘columns’}, default 0 //Take difference over rows (0) or columns (1). // For additional information on parameters, See https://pandas.pydata.org/pandas-docs/stable/reference/api/pandas.DataFrame.diff.html // Returns : DataFrame // NOTE: For boolean dtypes, this uses operator.xor() rather than operator.sub(). // Examples // Difference with previous column // df.diff() // Authors // Aditya Dhinavahi // Sundeep Akella endfunction
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function p=parallel(r1,r2) p=r1*r2/(r1+r2) endfunction Lbc=parallel(1/10,1/20) Leq=1/50+Lbc disp(Leq) Vbc=Lbc*150 disp(Vbc)
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//Exa 10.5 clc; clear; close; //given data format('v',13); P=3;// in atm P=P*10^5;// in N/m^2 r1=10;// in mm r1=r1*10^-3;// in m r2=20;// in mm r2=r2*10^-3;// in m R=4160;// in J/kg-K T=303;// in K D=3*10^-8;// in m^2/s S=3*0.05; // Solubility of hydrogen at a pressure of 3 atm in m^3/m^3 of rubber tubing del_x=r2-r1;// in m L=1;// in m Am=2*%pi*L*del_x/log(r2/r1); //Formula P*V= m*R*T V=S; m=P*V/(R*T);// in kg/m^3 of rubber tubing at the inner surface of the pipe C_A1=m; C_A2=0; //Diffusion flux through the cylinder is given M=D*(C_A1-C_A2)*Am/del_x; disp(M,"Diffusion flux through the cylinder in kg/sm")
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clc //initialisation of variables m= 1 //lb cp= 0.240 //btu/lb F T2= 150 //F T1= 50 //F //CALCULATIONS S= m*cp*(log(460+T2)-log(460+T1)) //RESULTS printf ('Entropy change = %.4f Btu/Fabs',S)
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//Ex14_7 clc Af = -20//closed loop gain of op-amp R = 10*10^3//output resistance Rf = -Af*R//feedback resistance disp("Af = "+string(Af)) disp("R = "+string(R)+"ohm") disp("Rf = -Af/R = "+string(Rf)+"ohm")
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// Exa 6.21 format('v',7);clc;clear;close; // Given data f = 1;// in kHz f = f * 10^3;// in Hz omega = 2*%pi*f;// in rad/sec Z1 = 200;// in ohm R2 = 200;// in ohm C2 = 5;// in µF C2 = C2 * 10^-6;// in F XC2= 1/(2*%pi*f*C2); Z2= R2-%i*XC2;// in Ω R3 = 500;// in ohm C3 = 0.2;// in µF C3 = C3 * 10^-6;// in F XC3= 1/(2*%pi*f*C3); Z3= R3-%i*XC3;// in Ω // From balance equation, Z1*Z4= Z2*Z3 Z4= Z2*Z3/Z1;// in Ω R4= real(Z4);// in Ω XC4= abs(imag(Z4));// in Ω C4= 1/(2*%pi*f*XC4);// in F C4= C4*10^6;// in µF disp("The components of Zx : ") disp("Rx= "+string(R4)+" Ω") disp("Cx= "+string(C4)+" nF")
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// Scilab code Ex4.3: Pg.158 (2008) clc; clear; theta = 45; // Scattering angle, Degrees delta_N = 450; // Number of alpha particles scattered per minute, particles/min // Since delta_N = C*sin((%pi/180)*(theta/2))^(-4), then solving for C, we get C = delta_N*(sin((%pi/180)*(theta/2)))^4; // Assumed constant theta_new = 90; // New scattered angle, Degrees delta_n = C*sin((%pi/180)*(theta_new/2))^(-4); // Number of alpha particles scattered per minute, particles/min printf("\nThe number of alpha particles scattered per minute = %2d particles/min", ceil(delta_n)); // Result // The number of alpha particles scattered per minute = 39 particles/min
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//To Find the Frequency of Oscillation clc //Given: m=1,m1=2.5 //kg s=1.8*10^3 //N/m l=(300+300)*10^-3 //m //Solution: //Calculating the Mass Moment of Inertia of the System IA=(m*l^2/3)+(m1*l^2) //kg-m^2 //Calculating the Ratio of Alpha to Theta //delta=0.3*theta //Restoring Force=s*delta=540*theta //Restoring torque about A=540*theta*0.3=162*theta N-m ...(i) //Torque about A= IA*alpha=1.02*alpha N-m ...(ii) //Equating (i) and (ii), 1.02*alpha=162*theta alphabytheta=162/1.02 //Calculating the Frequency of Oscillation n=1/(2*%pi)*sqrt(alphabytheta) //Results: printf("\n\n The Frequency of Oscillation, n = %.2f Hz.\n\n",n)
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function [F,G,H,ind]=OracleDH(lambda,ind) z = Ar'*pr + Ad'*lambda; q = (abs(z)./r).^(1/2).*sign(-z); if ind == 2 then F = -((1/3)*q'*(r.*q.*abs(q)) + pr'*Ar*q + lambda'*(Ad*q-fd)); G = 0; H = 0; end if ind == 3 then F = 0; G = -(Ad*q - fd); H = 0; end if ind == 4 then F = -((1/3)*q'*(r.*q.*abs(q)) + pr'*Ar*q + lambda'*(Ad*q-fd)); G = -(Ad*q - fd); H = 0; end if ind == 5 then [n,k] = size(z); F = 0; G = 0; H = Ad*diag( ones(n)./( 2*sqrt(r).*sqrt(abs(z)) ) )*Ad'; end if ind == 6 then F = 0; G = -(Ad*q - fd); H = Ad*diag( ones(n)./( 2*sqrt(r).*sqrt(abs(z)) ) )*Ad'; end if ind == 7 then [n,k] = size(z); F = -((1/3)*q'*(r.*q.*abs(q)) + pr'*Ar*q + lambda'*(Ad*q-fd)); G = -(Ad*q - fd); H = Ad*diag( ones(n)./( 2*sqrt(r).*sqrt(abs(z)) ) )*Ad'; end endfunction
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/3137/CH6/EX6.4/Ex6_4.sce
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FOSSEE/Scilab-TBC-Uploads
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Ex6_4.sce
//Intilization of variables F=[0;60;0] //Force defined as a matrix t1=[-3/7;6/7;-2/7] //Tension defined as a matrix t2=[4/4.47;0;-2/4.47] //tension defined as a mtrix t3=[-3/5;0;4/5] //Tension defined as a matrix //Calculations //Summation of forces in the y-direction T1=F(2,1)/t1(2,1) //N //Summation of forces in the x-direction and z direction M1=[t2(1,1) t3(1,1);t2(3,1) t3(3,1)] M2=-1*[t1(1,1)*T1;t1(3,1)*T1] R=inv(M1)*M2 //Result clc printf('The tension in the strings are T1=%f,T2=%f and T3=%f',T1,R(1),R(2))
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/1970/CH13/EX13.9/CH13Exa9.sce
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CH13Exa9.sce
// Scilab code Exa13.9 : : Page-602 (2011) clc; clear; E = 31.7; // Energy, MeV a_a = 5/9*2^(-2/3)*E; // Asymmetric binding energy term, mega electron volts printf("\nThe asymmetric binding energy term = %4.1f MeV", a_a); // Result // The asymmetric binding energy term = 11.1 MeV
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/1049/CH9/EX9.8/ch9_8.sce
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ch9_8.sce
clear; clc; V_s=230; V_m=sqrt(2)*V_s; a=60; R=20; V_or=sqrt((V_m^2/(2*%pi))*(a*%pi/180-sind(2*a)/2)+(2*V_m^2/(%pi))*(%pi-a*%pi/180+sind(2*a)/2)); printf("rms value of o/p voltage=%.2f V",V_or); I_T1r=(V_m/R)*sqrt(1/%pi*((%pi-a*%pi/180)+sind(2*a)/2)); printf("\nrms value of current for upper thyristors=%.3f A",I_T1r); I_T3r=(V_m/(2*R))*sqrt(1/%pi*((a*%pi/180)-sind(2*a)/2)); printf("\nrms value of current for lower thyristors=%.3f A",I_T3r); I1=sqrt(2)*I_T1r; I3=sqrt((sqrt(2)*I_T1r)^2+(sqrt(2)*I_T3r)^2); r=V_s*(I1+I3); printf("\nt/f VA rating=%.2f VA",r); P_o=V_or^2/R; pf=P_o/r; printf("\ni/p pf=%.4f",pf);
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/2891/CH4/EX4.4/Ex4_4.sce
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Ex4_4.sce
//Exa 4.4 clc; clear; close; //given : f=10 //frequency in Ghz f=10*10^9 //frequency in hertz c=3*10^8 //speed of light in m/s lambda=c/f //wavelength in meter N=50 // number of elements d=0.5*lambda // element spacing in meter Beta=2*(%pi)/lambda // phase shift alpha=Beta*d // progressive phase shift in radians l=N*d // Araay length in meter disp(alpha,"progressive phase shift in radians:") disp(l,"Array length in meter")
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/HUNGRY HUNGRY AIMERS.sce
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HUNGRY HUNGRY AIMERS.sce
Name=HUNGRY HUNGRY AIMERS PlayerCharacters=Character Profile BotCharacters=Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;hippo.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Character Profile AddedBots=Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;Pigeon.bot;hippo.bot;hippo.bot;hippo.bot PlayerMaxLives=0 BotMaxLives=0;0;0;0;0;0;0;0;0;0;0 PlayerTeam=1 BotTeams=2;2;2;2;2;2;2;2;1;1;1 MapName=hungry.map MapScale=4.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=0.85 BlockHealthbars=true TimeRefilledByKill=0.0 ScoreToWin=100000.0 ScorePerDamage=0.0 ScorePerKill=1.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=guess WeaponHeroTag=Pistol DifficultyTag=2 AuthorsTag=bozott BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=false Description=Based off bounce 180 GameVersion=2.0.0.1 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=Pigeon DodgeProfileNames=Long Strafes Jumping DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=2.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Clay Pigeon SeeThroughWalls=true NoDodging=false NoAiming=true AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=hippo DodgeProfileNames= DodgeProfileWeights= DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=0.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=Character Profile SeeThroughWalls=true NoDodging=true NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Character Profile MaxHealth=100.0 WeaponProfileNames=pistol;pistol4botz;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1000.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=20.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=20.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.25 ThirdPersonCamera=false TPSArmLength=500.0 TPSOffset=X=0.000 Y=125.000 Z=40.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Clay Pigeon MaxHealth=1.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.001 MaxRespawnDelay=0.001 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1100.0 MaxCrouchSpeed=500.0 Acceleration=12000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=4.0 JumpVelocity=2000.0 Gravity=4.0 AirControl=0.2 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Spheroid MainBBHeight=150.0 MainBBRadius=45.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=50.0 ProjBBRadius=25.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.05 StrafeSpeedMult=1.2 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=10.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Long Strafes Jumping MaxTargetDistance=3000.0 MinTargetDistance=500.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=3.0 MinFBTimeChange=0.5 MaxFBTimeChange=1.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.00001 MaxJumpTime=0.00001 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 [Weapon Profile] Name=pistol Type=Hitscan ShotsPerClick=1 DamagePerShot=50.0 KnockbackFactor=4.0 TimeBetweenShots=0.1 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.5 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Flare ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=pistol4botz Type=Hitscan ShotsPerClick=1 DamagePerShot=50.0 KnockbackFactor=4.0 TimeBetweenShots=0.5 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.5 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=Gunshot ParticleBodyImpact=Flare ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 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//Transport Processes and Seperation Process Principles //Chapter 11 //Example 11.3-1 //Vapour Liquid Seperation Processes //given data //85 deg C Pa1=116.9; Pb1=46; alpha1=Pa1/Pb1; // 105 deg C Pa2=204.2; Pb2=86; alpha2=Pa2/Pb2; mprintf("alpha at 85 deg C = %f",alpha1); mprintf(" alpha at 105 deg C = %f",alpha2); p=((alpha1-alpha2)/alpha2)*100; mprintf(" percentage variation=%f",p)
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//example3.27 clc disp("Load distribution in hours is as give in the table.") disp("P_i=Iron loss=1.6 kW, P_cu(FL)=3.02 kW") disp("As iron losses are constant for 24 hours, energy spent due to iron losses,") p=1.6*24 disp(p,"P_i(in kWh)=1.6*24= ") e=(6*160)+(4*80)+(1*0) disp(e,"Energy Output(in kWh)= (6*160)+(4*80)+(1*0) = ") disp("To calulate energy spent due to copper loss:") disp("Load 1: 160 kW, cos(phi)=0.8") k=160/0.8 disp(k,"Therefore, kVA=kW/cos(phi)=160/0.8=") e=3.02*6 disp(e,"Therefore, E1(in kWh)=P_cu(FL)*hours=3.02*6= ") disp("Load 2: 80kW, cos(phi)=1") k=80/1 disp(k,"Therefore, kVA=kW/cos(phi)=80/1=") n=80/200 disp(n,"Therefore, n=Fraction of load=(load kVA)/(kVA rating)=80/200=") p=(0.4^2)*3.02 format(7) disp(p,"Therefore, P_cu(in kW)=(n^2)*P_cu(FL)=(0.4^2)*3.02=") e=0.4832*4 disp(e,"Therefore, E2(in kWh)=P_cu*hours=0.4832*4=") t=38.4+18.12+1.9328 format(8) disp(t,"Total energy spent(in kWh)=P_i+E1+E2=38.4+18.12+1.9328= ") n=(1280*100)/(1280+58.4528) disp(n,"Therefore, All day eta=(total energy output in 24 hours*100)/(total energy output for 24 hours+total energy spent)=(1280*100)/(1280+58.4528)=")
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////Variable Declaration LMg = 0.0106 //Ionic conductance for Mg, S.m2/mol LCl = 0.0076 //Ionic conductance for Cl, S.m2/mol [nMg,nCl] = (1,2) //Calculations LMgCl2 = nMg*LMg + nCl*LCl //Results printf("\n Molar conductivity of MgCl2 on infinite dilution is %5.4f S.m2/mol",LMgCl2)
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function Comp_Coef = iqimbal2coef(Amp_Imb_dB, Ph_Imb_Deg) // IQIMBAL2COEF returns the I/Q imbalance compensator coefficient for given amplitude and phase imbalance. // COMP_COEF = IQIMBAL2COEF(AMP_IMB_DB, PH_IMB_DEG) returns the I/Q imbalance // compensator coefficient for given amplitude and phase imbalance. // Comp_Coef is a scalar or a vector of complex numbers. // AMP_IMB_DB and PH_IMB_DEG are the amplitude imbalance in dB // and the phase imbalance in degrees and should be of same size. // Reference: http://in.mathworks.com/help/comm/ref/iqimbal2coef.html // Written by POLA LAKSHMI PRIYANKA, FOSSEE, IIT BOMBAY // //Input argument check [out_a,inp_a]=argn(0); if (inp_a > 2) | (out_a > 1) then error('comm:iqimbal2coef: Invalid number of arguments') end if ( or(Comp_Coef==%nan) | or(Comp_Coef==%inf)) error('comm:iqimbal2coef: Input arguments should be finte') end if ( size(Amp_Imb_dB) ~= size(Ph_Imb_Deg) ) then\ error('comm:iqimbal2coef: Input arguments should be of same size') end Comp_Coef = complex(zeros(size(Amp_Imb_dB))); for i = 1:length(Amp_Imb_dB) Igain = 10^(0.5*Amp_Imb_dB(i)/20); Qgain = 10^(-0.5*Amp_Imb_dB(i)/20); angle_i = -0.5*Ph_Imb_Deg(i)*%pi/180; angle_q = %pi/2 + 0.5*Ph_Imb_Deg(i)*%pi/180; K = [Igain*cos(angle_i) Qgain*cos(angle_q); ... Igain*sin(angle_i) Qgain*sin(angle_q)]; R = inv(K); w1r = (R(1,1)+R(2,2))/2; w1i = (R(2,1)-R(1,2))/2; w2r = (R(1,1)-R(2,2))/2; w2i = (R(2,1)+R(1,2))/2; w1 = w1r + complex(0,1) * w1i; w2 = w2r + complex(0,1) * w2i; Comp_Coef(i) = w2/w1; end
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//Graphical// //Implementation of Equation 2.1.9 in Chapter 2 //Digital Signal Processing by Proakis, Third Edition, PHI //Page 46 clear; clc; close; a =1.5; n =1:10; x = (a)^n; a=gca(); a.thickness = 2; plot2d3('gnn',n,x) xtitle('Graphical Representation of Exponential Signal','n','x[n]');
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function [classe]=classifieur_barycentre(attributs_normalises,img_gris,moyenne,ecart_type,num_classe) C=zeros(1,4); [aire,perimetre,longueur,largeur]=AttributsForme(img_gris); res=[aire,perimetre,longueur,largeur]; for i=1:4 res(i)=(res(i)-moyenne(i))./ecart_type(i); end l=1; for i=1:4 attributs_barycentre(i,:)=[sum(attributs_normalises((l:l+4),1))/5,sum(attributs_normalises((l:l+4),2))/5,sum(attributs_normalises((l:l+4),3))/5,sum(attributs_normalises((l:l+4),4))/5]; l=l+5; end for app = 1:4 distance(app)=sum(abs(attributs_barycentre(app,:)-res(1,:))); end [dist_mini,ind] = min(distance); classe=ind; endfunction
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//Chapter-4,Example4_15_17,pg 4-35 S=29 //salinity t=2 //time l=0.01 //wavelength T=30 //temperature v=1510+1.14*S+4.21*T-0.037*T^2 //velocity of ultrasound in sea d=v*t/2 //depth of sea bed printf("1)depth of sea bed =") disp(d) printf("meter") f=v/l //frequency printf("2) frequency =") disp(f) printf("Hz")
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//water// //page 1.85 example 1// clc volume_hardwater=1//in litres// CaCl2=4.5//Hardness of water(gms/lit)// moles_NaCl=2;//Na3Ze giving NaCl and CaZe// mol_wt_NaCl=58.5; mol_wt_Na3Ze=111; NaCl=CaCl2*moles_NaCl*mol_wt_NaCl/mol_wt_Na3Ze; printf("\Quantity of NaCl produced is %.2f gm",NaCl);
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function [Emel] = mel_energy(Y_in, fhz, FreqBands, pl) exec('hz2mel.sci'); exec('mel2hz.sci'); exec('trianglefilter.sci'); n = length(FreqBands) - 2; fmel = linspace(FreqBands(1), FreqBands(length(FreqBands)),2000); Emel = zeros(n, 1); for i = 1:n [a start] = min(abs(fhz - mel2hz(FreqBands(i)) * ones(1, length(fhz)))); [a mid] = min(abs(fhz - mel2hz(FreqBands(i+1)) * ones(1, length(fhz)))); [a last] = min(abs(fhz - mel2hz(FreqBands(i+2)) * ones(1, length(fhz)))); fil = trianglefilter(start, mid, last, length(Y_in)); [a start] = min(abs(fmel - (FreqBands(i)) * ones(1, length(fmel)))); [a mid] = min(abs(fmel - (FreqBands(i+1)) * ones(1, length(fmel)))); [a last] = min(abs(fmel - (FreqBands(i+2)) * ones(1, length(fmel)))); fil2 = trianglefilter(start, mid, last, length(fmel)); if(pl == 1) then subplot(2,1,1); plot(fhz, fil); xlabel('Frequency in Hz'); title('Non-Uniform Filter Bank on Physical Frequency Scale'); a = gca(); a.tight_limits = "on"; subplot(2,1,2); plot(fmel,fil2); xlabel('Mel Frequency'); title('Uniform Filter Bank on Mel Frequency Scale'); a = gca(); a.tight_limits = "on"; end Emel(i) = sum((Y_in.*fil').^2); end endfunction
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P0 = 10; //atm yA0 = 0.5; T0 = 422.2;//K R = 0.082;// dm^3.atm/mol.K v0 = 6;//dm^3/s
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errcatch(-1,"stop");mode(2);//example 2.13 //page 84 ; funcprot(0); //initialisation of variable GammaB=9810*0.9;//unit weight barrage Gamma=9.81*1.09*1000;//unit weight of liquid Area=15*4; Volume=3*Area; AW=150*1000;//additional weight W=GammaB*Volume; TW=AW+W;//total weight depth=TW/Gamma/Area; disp(depth,"depth submerged (m)="); exit();
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// Scilab Code Ex4.8: Page-121 (2006) clc; clear; h = 6.626e-034; // Planck's constant, Js h_cross = h/(2*%pi); // Reduced Planck's constant, Js m = 9.1e-031; // Mass of an electron, kg e = 1.6e-019; // Energy equivalent of 1 eV, J/eV V = 1e-06; // Volume of cubical box, metre cube E_F = 7.13*e; // Fermi energy for Mg, J D_EF = V/(2*%pi^2)*(2*m/h_cross^2)^(3/2)*E_F^(1/2); // Density of states at Fermi energy for Cs, states/eV E_Mg = 1/D_EF; // The energy separation between adjacent energy levels of Mg, J printf("\nThe energy separation between adjacent energy levels of Mg = %5.3e eV", E_Mg/e); E_F = 1.58*e; // Fermi energy for Cs, J D_EF = V/(2*%pi^2)*(2*m/h_cross^2)^(3/2)*E_F^(1/2); // Density of states at Fermi energy for Mg, states/eV E_Mg = 1/D_EF; // The energy separation between adjacent energy levels of Cs, J printf("\nThe energy separation between adjacent energy levels of Cs = %5.3e eV", E_Mg/e); // Result // The energy separation between adjacent energy levels of Mg = 5.517e-023 eV // The energy separation between adjacent energy levels of Cs = 1.172e-022 eV
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// to check if zener diode shown in the figure is operating in the breakdown region // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 5-2, page 149 clear;clc; close; // Given data Rl=1*10^3;// in ohms Rs=270;// in ohms Vs=18;// in volts Vz=10;// zener voltage in volts // Calculations Vth=(Rl/(Rs+Rl))*Vs;// Thevenin voltage facing the diode disp("Volts",Vth,"Thevenin voltage=") disp("Vth>Vz") // Result // Since thevenin voltage is greater than zener voltage,zener diode is operating in the breakdown region
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//determine dc current through load and rectification efficiency and peak inverse voltage clear; clc; //soltion //given TR=31/2;//Turn ratio of the transformer rf=20;//Ω//Dynamic forward resistance Rl=1000;//Ω//Load resistance Vt=0.66;//V//Threshold voltage of diode V=220;//V//input voltage of transformer Vp=sqrt(2)*220//V//peak value of primary voltage Vm=(1/TR)*Vp; Im=(Vm-Vt)/(rf+Rl); Idc=Im/%pi; n=40.6/(1+rf/Rl); printf("The dc current through load is %d mA\n",Idc*1000); printf("The rectification efficiency is %.1f percent\n",n); printf("Peak inverse voltage =Vm = %.2f V\n",Vm)
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function [x,y]=convertABCToXY(A,B,C); // x=B + 0.5*C; x=0.5 + -0.5*A + 0.5*B; y=0.5*sqrt(3)*(1.0-A-B); endfunction
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//List of words in a linked list. clear; clc; printf("\n Exapmle 4.1\n"); x=list('sci','lab','text','companionship','project'); disp("x="); disp(x);
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m=6 gammaa=%pi/m Kb=sin(m*gammaa/2)/m/sin(gammaa/2) m=4 Kb=sin(m*gammaa/2)/m/sin(gammaa/2)
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//Example 6.12 clear; clc; C=10*10^(-9); H0bpdB=0; f0=10*10^3; Q=10; H0bp=10^(H0bpdB/20); R1=Q/(2*%pi*f0*C*H0bp); R2=(R1/((2*(Q^2))/(H0bp)))-1; R3=(2*Q)/(2*%pi*f0*C); BW=f0/Q; BWer=0.01;//BW deviation from its design value is 1% GBPmin=(2*Q*f0)/BWer; printf("Components for the mentioned circuit :"); printf("\nR1=%.2f kohms",R1*10^(-3)); printf("\nR2=%.2f ohms",R2); printf("\nR3=%.2f kohms",R3*10^(-3)); printf("\nGBP>=%.2f MHz",GBPmin*10^(-6));
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clear; clc; close; Vp = -4; gmo = 4*10^(-3); vgs1 = -4; gm1 = gmo*(1-(vgs1/Vp)); vgs2 = -2.5; gm2 = gmo*(1-(vgs2/Vp)); vgs3 = -1.5; gm3 = gmo*(1-(vgs3/Vp)); vgs4 = -1.5; gm4 = gmo*(1-(vgs4/Vp)); vgs5 = 0; gm5 = gmo*(1-(vgs5/Vp)); x = [vgs1 vgs2 vgs3 vgs4 vgs5]; y = [gm1 gm2 gm3 gm4 gm5]; plot2d(x,y); a = gca(); a.thickness = 2; a.y_location = 'right'; a.x_label.text = 'Vgs'; a.y_label.text = 'gm(S)'; a.title.text = 'gm vs Vgs';
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clc disp("Example 14.7") printf("\n") //From figure 14.9 disp("V1=50*I1 (1)"); disp("I2=300*I1 (2)"); //The equations which contain h parameters are //V1=h11*I1+h12*V2 //I2=h21*I1+h22*V2 //On comparing (1) and (2) with above equations printf("\nh11=%d\n",50); printf("h12=%d\n",0); printf("h21=%d\n",300); printf("h22=%d\n",0);
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Testdes2phase.tst
$thermo = VirtualMaterials.NRTL/Ideal/HC / -> $thermo $thermo + HYDROGEN METHANE PROPANE WATER units SI V101 = Flash.SimpleFlash() V101.LiquidPhases = 1 sep101.In.T = 45 sep101.In.P = 165 psia sep101.In.MassFlow = 852143 sep101.In.Fraction = 2 2 2 1 sep101.Vap sep101.Liq0 sep101.Vertical = DesignSep2Phase.Vertical() sep101.Horizontal = DesignSep2Phase.Horizontal() # can try: Vertical or Horizontal sep101.Vertical.Input.HoldupTime = 1500 sep101.Vertical.Input.SurgeTime = 300 sep101.Vertical.Input.Mist = 1 # boolean 1 or 0 sep101.Vertical.Input.Liq-LiqSepType = 'HC-Water' # 'HC-Caustic', 'Others' sep101.Horizontal.Input.HoldupTime = 1400 sep101.Horizontal.Input.SurgeTime = 500 sep101.Horizontal.Input.Mist = 0 # boolean 1 or 0 sep101.Horizontal.Input.Liq-LiqSepType = 'HC-Caustic' # 'HC-Caustic', 'Others' sep101.TryToSolveDesign = 1 # boolean 1 or 0 # common results sep101.Vertical.Input sep101.Vertical.Output sep101.Horizontal.Input sep101.Horizontal.Output
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5_1.sce
//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 5.1 //calculation of force exerted by the string on a particle //given data m=.5//mass(in kg) of the particle g=9.8//gravitational acceleration(in m/s^2) of the earth //calculation T=m*g//tension in the string is equal to the downward force exerted by earth printf('the force exterted by the string on particle in vertically upward direction is %3.2f N',T);
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Ex3_2.sce
// Example 3_2 clc;funcprot(0); // Given data d=110/10^3;// The diameter of the cylinder in m V_1=100;// The volume of the water in cm^3 m=50;// kg g=9.81;// The acceleration due to gravity in m/s^2 P_atm=1*10^5;// Pa // Calculation A=(%pi*d^2)/4;// m^2 P=((m*g)/A)+P_atm;// Pa V_1=V_1*10^-6;// m^3 v_1=0.001017;// m^3/kg m=V_1/v_1;// kg v_2=1.444;// m^3/kg V_2=m*v_2;// m^3 W=P*(V_2-V_1);// The work done in J printf("\nThe work done,W=%5.0f J or %2.1f kJ",W,W/10^3);
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exa8_1.sce
//Caption:Program to determine the loss limit and the multimode dispersion limit of a graded index FOC //Example 8.1 //Page 388 //Refer to figure 8.2 on page 385 Pin=42//input power = 42dB A=3//attenuation LL=(Pin/A)//Loss Limit disp('Using 2 Gbps-km as typical BDP of graded index multimode fiber, the multimode dispersion distance is determined as') Dl=(2000/90)//Dispersion limit //Result //Loss Limit = 14 km //Dispersion Limit = 22.2 km
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Ex3_2.sce
clc // Given that A = 150*6 // Cross-section of strips in mm^2 w = 150 // Width of the strip in mm ti = 6 // Thickness in mm pA = 0.20 // Reduction in area d = 400 // Diameter of steel rolls in mm Ys = 0.35// Shear Yield stress of the material before rolling in KN/mm^2 Ys_ = 0.4// Shear Yield stress of the material after rolling in KN/mm^2 mu = 0.1 // Cofficient of friction v = 30 // Speed of rolling in m/min // Sample Problem 2 on page no. 113 printf("\n # PROBLEM 3.2 # \n") tf =0.8*ti Ys_a = (Ys + Ys_)/2 r=d/2 thetaI = sqrt((ti-tf)/r) lambdaI=2*sqrt(r/tf)*atan(thetaI *sqrt(r/tf)) lambdaN = (1/2)*((1/mu)*(log(tf/ti)) + lambdaI) thetaN =(sqrt(tf/r))*(tan((lambdaN/2)*(sqrt(tf/r)))) Dtheta_a = thetaN/4 Dtheta_b = (thetaI- thetaN)/8 printf("The values of P_after are\n") i = 0 for i = 0:4 theta = i*Dtheta_a y = (1/2)* (tf+r*theta^2) lambda = 2*sqrt(r/tf)*atand(theta*(%pi/180) *sqrt(r/tf)) p_a = 2*Ys_a*(2*y/tf)*(exp(mu*lambda)) printf("%f \n",p_a) end I1 = (Dtheta_a/3) *(0.75+.925+4*(.788+.876)+2*.830)// By Simpson's rule printf("The values of P_before are\n") for i = 0:8 theta1 = i*Dtheta_b + thetaN y = (1/2)* (tf+r*theta1^2) lambda = 2*sqrt(r/tf)*atand(theta1*(%pi/180) *sqrt(r/tf)) p_b = 2*Ys_a*(2*y/ti)*(exp(mu*(lambdaI-lambda))) printf(" %f \n",p_b) end I2 = (Dtheta_b/3)*(0.925+.75+4*(.887+.828+.786+.759) + 2*(.855+.804+.772))//By Simpson's rule F = r*(I1 + I2) F_ = F*w T = (r^2)*mu*(I2-I1) T_ =T*w W = v*(1000/60)/r P = 2*T_*W printf("\n The roll separating force = %d kN,\n The power required in the rolling process = %f kW",ceil(F_),P/1000) // Answer in the book for the power required in the rolling process is given as 75.6 kW
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Ex1_9.txt
//Ex:1.9 clc; clear; close; Irms=25;// current in Amp f=0.150;// frequency in MHz y=2000; Erms=1.5*10^-3;// strength of electric field in V/m r=25*1000;// distance in m le=(Erms*y*r)/(60*%pi*Irms);// effective height of antenna in m printf("The effective height of antenna = %f m", le);
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Ex6_17.sce
clear all; clc; disp("Scilab Code Ex 6.17 : ") //Given: b = 60/1000; //m h = 30/1000; //m M = 40; //Nm c1= h/2; rib_t = 5/1000; //m rib_w = 10/1000;//m //Without Ribs: I1 = (1/12)*(b*h^3); sigma_max1 = (M*c1)/(I1*10^6); //With Ribs: y1 = c1; y2 = h+(rib_t/2); A1 = h*b; A2 = rib_t*rib_w; y_bar = ((y1*A1)+2*(y2*A2))/(A1 + 2*A2); c2 = h+rib_t - y_bar; I2 = I1 + (b*h*(y_bar - y1)^2); I3 = (1/12)*rib_w*rib_t^3 + (rib_w*rib_t*(y2 - y_bar)^2); I = I2 + 2*I3; sigma_max2 = (M*c2)/(I*10^6); if(sigma_max2>sigma_max1) printf("\n\nThe maximum normal stress in the member without ribs = %1.2f MPa',sigma_max1); printf("\nThe maximum normal stress in the member with ribs = %1.2f MPa',sigma_max2); printf("\nThe ribs should be omitted."); end //-----------------------------------------------------------------END--------------------------------------------------------------------------