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//Copyright INRIA files=G_make(['/tmp/ext4c.o'],'ext4c.dll'); link(files,'ext4c','C'); a=[1,2,3];b=[4,5,6];n=3;YesOrNo='yes'; c=call('ext4c',n,1,'i',a,2,'d',b,3,'d','out',[1,3],4,'d'); if norm(c-(sin(a)+cos(b))) > %eps then pause,end YesOrNo='no'; c=call('ext4c',n,1,'i',a,2,'d',b,3,'d','out',[1,3],4,'d'); if norm(c-(a+b)) > %eps then pause,end //clear yes --> undefined variable : yes
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result3s0.tst
@relation vehicle @attribute COMPACTNESS integer[73,119] @attribute CIRCULARITY integer[33,59] @attribute DISTANCECIRCULARITY integer[40,112] @attribute RADIUSRATIO integer[104,333] @attribute PRAXISASPECTRATIO integer[47,138] @attribute MAXLENGTHASPECTRATIO integer[2,55] @attribute SCATTERRATIO integer[112,265] @attribute ELONGATEDNESS integer[26,61] @attribute PRAXISRECTANGULAR integer[17,29] @attribute LENGTHRECTANGULAR integer[118,188] @attribute MAJORVARIANCE integer[130,320] @attribute MINORVARIANCE integer[184,1018] @attribute GYRATIONRADIUS integer[109,268] @attribute MAJORSKEWNESS integer[59,135] @attribute MINORSKEWNESS integer[0,22] @attribute MINORKURTOSIS integer[0,41] @attribute MAJORKURTOSIS integer[176,206] @attribute HOLLOWSRATIO integer[181,211] @attribute class{van,saab,bus,opel} @inputs COMPACTNESS,CIRCULARITY,DISTANCECIRCULARITY,RADIUSRATIO,PRAXISASPECTRATIO,MAXLENGTHASPECTRATIO,SCATTERRATIO,ELONGATEDNESS,PRAXISRECTANGULAR,LENGTHRECTANGULAR,MAJORVARIANCE,MINORVARIANCE,GYRATIONRADIUS,MAJORSKEWNESS,MINORSKEWNESS,MINORKURTOSIS,MAJORKURTOSIS,HOLLOWSRATIO @outputs class @data van van bus bus van van van van saab opel saab van van van opel saab opel opel van van opel saab bus bus bus bus bus bus saab saab bus bus van bus bus van saab saab van van opel saab opel opel van bus van bus saab opel van van bus bus van van bus van bus bus bus bus saab saab van van bus bus saab van saab saab van van opel saab van bus saab van saab opel opel saab opel bus saab saab opel saab van opel saab opel opel opel saab bus saab opel bus bus saab saab van bus saab saab van van saab saab opel van bus bus van van opel van bus bus saab van opel opel opel saab opel saab bus bus bus bus saab opel bus bus saab saab opel opel opel van van van van van bus bus bus bus bus van saab saab opel bus bus bus opel opel opel opel bus bus opel opel saab saab
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1;r;0 4;- p1;-;-;-;2;2;- blizzard 1 status
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//Fourier Series coefficients of half-wave rectifier output //Assume the period of the signal T=1 t=-0.5:0.01:1; T = 1; for i=1:length(t) if t(i)<T/2 then x(i)=sin(2*%pi*t(i)); else x(i)=0; end end k=-10:10; for i=1:length(k) if k(i)==1 then ak(i)=1/(4*%i); elseif k(i)==-1 ak(i)=-1/(4*%i); else ak(i)=(cos(k(i)*%pi/2)*exp(-k(i)*%pi/2*-%i))/(%pi-(%pi*k(i)*k(i))); end end disp("The fourier series coefficients are...") disp(ak) disp("magnitude of Fourier series coefficient") disp(abs(ak)) //PLotting frequency spectrum subplot(2,1,1) plot(k,abs(ak),'.'); xtitle("Magnitude Spectrum","k","|ak|"); for i=1:length(k) if k(i)==0 | k(i)==3 | k(i)==-3 | k(i)==-5 |k(i)==5 then phase(i)=0; elseif k(i)==-1 then phase(i)=%pi/2; elseif k(i)==1 then phase(i)=-%pi/2; elseif k(i)==-2 | k(i)==-4 phase(i)=%pi; elseif k(i)==2 | k(i)==4 phase(i)=-%pi; else phase(i) = 0; end end subplot(2,1,2) plot(k,phase,'.'); xtitle("Phase Spectrum","k","angle(ak)"); disp(phase)
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SPlIttEr r {} FIlter O { NoT UP ( ) or Not 7 << BitAND ( E::b:E:Cc:db:CF:C/1, ) or BItOr () <= oR NoT 63.250.123.140/85 <= -1. 234.7.255.31 >= v oR BITAND ( , 120.252.246.224, f:Db::c:b, s, ) NOt biTANd ( ) } fIltEr fg {noT Ux or dN } h -> xUOlDeX -> A gRouPeR la {AggrEgAte BiTanD(c.mb) as N ,h ,O.Fn ,eR.n ,LZRu.GO ,CoUnT(S) aS nk } UNGRoUper x { } gROupfilteR hI {nOT Pd < K GTOA ( g ( ::111.6.193.252/24, e6:aA:AB:FB:DF:AD , ), ) or nOt 88.252.1.81 = 8 or BITOr () not bItanD ( D, ) In :: } mErgEr Xj { mODULE za { BRanchEs RT, u } mODULe tp { BraNchES HB 255.243.3.227/35 < f } expORt hVjegBdQ }
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mayank1513/littleBird_RD_ResourceManagementSystem
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registerNewEntry.sce
if ~isdir(baseDir + '\Cumulative') then mkdir(baseDir + '\Cumulative'); end if ~isdir(baseDir + '\Cumulative\'+blkStr) then [status, msg] = mkdir(baseDir + '\Cumulative\'+blkStr); if status~=1 then messagebox(['directory Cumulative\'+blkStr+' could not be created'; msg],'littleBird'); end end fc_name = baseDir + '\Cumulative\' + blkStr + '\Cumulative_' + vilStr +'.csv'; wrd(1,1:2:2*size(wrdSupportType,2)) = 'WRD: '+wrdSupportType; wrd(1,2:2:$) = 'Date'; wrd(1,2*size(wrdSupportType,2):2*size(wrdSupportType,2)+1) = ['Remarks' 'Date']; if isfile(fc_name) then regNoList = csvRead(fc_name,',','.','string'); if isempty(regNoList) then messagebox('File could not be read or it was empty'); regNoList = ['Reg. No.','#familyMemebrs','SEWA', 'Starting Date',wrd,'Women Empowerment', 'Starting Date',... 'Landless', 'Starting Date','Community Care', 'Starting Date','Rural Education', 'Starting Date']; end regNo = createNewRegfile(fc_name,regNoList,nFamily,regColInd,regValues,vilStr,regDate,nReg); // exec('createNewRegfile.sce'); else regNoList = ['Reg. No.','#familyMemebrs','SEWA', 'Starting Date',wrd,'Women Empowerment', 'Starting Date',... 'Landless', 'Starting Date','Community Care', 'Starting Date','Rural Education', 'Starting Date']; regNo = createNewRegfile(fc_name,regNoList,nFamily,regColInd,regValues,vilStr,regDate,nReg); end
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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12_7.sce
clc //initialisation of variables dtp= 120 //in dpd= 48 //in vim= 1.25 //ft/sec vip= 5 //ft/sec lp = 600 //ft lm= 40 //ft //CALCULATIONS Rm= (dtp/dpd)^2/((lp/lm)*(vim/vip)^2) d= sqrt(4*Rm) //RESULTS printf ('Diameter = %.2f in ',d)
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//Exa 11.5 clc; clear; close; //Given data : VL=33*1000;//Volt f=50;//Hz l=3.4;//km d=2.5;//cm radial_thick=0.6;//cm epsilon_r=3.1;//relative permitivity V=VL*sqrt(2)/sqrt(3);//V(assuming 3 phase system) D=d+2*radial_thick;//cm D=D/100;//cm d=d/100;//m gmax=2*V/d/log(D/d);//V/m disp(gmax,"Maximum electrostatic stress(V/m)"); C=0.024*epsilon_r*l/log10(D/d);//micro F Vp=VL/sqrt(3);//V Ic=2*%pi*f*C*10^-6*Vp;//A kVA=sqrt(3)*VL*Ic*10^-3;//kVAR disp(kVA,"Total charging kVA(kVAR)");
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/Scilab Proyect/MenuPrincipal.sce
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elrick97/Numerical-Methods-FinalProyect
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2020-05-19T21:38:19.748544
2019-05-06T16:07:38
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MenuPrincipal.sce
// This GUI file is generated by guibuilder version 4.2.1 ////////// f=figure('figure_position',[400,50],'figure_size',[640,480],'auto_resize','on','background',[33],'figure_name','Graphic window number %d','dockable','off','infobar_visible','off','toolbar_visible','off','menubar_visible','off','default_axes','on','visible','off'); ////////// handles.dummy = 0; handles.raicesSelected=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0279688,0.6548035,0.2059375,0.0971616],'Relief','default','SliderStep',[0.01,0.1],'String','Raices: Bisección','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','raicesSelected','Callback','raicesSelected_callback(handles)') handles.ecuacionesSelected=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.2551563,0.6548035,0.3559375,0.0971616],'Relief','default','SliderStep',[0.01,0.1],'String','Ecuaciones Lineales: Gauss Jordan','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','ecuacionesSelected','Callback','ecuacionesSelected_callback(handles)') handles.minimosSelected=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.6309375,0.6548035,0.3659375,0.0971616],'Relief','default','SliderStep',[0.01,0.1],'String','Mínimos Cuadrados: Regresion Lineal','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','minimosSelected','Callback','minimosSelected_callback(handles)') handles.interpolacionSelected=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.1478125,0.5048035,0.3659375,0.0971616],'Relief','default','SliderStep',[0.01,0.1],'String','Interpolación: Lagrange','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','interpolacionSelected','Callback','interpolacionSelected_callback(handles)') handles.integracionSelected=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.5565625,0.5048035,0.3659375,0.0971616],'Relief','default','SliderStep',[0.01,0.1],'String','Integración: Simpson 1/3','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','integracionSelected','Callback','integracionSelected_callback(handles)') handles.titulo=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[22],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.3823438,0.8377729,0.246875,0.1205677],'Relief','default','SliderStep',[0.01,0.1],'String','Proyecto Final ','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','titulo','Callback','') handles.buttonB=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Lucida Grande','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.13875,0.8462882,0.128125,0.0915721],'Relief','default','SliderStep',[0.01,0.1],'String','Exit Program','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','buttonB','Callback','buttonB_callback(handles)') f.visible = "on"; direccion = pwd(); ////////// // Callbacks are defined as below. Please do not delete the comments as it will be used in coming version ////////// function buttonB_callback(handles) //Write your callback for buttonB here close() endfunction function raicesSelected_callback(handles) //Write your callback for raicesSelected here exec(direccion+'/BiseccionTerminado.sce',-1) endfunction function ecuacionesSelected_callback(handles) //Write your callback for ecuacionesSelected here exec(direccion+'/GaussTerminado.sce', -1) endfunction function minimosSelected_callback(handles) //Write your callback for minimosSelected here exec(direccion+'/RegresionLinealTerminado.sce', -1) endfunction function interpolacionSelected_callback(handles) //Write your callback for interpolacionSelected here exec(direccion+'/LagrangeTerminado.sce', -1) endfunction function integracionSelected_callback(handles) //Write your callback for integracionSelected here exec(direccion+'/SimpsonFinal.sce', -1) endfunction
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clc clear //input data m1=3600 //internal mass in kg Cj=2070 //average effective jet velocity in m/s tp=80 //rocket operation duration in sec g=9.81 //acceleration due to gravity in m/s^2 //calculation up=2*Cj //flight velocity in m/s MR=1/exp((up+(g*tp))/Cj) //mass ratio m2=MR*m1 //mass after rocket operation in kg PMF=1-MR //propellant mass fraction Mp=m1-m2 //mass of propellant in kg mp=Mp/tp //propellent flow rate in kg/s F=Cj*mp*10^-3 //thrust in kN Zp=(((1+((1-(1/PMF))*log(1/MR)))*Cj*tp)-(0.5*g*tp^2))*10^-3 //powered altitude gain in km Zc=((0.5*up^2)/g)*10^-3 //coasting altitude gain in km Z=Zp+Zc //maximum altitude in km //output printf('(A)flow rate of propellent is %3.2f kg/s\n (B)thrust developed is %3.3f kN\n (C)altitude gains during powered and coasting flights are %3.3f km and %3.3f km respectively',mp,F,Zp,Zc)
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impr=[0.00482434335771622 0.0307287177680858 0.0905946819548830 0.167944821844737 0.224641271344028 0.233457187867600 0.193512552162805 0.123765243571014 0.0496036031380564 -0.00850905187491905 -0.0406738350178078 -0.0475631979469693 -0.0368517338223927 -0.0185628385243508 -0.00125221912683350 0.0100331628527344 0.0139990059845170 0.0121118272327119 0.00712186446378611 0.00173298095479109]; num_ord=4; den_ord=4; [num,den]=prony(impr,num_ord,den_ord); disp(num); disp(den); //output // 0.0048243 0.0192974 0.0289461 // // column 4 to 5 // // 0.0192974 0.0048243 // // // column 1 to 3 // // 1. - 2.369513 2.3139884 // // column 4 to 5 // // - 1.0546654 0.1873795 //
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//EXERCISE 1 - QUESTION 3 close(); exec('amplify.sce'); n = [0:10]; x = 2+3*n; y = amplify(x, 5); z = amplify(x, -3); plot(n,x,'b-o'); plot(n,y,'r--*'); plot(n,z,'g:+'); title('Amplifier'); xlabel('n'); ylabel('Signal'); legend('x[n]= 2+3*n','y[n]=x+5','z[n]=x-3');
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//**************************** LOOKUP Table ******************************** if(blk_name.entries(bl)=='lkuptb') then mputl("# LOOKUP Table-> "+scs_m.objs(blk_objs(bl)).model.opar(1),fd_w); truecase=strsplit(scs_m.objs(blk_objs(bl)).model.opar(2)," ") if scs_m.objs(bl).model.ipar(1) == 1 then lkuptb_str='.names'+' net' + string(blk(blk_objs(bl),2))+"_" + string(1)+' tg4logic_1 tg4logic_2 tg4logic_3'+' net'+ string(blk(blk_objs(bl),2+numofip))+"_" + string(1); end if scs_m.objs(bl).model.ipar(1) == 2 then lkuptb_str='.names'+' net' + string(blk(blk_objs(bl),2))+"_" + string(1)+' net'+ string(blk(blk_objs(bl),3))+"_" + string(1)+' tg4logic_1 tg4logic_2'+' net'+ string(blk(blk_objs(bl),2+numofip))+"_" + string(1); end if scs_m.objs(bl).model.ipar(1) == 3 then lkuptb_str='.names'+' net' + string(blk(blk_objs(bl),2))+"_" + string(1)+' net'+ string(blk(blk_objs(bl),3))+"_" + string(1)+' net' + string(blk(blk_objs(bl),4))+"_" + string(1)+' tg4logic_1'+' net'+ string(blk(blk_objs(bl),2+numofip))+"_" + string(1); end if scs_m.objs(bl).model.ipar(1) == 4 then lkuptb_str='.names'+' net' + string(blk(blk_objs(bl),2))+"_" + string(1)+' net'+ string(blk(blk_objs(bl),3))+"_" + string(1)+' net' + string(blk(blk_objs(bl),4))+"_" + string(1)+' net'+ string(blk(blk_objs(bl),5))+"_" + string(1)+' net'+ string(blk(blk_objs(bl),2+numofip))+"_" + string(1); end mputl(lkuptb_str,fd_w); for i=1:size(truecase,1) mputl(truecase(i)+' 1',fd_w); end mputl(" ",fd_w) if scs_m.objs(bl).model.rpar(1) == 1 then plcvpr = %t; plcloc=[plcloc;'net'+string(blk(blk_objs(bl),2+numofip))+'_1',string(scs_m.objs(bl).model.rpar(2))+' '+string(scs_m.objs(bl).model.rpar(3))+' 0']; end //**************************** LPF ************************************* elseif (blk_name.entries(bl) =='lpf') then mputl("# lpf",fd_w); for otabuf_i = 1:scs_m.objs(bl).model.rpar(1) lpf_str=".subckt lpf in[0]=net"+string(blk(blk_objs(bl),2))+ "_" + string(otabuf_i)+" out[0]=net"+ string(blk(blk_objs(bl),2+numofip))+ "_" + string(otabuf_i)+ " #ota_biasfb[0] =" +string(sprintf('%1.12f',scs_m.objs(blk_objs(bl)).model.rpar(2)))+" &lpf_fg[0] =0"; lpfcap = scs_m.objs(blk_objs(bl)).model.rpar(3) select lpfcap case 1 then lpf_str= lpf_str +"&lpf_cap_1x[0] =0"; case 2 then lpf_str= lpf_str +"&lpf_cap_2x[0] =0"; case 3 then lpf_str= lpf_str +"&lpf_cap_3x[0] =0"; case 4 then lpf_str= lpf_str +"&lpf_cap_3x[0] =0"+"&lpf_cap_1x[1] =0"; case 5 then lpf_str= lpf_str +"&lpf_cap_3x[0] =0"+"&lpf_cap_2x[1] =0"; case 6 then lpf_str= lpf_str +"&lpf_cap_3x[0] =0"+"&lpf_cap_2x[1] =0"+"&lpf_cap_1x[2] =0"; case 18 then lpf_str= lpf_str +"&lpf_cap_3x[0] =0"+"&lpf_cap_2x[0] =0"+"&lpf_cap_1x[0] =0"+"&lpf_cap_3x[2] =0"+"&lpf_cap_2x[2] =0"+"&lpf_cap_1x[2] =0" +"&lpf_cap_3x[3] =0"+"&lpf_cap_2x[3] =0"+"&lpf_cap_1x[3] =0"; else error("LPF capacitor cannot be compiled."); end mputl(lpf_str,fd_w); mputl(" ",fd_w); end end
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clc;funcprot(0); //Example 4.1 //Initializing the variables y = linspace(0,80,9); x = [0 23 28 31 32 29 22 14 0]; xlabel('Velocity (m/s)'); ylabel('Distance from one side(mm)'); xgrid(1); //Calculations plot(x,y,'-*'); mu=[17.5 26.0 29.6 31.9 30.7 25.4 18.1 7.7]; // mean velocity disp(mean(mu),"Mean velocity (m/s):"); // the plot is attached as 4.1.png
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// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Manoj Sree Harsha & M Avinash Reddy // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in // function [] = opticalflow(a) //Calculates optical flow. // //Calling Sequence //opticalflow(vid) // //Parameters //vid : a video // //Description //opticalflow(vid) returns an opticalflow video and it will be written to 'out.avi' file (In the current working directory). // //Examples //opticalflow('ball.mp4'); //opticalflow('vtest.avi'); //Authors // Manoj Sree Harsha , M Avinash Reddy raw_opticalflow(a); endfunction
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// exa 6.2 Pg 170 clc;clear;close; // Given Data Tmax=400;// N.m Tmin=140;// N.m Mmax=500;// N.m Mmin=250;// N.m Sut=540;// MPa Syt=400;// MPa n=2;// factor of safety Kf=1.25;// given Se_dash=0.4*Sut;// Mpa Se=Se_dash/Kf;//MPa Sys=0.577*Syt;// MPa Ses=0.577*Se;// MPa Mm=(Mmax+Mmin)/2;// N.m Ma=(Mmax-Mmin)/2;// N.m Tm=(Tmax+Tmin)/2;// N.m Ta=(Tmax-Tmin)/2;// N.m // Max. Distortion energy theory - Syt/n = 32/%pi/d**3*sqrt((Mm+Ma*(Syt/Se)**2)+0.75*(Tm+Ta*(Sys/Ses))**2) d = (32/%pi*sqrt((Mm+Ma*(Syt/Se))**2+0.75*(Tm+Ta*(Sys/Ses))**2)*1000/(Syt/n))**(1/3) ; // mm printf('shaft diameter = %.2f mm. Use %.f mm.',d,d)
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clc; clear all; Ef=5.51 //in eV E=(3/5)*Ef;//The average energy of a free electron in silver at 0k disp(+'eV',E,'The average energy of a free electron in silver at 0k =')
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//Chapter 13 Thermodynamics Entropy and Free Energy clc; clear; //Initialisation of Variables H= 540 //cal per gram m= 9 //gms T= 100 //C //CALCULATIONS S= H*m/(273+T) //RESULTS mprintf("Entropy change = %.2f E.U",S)
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d1 = 2.78 * 10^19; //max density for Si d2 = 7.72 * 10^18; // max density for GaAs Nd = 10^17; Ni = 1.5*10^10; Ni2 = 1.84 * 10^6; Pi2 = 1.84 * 10^6; Pi = 1.5*10^10; un1 = 1000; up1 = 350; un2 = 8000; up2 = 400; Nn = 0.5*Nd; Pn = Ni^2/Nn; q = 1.6*10^-19; s1 = d1*q*un1; s2 = d2*q*up2; //To find the minimum we take the derivative with respect to p and equate the result to zero, which gives the below expression p = Ni*(un1/up1)^0.5; smin1 = Ni*q*(un1*(up1/un1)^0.5 + up1*(un1/up1)^0.5); smin2 = Ni2*q*(un2*(up2/un2)^0.5 + up2*(un2/up2)^0.5); disp(s1,"maximum conductivity for Si = ") disp(s2,"maximum conductivity for GaAs = ") disp(smin1,"minimum conductivity for Si = ") disp(smin2,"minimum conductivity for GaAs = ")
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//Example 17_14 clc(); clear; //To find the I1,I2,I3 values and charge on the capacitor v1=12 //Units in V r1=6 //Units in Ohms i1=v1/r1 //Units in A v2=4 //Units in V r2=8 //Units in Ohms i3=(v1+v2)/r2 //Units in A i2=i1+i3 //Units in A printf("Current in wire 1 is I1=%d A\nCurrent in wire 2 is I2=%d A\nCurrent in wire 3 is I3=%d A\n",i1,i2,i3) v3=10 //Units in V vfg=-v3+(r1*i1) //Units in V c=5*10^-6 //Units in F q=c*vfg //Units in C printf("The charge on the capacitor is q=%.5f C",q)
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fs = 1000;t = 0:1/fs:2; //x = vco(sin(2*pi*t),[10 490],fs); strips(x,0.25,fs) //plot is displayed
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// Scilab code: Ex3.17 : Mean energy per electron at 0K:Pg: 86 (2008) m = 9.1e-031; // Mass of an electron, kg a = 50e-010; // Length of molecule, m h = 6.624e-034; // Plancks constant, joule second E = h^2/(8*m*a^2); // Energy per electron, joule printf("\nThe mean energy per electron at 0K = %3.1e eV ", E/1.6e-019); // Result // The mean energy per electron at 0K = 1.5e-002 eV
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clear clc //Example 11.9 NEGATIVE LIFT ON A RACE CAR l=1.5; //[m] c=0.25; //[m] A=l/c //aspect ratio //Interpolating for A, from fig 11.23 CL=0.93; //lift coefficient CD=0.07; //drag coefficient S=l*c //area [m^2] Vo=75; //velocity [m/s] rho=1.17; //[Kg/m^3] //Lift force FL=CL*S*rho*Vo^2/2 //[N] printf("\nThe downward thrust from the vane = %.f N.\n",FL) //Drag force FD=CD*S*rho*Vo^2/2 printf("\nThe drag from the vane = %.1f N.\n",FD)
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// example 5.13 // caption: simpson 3-8 rule // let integration of f(x)=1/(1+x) in the range [0,1] by simpson 3-8 rule is equal to I x=0:1/3:1; deff('[y]=f(x)','y=1/(1+x)') [I] = simpson38(x,f)
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//problem 25 pagenumber 2.108 //given format(7); rf1=10e3;//ohm vi=1e-2;//volt vt=0.0257;//volt //determine output voltage vi=exp(vi/vt); v0=-vi*rf1; disp('Output voltage = '+string(v0)+' V');
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~BivLCM-SR-bfas_ea_vrt_col_d-PLin-VLin.tst
THE OPTIMIZATION ALGORITHM HAS CHANGED TO THE EM ALGORITHM. ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.416625D+00 2 -0.621651D-02 0.296334D-02 3 0.178205D-01 -0.113112D-02 0.391541D+00 4 -0.186012D-02 -0.131282D-04 -0.177972D-02 0.335055D-02 5 0.933882D-04 0.411844D-04 -0.190447D-02 0.261562D-03 0.438777D-02 6 0.129307D-03 0.832393D-04 0.429632D-03 -0.786903D-04 -0.391552D-04 7 0.141304D-02 0.710851D-04 0.900216D-03 -0.189187D-04 0.905029D-03 8 0.626389D-03 0.389497D-04 -0.130462D-02 0.113769D-03 -0.904103D-04 9 -0.442002D+00 0.777315D-02 0.160985D+00 0.178483D-02 0.199162D+00 10 -0.128243D+00 -0.626679D-02 0.356068D-01 0.131039D-01 0.236273D+00 11 -0.246807D+00 0.983077D-02 -0.139934D-01 -0.385061D-02 0.373227D-01 12 0.115719D+00 -0.133993D-01 -0.122545D+01 0.514803D-01 0.141169D-01 13 0.982888D-01 0.903876D-02 0.682111D-01 -0.877265D-03 0.418738D-01 14 0.128199D+00 -0.210421D-02 -0.489423D+00 0.193619D-01 0.407215D-01 15 -0.379520D+01 -0.255480D-02 -0.776785D+00 -0.475027D-01 -0.165188D+00 16 0.610132D-02 -0.129884D-01 -0.170798D-01 0.142296D-02 0.714506D-03 17 0.438234D-02 0.270755D-04 0.575634D-02 0.531684D-04 -0.139258D-02 18 -0.946802D+00 -0.142351D-01 -0.734797D-01 -0.369884D-01 0.971933D-01 19 -0.165529D+00 0.668324D-02 0.102973D+00 0.519789D-02 0.177721D-01 20 0.319137D+00 -0.453525D-01 -0.332395D+01 -0.519026D-01 -0.458816D-01 21 0.102397D+00 -0.223870D-02 -0.726498D-01 0.863170D-04 -0.184927D-01 22 0.718006D-02 -0.338925D-03 0.398311D-02 0.725062D-03 -0.115639D-02 23 0.434118D-01 0.122145D-02 -0.474495D-01 -0.128162D-01 -0.561345D-02 24 -0.137761D-02 0.930987D-03 0.583619D-02 -0.746286D-03 0.267343D-03 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.675431D-03 7 0.607398D-03 0.322845D-02 8 0.532489D-04 -0.337057D-03 0.172764D-02 9 0.239022D-01 0.358865D-01 -0.557568D-02 0.612870D+02 10 -0.125596D-01 0.442649D-01 -0.101076D-01 0.111565D+02 0.249334D+02 11 0.193334D-01 0.253007D-01 -0.135052D-01 0.752801D+01 0.117744D+01 12 -0.155168D-01 -0.945766D-02 0.985470D-02 -0.952625D-01 0.349779D+00 13 0.446215D-01 0.137972D+00 -0.152840D-01 0.390227D+01 0.323032D+01 14 0.412861D-02 -0.253379D-01 0.145598D+00 0.176037D+01 0.362031D+01 15 -0.139326D-01 -0.748805D-01 -0.205399D-01 -0.154456D+02 -0.141633D+02 16 -0.699243D-03 -0.153326D-02 -0.123760D-02 0.108138D+01 0.142735D+00 17 0.143841D-03 0.163888D-03 0.946610D-04 -0.194800D+00 -0.952501D-01 18 -0.345659D-01 -0.386903D-01 -0.337965D-01 0.486039D+01 0.889287D+01 19 -0.104826D-01 0.510968D-02 -0.253186D-02 -0.278566D+00 0.918991D+00 20 0.513980D-02 0.890997D-01 -0.926279D-01 -0.126203D+01 0.234238D+01 21 0.824236D-02 -0.940340D-02 0.211073D-02 -0.262027D+00 -0.104090D+01 22 -0.505802D-04 -0.618372D-03 0.278023D-03 -0.109094D-01 -0.865654D-01 23 -0.291765D-03 -0.769619D-03 -0.445063D-03 -0.746316D+00 -0.224423D+00 24 0.646144D-04 -0.161724D-03 -0.131459D-03 0.665423D-01 -0.625500D-02 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.369036D+02 12 -0.409251D+01 0.125270D+03 13 -0.276342D+01 0.270584D+01 0.164687D+02 14 -0.144673D+01 -0.188921D+01 -0.283772D+01 0.567481D+02 15 -0.737176D+01 -0.885620D+01 -0.302458D+01 -0.564952D+01 0.488724D+03 16 0.190934D+00 -0.118344D+00 -0.639764D-01 -0.321687D+00 0.204134D+01 17 0.231767D-01 0.106040D+00 -0.250202D-01 0.381160D-01 -0.225668D+01 18 -0.657595D+01 0.137825D+01 -0.127694D+01 -0.597928D+01 0.684416D+02 19 0.276223D+00 -0.429796D+01 -0.888398D+00 0.116056D+01 0.364839D+01 20 -0.589602D+01 -0.149311D+02 0.525431D+01 -0.163845D+02 0.687246D+02 21 -0.214649D+00 0.378733D+01 0.520557D+00 -0.886897D+00 -0.505355D+01 22 0.134754D-01 0.346037D-01 -0.398733D-01 0.222373D-01 -0.478564D+00 23 0.607402D-01 -0.276069D+00 -0.126297D+00 0.177020D+00 0.959444D-01 24 0.573463D-01 -0.140755D+00 -0.188687D-02 -0.832759D-01 -0.252079D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.776129D+00 17 -0.603350D-01 0.264684D-01 18 -0.815393D+00 -0.566916D+00 0.301840D+03 19 0.248532D-01 -0.370101D-01 0.511340D+01 0.610062D+01 20 0.341981D+00 -0.357817D+00 0.254932D+01 -0.202395D+01 0.497623D+03 21 -0.157178D+00 0.610271D-01 -0.155029D+01 -0.555251D+01 0.802431D+00 22 0.113580D-01 0.430615D-02 -0.138352D+01 -0.406276D-01 -0.713813D-01 23 0.193793D-01 0.459978D-02 -0.156144D+01 -0.408660D+00 0.469525D+01 24 0.144042D-02 0.130794D-02 0.103950D+00 0.515470D-01 -0.248351D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.662849D+01 22 -0.109969D-01 0.134607D-01 23 0.315978D+00 0.460803D-02 0.646752D+00 24 -0.551165D-01 -0.153305D-02 -0.367901D-01 0.259853D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.177 1.000 3 0.044 -0.033 1.000 4 -0.050 -0.004 -0.049 1.000 5 0.002 0.011 -0.046 0.068 1.000 6 0.008 0.059 0.026 -0.052 -0.023 7 0.039 0.023 0.025 -0.006 0.240 8 0.023 0.017 -0.050 0.047 -0.033 9 -0.087 0.018 0.033 0.004 0.384 10 -0.040 -0.023 0.011 0.045 0.714 11 -0.063 0.030 -0.004 -0.011 0.093 12 0.016 -0.022 -0.175 0.079 0.019 13 0.038 0.041 0.027 -0.004 0.156 14 0.026 -0.005 -0.104 0.044 0.082 15 -0.266 -0.002 -0.056 -0.037 -0.113 16 0.011 -0.271 -0.031 0.028 0.012 17 0.042 0.003 0.057 0.006 -0.129 18 -0.084 -0.015 -0.007 -0.037 0.084 19 -0.104 0.050 0.067 0.036 0.109 20 0.022 -0.037 -0.238 -0.040 -0.031 21 0.062 -0.016 -0.045 0.001 -0.108 22 0.096 -0.054 0.055 0.108 -0.150 23 0.084 0.028 -0.094 -0.275 -0.105 24 -0.013 0.106 0.058 -0.080 0.025 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.411 1.000 8 0.049 -0.143 1.000 9 0.117 0.081 -0.017 1.000 10 -0.097 0.156 -0.049 0.285 1.000 11 0.122 0.073 -0.053 0.158 0.039 12 -0.053 -0.015 0.021 -0.001 0.006 13 0.423 0.598 -0.091 0.123 0.159 14 0.021 -0.059 0.465 0.030 0.096 15 -0.024 -0.060 -0.022 -0.089 -0.128 16 -0.031 -0.031 -0.034 0.157 0.032 17 0.034 0.018 0.014 -0.153 -0.117 18 -0.077 -0.039 -0.047 0.036 0.103 19 -0.163 0.036 -0.025 -0.014 0.075 20 0.009 0.070 -0.100 -0.007 0.021 21 0.123 -0.064 0.020 -0.013 -0.081 22 -0.017 -0.094 0.058 -0.012 -0.149 23 -0.014 -0.017 -0.013 -0.119 -0.056 24 0.015 -0.018 -0.020 0.053 -0.008 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 -0.060 1.000 13 -0.112 0.060 1.000 14 -0.032 -0.022 -0.093 1.000 15 -0.055 -0.036 -0.034 -0.034 1.000 16 0.036 -0.012 -0.018 -0.048 0.105 17 0.023 0.058 -0.038 0.031 -0.627 18 -0.062 0.007 -0.018 -0.046 0.178 19 0.018 -0.155 -0.089 0.062 0.067 20 -0.044 -0.060 0.058 -0.098 0.139 21 -0.014 0.131 0.050 -0.046 -0.089 22 0.019 0.027 -0.085 0.025 -0.187 23 0.012 -0.031 -0.039 0.029 0.005 24 0.059 -0.078 -0.003 -0.069 -0.071 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.421 1.000 18 -0.053 -0.201 1.000 19 0.011 -0.092 0.119 1.000 20 0.017 -0.099 0.007 -0.037 1.000 21 -0.069 0.146 -0.035 -0.873 0.014 22 0.111 0.228 -0.686 -0.142 -0.028 23 0.027 0.035 -0.112 -0.206 0.262 24 0.010 0.050 0.037 0.129 -0.691 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.037 1.000 23 0.153 0.049 1.000 24 -0.133 -0.082 -0.284 1.000
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/Octave/octave-4.2.1/share/octave/packages/interval-2.1.0/test/abs_rev.tst
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vohrahul/ML-ang-coursera
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abs_rev.tst
## DO NOT EDIT! Generated automatically from test/abs_rev.itl ## by the Interval Testing Framework for IEEE 1788. ## https://github.com/nehmeier/ITF1788/tree/92558f7e942665a78f2e883dbe7af52320100fba ## ## Copyright 2015-2016 Oliver Heimlich ## ## This program is free software; you can redistribute it and/or modify ## it under the terms of the GNU General Public License as published by ## the Free Software Foundation; either version 3 of the License, or ## (at your option) any later version. ## ## This program is distributed in the hope that it will be useful, ## but WITHOUT ANY WARRANTY; without even the implied warranty of ## MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the ## GNU General Public License for more details. ## ## You should have received a copy of the GNU General Public License ## along with this program; if not, see <http://www.gnu.org/licenses/>. ## %!#Test library imports %!#Arithmetic library imports pkg load interval %!#Preamble try; error ("__FILE__"); catch test (lasterror.stack.file, "quiet", stdout); end_try_catch; %!function assert_warn (observed_value, expected_value) %! if (not (isequal (observed_value, expected_value))) %! observed_expression = regexprep (argn(1, :), '\s+$', ''); %! expected_expression = regexprep (argn(2, :), '\s+$', ''); %! observed_as_char = disp (observed_value)(1 : end - 1); %! expected_as_char = disp(expected_value)(1 : end - 1); %! warning ([observed_expression, " != ", expected_expression, ... %! "\n ", observed_as_char, " != ", expected_as_char]); %! endif %!endfunction ## minimal.absRevBin_test %!test %! assert (isequal (absrev (infsup, infsup (-inf, inf)), infsup)); %!test %! assert (isequal (absrev (infsup (0.0, 1.0), infsup), infsup)); %!test %! assert (isequal (absrev (infsup (0.0, 1.0), infsup (7.0, 9.0)), infsup)); %!test %! assert (isequal (absrev (infsup, infsup (0.0, 1.0)), infsup)); %!test %! assert (isequal (absrev (infsup (-2.0, -1.0), infsup (-inf, inf)), infsup)); %!test %! assert (isequal (absrev (infsup (1.0, 1.0), infsup (-inf, inf)), infsup (-1.0, 1.0))); %!test %! assert (isequal (absrev (infsup (0.0, 0.0), infsup (-inf, inf)), infsup (0.0, 0.0))); %!test %! assert (isequal (absrev (infsup (-1.0, -1.0), infsup (-inf, inf)), infsup)); %!test %! assert (isequal (absrev (infsup (1.797693134862315708e+308, 1.797693134862315708e+308), infsup (-inf, inf)), infsup (-1.797693134862315708e+308, 1.797693134862315708e+308))); %!test %! assert (isequal (absrev (infsup (2.225073858507201383e-308, 2.225073858507201383e-308), infsup (-inf, inf)), infsup (-2.225073858507201383e-308, 2.225073858507201383e-308))); %!test %! assert (isequal (absrev (infsup (-2.225073858507201383e-308, -2.225073858507201383e-308), infsup (-inf, inf)), infsup)); %!test %! assert (isequal (absrev (infsup (-1.797693134862315708e+308, -1.797693134862315708e+308), infsup (-inf, inf)), infsup)); %!test %! assert (isequal (absrev (infsup (1.0, 2.0), infsup (-inf, inf)), infsup (-2.0, 2.0))); %!test %! assert (isequal (absrev (infsup (1.0, 2.0), infsup (0.0, 2.0)), infsup (1.0, 2.0))); %!test %! assert (isequal (absrev (infsup (0.0, 1.0), infsup (-0.5, 2.0)), infsup (-0.5, 1.0))); %!test %! assert (isequal (absrev (infsup (-1.0, 1.0), infsup (-inf, inf)), infsup (-1.0, 1.0))); %!test %! assert (isequal (absrev (infsup (-1.0, 0.0), infsup (-inf, inf)), infsup (0.0, 0.0))); %!test %! assert (isequal (absrev (infsup (0.0, inf), infsup (-inf, inf)), infsup (-inf, inf))); %!test %! assert (isequal (absrev (infsup (-inf, inf), infsup (-inf, inf)), infsup (-inf, inf))); %!test %! assert (isequal (absrev (infsup (-inf, 0.0), infsup (-inf, inf)), infsup (0.0, 0.0))); %!test %! assert (isequal (absrev (infsup (1.0, inf), infsup (-inf, 0.0)), infsup (-inf, -1.0))); %!test %! assert (isequal (absrev (infsup (-1.0, inf), infsup (-inf, inf)), infsup (-inf, inf))); %!test %! assert (isequal (absrev (infsup (-inf, -1.0), infsup (-inf, inf)), infsup)); %!test %! assert (isequal (absrev (infsup (-inf, 1.0), infsup (-inf, inf)), infsup (-1.0, 1.0)));
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/1523/CH4/EX4.3/ex4_3.sce
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ex4_3.sce
//AC Circuits:example 4.3:(pg4.5) f=50; I=20; t1=0.0025; t2=0.0125; I1=14.14; pi=3.14; disp("f=50 c/s"); disp("I=20 A"); mprintf("Im=I*sqrt(2)"); Im=(sqrt(2)*I); printf("\nIm=%.2f A",Im); mprintf("\nEquation of current, \ni=Im*sin(2*pi*f*t)"); disp("=28.28sin(2*pi*f*t)=28.28sin(100*pi*t)"); disp("(a)At t=0.0025 seconds"); i=(Im*sin(2*pi*f*t1)); printf("i=%.f A",i); //when t=0.0025seconds disp("(b)At t=0.0125 seconds"); i=(Im*sin(2*pi*f*t2)); printf("i=%.f A",i); //when t=0.0125seconds disp("(c) i=28.28sin(100*pi*t) "); t=(asind(I1/Im)/(2*pi*f)); printf("t=%.e second",t);// when I=14.14A
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20_5.sce
clear// //Variables V0 = 10 //Regulated dc supply (in volts) LR = 0.00002 //Line regulation //Calculation dV = LR * V0 //Change in output voltage (in volts) //Result printf("\n Change in output voltage is %0.3f mV.",dV * 10**3)
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example5.sce
// calculate ac output voltage and input impedance of the diff amp using second approximation // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 17-5, page 632 clear; clc; close; // Given data Vee=15;// in volts from the figure Vcc=15;// in volts from the figure Re=7.5*10^3;// emitter resistance in ohms Rc=5*10^3;// collector resistance in ohms Vin=10^-3;// in volts B=300;// given // Calculations It=(Vee-0.7)/Re;// tail current in amperes using second approximation Ie=It/2;// emitter current in amperes re=25*10^-3/Ie;// ac emitter resistance in ohms Av=Rc/re;// voltage gain Vout=Av*Vin;// ac output voltage in volts zin=2*B*re;// input impedance of either base in ohms disp("Volts",Vout,"output voltage=") disp("ohms",zin,"input impedance=") // Result // ac output voltage is 191 mVolts // Input impedance of the differential amplifier is 15.7 Kohms
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Ex24_4.sce
clear //Given v=2.1*10**7 //m/s a=4.8*10**7 //C/Kg Z=79 e=1.6*10**-19 m=9*10**9 //Calculation r0=(2*m*Z*e*a)/v**2 //Result printf("\n Distance of the closest approach is %0.1f *10**-14 m",r0*10**14)
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/581/CH5/EX5.7/Example5_7.sce
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Example5_7.sce
clear; clc; printf("\t Example 5.7\n"); //w=2*3.14 rad/yr , a=w*t=0 at present.first we find the depths at which a=0 curve reaches its local extrema.(we pick the a=0 curve because it) gives the highest temperature at t=o.).tan(o-e)=1 so e=3%pi/4, 7%pi/4....and the first minima occurs where e=3%pi/4=2.356. b=0.139*10^-6; //thermal diffusivity, m^2/s x=2.356/(2*3.14/(2*b*365*24*3600))^0.5; //depth of digging of earth to find the temperature wave printf("\t depth of digging of earth is :%.3f m, if we dug in the earth, we would find it growing older until it reached a maximum coldness at a depth of about 2.8 m.Farther down, it would begin to warm up again, but nt much. in midwinter, the reverse would be true \n",x); //end
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// Example 19_1 clc;funcprot(0); // Given data T=20.0+273.16;// K d=0.0100;// m alpha_cu=3.50*10^-6;// V/K rho_e=5.00*10^-9;// ohm m dphibydx=1.00;// Voltage gradient in V/m // Solution A=(%pi/4)*d^2;// m^2 I=(A/rho_e)*dphibydx;// A Q_P=alpha_cu*T*I;// W printf('\nThe Peltier heat flow,Q_P=%2.1f W',Q_P);
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//clear// //Caption:Program to find the refractive index of the prism material //Example13.8 //page463 clear; clc; n2 =1.00; //refractive index of air teta1 = 45; //incident angle in degrees teta1 = 45/57.3;//incident angle in radians n1 = n2/sin(teta1); disp(n1,'refractive index of prism material n1=') //Result //refractive index of prism material n1= // 1.4142954
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//Example No. 14_03 //Eigen Vectors //Pg No. 473 clear ; close ; clc ; A = [8 -4 ; 2 2 ] ; lamd = poly(0,'lamd') p = det(A - lamd*eye()) root = roots(p) mprintf('\n The roots are \n lamda1 = %f \n lamda2 = %f \n ',root(1),root(2)) A1 = A - root(1)*eye() X1 = [-1*A1(1,2)/A1(1,1) ; 1] disp(X1,'X1 = ') A2 = A - root(2)*eye() X2 = [-1*A2(1,2)/A2(1,1) ; 1] disp(X2,'X2 = ')
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clc //initialisation of variables L= 2.5 //ft H= 1 //ft g= 32.2 //ft/sec^2 Cd= 0.61 L1= 1.75 //ft L2= 2.25 //ft //CALCULATIONS Q1= 2*Cd*sqrt(2*g)*L*H/3 Q2= 2*Cd*sqrt(2*g)*L1*(L1^1.5-1)/3 Q3= 2*Cd*sqrt(2*g)*H*(L2^1.5-L1^1.5)/3 Q= Q1+Q2+Q3 //RESULTS printf ('Total discharge = %.1f cfs ',Q)
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BOOT.SCI
DSKCLS DFSCLS SCSICLS SCSIADTA SDSKDRV # CONDRV KBDADRV VGAADRV
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// Scilab Code Ex1.19 Electron speed equivalent of twice its rest mass: Pg: 28 (2008) m0 = 9.1e-031; // Rest mass of an electron, kg m = 2*m0; // Mass of moving electron, kg c = 3e+08; // Speed of light, m/s // As m = m0/sqrt(1 - (v/c)^2), Relativistic mass of electron, kg, solving for v, we have v = sqrt(1 - (m0/m)^2)*c; // Velocity of moving electron, m/s printf("\nThe speed of electron so that its mass becomes twice its rest mass = %5.3e m/s", v); // Result // The speed of electron so that its mass becomes twice its rest mass = 2.598e+008 m/s
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clear clc // Identifica sistema a partir de pontos entrada/saida // Pasta de leitura dos arquivos DATADIR='C:\Users\Álvaro\Google Drive\0 mestrado mecatronica\2017.2\INTRODUÇÃO À IDENTIFICAÇÃO DE SISTEMAS\Trabalho_final'; exec('C:\Users\Álvaro\Google Drive\0 mestrado mecatronica\2017.2\INTRODUÇÃO À IDENTIFICAÇÃO DE SISTEMAS\Trabalho_final\identificacao.sci', -1) // Armazena a pasta atual OLDDIR=pwd(); // Pasta de salvamento dos arquivos DATADIR='C:\Users\Álvaro\Google Drive\0 mestrado mecatronica\2017.2\INTRODUÇÃO À IDENTIFICAÇÃO DE SISTEMAS\Trabalho_final'; if (~chdir(DATADIR)) then error('Folder does not exist'); end // Arquivo a ser lido FILE='dryer.dat'; // Leitura dos dados data = read(FILE, -1, 2); // 70% dos pontos serao utilizados para identificacao // Os 30% restantes serao utilizados para validacao total_points = size(data,"r"); num_points = 7*total_points/10; //50 ou 100 // Pontos de identificacao // Sinal de entrada u = data(1:num_points,1);//angulo // Sinal de saida y = data(1:num_points,2);//bola plot(u,'b'); plot(y,'r'); // Pontos de verificacao // Sinal de entrada u_verif = data(num_points+1:total_points,1); // Sinal de saida y_verif = data(num_points+1:total_points,2); // Maxima ordem a ser pesquisada max_order = 5; // Maximo tempo de atraso a ser pesquisado max_delay = 5; // Cria e inicializa com zeros as matrizes de // best_resuo e best_AIC para cada modelo ordem/delay // Poderia ser dispensado, mas agiliza best_res = zeros(max_order,max_delay+1); best_AIC = zeros(max_order,max_delay+1); // Identifica o sistema disp(FILE); disp('LINHAS: ordem de 1 a max_order'); disp('COLUNAS: delay de 0 a max_delay'); // Identificacao ARX disp('Modelo ARX:'); for (order=1:max_order) for (delay=0:max_delay) num_equacoes = num_points-order-delay; [theta,res]=identifyARX(u,y,order,delay); res_verif = resARX(u_verif,y_verif,theta,delay); best_res(order,delay+1) = stdev(res_verif)^2; best_AIC(order,delay+1) = 2*(2*order) + num_equacoes*log(best_res(order,delay+1)); end end disp('RESIDUOS:'); disp(best_res); [val,index]=min(best_res); disp('Melhor:'); disp(index); order = index(1,1); delay = index(1,2)-1; [theta,res]=identifyARX(u,y,order,delay); disp(theta); disp('Criterio de AKAIKE:'); disp(best_AIC); [val,index]=min(best_AIC); disp('Melhor:'); disp(index); order = index(1,1); delay = index(1,2)-1; [theta,res]=identifyARX(u,y,order,delay); disp(theta); // Identificacao ARMAX disp('Modelo ARMAX:'); for (order=1:max_order) for (delay=0:max_delay) num_equacoes = num_points-order-delay; [theta,res]=identifyARMAX(u,y,order,delay); res_verif = resARMAX(u_verif,y_verif,theta,delay); best_res(order,delay+1) = stdev(res_verif)^2; best_AIC(order,delay+1) = 2*(3*order) + num_equacoes*log(best_res(order,delay+1)); end end disp('RESIDUOS:'); disp(best_res); [val,index]=min(best_res); disp('Melhor:'); disp(index); order = index(1,1); delay = index(1,2)-1; [theta,res]=identifyARMAX(u,y,order,delay); disp(theta); disp('Criterio de AKAIKE:'); disp(best_AIC); [val,index]=min(best_AIC); disp('Melhor:'); disp(index); order = index(1,1); delay = index(1,2)-1; [theta,res]=identifyARMAX(u,y,order,delay); disp(theta); // Volta para a pasta anterior chdir(OLDDIR);
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x=2;y=3 if (x==2) then disp('x equals 2');else disp('x is not 2');end if (y==2) then disp('y equals 2'); else disp('y is not 2');end
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clc;funcprot(0);//EXAMPLE 15.1 // Initialisation of Variables BP=90;.................//Brake Power in kW deltw=27;.................//Raise in temperature of water etaP=0.25;...................//Efficiency of petrol engine etaD=0.3;....................//Efficiency od diesel engine Pec=32;......................//Percentage of energy going to coolant in petrol engine Dec=28;......................//Percentage of energy going to coolant in diesel engine cp=4.187;..........//specific heat of water at constant pressure //Calculations hsP = BP/etaP;............//Heat supplied in kW or kJ/s ecP=hsP*(Pec/100);.............//Energy going to cooling water in kg/s mwP=ecP/(cp*deltw);.............//Mass of cooling water required hsD = BP/etaD;............//Heat supplied in kW or kJ/s ecD=hsD*(Dec/100);.............//Energy going to cooling water in kg/s mwD=ecD/(cp*deltw);.............//Mass of cooling water required disp(mwP*3600,"The mass of cooling water required (kg/h)for petrol engine:") disp(mwD*3600,"The mass of cooling water required (kg/h)for diesel engine:")
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clf; clear; clc; load('C:\Users\tangu\OneDrive\Documents\GitHub\Modelisation\TD4\NetworkData.sod') // Extraction des temps de service index_bool = ( data(:, 3) == 2 ) tabS2 = data(index_bool, :) t_s2 = tabS2(1:$,4); deciles=perctl(t_s2,10:10:90); for i=2:10 ClassesDeciles(i)=deciles(i-1) end ClassesDeciles(1)=min(t_s2) ClassesDeciles(11)=max(t_s2) histplot(ClassesDeciles,t_s2,style=2) legend("Histogramme d isofréquence du serveur 2") // Définition des paramètres d'affichages a=gca(); a.x_location = "origin"; a.grid=[5,5];
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clc(); clear; // To calculate the net radiant interchange between two parallel black planes T1=1660/100; // Temperature of first black plane in degR T2=1260/100; // Temperature of second black plane in degR s=0.174; // Stephan Boltzman's constant q=s*(T1^4-T2^4); printf("The net radiant interchange between two bodies of unit area is %d Btu/hr-ft^2",q);
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clc; disp("Principles of Heat Transfer, 7th Ed. Frank Kreith et. al Chapter - 3 Example # 3.3 ") //initial temperature of the sheet in C is given as: Tinitial = 500; //thickness of the sheet in m is given as th = 0.02; //density in kg/m3 is given for steel as rho = 8500; //specific heat in J/kg-K is given as c = 460; //thermal conductivity in W/m-K is given as k = 20; //The heat transfer coefficient in W/m2-K to the air is given as h = 80; //the ambient air temperature in degree C is Tinfinity = 20; //Final temperature required to achieve in C is Tfinal = 250; //The transient cooling of stainless steel sheet can be modeled as a semi-infinite slab //because the thickness of the sheet is much smaller than its width and length. L = th/2; //Length in m //Finding chart solution //Biot number shall be Bi = (h*L)/k; //Since Bi<0.1 and hence the sheet can be treated as a lumped capacitance. //To use fig. 2.42 on page 135, we need to calculate the following value: value = (Tfinal-Tinfinity)/(Tinitial-Tinfinity); //value required //So, now using fig. 2.42, we have alpha*dt/(L*L)=19 //BY the definition of thermal diffusivity,in SI units we have alpha = k/(rho*c); disp("By chart solution, time required in seconds comes out to be") //time required in seconds t = ((19*L)*L)/alpha //Proceeding to the numerical solution //consider half the sheet thickness,with x=0 being the exposed left face and //x=L being the sheet center-line //Using 20 control volumes N = 21; //Total number of grid points dx = L/20; //dx in m //Old temperature array for N = 1:21 //Old temp in degree C Told(1,N) = Tinitial; //New temp in degree C Tnew(1,N) = Tinitial; end; //Initialisation Time in sec t = 0; //Increment of Time in sec dt = 0.02; //Condition of looping while Told(21)>250 //C1 of governing equation in SI units C1 = (alpha*dt)/(dx*dx); //C2 of governing equation in SI units C2 = ((2*h)*dt)/((rho*c)*dx); //C3 of governing equation in SI units C3 = 2*C1; //New temp in C as given by the equations of finite difference method Tnew = mtlb_i(Tnew,1,Told(1)+C2*(Tinfinity-Told(1))+C3*(Told(2)-Told(1))); Tnew = mtlb_i(Tnew,21,Told(21)+C3*(Told(20)-Told(21))); for N = 2:20 //New temp in C as given by the equations of finite difference method Tnew = mtlb_i(Tnew,N,Told(N)+C1*(Told(N+1)-2*Told(N)+Told(N-1))); end; for N = 1:21 //Assigning old temp=new temp Told = mtlb_i(Told,N,Tnew(N)); end; //Modified time for new loop t = t+dt; end; // L.67: No simple equivalent, so mtlb_fprintf() is called. mtlb_fprintf("As per numerical solution time comes out to be %5.2f seconds\n",t) disp("This time is about 1.5% less than the chart solution")
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clear; clc; close; A1=[-1 0;0 -2] //Jacobian at (0,0) t1=det(A1) tau1=trace(A1) d1=((tau1)^2) - 4*t1 A2=[2 0;0 -2] //Jacobian at (1,0) and (-1,0) t2=det(A2) disp("So from Chapter 5, we come to following conclusion :") disp("1. As t1>0 and tau1<.0 and d1>0 --> Thus (0,0) is Stable Node.") disp("2. As t2<0 --> Thus, only possibility is Saddle points.") function xd=linear611(t,x) xd(1)=-(x(1))+x(1)^3; //x(dot); x(2) means y. xd(2)=-2*x(2); //y(dot); x(1) means x.; endfunction bound=[-4,-4,4,4]; //Bounds of x-axis and y-axis as [xmin ymin xmax ymax], change them according to your needs. nrect=15; //increase it to get more number of curves, i.e. more information will be available. set(gca(),"auto_clear","off") //hold on x=linspace(bound(1),bound(3),nrect); y=linspace(bound(2),bound(4),nrect); x0=[]; for i=1:15 x0=[x(i);y(i)]; t0=0; t=0:0.01:3000; xout=ode(x0,t0,t,linear611); plot2d(xout(1,:),xout(2,:)); end xtitle('Phase Portrait','x-axis ( x )','y-axis ( y )')
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// Variable declaration n = 5 k = 1 // Calculation X = [1 0 ; 1 1 ; 1 2 ; 1 3 ; 1 4] Y = [8 ; 9 ; 4 ; 3 ; 1] XT = X' XTX = XT*X XTXI = [0.6 -0.2; -0.2 0.1] XTY = XT*Y b = XTXI*XTY Y1 = X*b MMT = ((Y-Y1)')*(Y-Y1) MMT = int(MMT) Se_square = (1.0/(n-k-1))*MMT Final = Se_square*XTXI // Result printf ( "var(bo): %.2f",Final(1,1)) printf ( "var(b1): %.2f",Final(2,2) )
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errcatch(-1,"stop");mode(2);// Exa 1.2 ; ; format('v',7) // Given data n_i = 1.4*10^18;// in /m^3 N_D = 1.4*10^24;// in /m^3 n = N_D;// in /m^3 p = (n_i^2)/n;// in /m^3 // Ratio of electron to hole concentation, ratio = n/p; disp(ratio,"Ratio of electron to hole concentration is"); exit();
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//4.15 clc; Vc=200; Im=60; toff=15*10^-6; C1=toff*Im/Vc; C=5*10^-6*10^6; printf("\nCapacitance = %.0f uF", C) Ipc=Im*1.5-Im; L=C/(Ipc/Vc)^2*10^6; printf("\nInductance = %.1f uH", L)
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clc clear //Initialization of variables tin=298 //K tout=273 //K tout2=308 //K tin2=294 //K //calculations eta1=(tin-tout)/tin eta2=abs((tin2-tout2)/tin2) //results printf("Efficiency in case 1 = %.3f",eta1) printf("\n efficiency in case 2 = %.3f",eta2)
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Ex3_6.sce
clc T=300 //K k=8.617*10^-5 //eV/K q=1.6*10**-19 //C NA=5*10^16 //cm^-3 ND=10^16 //cm^-3 A=2*10^-4//cm^2 V=4//V taug=5*10^-7 ni=9.65*10^9//cm^-3 epsilonx=8.854*10^-14 //F/cm W=sqrt((2*epsilonx*11.9/q)*[(NA+ND)/(NA*ND)]*[(k*T/q)*log(NA*ND/ni^2)+V]) //value of V is not substituted in textbook disp(W,"W in cm=") Jgen=(q*ni*W/taug) disp(Jgen,"Jgen in A/cm^2") //value of V is not substituted in textbook
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detectBRIEFDescriptors.sci
// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Ashish Manatosh Barik & Shubham Lohakare // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in // function [varargout] = detectBRIEFDescriptors(srcImg, varargin) // This function is used for computing BRIEF descriptors using Star keypoints. // // Calling Sequence // [ a ] = detectBRIEFDescriptors(srcImg) // [ a ] = detectVRIEFDescriptors(srcImg, maxSize, responseThreshold, lineThresholdProjected, lineThresholdBinarized, suppressNonmaxSize, bytes, use_orientation ) // // Parameters // srcImg : Hyper of input image // maxSize : Choose the number of filters to be applied, the parameter value set the maximum size. // responseThreshold : To eliminate weak corners. // lineThresholdProjected : Harris of responses. // lineThresholdBinarized : Harris of sizes. // suppressNonmaxSize : Window size (n-by-n) to apply the non-maximal suppression. // bytes : legth of the descriptor in bytes, valid values are: 16, 32 (default) or 64. // use_orientation : sample patterns using keypoints orientation, disabled by default. // a : It is a struct consisting of 'Type'(Type of Feature) , 'Features'(descriptors) , 'NumBits', 'NumFeatures', 'KeyPoints', 'keypointsCount'. // // Description // For extracting keypoints(StarDetector) and computing descriptors. BRIEF which gives the shortcut to find binary descriptors with less memory, faster matching, still higher recognition rate. // // Examples // // with default values // [ a ] = imread("/images/b1.jpeg"); // [ b ] = imread("/images/b2.jpeg"); // stacksize("max); // [ c ] = detectBRIEFDescriptors(a); // [ d ] = detectBRIEFDescriptors(b); // [ e f ] = matchFeatures(c.Features, d.Features); // out = drawMatch(a, b, c.KeyPoints, d.KeyPoints, e, f); // // Examples // // user assigned values // [ a ] = imread("/images/b1.jpeg"); // [ b ] = imread("/images/b2.jpeg"); // stacksize("max); // [ c ] = detectBRIEFDescriptors(a, 45, 30, 10, 8, 5, 32, %f); // [ d ] = detectBRIEFDEscriptors(b, 45, 30, 10, 8, 5, 32, %f); // [ e f ] = matchFeatures(c.Features, d.Features); // out = drawMatch(a, b, c.KeyPoints, d.KeyPoints, e, f); // // Authors // Ashish Manatosh Barik, NIT Rourkela // Shubham Lohakare, NITK Surathkal srcMat = mattolist(srcImg) [lhs, rhs] = argn(0) if rhs > 8 then error(msprintf("Too many input arguments")) end if lhs > 1 then error(msprintf("Too many output arguments")) end select rhs case 1 then [a b c d e] = raw_detectBRIEFDescriptors(srcMat) case 8 then [a b c d e] = raw_detectBRIEFDescriptors(srcMat, varargin(1), varargin(2), varargin(3), varargin(4), varargin(5), varargin(6), varargin(7)) end varargout(1) = struct('Type','Brief features','Features',a,'NumBits',b,'NumFeatures',c,'KeyPoints',d,'keypointsCount',e); endfunction
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// Exa 8.10 clc; clear; close; // Given data mC= 0.88;//mass of carbon in kg mH2= 0.03;//mass of H2 in kg mS= 0.005;//mass of S in kg O2_mass= 2.66*mC + 8*mH2 + 2*mS;// in kg Air_mass= O2_mass/0.23;// in kg Air_mass= 1.5*Air_mass;// in kg (as 50% excess air is supplied) disp(Air_mass,"Actula mass of air required per kg of fuel for complete combustion in kg is : ") // The flue gases per kg of fuel will be: CO2= 3.226;// in kg N2= 13.04;// in kg O2= 1.298;// in kg total_mass= CO2+N2+O2;// in kg CO2_per_by_mass= CO2/total_mass*100;// in % O2_per_by_mass= O2/total_mass*100;// in % N2_per_by_mass= N2/total_mass*100;// in % disp(CO2_per_by_mass,"Percentage of CO2 by mass is : ") disp(O2_per_by_mass,"Percentage of O2 by mass is : ") disp(N2_per_by_mass,"Percentage of N2 by mass is : ") M_wt_CO2= 44; CO2_Per_M_com_M_wt= CO2_per_by_mass/M_wt_CO2;// % Mass composition molecular weight M_wt_O2= 32; O2_Per_M_com_M_wt= O2_per_by_mass/M_wt_O2;// % Mass composition molecular weight M_wt_N2= 28; N2_Per_M_com_M_wt= N2_per_by_mass/M_wt_N2;// % Mass composition molecular weight total= CO2_Per_M_com_M_wt + O2_Per_M_com_M_wt + N2_Per_M_com_M_wt; CO2_per_by_vol= CO2_Per_M_com_M_wt/total*100;// in % O2_per_by_vol= O2_Per_M_com_M_wt/total*100;// in % N2_per_by_vol= N2_Per_M_com_M_wt/total*100;// in % disp(CO2_per_by_vol,"Percentage of CO2 by volume is : ") disp(O2_per_by_vol,"Percentage of O2 by volume is : ") disp(N2_per_by_vol,"Percentage of N2 by volume is : ")
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errcatch(-1,"stop");mode(2);//Chapter 20, Problem 6 ; Il=15; //line current Vl=415; //3 phase supply f=50; //supply frequency Ip=Il/sqrt(3); //phase current Xc=Vl/Ip; //capacitive reactance C=1/(2*%pi*f*Xc); //capacitance printf("Capacitance = %.3f uF",C*10^6); exit();
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CHOLESKY.sci
A = [2 1 -1;1 1 1;-1 1 6] function A=CHOLESKY(A) // [m,n]=size(A); if m~=n then, error('la matrice n''est pas carree'), end; zero=1.e-10; if norm(A-A','inf')>zero then, error('matrice non symetrique'), end; for j=1:n for k=1:j-1 A(j,j)=A(j,j)-A(j,k)*A(j,k); end; if A(j,j)< zero then, error('matrice non positive '), end; if abs(A(j,j))< zero then, error('matrice non définie'), end; A(j,j)=sqrt(A(j,j)); for i=j+1:n for k=1:j-1 A(i,j)=A(i,j)-A(j,k)*A(i,k); end; A(i,j)=A(i,j)/A(j,j); end; end; endfunction
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// Scilab Code Ex6.14 Diffusion depth of P-type semiconductor (B into Si): Page 212 (2010) C0 = 0; // Initial boron concentration of silicon Cx = 1e+17; // Boron concentration at depth x below the silicon surface Cs = 1e+18; // Boron concentration of silicon at the surface T = 1100+273; // Absolute temperature of the system, kelvin t = 2*60*60; // Time taken to diffuse boron into silicon, sec D_1100 = 4e-013; // Diffusion coefficient for boron in silicon, cm square per sec erf_Z = abs((Cs-Cx)/(Cs-C0)); // Error function of Z as a solution to Fick's second law Z1 = 1.1, Z2 = 1.2; // Preceding and succeeding values about Z from error function table erf_Z1 = 0.8802, erf_Z2 = 0.9103; // Preceding and succeeding values about erf_Z from error function table Z = poly(0,'Z'); Z = roots((Z-Z1)/(Z2-Z1)-(erf_Z-erf_Z1)/(erf_Z2-erf_Z1)); // As Z = x/(2*sqrt(D_927*t)), where Z is a constant argument of error function as erf(Z) // Solving for x, we have x = Z*2*sqrt(D_1100*t); // Diffusion depth of boron into silicon printf("\nThe diffusion depth of boron into silicon = %4.2e cm", x); // Result // The diffusion depth of boron into silicon = 1.25e-004 cm
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ok_printSuccess.tst
; Tests whether :print-success can be written and turns printing success off (get-option :print-success) ; value result (set-option :print-success false) ; no success result (get-option :print-success) ; value result (set-option :print-success true) ; success result (get-option :print-success) ; value result (set-option :print-success false) ; no success result (exit) ; no success result
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var a:int;void myProc(){ const test=5; test1=test==5;}
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clc // // // Variable declaration M0=1500 // Couple of magnitude(kN) yA=50 // Distance() zA=74 Iy=(3.25*((10**-6))) // Moment of inertia(m**4) Iz=(4.18*((10**-6))) // Moment of inertia(m**4) Iyz=(2.87*((10**-6))) // Moment of inertia(m**4) // Calculation // Principal axes Theta=(80.8)/2.0 // Angle R=sqrt((0.465**2)+(2.87**2)) // Radius R=2.91*((10**-6)) // Converting to meter Iu=3.72-2.91 // Moment of inertia(m**4) Iv=3.72+2.91 // Moment of inertia(m**4) //Loading Mu=(M0*sin(40.4)) // Applied couple(N.m) Mv=(M0*cos(40.4)) // Applied couple(N.m) //Case(a) Stress at A uA=50*cos(40.4*((2*%pi)/360.0))+74*sin(40.4*((2*%pi)/360.0)) // Perpendicular distances(mm) vA=-50*sin(40.4*((2*%pi)/360.0))+74*cos(40.4*((2*%pi)/360.0)) // Perpendicular distances(mm) sA=((972*0.0239)/(0.810*((10**-6))) - ((1142)*(0.0860))/(6.63*(10**-6)))/((10**6)) // Stress at A(MPa) //Case(b) Neutral Axis phy=81.8 // Angle neutral axis with the v axis(degree) B=81.8-40.4 // Angle neutral axis with the horizontal axis(degree) // Result printf("\n Stress at point A = %0.3f MPa' ,sA) printf("\n The angle formed by the neutral axis and the horizontal is = %0.3f degree' ,B)
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//Find the Amount of Heat needed to raise the temperature from 25 degree celsius to 35 degree celsius. //Example 27.1 clear; clc; Ao=0.32;//Mass of Oxygen kept in gram W=32;//Molecular weight of Oxygen in g/mol n=Ao/W;//Number of moles of oxygen Cv=20;//Molar Heat Capacity of Oxygen at constant volume T1=25;//Initial Temperature T2=35;//Final Temperature delT=T2-T1;//Change in Temperature Q=n*Cv*delT;//Amount of Heat needed printf("Amount of Heat required=%d joule",Q);
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plotCircle.sci
function plotCircle(netLocation, nodesPower, nodesFrequency, min_sensibility) [a,b]=size(nodesPower); plot(nodeLocation(1,:), nodeLocation(2,:),'ro'); for i=1:b //loss = 32.5 + 20*log10(d) + 20*log10(nodes_frequency(i)); loss = nodesPower(i)-min_sensibility; d=10^((loss-32.5-20*log10(nodesFrequency(i)))/20); x=nodeLocation(1,i)+d*cos(0:.1:2*%pi); y=nodeLocation(2,i)+d*sin(0:.1:2*%pi); plot2d(x,y,i); end endfunction
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SERVO_SB.tst
\name SERVO_WRITE_SB \palette Arduino \smalldescription Permet de piloter un servomoteur en renseignant l'angle de 0 à 180° souhaité \description Un servomoteur est un ensemble constitué d'un moteur électrique, d'un réducteur, d'un potentiomètre et d'une partie électronique analogique ou numérique pour la commande. C'est donc un asservissement de position (ou de vitesse pour les servomoteurs à rotation continue). L'utilisateur ne doit donc qu'envoyer la consigne de position ou de vitesse souhaitée. Cette consigne est transmise au servomoteur sous forme d'impulsions espacées de 10 à 20 ms. Le codage de ces impulsions est fait de telle façon qu'une impulsion de 1,5 ms correspond à la position centrée (de repos), une impulsion de 1 ms correspond à un angle de 90° dans le sens trigonométrique et enfin une impulsion de 2 ms correspond à un angle de 90° dans le sens horaire. Toutes les autres largeurs d'impulsion donneront des valeurs intermédiaires. Pour un servomoteur à rotation continue, la largeur des impulsions donne la vitesse de rotation ainsi que le sens. Il faut penser à utiliser un régulateur de tension plutôt que l'alimentation de la carte Arduino pour alimenter le servomoteur. Pour simplifier, le bloc ne demande en entrée que l'angle souhaité en degré de 0 à 180. Deux servomoteurs peuvent être pilotés avec la toolbox. On rappelle que l'échantillonnage est de 10 ms au minimum pour ce bloc. \dialogbox \image{SERVO_SB_dialogbox.png} Le bloc propose de choisir le numéro du servomoteur piloté. Le numéro de la carte ne peut pas être modifié pour l'instant. \example1 L'exemple ci-dessous montre l'utilisation du bloc servomoteur dont la position est donnée par un potentiomètre relié sur le port analogique 0. Un gain d'adaptation a été utilisé pour convertir les données numériques codées sur 10 bits en sortie du potentiomètre en une grandeur variant de 0 à 180 pour spécifier la position souhaitée du servomoteur. \image{SERVO_SB_exemple.png} \seealso DCMOTOR_SB
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statelevels15.sce
//i/p arg x is a matrix x=[1 2 3; 4 5 6; 8 6 7]; y=statelevels(x); disp(y); //output //!--error 10000 //Input x should be a vector //at line 31 of function statelevels called by : //y=statelevels(x);
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Example1_14_a.sce
//Example 1.14(a) clear; clc; R1=10*10^3; R2=20*10^3; RL=2*10^3;///Load Resistance vI=3;//Input Voltage IQ=0.5*10^(-3); vO=-(R2/R1)*vI;//Output Voltage iL=-vO/RL;//Current through RL i1=vI/R1;//Cuurent through R1 i2=i1;//Current through R2 (as current sunk by the op amp is 0) iO=i2+iL;//Output Current iCC=IQ; iEE=iCC+iO; printf("iCC=%.2f mA",(iCC*1000)); printf("\niEE=%.2f mA",(iEE*1000)); printf("\niO=%.2f mA",(iO*1000));
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clear; clc; // Illustration 11.8 // Page: 627 printf('Illustration 11.8 - Page: 627\n\n'); // Solution //******Data******// rate = 0.1;// [kg/s] conc = 3;// [kg vapour/100cubic m] Density_p = 720;// [kg/cubic m] Density_bed = 480;// [kg/cubic m] capablity = 0.45;// [kg vapour/kg carbon] dp = 0.0028;// [m] time = 3;// [h] //********************// Vap_adsorbed = time*3600*rate;// [kg] C_required = Vap_adsorbed/capablity; // Two beds will be needed: one adsorbing and another regenerated. totC_required = 2*C_required;// [kg] printf("Amount of caron required: %d kg\n",totC_required); Vol = (C_required/Density_bed); // Assume: Z = 0.5;// [m] Area = Vol/Z;// [square m] // From Eqn. 6.66: T = 35;// [OC] viscosity_air = 1.82*10^(-5);// [kg/m.s] Density_air = (29/22.41)*(273/(T+273)); e = 1-(Density_bed/Density_p); G = rate*(100/conc)*(Density_air/(Area));// [kg/square m.s] Re = dp*G/viscosity_air; Z = 0.5;// [m] deff('[y] = f78(delta_p)','y = ((delta_p/Z)*(e^3*dp*Density_air)/((1-e)*G^2))-(150*(1-e)/Re)-1.75'); delta_p = fsolve(7,f78); printf("The pressure drop is: %f N/square m\n",delta_p);
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midcross.sci
function [midcrossvalue, midreference, levels, t, tolerance, Tinput]= midcross(x, varargin) // This function estimate midcross values of real vector X. // Calling Sequence // midcrossvalue=midcross(x) // midcrossvalue=midcross(x, Fs) // midcrossvalue=midcross(x, t) // midcrossvalue=midcross(x, t, 'MidPercentReferenceLevels', N ) // midcrossvalue=midcross(x, t, 'Tolerance', M) // midcrossvalue=midcross(x, t,'StateLevels', O) // [midcrossvalue midreference]=midcross(x) // [midcrossvalue midreference]=midcross(x, Fs) // [midcrossvalue midreference]=midcross(x, t) // [midcrossvalue midreference]= midcross(x, t, 'MidPercentReferenceLevel', N ) // [midcrossvalue midreference]= midcross(x, t, 'Tolerance', M) // [midcrossvalue midreference]= midcross(x, t,'StateLevels', O) // [midcrossvalue midreference]= midcross(x, t,'StateLevels', O, 'fig', on or off) // // Parameters // x: real vector. // Fs: specifies the sample rate, Fs, as a positive scalar, where the first sample instant corresponds to a time of zero. // t: defiene instant sample time t as vector with same length of x, or specifies the sample rate, t, as a positive scalar // MidPercentReferenceLevels: specify the midpercentreferenceleves as a percentage, default value of N is 50. // Tolerance: define the tolerance value as real scaler value, where default value of M is 2.0. // StateLevels: define the lower and upper state levels as two element real vector. // fig: specify the logical input value to display figure as one of 'on' or 'off', where the default input in 'off'. // midcrossvalues: return the midcross values // midreference: return the midrefence values. // levels: return statelevels values. // t: return the instant sample time. // tolerance: retunr the tolerance value // Tinput: return t value, which given as input parameter. // Examples // x=[1.2, 5, 10, -20, 12] //t=1:length(x) // midcrossvalue=midcross(x, t) // See also // Authors // Jitendra Singh if or(type(x)==10) then error ('Input arguments must be double.') end if length(x) < 2 then // checking the length of input datasat error('X must be a vector with more than one element.'); // if length of X is less 2, it will give error end if length(varargin) >9 then // checking the length of input datasat error('Unexpected input/To many input'); // if length of X is less 2, it will give error end if length(varargin)==0 then t=1:length(x); Tinput=1:length(x); [levels hist]=statelevels(x); // run statelevels function before running this function midpercentval=50; tolerance=2; fig='off' end if length(varargin)>=1 & type(varargin(1))==1 then if length(varargin(1))==1 then t=(0:(length(x)-1))/varargin(1); Tinput=varargin(1); elseif length(varargin(1))==length(x) then t=varargin(1); Tinput=varargin(1); else error('T must be a same length as X.') end else t=1:length(x); end if length(varargin)>=2 & type(varargin(1))==1 & type(varargin(2))==1 then error ("Too many leading numeric arguments (at most 2 expected)."); end index=[]; if length(varargin)>=1 then a=1; for i=1:length(varargin) if type(varargin(i))==10 then index(a)=i; a=a+1; end end end if length(index)>5 then error('Unexpected argument.') end Nindex=[]; if length(varargin)>=1 then b=1; for i=1:length(varargin) if type(varargin(i))==1 then Nindex(b)=i; b=b+1; end end end d=[]; if length(Nindex)>=2 then c=1; for k=1:(length(Nindex)-1) d(c)=Nindex(k+1)-Nindex(k); c=c+1; end end if length(d)>=1 then f_one=find(d==1); if length(f_one)>0 then error('Unexpected input.') end end [levels hist]=statelevels(x); midpercentval=50; tolerance=2; fig='OFF'; if (~isempty(index)) then for j=1:length(index) select convstr(varargin(index(j)),'u') case {'STATELEVELS'} ////// if length(varargin) <=index(j) then error(strcat(['parameter StateLevels required a value'])); end if type(varargin(index(j)+1))==1 then levels=varargin(index(j)+1); elseif type(varargin(index(j)+1))==10 & convstr(varargin(index(j)+1), 'u')=='MIDPERCENTREFERENCELEVEL' | convstr(varargin(index(j)+1),'u')== 'TOLERANCE' | convstr(varargin(index(j)+1), 'u')=='FIG' then error('parameter StateLevels required a value.') elseif type(varargin(index(j)+1))==10 then error('Expected STATELEVELS to be one of these types: double, Instead its type was char.') end if length(levels)~=2 then error ('Expected STATELEVELS to be of size 1x2') end if levels(2)<=levels(1) then error('The state levels must be in increasing order.') end /////// case {'MIDPERCENTREFERENCELEVEL'} if length(varargin) <=index(j) then error(strcat(['parameter MidPercentRefernceLevel required a value.'])); end if type(varargin(index(j)+1))==1 then midpercentval= varargin(index(j)+1); elseif type(varargin(index(j)+1))==10 & convstr(varargin(index(j)+1), 'u')=='STATELEVELS' | convstr(varargin(index(j)+1),'u')== 'TOLERANCE' | convstr(varargin(index(j)+1), 'u')=='FIG' then error('parameter MidPercentRefernceLevel required a value.') elseif type(varargin(index(j)+1))==10 then error('Expected MidPercentRefernceLevel to be one of these types: double, Instead its type was char.') end if length( midpercentval)~=1 then error ('Expected MidPercentRefernceLevel to be of size 1x1') end case {'FIG'} if length(varargin) <=index(j) then error(strcat(['parameter fig required a value.'])); end if type(varargin(index(j)+1))==1 then error ('Expected fig to match one of these strings: on or off'); elseif type(varargin(index(j)+1))==10 & convstr(varargin(index(j)+1), 'u')=='STATELEVELS' | convstr(varargin(index(j)+1), 'u')== 'TOLERANCE' | convstr(varargin(index(j)+1), 'u')=='MIDPERCENTREFERENCELEVEL' then error('parameter fig required a value.') else fig= convstr(varargin(index(j)+1), 'u'); end if fig == 'OFF' | fig == 'ON' then else error('Expected fig to match one of these strings: on or off'); end case{'ON'} if length(varargin) == 1 then error ('Unexpected input.') elseif type(varargin(index(j)-1))==1 then error ('Unexpected input.'); elseif convstr(varargin(index(j)-1), 'u')~='FIG' then error('Unexpected input'); end case{'OFF'} if length(varargin) == 1 then error ('Unexpected input.') elseif type(varargin(index(j)-1))==1 then error ('Unexpected input.'); elseif convstr(varargin(index(j)-1), 'u')~='FIG' then error('Unexpected input'); end ////// case {'TOLERANCE'} if length(varargin) <=index(j) then error(strcat(['parameter Tolerance required a value"])); elseif type(varargin(index(j)+1))==1 then tolerance= varargin(index(j)+1); elseif type(varargin(index(j)+1))==10 & convstr(varargin(index(j)+1), 'u')== 'STATELEVELS' | convstr(varargin(index(j)+1), 'u')== 'MIDPERCENTREFERENCELEVEL' | convstr(varargin(index(j)+1), 'u')=='FIG' then error('parameter Tolerance required a value.'); elseif type(varargin(index(j)+1))==10 then error('Expected Tolerance to be one of these types: double, Instead its type was char.'); end if length(tolerance)~=1 then error ('Expected Tolerance to be of size 1x1'); end else error(strcat(['Invalid optional argument'," ", varargin(index(j))])); end // switch end // for end // if tolerance=tolerance; if tolerance>=50 then error('Expected Toleracne to be an array with all of the values < 50.') end if tolerance>= midpercentval then error ('The percent state level tolerance must be less than the mid/lower percent reference level.') end if tolerance+midpercentval>=100 then error('The sum of the percent state level Tolerance and the mid/upper percent reference level must be less than 100.') end midref=levels(1)+ (midpercentval/100)*(levels(2)-levels(1)); upperbound= levels(2)- (tolerance/100)*(levels(2)-levels(1)); mostupperbound=levels(2)+ (tolerance/100)*(levels(2)-levels(1)); lowerbound= levels(1)+ (tolerance/100)*(levels(2)-levels(1)); mostlowerbound=levels(1)- (tolerance/100)*(levels(2)-levels(1)); istate = find(x<lowerbound | x>upperbound); n=length(istate); istatepre = istate(1:(n-1)); istatepost = istate(2:n); itrans = find(x(istatepre) < lowerbound & upperbound < x(istatepost) | ... x(istatepre) > upperbound & lowerbound > x(istatepost) ); ipre = istatepre(itrans); ipost = istatepost(itrans); polarity = 2 * (x(ipre) < lowerbound) - 1; numtrans = length(itrans); iRMid = zeros(numtrans, 1); for i = 1:numtrans // define convenience indices for compactness ia = ipre(i); ib = ipost(i); if polarity(i) > 0 // checking for first positive crossing of midrefence iX = find((x(ia:ib-1) <= midref & midref < x(ia+1:ib))); iRMid(i) = iX(1) + ia - 1; else // checking for negative crossing for midrefenrce iX = find(x(ia:ib-1)>= midref & midref > x(ia+1:ib)); iRMid(i) = iX(1) + ia - 1; end end x=x(:); x=x'; t=t(:); t=t'; if numtrans > 0 // interpolation to get instant values midcrossvalue=t(iRMid)+(t(iRMid+1)-t(iRMid)).*(midref-x(iRMid))./( x(iRMid+1)-x(iRMid)); else midcrossvalue = []; end midreference=midref; if fig=='ON' then // if the defined output is only 1, the it will return the graphical representation of //levels ////// if length(midcrossvalue)==0 then plot(t,x, 'LineWidth',1, 'color', 'black' ) plot(t,midref * ones(1, length(t)),'-r', 'LineWidth',0.5) plot(t,mostupperbound * ones(1, length(t)),'--r', 'LineWidth',0.5) plot(t,levels(2) * ones(1, length(t)),'--k', 'LineWidth',0.5) plot(t,upperbound * ones(1, length(t)),'--r', 'LineWidth',0.5) plot(t,lowerbound *ones(1, length(t)),'--g', 'LineWidth',0.5) plot(t,levels(1) * ones(1, length(t)),'--k', 'LineWidth',0.5) plot(t,mostlowerbound * ones(1, length(t)),'--g', 'LineWidth',0.5) xlabel("Time (second)", "fontsize",3, "color", "black" ) ylabel("Level (Volts)", "fontsize",3, "color", "black" ) legends(["Signal"; "upper boundary"; "upper state"; "lower boundary"; "mid reference"; "upper boundary"; "lower state"; "lower boundary"], [[1;1], [5;2], [1;2], [5;2], [5;1], [3;2],[1;2], [3;2]], opt='?') else plot(t,x, 'LineWidth',1, 'color', 'black') plot(t,midref * ones(1, length(t)),'-r', 'LineWidth',0.5) plot(midcrossvalue, midreference*ones(midcrossvalue), "r*", 'MarkerSize',15); plot(t,mostupperbound * ones(1, length(t)),'--r', 'LineWidth',0.5) plot(t,levels(2) * ones(1, length(t)),'--k', 'LineWidth',0.5) plot(t,upperbound * ones(1, length(t)),'--r', 'LineWidth',0.5) plot(t,lowerbound *ones(1, length(t)),'--g', 'LineWidth',0.5) plot(t,levels(1) * ones(1, length(t)),'--k', 'LineWidth',0.5) plot(t,mostlowerbound * ones(1, length(t)),'--g', 'LineWidth',0.5) xlabel("Time (second)", "fontsize",3, "color", "black" ) ylabel("Level (Volts)", "fontsize",3, "color", "black" ) legends(["Signal"; "mid cross"; "upper boundary"; "upper state"; "lower boundary"; "mid reference"; "upper boundary"; "lower state"; "lower boundary"], [[1;1], [-10;5], [5;2], [1;2], [5;2], [5;1], [3;2],[1;2], [3;2]], opt='?') ////////////// end end endfunction
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// Calculating the continuous rating of motor clc; disp('Example 4.35, Page No. = 4.67') // Given Data Psh = 37.5;// Power rating of motor (in kW) th = 30;// Time (in minuts) Th = 90;// Heating time constant (in minuts) // Calculation of the continuous rating of motor ph = 1/(1-%e^(-th/Th));// Heating overload ratio K = 0.7^(2);// Maximum efficiency occurs at 70% full load pm = ((K+1)*ph-K)^(1/2);// Mechanical overload ratio Pnom = Psh/pm;// Continuous rating of motor (in kW) disp(Pnom,'Continuous rating of motor (kW)='); //in book answer is 17.2 kW. The answers vary due to round off error
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echo "### Test Ex14-1" ../bin/carat/KSubgroups -a -t -n Ex14_R 2 echo "### Ex14-1 return code $?" echo "### Test Ex14-2" ../bin/carat/KSupergroups -a -t -n Ex14_R 2 echo "### Ex14-2 return code $?" echo "### Test Ex14-3" ../bin/carat/TSubgroups -a -t Ex14_R echo "### Ex14-3 return code $?" # this one segfaults: # echo "### Test Ex14-4" # ../bin/carat/TSupergroups -t Ex14_R # echo "### Ex14-4 return code $?" # who creates this? rm -f ZZ.tmp
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sci
primpoly.sci
funcprot(0); // Find primitive polynomials for Galois field // pr = primpoly(m) computes one degree-M primitive polynomial for gf(2^m). // // pr = primpoly(m, option) computes primitive polynomial(s) for GF(2^m). // option = 'min' find one primitive polynomial of minimum weight. // option = 'max' find one primitive polynomial of maximum weight. // option = 'all' find all primitive polynomials. // option = L find all primitive polynomials of weight L. // // pr = primpoly(m, option, 'nodisplay') or pr = primpoly(m, 'nodisplay') disables printing of primitive polynomials // // The output vector is the decimal equivalent of the primitive polynomials. function pr = primpoly(m,fd,display) // Input checking if (argn(2)<1 | argn(2)>3) then error('Incorrect number of inputs. Number of inputs should be between 1 and 3') end // Check m if (isempty(m) | ~isreal(m) | m<1 | m>16 | (floor(m)~=m) | (size(m(:),1) * size(m(:),2)) ~= 1 ) then error('m must be a single real integer between 1 and 16'); end // Check fd and display // no specified fd or display if (argn(2) == 1) then fd = 'one'; display = ''; // 2 inputs specified elseif (argn(2)==2) then if (type(fd)==10) then fd = convstr(fd,"l"); if (~( strcmp(fd,'min') | strcmp(fd,'max') | strcmp(fd,'all') | strcmp(fd,'nodisplay') | strcmp(fd,'one') )) then error('Invalid Input String'); end if (fd == 'nodisplay') then display = 'nodisplay'; fd = 'one'; else display = ''; end elseif ( isempty(fd) | floor(fd)~=fd | ~isreal(fd) | prod(size(fd))~=1 | fd<2 | fd>m+1 ) then error('Invalid Input Option') else display = ''; end elseif (argn(2) > 2) then if (type(display)==10) then if (~(strcmp(display,'nodisplay'))) then error('Invalid Input String') end else error('Input must be in string format') end end // Load the poly values and assign if (m==1) then prims = poly1; elseif (m==2) then prims = poly2; elseif(m==3) then prims = poly3; elseif(m==4) then prims = poly4; elseif(m==5) then prims = poly5; elseif (m==6) then prims = poly6; elseif(m==7) then prims = poly7; elseif(m==8) then prims = poly8; elseif(m==9) then prims = poly9; elseif (m==10) then prims = poly10; elseif(m==11) then prims = poly11; elseif(m==12) then prims = poly12; elseif(m==13) then prims = poly13; elseif(m==14) then prims = poly14; elseif(m==15) then prims = poly15; else prims = poly16; end // Calculate weights of the polynomials polyweight =zeros(length(prims),1); for i = 1:length(prims) polyweight(i) = sum(strtod(strsplit(dec2bin(prims(i))))); end // Find specified primitive polynomials, 'one' is default case. if (fd == 'one') then // the defaults from gf.m p_vec = [3 7 11 19 37 67 137 285 529 1033 2053 4179 8219 17475 32771 69643]; pr = p_vec(m); elseif (fd =='all') then pr = prims'; elseif (fd =='min') then pr=min(prims); elseif (fd =='max') then pr=max(prims); elseif (or(type(fd)==[1 5 8])) then //Check weight L if ( ~isreal(fd) | fd<1 | floor(fd)~=fd | prod(size(fd))~=1) then error('L must be a real,positive scalar '); end // Find the primitive polynomials of weight L polydec=find(polyweight==fd); if (~isempty(polydec)) then pr=prims(polydec)'; else pr=[]; end end if (isempty(pr)) then warning(('No primitive polynomial satisfies the given constraints')); end; if (~isempty(pr) & ~(display=='nodisplay')) then disp(' ') disp('Primitive polynomial(s) = ') disp(' ') disp_primpoly(pr) end endfunction // Display the polynomials function disp_primpoly(pr) for (j = 1:length(pr)) pr_temp = pr(j); pr_temp = strtod(strsplit(dec2bin(pr_temp))); pr_temp = pr_temp'; pr_temp = pr_temp(:,$:-1:1); s=find(pr_temp); if (s(1)==1) then init_str='1'; else init_str='0'; end s(1)=[]; s=s-1; if (~isempty(s)) then s = s(:,$:-1:1); str1 = []; for k = 1:length(s) str1 = [str1, msprintf('D^%d+',s(k))]; end str1 = [str1 init_str]; if (str1($)=='0') then str1($-1:$)=[]; end disp(str1) end end endfunction
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example1_28.sce
// To prove,resistivity is 45 ohm-cm // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 1-28 in page 53 clear; clc; close; // Data given ni=2.5*10^13; // Intrinsic concentration /cm^3 mu=5600; // Sum of mobilities of holes and electrons e=1.6*10^-19; // Charge on an electron in C // Calculation sigma=e*ni*mu; printf("Conductivity of germanium is %0.3f (s/cm)^-1\n",sigma); rho=1/sigma; printf("Therefore resistivity is %0.1f ohm-cm",rho); // Result // Conductivity of germanium = 0.0232 (s/cm)^-1 // Resistivity = 44.6 ohm-cm
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Exercice3_tp1.sce
function [c]=matmat3b(a,b,n) c=zeros(n,n); for i=1:n for j=1:n for k=1:n c(i,j)=a(i,k)*b(k,j)+c(i,j); end end end endfunction function [c]=deux_boucle(a,b,n) c=zeros(n,n); for i=1:n for j=1:n c(i,j)=a(i,:)*b(:,j)+c(i,j); end end endfunction function [c]=une_boucle(a,b,n) c=zeros(n,n); for i=1:n c(i,:)=a(i,:)*b+c(i,:); end endfunction
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/Quick Flick.sce
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Quick Flick.sce
Name=Quick Flick PlayerCharacters=player_char BotCharacters=QFmain.bot;QFsub.bot IsChallenge=true Timelimit=60.0 PlayerProfile=player_char AddedBots=QFmain.bot;QFsub.bot;QFsub.bot PlayerMaxLives=1 BotMaxLives=0;0;0 PlayerTeam=1 BotTeams=2;2;2 MapName=quick_flick.map MapScale=10.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=0.0 ScorePerDamage=1.0 ScorePerKill=50.0 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=Quick Flick WeaponHeroTag=AR DifficultyTag=3 AuthorsTag=NFNT BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=false Description=Do not drop the center target. Flick the small target around. GameVersion=2.0.0.2 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 [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=QFmain DodgeProfileNames= DodgeProfileWeights= DodgeProfileMaxChangeTime=60.0 DodgeProfileMinChangeTime=60.0 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=QFmain_char SeeThroughWalls=false NoDodging=true NoAiming=false AbilityUseTimer=1.0 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.1 UseAbilityFreqMaxTime=0.1 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=QFsub DodgeProfileNames= DodgeProfileWeights= 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=QFsub_char SeeThroughWalls=false NoDodging=true NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.1 UseAbilityFreqMaxTime=0.1 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=player_char MaxHealth=100.0 WeaponProfileNames=AR;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=0.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.25 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=QFmain_char MaxHealth=100.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=160.0 Acceleration=2560.0 AirAcceleration=16000.0 Friction=1.0 BrakingFrictionFactor=0.5 JumpVelocity=0.0 Gravity=2.0 AirControl=0.0 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=0.000 Y=0.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=true BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cuboid MainBBHeight=300.0 MainBBRadius=59.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cuboid ProjBBHeight=300.0 ProjBBRadius=59.0 ProjBBHasHead=false ProjBBHeadRadius=10.0 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=QFmain_pop.abilmov;Player_kill.abilmelee;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=false 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=512.0 VerticalSpawnOffset=4000.0 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=QFsub_char MaxHealth=1.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=160.0 Acceleration=2560.0 AirAcceleration=16000.0 Friction=1.0 BrakingFrictionFactor=0.5 JumpVelocity=256.0 Gravity=0.0 AirControl=1.0 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=0.000 Y=0.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Spheroid MainBBHeight=50.0 MainBBRadius=25.0 MainBBHasHead=false MainBBHeadRadius=8.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=50.0 ProjBBRadius=25.0 ProjBBHasHead=false ProjBBHeadRadius=8.0 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=0.2 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=128.0 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=512.0 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 [Weapon Profile] Name=AR Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.25 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=0.1 ReloadTimeFromPartial=0.1 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=0.001 HitSoundCooldown=0.001 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 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=0.2 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=103.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false 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=0.1 IncReloadLoopTime=0.1 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.1 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=-50.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=false 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash= ParticleWallImpact= ParticleBodyImpact= ParticleProjectileTrail= ParticleHitscanTrace= ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=0.0,0.1,0.0,0.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=0.0,0.1,0.0,0.0 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=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=QFmain_pop MaxCharges=1.0 ChargeTimer=0.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.0 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=800.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=false UpVelocity=800.0 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=false AIUseOutOfCombat=false AIUseOnGround=false AIUseInAir=true AIReuseTimer=0.1 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=0.0 AIMaxTargFOV=360.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.1 AIDamageReactionMaxDelay=0.1 AIDamageReactionCooldown=0.1 AIDamageReactionThreshold=1.0 AIDamageReactionResetTimer=0.1 [Melee Ability Profile] Name=Player_kill MaxCharges=1.0 ChargeTimer=0.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.1 HurtboxRadius=4000.0 HurtboxDamage=100.0 HurtboxGroundKnockbackFactor=0.0 HurtboxAirKnockbackFactor=0.0 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//Section-14,Example-2,Page no.-PC.54 //To calculate force necessary to lift a ring of 1.0 cm radius from liquid water. clc; y=72.8 r=1 F=2*(2*%pi*r)*y disp(F,'Force necessary to lift a ring of radius r from a liquid of surface tension y)
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function [r]=%c_o_l(l1,l2) //%c_o_l(l1,l2) : l1==l2 //! // Copyright INRIA r=%f
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//example 3.22 //calculate //discharge required at head of distributory clc; //given GCA=10000; //gross commanded area CCA=0.75*GCA; //Culturable commanded area IR=0.6; //intensity of irrigation during rabi season IK=0.3; //intensity of irrigation during kharif season DuR=2500; //duty during rabi season DuK=1000; //duty during kharif season AR=IR*CCA; //area under irrigation in rabi season AK=IK*CCA; //area under irrigation in kharif season DR=AR/DuR; DK=AK/DuK; mprintf("discharge required at head of distributory=%f cumecs.",DK);
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//less than 2 i/p args are passed to the function b=[0.1 2 3 4 0.12]; y=fftfilt(b); disp(y); //output //!--error 4 //Undefined variable: nfft //at line 128 of function fftfilt called by : //y=fftfilt(b);
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java -ea trip.Main -m trip-tests/explore02 <<EOF Fort_Lee, East_Harlem, Troy, Fishkill EOF
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clear; //clc(); // Example 10.2 // Page: 262 printf("Example-8.2 Page no.-262\n\n"); //***Data***// // The initial data for this example is same as that of example 10.2, i.e. P = 800;//[psia] Bubble point pressure x_e = 0.60;// Mole fraction of ethane in liquid phase x_h = (1-x_e);// Mole fraction of n-heptane in the liquid phase R = 0.08314;//( L*bar/(mol*K)) Universal gas constant // Changing the pressure in bar Pb = (800/14.7)*(1.01325);//[bar] // In this problem we will denote ethane by 'e' and that to n-heptane by 'h' // From table A.1 ( page 417 ) given in the book, critical temperatures of ethane and heptane are T_c_e = 305.3;//[K] T_c_h = 540.2;//[K] // and critical pressures are P_c_e = 48.72;//[bar] P_c_h = 27.40;//[bar] // also the accentric facors are w_e = 0.1; w_h = 0.35; // Thus we have P_r_e = Pb/P_c_e; P_r_h = Pb/P_c_h; // Now from equations (F.13) and (F.14) ( page 459 ) given in the book we have // A_e = 0.42747 + ( 1 + (0.480 + 1.574*w_e - 0.17*w_e^(2))*( 1 - T_r_e^(0.5)))^(2)*(P_r_e/T_r_e^(2)); // A_h = 0.42747 + ( 1 + (0.480 + 1.574*w_h - 0.17*w_h^(2))*( 1 - T_r_h^(0.5)))^(2)*(P_r_h/T_r_h^(2)); // and // B_e = 0.08664*(P_r_e/T_r_e); // B_h = 0.08664*(P_r_h/T_r_h); // We will take the help trial and error method both on Temperature and the vapor phase composition of ethane // Let us assume the starting temperature 200 deg F. Changing this temperature in K T = (200-32)*5/9 + 273.15;//[K] err = 1; while err > 10^(-4) T_r_e = T/T_c_e; T_r_h = T/T_c_h; A_e = 0.42747*( 1 + (0.480 + 1.574*w_e - 0.17*w_e^(2))*( 1 - T_r_e^(0.5)))^(2)*(P_r_e/T_r_e^(2)); A_h = 0.42747*( 1 + (0.480 + 1.574*w_h - 0.17*w_h^(2))*( 1 - T_r_h^(0.5)))^(2)*(P_r_h/T_r_h^(2)); B_e = 0.08664*(P_r_e/T_r_e); B_h = 0.08664*(P_r_h/T_r_h); // Now we will take the starting value of vapor phase composition of ethane as y_e = 0.9; err1 = 1; while err1 > 10^(-6) // Now value of A_mix and B_mix for both liquid and vapor phase are calculated as A_mix_l = (x_e*sqrt(A_e) + x_h*sqrt(A_h))^(2);// For liquid phase A_mix_v = (y_e*sqrt(A_e) + (1 - y_e)*sqrt(A_h))^(2);// For vapor phase B_mix_l = (x_e*B_e + x_h*B_h);// For liquid B_mix_v = (y_e*B_e + (1 - y_e)*B_h);// For liquid deff('[y]=f(z1)','y = z1^(3) - z1^(2) + z1*(A_mix_l - B_mix_l - B_mix_l^(2)) - A_mix_l*B_mix_l'); z_l = fsolve(0.2,f); // and deff('[y]=g(z2)','y = z2^(3) - z2^(2) + z2*(A_mix_v - B_mix_v - B_mix_v^(2)) - A_mix_v*B_mix_v'); z_v = fsolve(0.3,g); // Now phi_el = B_e/B_mix_l*( z_l - 1) - log(z_l - B_mix_l) - (A_mix_l/B_mix_l)*(2*sqrt(A_e/A_mix_l)-B_e/B_mix_l)*log(1-B_mix_l/z_l); phi_hl = B_h/B_mix_l*( z_l - 1) - log(z_l - B_mix_l) - (A_mix_l/B_mix_l)*(2*sqrt(A_h/A_mix_l)-B_h/B_mix_l)*log(1-B_mix_l/z_l); phi_ev = B_e/B_mix_v*( z_v - 1) - log(z_v - B_mix_v) - (A_mix_v/B_mix_v)*(2*sqrt(A_e/A_mix_v)-B_e/B_mix_v)*log(1-B_mix_v/z_v); phi_hv = B_h/B_mix_v*( z_v - 1) - log(z_v - B_mix_v) - (A_mix_v/B_mix_v)*(2*sqrt(A_h/A_mix_v)-B_h/B_mix_v)*log(1-B_mix_v/z_v); K_e = phi_el/phi_ev; K_h = phi_hl/phi_hv; y_e1 = K_e*x_e; y_h1 = K_h*x_h; err1 =abs((y_e1 - y_e)); y_e = y_e1; end err = abs((y_e1 + y_h1) -1); T = T + 0.1; end // Changing the temperature in deg F, we have Tf = ( T - 273.15)*9/5 + 32;//[F] printf(" Bubble point of the given ethanol and n-heptane mixture at 800 psia is %f deg F\n",Tf); printf(" Amount of ethanol in the vapour phase of the mixture at the given condition is %f \n",y_e1); printf(" Amount of n-heptane in the vapour phase of the mixture at the given condition is %f ",y_h1);
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Oscillators_Ex_7_9.sce
clc //Chapter 7:Conditions for Oscillation //example 7.9 page no 284 //given rd=50*10^3 gm=5*10^-3//transconductance f=16*10^6//frequency of oscillation Rs=15 XC1=1*10^3//capacitive reactance of first capacitor XC2=Rs/(gm*XC1)//capacitive reactance of second capacitor C1=(2*%pi*f*XC1)^-1//value of first capacitor C2=(2*%pi*f*XC2)^-1//value of second capacitor mprintf('the value of first capacitor is %3.2e pF\n the value of second capacitor is %3.2e pF\n ',C1,C2) disp('This value of C1 may be so small that the transistor output capacitance has a effect. therefore it is desirable to incease C1.If C1 is increased by a factor of 10,so that XC1=100,then C2 must also be increased ') XC_2=Rs/(gm*100)//new value of reactance XL=100+XC_2//inductive reactance L=XL/(2*%pi*f)//value of inductor mprintf('the value of inductor is %3.2e H',L)
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clear; clc; disp('Example 5.1'); // aim : To determine // new pressure exerted on the air and the difference in two mercury column level // Given values P1 = 765;// atmospheric pressure, [mmHg] V1 = 20000;// [mm^3] V2 = 17000;// [mm^3] // solution // using boyle's law P*V=constant // hence P2 = P1*V1/V2;// [mmHg] mprintf('\n The new pressure exerted on the air is = %f mmHg \n',P2); del_h = P2-P1;// difference in Height of mercury column level mprintf('\n The difference in the two mercury column level is = %f mm\n',del_h); // End
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//SCI2C: DEFAULT_PRECISION= FLOAT function mattranspose() a = int8([1,-2,3;4,5,6;-7,8,9]); b = int16([10,-11,19;1,2,-3;0,-10,18]); c = uint8([21,1,0;3,56,90;1,2,3]); d = uint16([1,2,4;10,15,20;90,12,100]); e = a'; f = b'; g = c'; h = d'; disp(e); disp(f); disp(g); disp(h); endfunction
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Ch08Ex09.sce
// Scilab code Ex8.9: Pg.350 (2008) clc; clear; // For simplicity let h & f be unity // At low temperatures h = 1; // Plank's constant, J-s f = 1; // Frequency, Hz kT = 0.5*h*f; // Product of Boltzman's constant & temperature, J n = 1; // Integer value f_1_0 = exp(-(h*f)/kT); // Ratio of fraction of oscillators in first excited state to that in ground state printf("\nThe ratio of fraction of oscillators in first excited state to that in ground state = %5.3f", f_1_0); // At high temeratures kT = 4*h*f; f_1_0 = exp(-(h*f)/kT); // Ratio of fraction of oscillators in first excited state to that in ground state printf("\nThe ratio of fraction of oscillators in first excited state to that in ground state = %5.3f", f_1_0); // Result // The ratio of fraction of oscillators in first excited state to that in ground state = 0.135 // The ratio of fraction of oscillators in first excited state to that in ground state = 0.779
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# start Schwering-Kuehne.X07 3*p^3*r + 3*p^2*q*r + 3*p*q^2*r - 9*r^4 # start Schwering-Kuehne.X07 - 3*p^2*q*r - 3*p*q^2*r - 3*q^3*r + 9*r^4 # start Schwering-Kuehne.X07 p^4 + 2*p^3*q + 3*p^2*q^2 + 2*p*q^3 + q^4 - 9*p*r^3 # start Schwering-Kuehne.X07 - p^4 - 2*p^3*q - 3*p^2*q^2 - 2*p*q^3 - q^4 + 9*q*r^3 Schwering-Kuehne.X07 [0,0,0] 0 3*P^3*R + 3*P^2*Q*R + 3*P*Q^2*R - 9*R^4 Schwering-Kuehne.X07 [0,0,0] 1 - 3*P^2*Q*R - 3*P*Q^2*R - 3*Q^3*R + 9*R^4 Schwering-Kuehne.X07 [0,0,0] 2 P^4 + 2*P^3*Q + 3*P^2*Q^2 + 2*P*Q^3 + Q^4 - 9*P*R^3 Schwering-Kuehne.X07 [0,0,0] 3 - P^4 - 2*P^3*Q - 3*P^2*Q^2 - 2*P*Q^3 - Q^4 + 9*Q*R^3 Schwering-Kuehne.X07 [1,0,0] 0 3*R + 9*P*R + 9*P^2*R + 3*P^3*R + 3*Q*R + 6*P*Q*R + 3*P^2*Q*R + 3*Q^2*R + 3*P*Q^2*R - 9*R^4 Schwering-Kuehne.X07 [1,0,0] 1 - 3*Q*R - 6*P*Q*R - 3*P^2*Q*R - 3*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 9*R^4 Schwering-Kuehne.X07 [1,0,0] 2 4*P + 6*P^2 + 4*P^3 + P^4 + 2*Q + 6*P*Q + 6*P^2*Q + 2*P^3*Q + 3*Q^2 + 6*P*Q^2 + 3*P^2*Q^2 + 2*Q^3 + 2*P*Q^3 + Q^4 - 9*R^3 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [1,0,0] 3 - 4*P - 6*P^2 - 4*P^3 - P^4 - 2*Q - 6*P*Q - 6*P^2*Q - 2*P^3*Q - 3*Q^2 - 6*P*Q^2 - 3*P^2*Q^2 - 2*Q^3 - 2*P*Q^3 - Q^4 + 9*Q*R^3 - 1 Schwering-Kuehne.X07 [-1,0,0] 0 - 3*R + 9*P*R - 9*P^2*R + 3*P^3*R + 3*Q*R - 6*P*Q*R + 3*P^2*Q*R - 3*Q^2*R + 3*P*Q^2*R - 9*R^4 Schwering-Kuehne.X07 [-1,0,0] 1 - 3*Q*R + 6*P*Q*R - 3*P^2*Q*R + 3*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 9*R^4 Schwering-Kuehne.X07 [-1,0,0] 2 - 4*P + 6*P^2 - 4*P^3 + P^4 - 2*Q + 6*P*Q - 6*P^2*Q + 2*P^3*Q + 3*Q^2 - 6*P*Q^2 + 3*P^2*Q^2 - 2*Q^3 + 2*P*Q^3 + Q^4 + 9*R^3 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [-1,0,0] 3 4*P - 6*P^2 + 4*P^3 - P^4 + 2*Q - 6*P*Q + 6*P^2*Q - 2*P^3*Q - 3*Q^2 + 6*P*Q^2 - 3*P^2*Q^2 + 2*Q^3 - 2*P*Q^3 - Q^4 + 9*Q*R^3 - 1 Schwering-Kuehne.X07 [0,1,0] 0 3*P*R + 3*P^2*R + 3*P^3*R + 6*P*Q*R + 3*P^2*Q*R + 3*P*Q^2*R - 9*R^4 Schwering-Kuehne.X07 [0,1,0] 1 - 3*R - 3*P*R - 3*P^2*R - 9*Q*R - 6*P*Q*R - 3*P^2*Q*R - 9*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 9*R^4 Schwering-Kuehne.X07 [0,1,0] 2 2*P + 3*P^2 + 2*P^3 + P^4 + 4*Q + 6*P*Q + 6*P^2*Q + 2*P^3*Q + 6*Q^2 + 6*P*Q^2 + 3*P^2*Q^2 + 4*Q^3 + 2*P*Q^3 + Q^4 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [0,1,0] 3 - 2*P - 3*P^2 - 2*P^3 - P^4 - 4*Q - 6*P*Q - 6*P^2*Q - 2*P^3*Q - 6*Q^2 - 6*P*Q^2 - 3*P^2*Q^2 - 4*Q^3 - 2*P*Q^3 - Q^4 + 9*R^3 + 9*Q*R^3 - 1 Schwering-Kuehne.X07 [0,-1,0] 0 3*P*R - 3*P^2*R + 3*P^3*R - 6*P*Q*R + 3*P^2*Q*R + 3*P*Q^2*R - 9*R^4 Schwering-Kuehne.X07 [0,-1,0] 1 3*R - 3*P*R + 3*P^2*R - 9*Q*R + 6*P*Q*R - 3*P^2*Q*R + 9*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 9*R^4 Schwering-Kuehne.X07 [0,-1,0] 2 - 2*P + 3*P^2 - 2*P^3 + P^4 - 4*Q + 6*P*Q - 6*P^2*Q + 2*P^3*Q + 6*Q^2 - 6*P*Q^2 + 3*P^2*Q^2 - 4*Q^3 + 2*P*Q^3 + Q^4 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [0,-1,0] 3 2*P - 3*P^2 + 2*P^3 - P^4 + 4*Q - 6*P*Q + 6*P^2*Q - 2*P^3*Q - 6*Q^2 + 6*P*Q^2 - 3*P^2*Q^2 + 4*Q^3 - 2*P*Q^3 - Q^4 - 9*R^3 + 9*Q*R^3 - 1 Schwering-Kuehne.X07 [1,1,0] 0 9*R + 18*P*R + 12*P^2*R + 3*P^3*R + 9*Q*R + 12*P*Q*R + 3*P^2*Q*R + 3*Q^2*R + 3*P*Q^2*R - 9*R^4 Schwering-Kuehne.X07 [1,1,0] 1 - 9*R - 9*P*R - 3*P^2*R - 18*Q*R - 12*P*Q*R - 3*P^2*Q*R - 12*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 9*R^4 Schwering-Kuehne.X07 [1,1,0] 2 18*P + 15*P^2 + 6*P^3 + P^4 + 18*Q + 24*P*Q + 12*P^2*Q + 2*P^3*Q + 15*Q^2 + 12*P*Q^2 + 3*P^2*Q^2 + 6*Q^3 + 2*P*Q^3 + Q^4 - 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11*P + 3*P^2 - 2*P^3 + P^4 - 4*Q + 6*P*Q - 6*P^2*Q + 2*P^3*Q + 6*Q^2 - 6*P*Q^2 + 3*P^2*Q^2 - 4*Q^3 + 2*P*Q^3 + Q^4 - 27*P*R - 27*P*R^2 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [0,-1,1] 3 2*P - 3*P^2 + 2*P^3 - P^4 + 13*Q - 6*P*Q + 6*P^2*Q - 2*P^3*Q - 6*Q^2 + 6*P*Q^2 - 3*P^2*Q^2 + 4*Q^3 - 2*P*Q^3 - Q^4 - 27*R + 27*Q*R - 27*R^2 + 27*Q*R^2 - 9*R^3 + 9*Q*R^3 - 10 Schwering-Kuehne.X07 [0,1,-1] 0 - 3*P - 3*P^2 - 3*P^3 - 6*P*Q - 3*P^2*Q - 3*P*Q^2 + 36*R + 3*P*R + 3*P^2*R + 3*P^3*R + 6*P*Q*R + 3*P^2*Q*R + 3*P*Q^2*R - 54*R^2 + 36*R^3 - 9*R^4 - 9 Schwering-Kuehne.X07 [0,1,-1] 1 3*P + 3*P^2 + 9*Q + 6*P*Q + 3*P^2*Q + 9*Q^2 + 3*P*Q^2 + 3*Q^3 - 39*R - 3*P*R - 3*P^2*R - 9*Q*R - 6*P*Q*R - 3*P^2*Q*R - 9*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 - 36*R^3 + 9*R^4 + 12 Schwering-Kuehne.X07 [0,1,-1] 2 11*P + 3*P^2 + 2*P^3 + P^4 + 4*Q + 6*P*Q + 6*P^2*Q + 2*P^3*Q + 6*Q^2 + 6*P*Q^2 + 3*P^2*Q^2 + 4*Q^3 + 2*P*Q^3 + Q^4 - 27*P*R + 27*P*R^2 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [0,1,-1] 3 - 2*P - 3*P^2 - 2*P^3 - P^4 - 13*Q - 6*P*Q - 6*P^2*Q - 2*P^3*Q - 6*Q^2 - 6*P*Q^2 - 3*P^2*Q^2 - 4*Q^3 - 2*P*Q^3 - Q^4 + 27*R + 27*Q*R - 27*R^2 - 27*Q*R^2 + 9*R^3 + 9*Q*R^3 - 10 Schwering-Kuehne.X07 [0,-1,-1] 0 - 3*P + 3*P^2 - 3*P^3 + 6*P*Q - 3*P^2*Q - 3*P*Q^2 + 36*R + 3*P*R - 3*P^2*R + 3*P^3*R - 6*P*Q*R + 3*P^2*Q*R + 3*P*Q^2*R - 54*R^2 + 36*R^3 - 9*R^4 - 9 Schwering-Kuehne.X07 [0,-1,-1] 1 3*P - 3*P^2 + 9*Q - 6*P*Q + 3*P^2*Q - 9*Q^2 + 3*P*Q^2 + 3*Q^3 - 33*R - 3*P*R + 3*P^2*R - 9*Q*R + 6*P*Q*R - 3*P^2*Q*R + 9*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 - 36*R^3 + 9*R^4 + 6 Schwering-Kuehne.X07 [0,-1,-1] 2 7*P + 3*P^2 - 2*P^3 + P^4 - 4*Q + 6*P*Q - 6*P^2*Q + 2*P^3*Q + 6*Q^2 - 6*P*Q^2 + 3*P^2*Q^2 - 4*Q^3 + 2*P*Q^3 + Q^4 - 27*P*R + 27*P*R^2 - 9*P*R^3 + 1 Schwering-Kuehne.X07 [0,-1,-1] 3 2*P - 3*P^2 + 2*P^3 - P^4 - 5*Q - 6*P*Q + 6*P^2*Q - 2*P^3*Q - 6*Q^2 + 6*P*Q^2 - 3*P^2*Q^2 + 4*Q^3 - 2*P*Q^3 - Q^4 - 27*R + 27*Q*R + 27*R^2 - 27*Q*R^2 - 9*R^3 + 9*Q*R^3 + 8 Schwering-Kuehne.X07 [1,1,1] 0 18*P + 12*P^2 + 3*P^3 + 9*Q + 12*P*Q + 3*P^2*Q + 3*Q^2 + 3*P*Q^2 - 27*R + 18*P*R + 12*P^2*R + 3*P^3*R + 9*Q*R + 12*P*Q*R + 3*P^2*Q*R + 3*Q^2*R + 3*P*Q^2*R - 54*R^2 - 36*R^3 - 9*R^4 Schwering-Kuehne.X07 [1,1,1] 1 - 9*P - 3*P^2 - 18*Q - 12*P*Q - 3*P^2*Q - 12*Q^2 - 3*P*Q^2 - 3*Q^3 + 27*R - 9*P*R - 3*P^2*R - 18*Q*R - 12*P*Q*R - 3*P^2*Q*R - 12*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 + 36*R^3 + 9*R^4 Schwering-Kuehne.X07 [1,1,1] 2 9*P + 15*P^2 + 6*P^3 + P^4 + 18*Q + 24*P*Q + 12*P^2*Q + 2*P^3*Q + 15*Q^2 + 12*P*Q^2 + 3*P^2*Q^2 + 6*Q^3 + 2*P*Q^3 + Q^4 - 27*R - 27*P*R - 27*R^2 - 27*P*R^2 - 9*R^3 - 9*P*R^3 Schwering-Kuehne.X07 [1,1,1] 3 - 18*P - 15*P^2 - 6*P^3 - P^4 - 9*Q - 24*P*Q - 12*P^2*Q - 2*P^3*Q - 15*Q^2 - 12*P*Q^2 - 3*P^2*Q^2 - 6*Q^3 - 2*P*Q^3 - Q^4 + 27*R + 27*Q*R + 27*R^2 + 27*Q*R^2 + 9*R^3 + 9*Q*R^3 Schwering-Kuehne.X07 [-1,1,1] 0 6*P - 6*P^2 + 3*P^3 - 3*Q + 3*P^2*Q - 3*Q^2 + 3*P*Q^2 - 39*R + 6*P*R - 6*P^2*R + 3*P^3*R - 3*Q*R + 3*P^2*Q*R - 3*Q^2*R + 3*P*Q^2*R - 54*R^2 - 36*R^3 - 9*R^4 - 12 Schwering-Kuehne.X07 [-1,1,1] 1 3*P - 3*P^2 - 6*Q - 3*P^2*Q - 6*Q^2 - 3*P*Q^2 - 3*Q^3 + 33*R + 3*P*R - 3*P^2*R - 6*Q*R - 3*P^2*Q*R - 6*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 + 36*R^3 + 9*R^4 + 6 Schwering-Kuehne.X07 [-1,1,1] 2 - 11*P + 3*P^2 - 2*P^3 + P^4 + 2*Q + 2*P^3*Q + 3*Q^2 + 3*P^2*Q^2 + 2*Q^3 + 2*P*Q^3 + Q^4 + 27*R - 27*P*R + 27*R^2 - 27*P*R^2 + 9*R^3 - 9*P*R^3 + 10 Schwering-Kuehne.X07 [-1,1,1] 3 2*P - 3*P^2 + 2*P^3 - P^4 + 7*Q - 2*P^3*Q - 3*Q^2 - 3*P^2*Q^2 - 2*Q^3 - 2*P*Q^3 - Q^4 + 27*R + 27*Q*R + 27*R^2 + 27*Q*R^2 + 9*R^3 + 9*Q*R^3 + 8 Schwering-Kuehne.X07 [1,-1,1] 0 6*P + 6*P^2 + 3*P^3 - 3*Q + 3*P^2*Q + 3*Q^2 + 3*P*Q^2 - 33*R + 6*P*R + 6*P^2*R + 3*P^3*R - 3*Q*R + 3*P^2*Q*R + 3*Q^2*R + 3*P*Q^2*R - 54*R^2 - 36*R^3 - 9*R^4 - 6 Schwering-Kuehne.X07 [1,-1,1] 1 3*P + 3*P^2 - 6*Q - 3*P^2*Q + 6*Q^2 - 3*P*Q^2 - 3*Q^3 + 39*R + 3*P*R + 3*P^2*R - 6*Q*R - 3*P^2*Q*R + 6*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 + 36*R^3 + 9*R^4 + 12 Schwering-Kuehne.X07 [1,-1,1] 2 - 7*P + 3*P^2 + 2*P^3 + P^4 - 2*Q + 2*P^3*Q + 3*Q^2 + 3*P^2*Q^2 - 2*Q^3 + 2*P*Q^3 + Q^4 - 27*R - 27*P*R - 27*R^2 - 27*P*R^2 - 9*R^3 - 9*P*R^3 - 8 Schwering-Kuehne.X07 [1,-1,1] 3 - 2*P - 3*P^2 - 2*P^3 - P^4 + 11*Q - 2*P^3*Q - 3*Q^2 - 3*P^2*Q^2 + 2*Q^3 - 2*P*Q^3 - Q^4 - 27*R + 27*Q*R - 27*R^2 + 27*Q*R^2 - 9*R^3 + 9*Q*R^3 - 10 Schwering-Kuehne.X07 [-1,-1,1] 0 18*P - 12*P^2 + 3*P^3 + 9*Q - 12*P*Q + 3*P^2*Q - 3*Q^2 + 3*P*Q^2 - 45*R + 18*P*R - 12*P^2*R + 3*P^3*R + 9*Q*R - 12*P*Q*R + 3*P^2*Q*R - 3*Q^2*R + 3*P*Q^2*R - 54*R^2 - 36*R^3 - 9*R^4 - 18 Schwering-Kuehne.X07 [-1,-1,1] 1 - 9*P + 3*P^2 - 18*Q + 12*P*Q - 3*P^2*Q + 12*Q^2 - 3*P*Q^2 - 3*Q^3 + 45*R - 9*P*R + 3*P^2*R - 18*Q*R + 12*P*Q*R - 3*P^2*Q*R + 12*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 + 36*R^3 + 9*R^4 + 18 Schwering-Kuehne.X07 [-1,-1,1] 2 - 27*P + 15*P^2 - 6*P^3 + P^4 - 18*Q + 24*P*Q - 12*P^2*Q + 2*P^3*Q + 15*Q^2 - 12*P*Q^2 + 3*P^2*Q^2 - 6*Q^3 + 2*P*Q^3 + Q^4 + 27*R - 27*P*R + 27*R^2 - 27*P*R^2 + 9*R^3 - 9*P*R^3 + 18 Schwering-Kuehne.X07 [-1,-1,1] 3 18*P - 15*P^2 + 6*P^3 - P^4 + 27*Q - 24*P*Q + 12*P^2*Q - 2*P^3*Q - 15*Q^2 + 12*P*Q^2 - 3*P^2*Q^2 + 6*Q^3 - 2*P*Q^3 - Q^4 - 27*R + 27*Q*R - 27*R^2 + 27*Q*R^2 - 9*R^3 + 9*Q*R^3 - 18 Schwering-Kuehne.X07 [1,1,-1] 0 - 18*P - 12*P^2 - 3*P^3 - 9*Q - 12*P*Q - 3*P^2*Q - 3*Q^2 - 3*P*Q^2 + 45*R + 18*P*R + 12*P^2*R + 3*P^3*R + 9*Q*R + 12*P*Q*R + 3*P^2*Q*R + 3*Q^2*R + 3*P*Q^2*R - 54*R^2 + 36*R^3 - 9*R^4 - 18 Schwering-Kuehne.X07 [1,1,-1] 1 9*P + 3*P^2 + 18*Q + 12*P*Q + 3*P^2*Q + 12*Q^2 + 3*P*Q^2 + 3*Q^3 - 45*R - 9*P*R - 3*P^2*R - 18*Q*R - 12*P*Q*R - 3*P^2*Q*R - 12*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 - 36*R^3 + 9*R^4 + 18 Schwering-Kuehne.X07 [1,1,-1] 2 27*P + 15*P^2 + 6*P^3 + P^4 + 18*Q + 24*P*Q + 12*P^2*Q + 2*P^3*Q + 15*Q^2 + 12*P*Q^2 + 3*P^2*Q^2 + 6*Q^3 + 2*P*Q^3 + Q^4 - 27*R - 27*P*R + 27*R^2 + 27*P*R^2 - 9*R^3 - 9*P*R^3 + 18 Schwering-Kuehne.X07 [1,1,-1] 3 - 18*P - 15*P^2 - 6*P^3 - P^4 - 27*Q - 24*P*Q - 12*P^2*Q - 2*P^3*Q - 15*Q^2 - 12*P*Q^2 - 3*P^2*Q^2 - 6*Q^3 - 2*P*Q^3 - Q^4 + 27*R + 27*Q*R - 27*R^2 - 27*Q*R^2 + 9*R^3 + 9*Q*R^3 - 18 Schwering-Kuehne.X07 [-1,1,-1] 0 - 6*P + 6*P^2 - 3*P^3 + 3*Q - 3*P^2*Q + 3*Q^2 - 3*P*Q^2 + 33*R + 6*P*R - 6*P^2*R + 3*P^3*R - 3*Q*R + 3*P^2*Q*R - 3*Q^2*R + 3*P*Q^2*R - 54*R^2 + 36*R^3 - 9*R^4 - 6 Schwering-Kuehne.X07 [-1,1,-1] 1 - 3*P + 3*P^2 + 6*Q + 3*P^2*Q + 6*Q^2 + 3*P*Q^2 + 3*Q^3 - 39*R + 3*P*R - 3*P^2*R - 6*Q*R - 3*P^2*Q*R - 6*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 - 36*R^3 + 9*R^4 + 12 Schwering-Kuehne.X07 [-1,1,-1] 2 7*P + 3*P^2 - 2*P^3 + P^4 + 2*Q + 2*P^3*Q + 3*Q^2 + 3*P^2*Q^2 + 2*Q^3 + 2*P*Q^3 + Q^4 + 27*R - 27*P*R - 27*R^2 + 27*P*R^2 + 9*R^3 - 9*P*R^3 - 8 Schwering-Kuehne.X07 [-1,1,-1] 3 2*P - 3*P^2 + 2*P^3 - P^4 - 11*Q - 2*P^3*Q - 3*Q^2 - 3*P^2*Q^2 - 2*Q^3 - 2*P*Q^3 - Q^4 + 27*R + 27*Q*R - 27*R^2 - 27*Q*R^2 + 9*R^3 + 9*Q*R^3 - 10 Schwering-Kuehne.X07 [1,-1,-1] 0 - 6*P - 6*P^2 - 3*P^3 + 3*Q - 3*P^2*Q - 3*Q^2 - 3*P*Q^2 + 39*R + 6*P*R + 6*P^2*R + 3*P^3*R - 3*Q*R + 3*P^2*Q*R + 3*Q^2*R + 3*P*Q^2*R - 54*R^2 + 36*R^3 - 9*R^4 - 12 Schwering-Kuehne.X07 [1,-1,-1] 1 - 3*P - 3*P^2 + 6*Q + 3*P^2*Q - 6*Q^2 + 3*P*Q^2 + 3*Q^3 - 33*R + 3*P*R + 3*P^2*R - 6*Q*R - 3*P^2*Q*R + 6*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 - 36*R^3 + 9*R^4 + 6 Schwering-Kuehne.X07 [1,-1,-1] 2 11*P + 3*P^2 + 2*P^3 + P^4 - 2*Q + 2*P^3*Q + 3*Q^2 + 3*P^2*Q^2 - 2*Q^3 + 2*P*Q^3 + Q^4 - 27*R - 27*P*R + 27*R^2 + 27*P*R^2 - 9*R^3 - 9*P*R^3 + 10 Schwering-Kuehne.X07 [1,-1,-1] 3 - 2*P - 3*P^2 - 2*P^3 - P^4 - 7*Q - 2*P^3*Q - 3*Q^2 - 3*P^2*Q^2 + 2*Q^3 - 2*P*Q^3 - Q^4 - 27*R + 27*Q*R + 27*R^2 - 27*Q*R^2 - 9*R^3 + 9*Q*R^3 + 8 Schwering-Kuehne.X07 [-1,-1,-1] 0 - 18*P + 12*P^2 - 3*P^3 - 9*Q + 12*P*Q - 3*P^2*Q + 3*Q^2 - 3*P*Q^2 + 27*R + 18*P*R - 12*P^2*R + 3*P^3*R + 9*Q*R - 12*P*Q*R + 3*P^2*Q*R - 3*Q^2*R + 3*P*Q^2*R - 54*R^2 + 36*R^3 - 9*R^4 Schwering-Kuehne.X07 [-1,-1,-1] 1 9*P - 3*P^2 + 18*Q - 12*P*Q + 3*P^2*Q - 12*Q^2 + 3*P*Q^2 + 3*Q^3 - 27*R - 9*P*R + 3*P^2*R - 18*Q*R + 12*P*Q*R - 3*P^2*Q*R + 12*Q^2*R - 3*P*Q^2*R - 3*Q^3*R + 54*R^2 - 36*R^3 + 9*R^4 Schwering-Kuehne.X07 [-1,-1,-1] 2 - 9*P + 15*P^2 - 6*P^3 + P^4 - 18*Q + 24*P*Q - 12*P^2*Q + 2*P^3*Q + 15*Q^2 - 12*P*Q^2 + 3*P^2*Q^2 - 6*Q^3 + 2*P*Q^3 + Q^4 + 27*R - 27*P*R - 27*R^2 + 27*P*R^2 + 9*R^3 - 9*P*R^3 Schwering-Kuehne.X07 [-1,-1,-1] 3 18*P - 15*P^2 + 6*P^3 - P^4 + 9*Q - 24*P*Q + 12*P^2*Q - 2*P^3*Q - 15*Q^2 + 12*P*Q^2 - 3*P^2*Q^2 + 6*Q^3 - 2*P*Q^3 - Q^4 - 27*R + 27*Q*R + 27*R^2 - 27*Q*R^2 - 9*R^3 + 9*Q*R^3
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/2093/CH4/EX4.12/exa_4_12.sce
9fa83d293a42714187e770b90abb33141c03b3b2
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
12
null
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UTF-8
Scilab
false
false
543
sce
exa_4_12.sce
// Exa 4.12 clc; clear; close; // Given data I=0.8;// in mA I=I*10^-3;//in A V_A= 100;// in V Bita=160; VT=25;// in mV VT= VT*10^-3;//in V gm= (I/2)/VT;// in A/V Gm= gm;// Short circuit trnsconductance in mA/V disp(Gm*10^3,"The value of Gm in mA/V") ro2= V_A/(I/2);// in ohm ro4= ro2;// in ohm Ro= ro2*ro4/(ro2+ro4);// in ohm disp(Ro*10^-3,"The value of Ro in kΩ is :") Ad= Gm*Ro;// in V/V disp(Ad,"Value of Ad in V/V is :") r_pi= Bita/gm;//in Ω Rid= 2*r_pi;// in Ω disp(Rid*10^-3,"The value of Rid in kΩ is :")
5083779272f60687b800922b77f36839bd6f7965
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/source/2.0/macros/robust/tf2des.sci
5c17f6c977416731de8fe4cb76cc4bb34bed91ca
[ "MIT", "LicenseRef-scancode-public-domain", "LicenseRef-scancode-warranty-disclaimer" ]
permissive
clg55/Scilab-Workbench
4ebc01d2daea5026ad07fbfc53e16d4b29179502
9f8fd29c7f2a98100fa9aed8b58f6768d24a1875
refs/heads/master
2023-05-31T04:06:22.931111
2022-09-13T14:41:51
2022-09-13T14:41:51
258,270,193
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tf2des.sci
function [S]=tf2des(G) //[S]=tf2des(G) // Transfer function to descriptor form: S=list('d',A,B,C,0,E) // E*dx=A*x+B*u // y=C*x+D*u //! Num=G(2);Den=G(3); %s=poly(0,varn(Den)); [n,m]=size(Num); pol=zeros(n,m);pro=pol; // Pro = strictly proper part of G // Pol = polynomial part of G. for l=1:n, for k=1:m, denlk=Den(l,k); [r,q]=pdiv(Num(l,k)+0*%s,denlk+0*%s); pol(l,k)=q; pro(l,k)=r/denlk; end; end; sp=tf2ss(pro); spol=tf2ss(horner(pol,1/%s)/%s); [n1,n1]=size(sp(2)); [n2,n2]=size(spol(2)); A=[sp(2),0*ones(n1,n2); 0*ones(n2,n1),eye(n2,n2)]; E=[eye(n1,n1),0*ones(n1,n2); 0*ones(n2,n1),spol(2)]; B=[sp(3); spol(3)]; C=[sp(4),-spol(4)]; S=list('des',A,B,C,0*C*B,E)
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/GS/SCENARIO/ManipulationTestGripper.sce
551b15e7de87371a72dc3b5b1b8214fa638a2fd5
[]
no_license
jmainpri/move3d-assets
a5b621daaedaaf8784fed0da1e80d029c83f3983
939db49d17a14e052bb58324b70e6112803d3105
refs/heads/master
2021-01-16T17:48:56.669119
2016-02-16T14:04:09
2016-02-16T14:04:09
20,237,987
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ManipulationTestGripper.sce
#************************************************************ # Scenario of grande_salle # # date : Fri Mar 18 13:37:23 2011 #************************************************************ p3d_sel_desc_name P3D_ENV grande_salle p3d_sel_desc_name P3D_ROBOT LOTR_TAPE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT WALLE_TAPE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT GREY_K7 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT GREY_TAPE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.243902 -2.858537 0.790244 -0.878049 0.000000 -85.170732 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT ACHILE_HUMAN1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PR2_ROBOT p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT LOWTABLE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT CHAIR1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT CHAIR2 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT TRASHBIN p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT HRP2TABLE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.536585 -1.970732 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SIMPLECHAIR p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT IKEA_SHELF p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 4.097561 -2.926829 0.000000 -0.878049 0.000000 -67.609756 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SURPRISE_BOX p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_RED p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_BLUE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_GREEN p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PLACEMAT_PURPLE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT ACCESSKIT p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT SPACENAVBOX p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT PAPERDOG p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT VISBALL_INTERNAL p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT JIDO_GRIPPER p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_constraint p3d_lin_rel_dofs 1 3 1 2 2 1 0.0 0 p3d_sel_desc_name P3D_ROBOT JIDOKUKA_ROBOT p3d_set_robot_steering_method Multi-Localpath p3d_set_robot_radius 1.000000 p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 3.539823 -2.163225 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 147.685808 27.533527 34.000000 108.398445 -49.078805 -96.761034 24.057510 0.032500 0.032500 2.736585 0.797133 3.820000 -2.550000 1.112195 0.000000 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//Example 4.14 10 life Insurance policies in a sample of 200 taken out of 50,000 were found to be insured for less than Rs 500 clc; clear; N=50000; n=200; p=10/200; q=1-p; S_E=sqrt(p*q/(n))*sqrt((N-n)/(N-1)); disp((p-1.96*S_E)*N,"and",(p+1.96*S_E)*N,"The number of each policies lies between ",(p-1.96*S_E),"to",(p+1.96*S_E),"The required 95% confidence limits for population proportion P are ");
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lab5_ec_diferentiale.sce
function y=f(t,y) y=10*sin(100*t)-y/0.5; endfunction a=0; b=1; y(1)=0; n=100; h=(b-a)/n; for i=1:n-1 t(i)=a+i*h; k1=(f(t(i),y(i))); k2=f(t(i)+h/2,y(i)+k1*h/2); k3=f(t(i)+h/2,y(i)+k2*h/2); k4=f(t(i)+h,y(i)+k3*h); y(i+1)=y(i)+h/6*(k1+2*k2+2*k3+k4); end plot(y)
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// clc; Kh=-1*10^-6; I=3; B=0.5; t=2*10^-3; Eh=Kh*I*B/t; disp(Eh,'output voltage (V)')
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class MaClasse public MaClasse() {} public void main() private void main(string arg1, string arg2) { VAR int a, b, c, d; if 1 = 3-2 then a := 5; else { b := 6; c := 7; while 1 do a := 2 + 7 * 8; if 2 then { VAR TEST t; a := 1 + 5; t := new TEST("arg1", 2, 3, 4, 5, 6+6); if 3=2-1-2-8*8 then { a := 11-2-8; a := 12--7846; a := 13-2-8; a := 14----------56456; a := 15-2-8; a := 16*0.5>2; } endif } endif } endif super(1, 2, 3, 4); return ("salut"); return (0+1*2); } end
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vepiteski/SolverComparator.jl
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bug_hprod_ampl_linux.sce
//using AmplNLReader //#nlp = AmplModel("../ampl/msqrtals") # loads the msqrtals.nl model [asl, x0, bl, bu, v, cl, cu] = ampl_init("msqrtals.nl"); //nlp = AmplModel("../ampl/curly10") # loads the msqrtals.nl model nvar = length(x0) //x0 = nlp.meta.x0 nbt=100000 mprintf("evaluating %i times the Hv product\n",nbt) gout=ampl_evalg(asl,x0); for i=1:nbt Hvout = ampl_eval_hvcomp(asl,v); //Hg = hprod!(nlp, x0, x0, Hg) end mprintf("done") // Scilab: no abnormal memory consumption. // Julia: //# consume ~7.3 Gb memory //# gc() frees nothing //# executing a second time eventually reaches my 16 Gb and begin swapping
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test_rootsearch_01.sce
function y = func1(x) y = x^3 - 10*x^2 + 5 endfunction exec("rootsearch.sce") dx = 0.1 a = 0 b = 1 [x1,x2] = rootsearch( func1, a, b, dx ) printf("x1 = %f, x2 = %f\n", x1, x2)
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example_3_3.sce
//Chapter 3 //Example 3-3 //ProbOnOpampParameters //Page 48,49,figure 3-2 clear;clc; //Given Rf=250*(10^3);//Feedback Resistance in Ohms Ri=10*(10^3);//Input Resistance in Ohms Ei=0.5;//Input voltage //Calculate //Example 3-3(a) I=Ei/(Ri); printf("\n\n Value of current through Rf = %.6f A \n\n",I) //Example 3-3(b) VRf=I*Rf; printf("\n\n Voltage through Rf = %.4f V \n\n",VRf) //Example 3-3(c) Ei1=-0.5; Vout=-(Rf/Ri)*Ei1; printf("\n\n Output Voltage = %.4f V \n\n",Vout) printf("\n\n Thus the magnitude of the output voltage does equal the voltage across Rf and Acl=-25")
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Example1_10.sce
//Chapter-1,Example1_4_2,pg 1-32 //For dark rings Dn=sqrt(4*R*n*wavelength) n=10 //10th ring Dn=0.5 //diameter of 10th ring wavelength=5*10^-5 //wavelength of light R=Dn^2/(4*n*wavelength) //radius of curvature t=Dn^2/(8*R) //thickness of film printf('\nThe radius of curvature is R = %.2f cm\n',R) printf('\nThe thickness of film is t = %.5f cm\n',t) //mistake in textbook
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Ex13_17.sce
//Introduction to Fiber Optics by A. Ghatak and K. Thyagarajan, Cambridge, New Delhi, 1999 //Example 13.17 //OS=Windows XP sp3 //Scilab version 5.5.2 clc; clear; //given lambda=1550e-9;//Operating wavekength of the system in m alpha=0.2;//Fiber loss in dB/km Pi=1e-3;//Input power in W Np=1000;//Minimum number of photons per bit of information B=2.5e9;//Bit rate in b/s h=6.63e-34;//Planck's constant in SI Units c=3e8;//Speed of photons in m/s v=c/lambda;//Frequency corresponding to the operating frequency Lmax=10/alpha*log10(2*Pi/(Np*B*h*v));//Maximum permissible loss-limited length in km mprintf("\n Maximum permissible loss-limited length Lmax=%.2f km",Lmax);//The answers vary due to round off error
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B-Rich/CATS
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ex23_2.sce
clc;clear; //Example 23.2 //calculation of electronic polarizability //given values e=8.85*10^-12;//permittivity in F/m er=1.0024;//relative permittivity at NTP N=2.7*10^25;//atoms per m^3 //calculation alpha=e*(er-1)/N; disp(alpha,'electronic polarizability (in F/m^2)is ');
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Ex19_6.sce
//chapter19 //example19.6 //page420 fc=1000 // kHz fs=5 // kHz m=0.5 Ec=100 // V lower_sideband=fc-fs upper_sideband=fc+fs amplitude=m*Ec/2 printf("lower and upper sideband frequencies = %.3f kHz and %.3f kHz \n",lower_sideband,upper_sideband) printf("amplitude of each sideband term = %.3f V \n",amplitude)
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Jaymee-Ericca-7/simple-compiler
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doubleAssignmentPrint.tst
main begin int x; int y; x=4; y=6; print(x); print(y); return x; end
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Example6_17.sce
//Example 6.17. clc format(6) beta=49 alpha=beta/(1+beta) disp("We know that, alpha = beta/(1+beta)") disp(alpha,"Therefore, the common base current gain is, alpha = ") disp("We also know that, alpha = IC / IE") IE=3*10^-3 IC=alpha*IE IC1=IC*10^3 disp(IC1,"Therefore, IC(mA) = alpha * IE = ")