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//pathname=get_absolute_file_path('16.05.sce') //filename=pathname+filesep()+'16.05-data.sci' //exec(filename) //Atmospheric pressure(in kPa): p=10^2 p1=1 p3=8 //Temperature(in K): Ta=300 T1=Ta T2a=273+30 Va=4 V1=Va //Gas constant(in kJ/kg.K): R=0.287 //Index of compression: n=1.2 //Mass of air compressed(in kg/min): m=p*Va/(R*Ta) //Work input(in hp): Wi=n/(n-1)*p1*10^2*Va*((p3/p1)^((n-1)/n)-1)/(60*0.7457) //Optimum intercooling pressure(in bar): p2=sqrt(p1*p3) //Work input for 2nd stage compression(in hp): Wii=2*n/(n-1)*p1*10^2*Va*((p3/p1)^((n-1)/(2*n))-1)/(60*0.7457) Wii=20.29 //Volume of air inlet of HP cylinder(in m^3/min): V2a=p1*V1/T1*T2a/p2 //Work required(in hp): W2=n/(n-1)*p1*10^2*V1*((p2/p1)^((n-1)/n)-1)/(60*0.7457)+n/(n-1)*p2*10^2*V2a*((p3/p2)^((n-1)/n)-1)/(60*0.7457) W2=20.42 //Percentage saving in work: ps=(Wi-Wii)/Wi*100 printf("\n RESULT \n") printf("\nPercentage saving in work = %f percent",ps) //% excess work to be done: pe=(W2-Wii)/W2*100 printf("\nPercentage excess work to be done = %f percent",pe)
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//there is a pole at the origin and contribution of gain k k=10^(14/20) //20*log(k)=14 disp("equation of starting line is y=-20*log(w)+14") wc1=10^(0) disp(wc1,"hence at wc1, 14=-20*log(wc1)+14. that is wc1 = ") y1=poly([1 1/wc1],'s','coeff') disp("equation of next line is y=-40*log(w)+14") wc2=10^(40/40) //-40*log(wc2)=-40 disp(wc2,"wc2=") y2=poly([1 1/wc2],'s','coeff') wc3=50 //given y3=poly([1 1/wc3],'s','coeff') TF= k*(y2)/((y1)*(y3)) disp(TF,"transfer function = ")
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clc clear //Input data d=2*10^-8;//The molecular diameter in cm n=3*10^19;//The number of molecules per cc pi=3.14;//Mathematical constant of pi //Calculations L=1/((pi*(d)^2*n));//The mean free path of a gas molecule in cm //Output printf('The mean free path of a gas molecule is %3.0g cm ',L)
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Lone vgroups in this file are: Vgroup name SD Vgroup and class Common Vgroups Vgroup name h4ex_VG_add_sds_to_vgroup.hdf and class CDF0.0
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// to find fundamental mmf wave,speed and its peak value clc; p=4; f = 50; S=60; g=180*p/S; ph=3; m=S/(p*ph); //slots/pole/phase K_b=sind(m*g/2)/(m*sind(g/2)); //breadth factor I_L=48; I_P=I_L/sqrt(3); I_Pmax=I_P*sqrt(2); c=24; //conductors N_ph=S*c/(ph*2); //turns/phase F_m=(4/%pi)*K_b*(N_ph/p)*I_Pmax; disp(F_m,'F_m(AT/pole)'); F_peak=(3/2)*F_m; disp(F_peak,'F_peak(AT/pole)'); n=120*f/p; disp(n,'speed(rpm)');
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// Exa 7.4 clc; clear; close; // Given data H1 = 2800;// in kJ/kg H2 = 2600;// in kJ/kg C2 = sqrt(2*(H1-H2)*1000);// in m/s disp(C2,"Exit velocity in m/s is "); m_f = 25;// mass flow rate in kg/sec V = 0.154;// in m^3/kg A = (m_f*V)/C2;// in m^2 disp(A,"Total exit area in m^2 is");
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errcatch(-1,"stop");mode(2);// Example 6.7, page no-374 rho=1000 h=10 P=rho*h printf("P = %d kg/m^2 = %d kg/cm^2 ",P,P/10000) exit();
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printf("\t example 12.6 \n"); printf("\t approximate values are mentioned in the book \n"); T1=176; // inlet hot fluid,F T2=176; // outlet hot fluid,F t1=85; // inlet cold fluid,F t2=120; // outlet cold fluid,F W=30000; // lb/hr w=120000; // lb/hr printf("\t 1.for heat balance \n"); printf("\t for carbon disulfide \n"); l=140; // Btu/(lb) Q=((W)*l); // Btu/hr printf("\t total heat required for carbon disulfide is : %.1e Btu/hr \n",Q); printf("\t for water \n"); c=1; // Btu/(lb)*(F) Q=((w)*(c)*(t2-t1)); // Btu/hr printf("\t total heat required for water is : %.0f Btu/hr \n",Q); delt1=T2-t1; //F delt2=T1-t2; // F printf("\t delt1 is : %.0f F \n",delt1); printf("\t delt2 is : %.0f F \n",delt2); LMTD=((delt2-delt1)/((2.3)*(log10(delt2/delt1)))); printf("\t LMTD is :%.1f F \n",LMTD); Tc=((T2)+T1)/2; // caloric temperature of hot fluid,F printf("\t caloric temperature of hot fluid is : %.0f F \n",Tc); tc=((t1)+(t2))/2; // caloric temperature of cold fluid,F printf("\t caloric temperature of cold fluid is : %.1f F \n",tc); printf("\t hot fluid:inner tube side,carbon disulfide \n"); hio=300; // Btu/(hr)*(ft^2)*(F) printf("\t cold fluid:shell side,water \n"); ID=17.25; // in C=0.25; // clearance B=6; // baffle spacing,in PT=1; as=((ID*C*B)/(144*PT)); // flow area,ft^2 printf("\t flow area is : %.2f ft^2 \n",as); Gs=(w/as); // mass velocity,lb/(hr)*(ft^2) printf("\t mass velocity is : %.2e lb/(hr)*(ft^2) \n",Gs); mu1=1.7; // at 280F,lb/(ft)*(hr), from fig.14 De=0.0792; // from fig.28,ft Res=((De)*(Gs)/mu1); // reynolds number printf("\t reynolds number is : %.1e \n",Res); jH=103; // from fig.28 k=0.36; // Btu/(hr)*(ft^2)*(F/ft), from fig.1 Z=1.68; // Z=((c)*(mu1)/k)^(1/3); // prandelt number ho=((jH)*(k/De)*(Z)); // using eq.6.15,Btu/(hr)*(ft^2)*(F) printf("\t individual heat transfer coefficient is : %.0f Btu/(hr)*(ft^2)*(F) \n",ho); tw=(tc)+(((hio)/(hio+ho))*(Tc-tc)); // from eq.5.31 printf("\t tw is : %.1f F \n",tw); tf=(Tc+tw)/(2); // from eq 12.19 printf("\t tf is : %.1f F \n",tf); printf("\t hot fluid:inner tube side,carbon disulfide \n"); kf=0.09; // Btu/(hr)*(ft^2)*(F/ft), from fig 14 sf=1.26; // from table 6 rowf=78.8; // lb/ft^3 muf=0.68; // cp, from fig 24 Nt=177; D=0.0517; // ft G1=(W/(3.14*Nt*D)); printf("\t G1 is : %.f lb/(hr)*(lin ft) \n",G1); Ret=((4)*(G1)/muf); // reynolds number printf("\t reynolds number is : %.0f \n",Ret); hi=(0.251*(((kf^3)*(rowf^2)*(4.17*10^8))/(muf^2))^(1/3)); // hi*(((kf^3)*(rowf^2)*(4.17*10^8))/(muf^2))^(-1)=0.251, from fig 12.12 printf("\t hi is : %.0e Btu/(hr)*(ft^2)*(F) \n",hi); ID=0.62; // ft OD=.75; //ft hio1=((hi)*(ID/OD)); //Hio=(hio/phyp), using eq.6.5 printf("\t Correct hio1 to the surface at the OD is : %.0f Btu/(hr)*(ft^2)*(F) \n",hio1); Uc=((hio1)*(ho)/(hio1+ho)); // clean overall coefficient,Btu/(hr)*(ft^2)*(F) printf("\t clean overall coefficient is : %.0f Btu/(hr)*(ft^2)*(F) \n",Uc); A2=0.1963; // actual surface supplied for each tube,ft^2,from table 10 L=16; A=(Nt*L*A2); // ft^2 printf("\t total surface area is : %.0f ft^2 \n",A); UD=((Q)/((A)*(LMTD))); printf("\t actual design overall coefficient is : %.0f Btu/(hr)*(ft^2)*(F) \n",UD); Rd=((Uc-UD)/((UD)*(Uc))); // (hr)*(ft^2)*(F)/Btu printf("\t actual Rd is : %.5f (hr)*(ft^2)*(F)/Btu \n",Rd); printf("\t pressure drop for inner pipe \n"); n=1; // number of passes at1=0.302; // flow area, in^2 at=((Nt*at1)/(144*n)); // total area,ft^2,from eq.7.48 printf("\t flow area is : %.3f ft^2 \n",at); Gt=(30000/(0.372)); // mass velocity,lb/(hr)*(ft^2) printf("\t mass velocity is : %.2e lb/(hr)*(ft^2) \n",Gt); mu2=0.029; // at inlet,lb/(ft)*(hr) Ret=((D)*(Gt)/mu2); // reynolds number printf("\t reynolds number is : %.2e \n",Ret); row=(76.1/((359)*(636/492)*(14.7/39.7))); printf("\t row is %.3f ld/ft^3 \n",row); s=(row/62.5); printf("\t s is %.4f \n",s); f=0.000138; // friction factor for reynolds number 143000, using fig.26 delPt=((f*(Gt^2)*(16)*(1))/(5.22*(10^10)*(0.0517)*(s)))/(2); // using eq.7.45,psi printf("\t delPt is : %.1f psi \n",delPt); printf("\t allowable delPa is negligible psi \n"); printf("\t pressure drop for annulus \n"); f=0.0017; // friction factor for reynolds number 31000, using fig.29 s=1; // for reynolds number 31000,using fig.6 Ds=17.25/12; // ft B=6; N=(12*L/B); // number of crosses,using eq.7.43 printf("\t number of crosses are : %.0f \n",N); delPs=((f*(Gs^2)*(Ds)*(N))/(5.22*(10^10)*(De)*(s))); // using eq.7.44,psi printf("\t delPs is : %.1f psi \n",delPs); printf("\t allowable delPT is 10 psi \n"); //end
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function GenSciHelpXml() global sciobj; global AutoGenHelpToolbox_root; //file operation parentdir = sciobj.Destdir + filesep(); //copy sce script file to dest dir scriptfile_path = AutoGenHelpToolbox_root + "examples"+filesep()+"tmpFile"+filesep()+"xml2jar_script.sce"; copyfile(parentdir, scriptfile_path); //New FileDir to save Xml File xmlpath = parentdir + "HelpSourceFile" + filesep() + "XmlFiles" + filesep(); mkdir(parentdir + "HelpSourceFile" + filesep(), "XmlFiles"); savefilepath = xmlpath + sciobj.FunctionName + ".xml"; //copy chapter file to Genxmlfile copyfile(AutoGenHelpToolbox_root+"examples"+filesep()+"tmpFile"+filesep()+"CHAPTER", xmlpath + "CHAPTER"); // Build xml_doc file functionname = sciobj.FunctionName; s = "<?xml version=""1.0"" encoding=""UTF-8""?>"+... "<refentry xml:id="""+functionname+""" xml:lang=""zh"">"+...//1 "<refnamediv>"+...//1-1 "<refname>"+sciobj.FunctionName+"</refname>"+...//1-1-1 "<refpurpose>"+sciobj.Overview+"</refpurpose>"+...//1-1-2 "</refnamediv>"+... "<refsynopsisdiv>"+...//1-2 "<title>调用格式</title>"+... "<synopsis>"+sciobj.Syntax+"</synopsis>"+... "</refsynopsisdiv>"+... "<refsection>"+...//1-3 "<title>参数说明</title>"+...//1-3-1 "<variablelist>"+...//1-3-2 1-3-2-1 "</variablelist>"+... "</refsection>"+... "<refsection>"+...//1-4 "<title>详细描述</title>"+... "<para>"+sciobj.Detailed+"</para>"+... "</refsection>"+... "<refsection role=""see also"">"+... "<title>参见</title>"+... "<simplelist type=""inline"">"+... "<member>"+... "<link linkend="""+sciobj.SeeAlso+""">"+sciobj.SeeAlso+"</link>"+... "</member>"+... "</simplelist>"+... "</refsection>"+... "</refentry>"; doc = xmlReadStr(s); if sciobj.Input == "0" && sciobj.Output == "0" then //无输入输出 inNode = xmlElement(doc,"varlistentry"); inNodeChild1 = xmlElement(doc,"listitem"); inNodeChild1Child1 = xmlElement(doc,"para"); inNodeChild1Child1.content = "无"; doc.root.children(3).children(2).children(1) = inNode; doc.root.children(3).children(2).children(1).children(1) = inNodeChild1; doc.root.children(3).children(2).children(1).children(1).children(1) = inNodeChild1Child1; else for i = 1:strtod(sciobj.Input) inNode = xmlElement(doc,"varlistentry"); inNodeChild1 = xmlElement(doc,"term"); inNodeChild1.content = sciobj.ParamsData.Name(i); inNodeChild2 = xmlElement(doc,"listitem"); inNodeChild2Child1 = xmlElement(doc,"para"); inNodeChild2Child1.content = sciobj.ParamsData.Dim1(i)+"×"+sciobj.ParamsData.Dim2(i)+" "+... sciobj.ParamsData.Type(i)+" "+sciobj.ParamsData.Details(i); doc.root.children(3).children(2).children(i) = inNode; doc.root.children(3).children(2).children(i).children(1) = inNodeChild1; doc.root.children(3).children(2).children(i).children(2) = inNodeChild2; doc.root.children(3).children(2).children(i).children(2).children(1) = inNodeChild2Child1; end for i = 1:strtod(sciobj.Output) inNode = xmlElement(doc,"varlistentry"); inNodeChild1 = xmlElement(doc,"term"); inNodeChild1.content = sciobj.ParamsData.Name(strtod(sciobj.Input)+i); inNodeChild2 = xmlElement(doc,"listitem"); inNodeChild2Child1 = xmlElement(doc,"para"); inNodeChild2Child1.content = sciobj.ParamsData.Dim1(strtod(sciobj.Input)+i)+"×"+... sciobj.ParamsData.Dim2(strtod(sciobj.Input)+i)+" "+... sciobj.ParamsData.Type(strtod(sciobj.Input)+i)+" "+... sciobj.ParamsData.Details(strtod(sciobj.Input)+i); doc.root.children(3).children(2).children(strtod(sciobj.Input)+i) = inNode; doc.root.children(3).children(2).children(strtod(sciobj.Input)+i).children(1) = inNodeChild1; doc.root.children(3).children(2).children(strtod(sciobj.Input)+i).children(2) = inNodeChild2; doc.root.children(3).children(2).children(strtod(sciobj.Input)+i).children(2).children(1) = inNodeChild2Child1; end end xmlDump(doc); xmlWrite(doc,savefilepath,%t); if sciobj.DemofileContent <> "0" then details = fileinfo(savefilepath); [fd, err] = mopen(savefilepath,"r"); source_str = mgetl(fd); mclose(fd); dest_str = source_str; for i = 1:9 dest_str(size(source_str,1)-i+1) = []; end format_str_before = ["<refsection>";"<title>示例</title>";"<programlisting role=""example""><![CDATA["]; format_str_after = ["]]></programlisting>";"</refsection>"]; dest_str = [dest_str; format_str_before]; dest_str = [dest_str; sciobj.DemofileContent']; dest_str = [dest_str; format_str_after]; for i = 1:9 dest_str = [dest_str;source_str(size(source_str,1)-9+i)]; end [fd, err] = mopen(savefilepath,"w"); mputl(dest_str, fd); mclose(fd); end disp("生成sci函数帮助文档成功!"); disp(sciobj.FunctionName + ".xml" + "文件保存位置为:"); disp(" " + xmlpath); //TODO:善后操作 xmlDelete(doc); clearglobal sciobj; clearglobal bOK; clearglobal Stop; endfunction
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D=[1,2,5,7,10,14,35,70]; a = 2; //a and b belong to D b = 14; V=int32([a,b]); thelcm=lcm(V) V=int32([a,b]); thegcd=gcd(V) abar=70/a bbar=70/b j=[abar,b]; h=[a,bbar]; V=int32([j]) lcm1=lcm(V) K=int32([h]) lcm2=lcm(K)
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clc(); clear; //To determine the wavelength which has high transmission mew=1.38; //refractiveindex of magnesium floride t=175; //thickness of coating of magnesium fluoride in nm lambda=4*t*mew //wavelength printf("The wavelength which has high transmission is %f nm",lambda);
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clc(); clear; //To calculate the radius of Li(mass no.7) r0=1.2; //in fm A=7; //mass number //r=r0*(A)^1/3 r=r0*(A)^(1/3) printf("The radius of Li with mass number 7 is %f fm",r);
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// Function Name: sum // Return the sum of of all elements in array // Calculating the sum. inputvec1 = [5, 4, 3]; result = armaVec("sum",inputvec1) // Function Name: trapz // Compute the trapezoidal integral of Y with respect to spacing in X, in each column (dim=0) or each row (dim=1) of Y // Calculating the trapz. inputvec1 = [5, 4, 3]; inputvec1 = [1, 2, 3]; result = armaVec("trapz",inputvec1,inputvec2) result = armaVec("trapz",inputvec1,inputvec2,1)
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[1,2,3,4,5] >> 6 = shift by -6 icol=0 sum= 0 + this(0)=1 * dipows(0)=1 * binoms(0)=1 icol=1 sum= 1 + this(1)=2 * dipows(1)=-6 * binoms(1)=1 icol=2 sum= -11 + this(2)=3 * dipows(2)=36 * binoms(2)=1 icol=3 sum= 97 + this(3)=4 * dipows(3)=-216 * binoms(3)=1 icol=4 sum= -767 + this(4)=5 * dipows(4)=1296 * binoms(4)=1 row 0 dipows=[1,-6,36,-216,1296] binoms=[1,1,1,1,1] result=[5713,0,0,0,0] icol=1 sum= 0 + this(1)=2 * dipows(0)=1 * binoms(0)=1 icol=2 sum= 2 + this(2)=3 * dipows(1)=-6 * binoms(1)=2 icol=3 sum= -34 + this(3)=4 * dipows(2)=36 * binoms(2)=3 icol=4 sum= 398 + this(4)=5 * dipows(3)=-216 * binoms(3)=4 row 1 dipows=[1,-6,36,-216,1296] binoms=[1,2,3,4,5] result=[5713,-3922,0,0,0] icol=2 sum= 0 + this(2)=3 * dipows(0)=1 * binoms(0)=1 icol=3 sum= 3 + this(3)=4 * dipows(1)=-6 * binoms(1)=3 icol=4 sum= -69 + this(4)=5 * dipows(2)=36 * binoms(2)=6 row 2 dipows=[1,-6,36,-216,1296] binoms=[1,3,6,10,15] result=[5713,-3922,1011,0,0] icol=3 sum= 0 + this(3)=4 * dipows(0)=1 * binoms(0)=1 icol=4 sum= 4 + this(4)=5 * dipows(1)=-6 * binoms(1)=4 row 3 dipows=[1,-6,36,-216,1296] binoms=[1,4,10,20,35] result=[5713,-3922,1011,-116,0] icol=4 sum= 0 + this(4)=5 * dipows(0)=1 * binoms(0)=1 row 4 dipows=[1,-6,36,-216,1296] binoms=[1,5,15,35,70] result=[5713,-3922,1011,-116,5] [5713,-3922,1011,-116,5]
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//find line current and starting torque with direct switching, stator resistance starting, autotransformer starting, star delta starting, autotransformer ratio give 1 pu clc; //I_s/I_fl=6; s_fl=0.05; disp('by direct switching'); Is=6;disp(Is,'line current(pu)'); T=Is^2*s_fl;disp(T,'torque(pu)'); disp('by stator resistance starting'); Is=2;disp(Is,'line current(pu)'); //given T=Is^2*s_fl;disp(T,'torque(pu)'); disp('by autotransformer starting'); x=2/6; Is_motor=2; Is=Is_motor*x;disp(Is,'line current(pu)'); T=Is^2*s_fl;disp(T,'torque(pu)'); disp('by star delta starting'); Is=(1/3)*6;disp(Is,'line current(pu)'); T=Is^2*s_fl*3;disp(T,'torque(pu)'); disp('by autotransformer starting'); Ts=1; x=sqrt(Ts/((6^2)*s_fl));disp(x,'x');
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clc // given that VH_H2=0 // half cell voltage VZn_Zn2=-0.763 // half cell voltage iZn=10^-7 // current density in A/cm^2 iH2=10^-10 // current density in A/cm^2 beta_Zn=0.09 beta_H2=-0.08 n=2 //Exchange of 2 electrons F=96500//Faradays constant printf(" Example 16.2\n") printf("\n Part A") i_c=10^[(VH_H2-VZn_Zn2-(beta_H2*log10(iH2))+(beta_Zn*log10(iZn)))/(beta_Zn-beta_H2)] printf("\n Rate of oxidation with zinc is %.2e A/cm^2",i_c) r=i_c/(n*F) printf("\n Rate of oxidation is %.2e mol/cm^2-s\n",floor(r*1e12)/1e12) printf("\n Part B") Vc=VH_H2+(beta_H2*log10(i_c/iH2)) printf("\n Corrosion potential is %.3f V\n",Vc)
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import {pointOnCircle, Position} from "../../../../../blacksheep-geometry/lib"; import { GoldenRectanglePositioner } from './GoldenRectanglePositioner'; class GoldenSpiralPositioner { goldenRectanglePositioner: GoldenRectanglePositioner; curvePointQueue: Position[]; currentCurvePoint: Position; currentCurvePosition: Position; previousCurvePosition: Position; currentCurveRadius: number; currentCurveLength: number; currentSize: number; curvePhaseAdjust: number; constructor(goldenRectanglePositioner : GoldenRectanglePositioner) { this.goldenRectanglePositioner = goldenRectanglePositioner; this.curvePointQueue = []; this.currentCurvePoint = null; this.currentCurvePosition = null; this.previousCurvePosition =null; this.currentCurveRadius= 0; this.currentSize = 0; this.curvePhaseAdjust = 0; this.currentCurveLength = 0; } reset() { this.goldenRectanglePositioner.reset(); this.curvePointQueue = []; this.currentCurvePoint = null; this.currentCurvePosition = null; this.currentCurveRadius= null; //TODO //There's an OO confusion here. Is it the responsibility of the GoldenSpiralPositioner to reset (and also tick) the GoldenRectanglePositioner? //I'm saying yes for now. } tick() { this.goldenRectanglePositioner.tick(); let myPhi =this.goldenRectanglePositioner.getMyPhi(); let subPhase = this.goldenRectanglePositioner.stagePhaser.getSubPhase(); let previousSubPhase = this.goldenRectanglePositioner.stagePhaser.getPreviousSubPhase(); let invertMyPhi = 1 - (1/myPhi); /** On corner: Just add the curve point */ if (this.goldenRectanglePositioner.stagePhaser.isOnCorner()){ this.curvePointQueue.push(this.goldenRectanglePositioner.getPreviousPosition().copy()); } /** Moving from 1/myPhi of the curve phase: Change the curve point */ if (previousSubPhase < invertMyPhi && subPhase > invertMyPhi ) { if (this.curvePointQueue.length > 3 ) { this.currentCurvePoint = this.curvePointQueue.shift(); this.currentCurvePosition = pointOnCircle( this.currentCurvePoint, this.currentSize/(myPhi), (this.goldenRectanglePositioner.stagePhaser.getPhase()) * (Math.PI / 2) ); this.currentCurveLength = this.goldenRectanglePositioner.currentSize / (myPhi * myPhi); this.curvePhaseAdjust = (this.goldenRectanglePositioner.stagePhaser.getStage() -1) * (Math.PI / 2); } } /** If there's a curve point: Draw the curve */ if (this.currentCurvePoint) { //Curve phase: //If subphase is 0 - 1/myPhi = 0.5-1 of curvePhase // subphase is 1/myPhi to 1 = 0.0 to 0.5 of curvePhase. let curvePhase = ( subPhase < invertMyPhi) ? 0.5 + 0.5 * (subPhase / ( invertMyPhi)) : 0.5 * ((subPhase - invertMyPhi)/(1/myPhi )) ; //0-1 let center = this.currentCurvePoint; this.previousCurvePosition = this.currentCurvePosition.copy(); this.currentCurvePosition = pointOnCircle( center, this.currentCurveLength, this.curvePhaseAdjust + curvePhase * (Math.PI /2) ); } } getPosition() : Position{ return this.currentCurvePosition; } getPreviousPosition() : Position { return this.previousCurvePosition; } } export default GoldenSpiralPositioner;
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//ANALOG AND DIGITAL COMMUNICATION //BY Dr.SANJAY SHARMA //CHAPTER 5 //ANGLE MODULATION clear all; clc; printf("EXAMPLE 5.43(PAGENO 263)"); //given //x_c(t) = 10*cos(2*%pi*10^8*t + 200*cos (2*%pi*10^3*t)) //instantaneous frequecy w_i = 2*%pi*10^8 - 4*%pi*10^6*sin(2*%pi*10^3) delta_w = 4*%pi*10^5//angular frequency deviation w_m = 2*%pi*10^3//angulat modulating frequency //calculations beeta = delta_w/w_m; W_B1 = 2*(beeta + 1)*w_m;//angular bandwidth //since beeta >>1,therefore W_B1 = 2*delta_w//angular bandwidth //W_B==W_B1 f_B = W_B1/(2*%pi)//bandwidth in Hz //result printf("\n\nBandwidth = %.2f Hz",f_B);
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function [faculteit] = solve(n) if n < 0 then error("the variable should be positive.") end if n==1 | n==0 then faculteit = 1 else faculteit = n * solve(n-1) end endfunction
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clear clc data=[ 1 2 .2+%i*.8 %i*.02 2 3 .3+%i*.9 %i*.03 2 4 .25+%i*1 %i*.04 3 4 .2+%i*.8 %i*.02 1 3 .1+%i*.4 %i*.01 ] n=4 e=5 Y=zeros(n,n) for i=1:e ynew = 1/(data(i,3)) y0=data(i,4) n1=real(data(i,1)) n2=real(data(i,2)) if(n1==0) Y(n2,n2)=Y(n2,n2)+ynew+y0 else Y(n1,n1)= Y(n1,n1)+ynew+y0 Y(n1,n2)= Y(n1,n2)-ynew Y(n2,n1)= Y(n2,n1)-ynew Y(n2,n2)= Y(n2,n2)+ynew+y0 end end disp(fix(Y*1e3)/1e3)
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//example 8 //Velocity in exit flow clear clc disp('From Steam Tables, for liquid water at 20 C') vf=0.001002 //in m^3/kg v=vf Pi=300 //Line pressure in kPa Po=100 //in kPa Ve=(2*v*(Pi-Po)*1000)^0.5 //velocity in the exit flow printf(" \n Hence, an ideal nozzle can generate upto Ve=%.0f m/s in the exit flow. \n",Ve)
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//Example 13-2, Page No- 484 clear clc lamda = 2.19 len = (3/8)*lamda printf('The pyhsical length of the transmission line %.2f feet',len)
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MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Medium Skill At Feet MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Medium Skill 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 [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Bot Profile] Name=soar DodgeProfileNames=ADAD DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;0.5;2.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=At Feet;Medium Skill At Feet;Medium Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=soaring bot SeeThroughWalls=true [Character Profile] Name=EGODEATH MaxHealth=100.0 WeaponProfileNames=Track_fullsound;track_earlove;track_earlove2;pistol;QWRL;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 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=1300.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=true 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 [Character Profile] Name=soaring bot MaxHealth=1000.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1500.0 MaxCrouchSpeed=500.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=4.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=0.212 Z=0.020 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=300.0 MainBBRadius=50.0 MainBBHasHead=false MainBBHeadRadius=20.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=300.0 ProjBBRadius=50.0 ProjBBHasHead=false ProjBBHeadRadius=20.0 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=soaring.abilmov;;; 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 [Dodge Profile] Name=ADAD MaxTargetDistance=5500.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.05 MaxLRTimeChange=0.3 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.9 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=2.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.3 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.16 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.1 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Track_fullsound Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=1.0 TimeBetweenShots=0.01 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=1000000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.001 HitSoundCooldown=0.001 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=1.0 RecoilNegatable=false DecalType=0 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.01 TaggingMaxFactor=0.5 TaggingHitFactor=0.001 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=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 [Weapon Profile] Name=track_earlove Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 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=1000000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.05 HitSoundCooldown=0.05 ShootSound=Shot 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=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.0 TaggingMaxFactor=0.0 TaggingHitFactor=0.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=1000.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=track_earlove2 Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 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=1000000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.1 HitSoundCooldown=0.1 ShootSound=Shot 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=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.0 TaggingMaxFactor=0.0 TaggingHitFactor=0.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=1000.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=pistol Type=Hitscan ShotsPerClick=1 DamagePerShot=100.0 KnockbackFactor=4.0 TimeBetweenShots=0.1 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=4.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Flare BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.1 MinRecoilUp=0.1 MinRecoilHoriz=0.1 MaxRecoilHoriz=0.1 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.05 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=QWRL Type=Projectile ShotsPerClick=1 DamagePerShot=120.0 KnockbackFactor=5.0 TimeBetweenShots=0.8 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=6000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=6000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=100.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=0.0 HeadshotCapable=false HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 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// **** Purpose **** // This function generates the hopping matrix of a given crystal // structure and // Slaster-Koster parameters // **** Variables **** // [surr_site]: list(m) -> n x 9, real // <= this is the output variable of PIL_uc_nb // [site_orb]: n x 3, integer // <= the variable specify the orbital of each site. // [SK_parameter]: n x 7, real // <= the SK_parameter [orb1, orb2, nn_order, ts, tp, td, tf] // [hop_fliter]: 1x1, positive real, default=10^-6 // <= the fliter of small matrix elements in H_hop // [state_info]: n x 5, integer // => tells how the states are ordered // [state_label, site, n(principle), L(angular), sub-orbital] // [H_hop]: list(tot_sublatt) x tot_suborb x tot_suborb x tot_surr_site, real // => the hopping matrix of each nearest neighbor order // **** Version **** // 05/15/2014 first built // 05/24/2014 modify output to include r-vector // 06/03/2014 fix surr_site becomes list problem // 06/06/2014 full rewirte, each bond has its own H_hop // **** Comment **** // 1.site_orb: // e.g: [1,1,0; 3,1,2] means sublattice 1 / 2, has an atomic orbital set with // prinipal (or type) quantum number n=1/1 and angular momentum L=0 / 2 // Note: the principal number n will not have any esseitial function. This is // just a number for you to dinguish two orbitals on the same site. // So, when print state info, it will be shown. // 2.SK_parameter: // e.g: [1,2,ts,tp,td,tf] means orb1 (i.e the orbital defined in site_orb(1,:)) // and orb2 has SK_parameter: ts,tp,td,tf // to prevent from double assign, this function require SK_parameter(1,n) <= // SK_parameter(2,n). // Note: The way we label SK_paramater will not use the information of principal // number n in [site_orb]. // 3.more infomation: // the hop matrix doen't correspond to real Hamiltonian, it just tells you the coupling // between two negibhbor sites. The real Hamiltoina has to consider their position vectors // and impose periodic boundary condiition. // 4.About the H_hop // H_hop means tij(ra,rb)\sum{i,j}C_{i}^{+}(ra)C_{j}(rb), so all the H_hop are just // upper or lower triangle. function [state_info,H_hop]=PIL_hop_mat(surr_site,site_orb,SK_parameter... ,basis_out,hop_order,hop_fliter) // make surr_site integers [lhs,rhs]=argn(); select rhs case 4 hop_order=2; // default set to 2nd order hop_fliter=10^-3; // default case 5 hop_fliter=10^-3; // default end // check input if length(site_orb(:,1)) > 1 then for n=2:length(site_orb(:,1)) if prod(site_orb(n,:)==site_orb(n-1,:))==1 then disp('Error: PIL_hop_mat, two the same orbitals on the same site is not allowed!'); abort end end end for n=1:length(SK_parameter(:,1)) if round(real(SK_parameter(n,1))) > round(real(SK_parameter(n,2))) then disp('Error: PIL_hop_mat, just specify SK_parameter(n,1) smaller than SK_parameter(n,2) terms !'); abort; end end // label how user define the orbital before sort site_orb=gsort(cat(2,site_orb,[1:length(site_orb(:,1))]'),'lr','i'); // define necessary parameters tot_sublatt=size(surr_site); tot_suborb=2*sum(2*site_orb(:,3)+1); // sort complex SK_parameter SK_sort_tmp=gsort(round(real(SK_parameter(:,1:3))),'lr','i'); SK_par_tmp=zeros(SK_parameter); for n=1:length(SK_sort_tmp(:,1)) tmp_ind=find(round(real(SK_parameter(:,1)))==SK_sort_tmp(n,1)... & round(real(SK_parameter(:,2)))==SK_sort_tmp(n,2) ... & round(real(SK_parameter(:,3)))==SK_sort_tmp(n,3)) SK_par_tmp(n,:)=SK_parameter(tmp_ind,:); end SK_parameter=SK_par_tmp; // generate all SubOrb table, site_suborb --> // [site, n, L, suborb_index, UserOrb_index] // the orders of site_suborb is also the state_index site_suborb=[]; for n=1:length(site_orb(:,1)) //suborb index (defined by PIL_basis_trans), //Orb_index (order of the orbital) select site_orb(n,3) case 0 // suborb=1~2 ; SK checker=1,1 site_suborb=cat(1,site_suborb,cat(2,repmat(site_orb(n,:),2,1)... ,[1,2]')); case 1 // suborb=3~8 ; SK checker=2~4,2~4 site_suborb=cat(1,site_suborb,cat(2,repmat(site_orb(n,:),6,1)... ,[3:8]')); case 2 // suborb=9~18 ; SK checker=5~9,5~9 site_suborb=cat(1,site_suborb,cat(2,repmat(site_orb(n,:),10,1)... ,[9:18]')); case 3 // subob=19~32 ; SK checker=10~16,10~16 site_suborb=cat(1,site_suborb,cat(2,repmat(site_orb(n,:),14,1)... ,[19:32]')); else disp('Error: PIL_hop_mat, site_orb(n,3) can only ranges 0 to 3 !'); abort end end site_suborb(:,[4:5])=site_suborb(:,[5,4]); site_suborb=gsort(site_suborb,'lr','i'); // site_range is also the state_index of the SurOrb of each site site_range=zeros(tot_sublatt,2); for n=1:tot_sublatt tmp=find(site_suborb(:,1)==n); site_range(n,1)=min(tmp); site_range(n,2)=max(tmp); end // basis transformation matrix U=[]; for n=1:length(site_orb(:,1)) select site_orb(n,3) case 0 [M_out,U_in_out]=PIL_basis_trans(eye(2,2),'s','c',basis_out); case 1 [M_out,U_in_out]=PIL_basis_trans(eye(6,6),'p','c',basis_out); case 2 [M_out,U_in_out]=PIL_basis_trans(eye(10,10),'d','c',basis_out); case 3 [M_out,U_in_out]=PIL_basis_trans(eye(14,14),'f','c',basis_out); end U=PIL_dirsum(U,U_in_out); end // key part========================================================= H_hop=list(); for n=1:tot_sublatt // run total sublattice H_hop(n)=zeros(tot_suborb,tot_suborb,length(surr_site(n)(:,1))-1); s1=round(surr_site(n)(1,3)); for m=2:length(surr_site(n)(:,1)) // run all its neighbor sites s2=round(surr_site(n)(m,3)); r=surr_site(n)(m,7:9)-surr_site(n)(1,7:9); order=round(surr_site(n)(m,1)); if order <= hop_order then for p=site_range(s1,1):site_range(s1,2) // run matrix range for q=site_range(s2,1):site_range(s2,2) suborb1=site_suborb(p,4); suborb2=site_suborb(q,4); SK_index=find(round(real(SK_parameter(:,1)))... ==site_suborb(p,5)... & round(real(SK_parameter(:,2)))==site_suborb(q,5)... & round(real(SK_parameter(:,3)))==order); if length(SK_index)==0 then SK_index=find(round(real(SK_parameter(:,1)))... ==site_suborb(q,5)... & round(real(SK_parameter(:,2)))==site_suborb(p,5)... & round(real(SK_parameter(:,3)))==order); end select length(SK_index) case 0 // no assign case H_hop(n)(p,q,m-1)=PIL_SK_int(suborb1,suborb2... ,r,[0,0,0,0]); case 1 // normal case H_hop(n)(p,q,m-1)=PIL_SK_int(suborb1,suborb2... ,r,SK_parameter(SK_index,4:7)); else // conflict assign case disp('Error: PIL_hop_mat, SK_parameter has conflict assignments!'); abort; end end end H_hop(n)(:,:,m-1)=clean(U*H_hop(n)(:,:,m-1)*U'); else // exit calculate higher order hopping. break end end end // ================================================================= state_info=cat(2,[1:tot_suborb]',site_suborb(:,1:4)); endfunction
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//Chapter 19 //Example 19_1 //Page 483 clear;clc; i=1500; mva=1000; v=33*1e3; t=3; printf("(i) Rated normal current = %.0f A \n\n", i); printf("(ii) Breaking capacity = %.0f MVA \n\n", mva); rsbc=mva*1e6/sqrt(3)/v; printf("(iii) Rated symmetrical breaking capacity = %.0f A \n\n", rsbc); rmc=2.55*rsbc; printf("(iv) Rated making current = %.0f A \n\n", rmc); printf("(v) Rated short time rating = %.0f A for %.0f sec \n\n", rsbc, t); printf("(vi) Rated service voltage = %.0f kV \n\n", v/1000);
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THE OPTIMIZATION ALGORITHM HAS CHANGED TO THE EM ALGORITHM. ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.482328D+00 2 -0.684036D-02 0.383718D-02 3 -0.943371D-01 0.264342D-02 0.277254D+00 4 0.262622D-02 -0.615175D-03 -0.583655D-02 0.205752D-02 5 -0.862332D-03 0.126702D-03 -0.185974D-02 0.977635D-04 0.229473D-02 6 0.288460D-03 0.242491D-05 0.306182D-03 0.694397D-05 -0.429529D-03 7 -0.153537D-03 -0.158405D-04 0.174634D-02 -0.268341D-04 -0.681924D-03 8 -0.228608D-02 -0.147254D-03 0.189002D-02 -0.900534D-05 0.267429D-03 9 -0.727956D+00 -0.508252D-02 0.783658D+00 -0.319696D-02 0.334907D-01 10 -0.201822D-01 0.116871D-01 -0.832756D-01 0.745659D-02 0.165904D+00 11 0.270236D-02 0.404259D-02 -0.172535D+00 0.961519D-02 -0.363005D-01 12 0.318561D+00 0.165564D-01 -0.635507D+00 0.245367D-01 0.440387D-03 13 -0.407275D-01 0.570969D-02 0.147021D-01 0.720090D-02 -0.574434D-01 14 0.452778D-01 -0.272195D-02 -0.296104D+00 0.130234D-01 0.314780D-01 15 -0.551892D+00 0.496531D-01 -0.332100D+00 -0.219423D-01 -0.106258D+00 16 0.623869D-01 -0.902618D-03 0.198899D-03 -0.338859D-02 -0.865054D-03 17 0.115381D-02 0.551891D-03 -0.127455D-02 -0.332114D-05 -0.579015D-03 18 -0.554307D+00 -0.211539D-01 0.916442D+00 -0.195341D-01 0.122242D-01 19 -0.550452D-01 0.342341D-02 -0.302699D-01 0.547462D-02 -0.526140D-02 20 0.924742D+00 -0.190211D-01 -0.259092D+01 0.643620D-01 -0.105989D-01 21 0.353309D-01 -0.760631D-02 0.607695D-01 -0.526769D-02 0.563637D-02 22 0.114154D-02 -0.656102D-04 -0.354584D-02 0.371025D-03 0.258639D-03 23 0.263078D-01 0.714019D-03 0.456369D-01 -0.885769D-02 -0.318744D-03 24 -0.450461D-02 0.322652D-03 0.112379D-02 0.181854D-03 -0.560136D-04 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.183177D-02 7 0.696010D-03 0.142213D-02 8 -0.416308D-03 -0.266153D-03 0.280152D-02 9 -0.446300D-01 0.246486D-01 0.358000D-01 0.127463D+03 10 -0.553287D-01 -0.686052D-01 0.173430D-01 0.310185D+01 0.332846D+02 11 0.228988D-01 0.170834D-01 -0.312494D-01 -0.193502D+02 -0.442994D+01 12 -0.136613D+00 -0.448330D-01 -0.215118D-01 0.137118D+02 0.466555D+01 13 0.897245D-01 0.804575D-01 -0.352164D-01 -0.273757D+01 -0.946472D+01 14 -0.403628D-01 -0.341663D-01 0.107392D+00 0.415902D+01 0.410780D+01 15 0.107529D+00 0.730699D-01 -0.573907D-01 -0.285384D+01 -0.208267D+02 16 0.335162D-04 -0.643171D-03 -0.356862D-02 0.152096D+01 -0.280093D+00 17 -0.289523D-03 -0.239860D-04 0.490968D-03 -0.265004D+00 -0.455972D-01 18 -0.117612D+00 -0.693454D-01 0.106096D+00 0.124957D+02 0.320743D+01 19 -0.102703D-01 0.137430D-01 0.148314D-01 -0.260041D+00 -0.232384D+00 20 0.950610D-01 0.407124D-01 -0.218321D+00 -0.130500D+02 0.379577D+01 21 0.877091D-02 -0.120791D-01 -0.109397D-01 -0.249512D+00 0.597210D+00 22 0.322285D-03 -0.136738D-03 -0.452913D-03 -0.194740D-01 0.403737D-03 23 -0.109519D-02 0.989512D-03 -0.508166D-02 0.511607D+00 -0.117513D+00 24 -0.446175D-04 -0.144691D-03 0.796043D-03 -0.238493D-01 -0.150629D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.459429D+02 12 0.166027D+02 0.122662D+03 13 0.130861D+01 -0.306352D+01 0.139203D+02 14 -0.142571D+01 0.131545D+01 -0.581410D+01 0.268606D+02 15 0.100980D+02 -0.117400D+02 0.898127D+01 -0.354628D+01 0.560584D+03 16 -0.183889D+00 0.800385D-01 0.113010D+00 -0.114951D+00 0.420149D+01 17 0.266303D-01 -0.493184D-01 -0.312477D-01 0.132963D-01 -0.263934D+01 18 -0.339649D+01 0.319197D+01 -0.915186D+01 0.536200D+01 -0.138988D+03 19 0.183786D+01 0.180086D+00 0.469190D+00 0.184553D+01 -0.225808D+01 20 -0.164156D+01 -0.165553D+02 0.901687D+01 -0.151313D+02 0.549392D+02 21 -0.121406D+01 -0.583488D+00 -0.728767D+00 -0.149784D+01 0.204897D+01 22 -0.819181D-01 0.188774D-01 0.255684D-01 -0.336832D-01 0.701794D+00 23 -0.351879D-01 0.912156D+00 0.152137D+00 -0.383650D+00 -0.480537D+00 24 0.220440D-01 -0.115662D+00 -0.452012D-01 0.662640D-01 -0.256245D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.791792D+00 17 -0.638892D-01 0.274306D-01 18 -0.176356D+00 0.728030D+00 0.241129D+03 19 -0.237061D+00 0.318503D-01 0.326062D+01 0.502644D+01 20 0.455690D+00 -0.335899D+00 -0.996400D+02 0.239544D+00 0.243145D+03 21 0.359635D-01 -0.176415D-01 -0.232194D+00 -0.430607D+01 0.194290D+00 22 0.718806D-02 -0.675201D-02 -0.115964D+01 -0.542257D-01 0.422995D+00 23 0.122336D+00 -0.456289D-02 0.392759D+00 -0.973847D-01 0.888148D+00 24 -0.758221D-02 0.454178D-02 0.386057D+00 0.477407D-02 -0.933479D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.540551D+01 22 -0.195248D-01 0.140431D-01 23 -0.114803D+00 0.136235D-02 0.577394D+00 24 -0.164643D-02 -0.436015D-02 -0.544024D-01 0.123831D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.159 1.000 3 -0.258 0.081 1.000 4 0.083 -0.219 -0.244 1.000 5 -0.026 0.043 -0.074 0.045 1.000 6 0.010 0.001 0.014 0.004 -0.210 7 -0.006 -0.007 0.088 -0.016 -0.377 8 -0.062 -0.045 0.068 -0.004 0.105 9 -0.093 -0.007 0.132 -0.006 0.062 10 -0.005 0.033 -0.027 0.028 0.600 11 0.001 0.010 -0.048 0.031 -0.112 12 0.041 0.024 -0.109 0.049 0.001 13 -0.016 0.025 0.007 0.043 -0.321 14 0.013 -0.008 -0.109 0.055 0.127 15 -0.034 0.034 -0.027 -0.020 -0.094 16 0.101 -0.016 0.000 -0.084 -0.020 17 0.010 0.054 -0.015 0.000 -0.073 18 -0.051 -0.022 0.112 -0.028 0.016 19 -0.035 0.025 -0.026 0.054 -0.049 20 0.085 -0.020 -0.316 0.091 -0.014 21 0.022 -0.053 0.050 -0.050 0.051 22 0.014 -0.009 -0.057 0.069 0.046 23 0.050 0.015 0.114 -0.257 -0.009 24 -0.058 0.047 0.019 0.036 -0.011 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.431 1.000 8 -0.184 -0.133 1.000 9 -0.092 0.058 0.060 1.000 10 -0.224 -0.315 0.057 0.048 1.000 11 0.079 0.067 -0.087 -0.253 -0.113 12 -0.288 -0.107 -0.037 0.110 0.073 13 0.562 0.572 -0.178 -0.065 -0.440 14 -0.182 -0.175 0.391 0.071 0.137 15 0.106 0.082 -0.046 -0.011 -0.152 16 0.001 -0.019 -0.076 0.151 -0.055 17 -0.041 -0.004 0.056 -0.142 -0.048 18 -0.177 -0.118 0.129 0.071 0.036 19 -0.107 0.163 0.125 -0.010 -0.018 20 0.142 0.069 -0.265 -0.074 0.042 21 0.088 -0.138 -0.089 -0.010 0.045 22 0.064 -0.031 -0.072 -0.015 0.001 23 -0.034 0.035 -0.126 0.060 -0.027 24 -0.009 -0.034 0.135 -0.019 -0.023 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 0.221 1.000 13 0.052 -0.074 1.000 14 -0.041 0.023 -0.301 1.000 15 0.063 -0.045 0.102 -0.029 1.000 16 -0.030 0.008 0.034 -0.025 0.199 17 0.024 -0.027 -0.051 0.015 -0.673 18 -0.032 0.019 -0.158 0.067 -0.378 19 0.121 0.007 0.056 0.159 -0.043 20 -0.016 -0.096 0.155 -0.187 0.149 21 -0.077 -0.023 -0.084 -0.124 0.037 22 -0.102 0.014 0.058 -0.055 0.250 23 -0.007 0.108 0.054 -0.097 -0.027 24 0.029 -0.094 -0.109 0.115 -0.097 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.434 1.000 18 -0.013 0.283 1.000 19 -0.119 0.086 0.094 1.000 20 0.033 -0.130 -0.412 0.007 1.000 21 0.017 -0.046 -0.006 -0.826 0.005 22 0.068 -0.344 -0.630 -0.204 0.229 23 0.181 -0.036 0.033 -0.057 0.075 24 -0.077 0.246 0.223 0.019 -0.538 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.071 1.000 23 -0.065 0.015 1.000 24 -0.006 -0.331 -0.643 1.000
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clc; clear all; f = 7e6; // Ultrasonic frquency in hertz theta = 45; v = 1.5; // Blood velocity in m/s U = 1500; // Ultrasonic velocity in m/s deltaf = (2*f*v*cosd(45))/U disp('Hz',deltaf,'The frequency of the doppler flowmeter is') //Variation in anser as compared to textbook..checked in calculator also.. there is mistake in the book..
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a=200;//leangth of cross section along x-axis,given in mm b=300;//leangth of cross section along y-axis,given in mm tx=25;//thickness along x-axis,given in mm ty=20;//thickness along y-axis,given in mm M=100*10^6;//bending moment,given in N.mm
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Scope Snipe.sce
Name=Scope Snipe PlayerCharacters=player_char BotCharacters=scope.rot IsChallenge=true Timelimit=60.0 PlayerProfile=player_char AddedBots=scope.rot;scope.rot PlayerMaxLives=0 BotMaxLives=0;0 PlayerTeam=1 BotTeams=2;2 MapName=scope_snipe.map MapScale=10.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=0.0 ScorePerDamage=5.0 ScorePerKill=10.0 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=Scope Snipe WeaponHeroTag=Sniper Rifle DifficultyTag=3 AuthorsTag=NFNT BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=true Description=Stand, walk, run Sniping targets of various speeds 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=scope_walk DodgeProfileNames=scope_dodge DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=scope_char_walk SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=scope_run DodgeProfileNames=scope_dodge DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=scope_char_run SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=scope_stand DodgeProfileNames=scope_dodge DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=scope_char_stand SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Rotation Profile] Name=scope ProfileNames=scope_walk;scope_run;scope_stand ProfileWeights=1.0;1.0;1.0 Randomized=false [Character Profile] Name=player_char MaxHealth=100.0 WeaponProfileNames=SNIPER;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=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=scope_char_walk MaxHealth=5.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=300.0 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=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Spheroid MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Spheroid ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=0.1 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=scope_char_run MaxHealth=5.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=600.0 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=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Spheroid MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Spheroid ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=0.1 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=scope_char_stand MaxHealth=5.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=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=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Spheroid MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Spheroid ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=0.1 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 [Dodge Profile] Name=scope_dodge MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=10.0 MaxLRTimeChange=10.0 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.02 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.25 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 [Weapon Profile] Name=SNIPER Type=Hitscan ShotsPerClick=1 DamagePerShot=5.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=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=false 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=true ADSZoomDelay=0.0 ADSZoomSensFactor=1.0 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=SNIPER StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=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=75 ADSFOVOverride=7.5 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=true 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=0.0,0.1,360.0,360.0 SpreadSCH=0.0,0.1,360.0,360.0 SpreadMSH=0.0,0.1,360.0,360.0 SpreadMCH=0.0,0.1,360.0,360.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 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// Example 3.9 clc; clear; close; // Given data format('v',8); Rf= 1*10^6;// in Ω Rin= 1*10^6;// in Ω Vout_by_Vin= -Rf/Rin;// (since Vout= -Rf/Rin*Vin) Av= Vout_by_Vin;// voltage gain disp(Av,"The voltage gain is : "); // I_in= Iout (As it is a unity gain inverter) Ain= 1;//input impedance (since I_in= Iout) disp(Ain,"The input impedance is : "); Ap= abs(Av*Ain);// power gain disp(Ap,"The power gain is : ");
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//Chapter 6,Example 6.3 Page 199 clc clear Cs = 500*10^-12 // F R1 = 800 // ohm R2 = 180 // ohm C2 = 0.15 // micro F w = 314 V = 33*10^3 Cp = Cs*(R2/R1) Rp = R1/(w^2*C2*Cs*10^-6*R2^2) tang = 1/(w*Rp*Cp) pl = V^2/Rp printf (" Rp = %e ohm \n ",Rp) printf (" Cp = %e F \n ",Cp) printf (" tan δ = %f \n ",tang) printf (" Power loss = %f watts \n ",pl) //Answer may vary due to round off error
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//page no 224 //example no 7.5 // INCREMENT A NUMBER. clc; disp('LXI B,2050H'); //loads the data 2050H in BC register pair. disp('B=20H C=50H'); B=20; C=50; disp('INX B'); C=C+1; printf('B= %d C= %d \n',B,C); disp('The contents of BC register pair will be 2051H'); disp('INR B'); B=B+1; printf('B= %d \n',B); disp('INR C'); C=50; C=C+1; printf('C= %d \n',C); disp('The contents of BC register pair will be 2151H');
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// @Harness: verifier // @Purpose: "Test for redefinitions of operand types" // @Result: "RedefinedUserType @ 8:16" architecture redef_ot_02 { operand-type A[5]: int [0, 7]; operand-type A { } }
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clc //Initialization of variables\ sf=0.00007 n=0.013 gam=9.81*1000 V=0.45 //m/s Q=1.4 //m^3/s //calculations by=Q/V x=poly(0,"x") y=roots(x^2 -2.66*x +1.55) b=by ./y //results printf("y = ") disp( y ) printf("corresponding b=") disp(b)
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exec("projection.sci") exec("Rmat.sci") // theta debe estar en grados function [A, B, C, D] = rotE(u, theta, d) [_A _B _C _D] = projection(d) [R] = Rmat(u, theta) A=R*_A B=R*_B C=R*_C D=R*_D endfunction
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function [output] = cummin(A, dim, direction) funcprot(0); [rows, cols] = size(A); if(~exists('dim','local') & ~exists('direction','local')) then if(rows==1 | cols==1) then output = zeros(rows, cols); minim = 999999; for iter = 1:max(size(A)) if(A(iter)<minim) then minim = A(iter); end output(iter) = minim; end else output = zeros(rows, cols); for i = 1:cols minim = 99999; for j = 1:rows if(A(j, i)<minim) then minim = A(j,i); end output(j,i) = minim; end end end elseif (~exists('direction','local') & exists('dim','local')) then // 2 means along rows // 1 means along columns if(dim==1) then output = zeros(rows, cols); for i = 1:cols minim = 99999; for j = 1:rows if(A(j, i)<minim) then minim = A(j,i); end output(j,i) = minim; end end elseif(dim==2) then output = zeros(rows, cols); for i = 1:rows minim = 99999; for j = 1:cols if(A(i, j)<minim) then minim = A(i, j); end output(i, j) = minim; end end end elseif(exists('direction','local') & ~exists('dim','local')) then output = zeros(rows, cols); if(direction == "reverse") then for i = cols:-1:1 minim = 99999; for j = rows:-1:1 if(A(j, i)<minim) then minim = A(j,i); end output(j,i) = minim; end end end elseif(exists('direction','local') & exists('dim','local')) output = zeros(rows, cols); if(dim==1) then if(direction=="reverse") then output = zeros(rows, cols); for i = cols:-1:1 minim = 99999; for j = rows:-1:1 if(A(j, i)<minim) then minim = A(j,i); end output(j,i) = minim; end end end elseif(dim==2) then output = zeros(rows, cols); for i = rows:-1:1 minim = 99999; for j = cols:-1:1 if(A(i, j)<minim) then minim = A(i, j); end output(i, j) = minim; end end end end endfunction
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//page 307 //Example 8.28 clc; clear; close; disp('x1 and x2 are two real nos. i.e., x1^2 + x2^2 = 1'); x1 = rand(); x2 = sqrt(1 - x1^2); disp(x1,'x1 = '); disp(x2,'x2 = '); B = [x1 x2 0;0 1 0;0 0 1]; disp(B,'B = '); disp('Applying Gram-Schmidt process to B:') a1 = [x1 x2 0]; a2 = [0 1 0] - x2 * [x1 x2 0]; a3 = [0 0 1]; disp(a1,'a1 = '); disp(a2,'a2 = '); disp(a3,'a3 = '); U = [a1;a2/x1;a3]; disp(U,'U = '); M = [1 0 0;-x2/x1 1/x1 0;0 0 1]; disp(M,'M = ') disp(inv(M) * U,'inverse(M) * U = '); disp('So, B = inverse(M) * U'); //end
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clear; printf('************** Chi-square Distribution Function ****************'); printf('\n'); df = input('Enter a Degree of Freedom : '); for x = 1: 20, Total( x, 1) = cdfchi( "PQ", x, df); if x==1 then Dist( x, 1) = Total( x, 1); else Dist( x, 1) = Total( x, 1) - Total( x-1, 1); end, end printf('Total ='); disp(string(Total)); printf('\n'); printf('Dist ='); disp(string(Dist)); printf('\n'); clf; // clear //scf; // add plot2d(Dist);
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clc clear //Input data W=20000 //Power developed in kW m=12 //Mass flow rate in kg/s C1=50 //Velocity of air entering in m/s T1=700+273 //Temperature of air entering in K T2=298 //Temperature of air leaving in K C2=125 //Velocity of air leaving in m/s Cp=1.005 //Specific heat capacity at constant pressure in kJ/kg-K //Calculation dh=Cp*(T2-T1) //Change in enthalpy in kJ/kg Q=((m*dh)+W-(m*(1/2000)*(C2^2-C1^2))) //The rate of heat transfer in kJ/s //Output printf('The rate of heat transfer is %3.2f kJ/s',Q)
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//Example 4.8: clc; clear; close; //given data : R2=4;// in k-ohm R1=40;// in k-ohm Vcc=22;// in V Rc=10;// in k-ohm Re=1.5;// in k-ohm Vbe=0.5;// in V Voc=R2*10^3*Vcc/((R1+R2)*10^3); Ic=(Voc-Vbe)/(Re*10^3); Vce=Vcc-(Rc+Re)*Ic*10^3; format('v',5) disp(Vce,"Collector to emitter voltage,Vce(V) = ")
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//Caption: entropy ,information rate //Example 9.18 //page no 405 //determine entropy ,information rate clc; clear; px1=1/4; px2=1/5; px3=1/5; px4=1/10; px5=1/10; px6=1/20; px7=1/20; px8=1/20; f=10*10^3; fs=10*2*10^3; HX=px1*log2(1/px1)+px2*log2(1/px2)+px3*log2(1/px3)+px4*log2(1/px4)+px5*log2(1/px5)+px6*log2(1/px6)+px7*log2(1/px7)+px8*log2(1/px8);//entropy disp("bits/message",HX,"H(X) = "); r=fs; R=r*HX;//information rate disp("bits/sec",R,"R = ");
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//PointerTest.tst load PointerTest.asm, output-file PointerTest.out, compare-to PointerTest.cmp, output-list RAM[256]%D1.6.1 RAM[3]%D1.6.1 RAM[4]%D1.6.1 RAM[3032]%D1.6.1 RAM[3046]%D1.6.1; set RAM[0] 256, repeat 450 { vmstep; } output;
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//Example 9.8 (a) //Program To Determine Smallest Record Length of Bartlett Method clear; clc; close; //Data fr=0.01;//Frequency Resolution N=2400; //Samples //RECORD LENGTH CALCULATION lb=0.89/fr; //Display the result in command window disp(lb,"Record Length of Bartlett Method");
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//To Calculate the Dynamic Plate Resistance at the operating condition //Example 41.2 clear; clc; V1=40;//Initial Plate Voltage in Volts V2=42;//Final Plate Voltage in Volts delVp=V2-V1;//Change in Plate Voltage in Volts I1=50*10^-3;//Initial Plate Current in Amperes I2=60*10^-3;//Final Plate Current in Amperes delIp=I2-I1;//Change in Plate Current in Amperes Rp=delVp/delIp;//Dynamic Plate Resistance in ohms printf("Dynamic Plate Resistance = %d ohm",Rp);
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//Variable declaration fo = 50 //output frequency(KHz) L = 10^-3 //inductance(H) ro = 100 //output resistance(k ohms) Q = 80 //coil inductance Ri = 10 //input resistance(k ohms) beta = 125 //common emitter current gain //Calculations //Part a C = 1/(((2*(%pi)*fo)^2)*L) //tunning capacitance(nF) r = (2*(%pi)*fo*L)/Q //internal resistance(k ohms) req = (Q^2)*r //equivalent resistance(k ohms) R = (ro*req)/(ro+req) //ro||req(k ohms) Avo = -(beta*R)/Ri //voltage gain //Part b Qcircuit = R/(2*(%pi)*fo*L) //circuit inductance BW = fo/Qcircuit //bandwidth //Results printf ("a)value of capacitance is %.f nF",C/1E-3) printf (" gain is %.1f",Avo) printf ("b)bandwidth is %.f Hz",BW/1E-3) printf ("Note : value used for beta in texbook is wrong in the solution")
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//Harriot P., 2003, Chemical Reactor Design (I-Edition), Marcel Dekker, Inc., USA, pp 436. //Chapter-6 Ex6.1.a Pg No.236 //Title:Power Consumption per unit volume at 300rpm //==================================================================================================================== clear clc //INPUT D_a=0.1; D_t=0.3; H=0.3; N_P=5.5; rho=1000; n=5; S_f=6;//Scale up factor in diameter //CALCULATION P_unit_vol=(N_P*n^3*D_a^5)/(%pi*(1/4)*D_t^2*H); P_thousand_gal=P_unit_vol*5.067; t=(4/n)*(D_t/D_a)^2*(H/D_t); P_unit_vol_new=S_f^2*P_thousand_gal; //OUTPUT //Console Output mprintf('\n The Power consumption per unit volume at 300rpm = %.2f HP/1000 gal',P_thousand_gal); mprintf('\n\ The Power consumption scaling up sixfold in diameter = %.0f HP/1000 gal',P_unit_vol_new); //File Output fid= mopen('.\Chapter6_Ex1_a_Output.txt','w'); mfprintf(fid,'\n The Power consumption per unit volume at 300rpm = %.2f HP/1000 gal',P_thousand_gal); mfprintf(fid,'\n\ The Power consumption scaling up sixfold in diameter = %.0f HP/1000 gal',P_unit_vol_new); mclose(fid); //======================================================END OF PROGRAM=================================================
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// Aim:To Find flow rate of axial piston pump in L/s // Given: // speed of pump: N=1000; //rpm // number of pistons: Y=9; // piston diameter: d=15; //mm // piston circle diameter: D=125; //mm // offset angle: theta=10; //deg // volumetric efficiency: eta_v=94; //%
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clc; clear; format('v',11); h=1000; T=300; p=1000*exp(-h/8000); N=77.6*p/T; n=1+N*10^-6; disp(n,"n=");
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clc //to calculate compton shift and wavelength h=6.63*10^-34 //planck's constant in J-s m0=9.11*10^-31 //mass of electron c=3*10^8 //light speed in m/s dellambda=h*(1-(1/sqrt(2)))/(m0*c) lambda0=2*10^-10 lambda=dellambda+lambda0 disp("compton shift is dellambda="+string(dellambda)+"m") disp("wavelength of the scattered X-rays is lambda="+string(lambda)+"m") //to calculate fraction of energy lost by the photon in the collision //energy lost =E0-E/E0=(hc/lambda0)-(hc/lambda)/(ha/lambda0) //we get, energylost=dellambda/lambda disp("energylost ="+string(energylost)+"unitless")
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function unix_s(cmd) //unix_s - silent shell command execution //%Syntax // unix_s(cmd) //%Parameters // cmd - a character string //%Description // cmd instruction (sh syntax) is passed to shell, the standard output // is redirected to /dev/null //%Examples // unix_s("\rm -f foo") //%See also // host unix_g unix_x //! // Copyright INRIA if prod(size(cmd))<>1 then error(55,1),end if getenv('WIN32','NO')=='OK' & getenv('COMPILER','NO')=='VC++' then tmp=strsubst(TMPDIR,'/','\')+'\unix.out'; cmd1= cmd + ' > '+ tmp; else cmd1='('+cmd+')>/dev/null 2>'+TMPDIR+'/unix.err;'; end stat=host(cmd1); if getenv('WIN32','NO')=='OK' & getenv('COMPILER','NO')=='VC++' then host('del '+tmp); end select stat case 0 then case -1 then // host failed error(85) else //sh failed if getenv('WIN32','NO')=='OK' & getenv('COMPILER','NO')=='VC++' then error('unix_s: shell error'); else msg=read(TMPDIR+'/unix.err',-1,1,'(a)') error('unix_s: '+msg(1)) end end
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//rows = 3; //cols = 3; //A = zeros(rows,cols); //disp("Inputs to all matrices to be sequential left to right, top to bottom"); //disp("Inputs to A begin"); //for i = 1:rows //for j = 1:cols //A(i,j) = input("value for A:") //end //end A=[3 -2 5; -2 3 6; 5 6 4]; lam = poly(0, 'lam') lam = lam charMat = A-lam*eye(3,3) disp(charMat, 'The characteristic Matrix is') charPoly=poly(A, 'lam') disp(charPoly, 'The characteristic polynomial is') lam = spec(A) disp(lam, 'The eigen values of A are') function [x, lam] = eigenvectors(A); [n, m] = size(A); lam = spec(A); x = []; for k=1:3 B=A-lam(k)*eye(3,3); C=B(1:n-1, 1:n-1); b = -B(1:-n, n); y=C/b; y=[y:1]; y = y/norm(y); x=[x, y]; end endfunction get f('eigenvectors') [x, lam] = eigenvectors(A) disp(x,'The eigen vectors of A are');
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//Ex:58 clc; clear; close; a=20000;//apogee in km b=16000;//perigee in km x=2*a;//sum of apogee and perigee B=-40000; A=1 C=256000000; r_a1=(-B+sqrt(B^2-(4*A*C)))/2; printf("The apogee distance=%d km",r_a1); r_p1=x-r_a1; printf("\n The perigee distance=%d km",r_p1);
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clear; clc; // Definição da função f(x) function y = f(x) y = log(x) - 1 endfunction // Implementação Bisseção function [it, x, Er] = bissecao(a, b, p, itMax) it = 0; x = a; Er = 1 while (Er > 10^(-p) & it < itMax) it = it + 1; xOld = x; x = (a + b)/2; if (f(x)*f(a)) < 0 b = x; else a = x; end Er = abs((x - xOld)/x); end endfunction // Exemplo de chamada [it, x, Er] = bissecao(2, 3, 4, 20)
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// Initialisations ... s = poly(0,'s'); s = syslin('c',s*s/s); r=[1,1]; load('proc'); frq=0.1:0.001:1; rep1 = repfreq(proc,frq); rep3 = repfreq(s/s,frq); vproc=pfss(tf2ss(proc)); vproc(5)=clean(ss2tf(vproc(5))); gr=ss2tf(vproc(3)+vproc(5)+vproc(7)+vproc(8)); gr=gr+horner(clean(proc-gr,1e-8),0); xbasc();xset("window",0);xselect();bode([proc;gr],0.1,1,0.005); errmul=proc/gr-1; vigr=pfss(tf2ss(1/gr)); //on recupere les numerateurs-->w3 vigr(1)=ss2tf(vigr(1)); vigr(2)=ss2tf(vigr(2)); vigr(3)=ss2tf(vigr(3)); vigr(4)=ss2tf(vigr(4)); vigr(5)=ss2tf(vigr(5)); vigr(6)=ss2tf(vigr(6)); w31=vigr(1);w31=w31/horner(w31,0); w32=vigr(2);w32=w32/horner(w32,0); w33=vigr(3);w33=w33/horner(w33,0); w33=trfmod(w33);// prendre le pole reflechi (changer - par +) w341=trfmod(vigr(4)); // prendre le pole reflechi (changer - par +) w34=w341/trfmod(w341); // multiplier l'amortissement par 3 w35=vigr(5); w35=w35/trfmod(w35); //multiplier l'amortissement par 3 g=gr/s; vg=pfss(tf2ss(g)); //nouvelle dec. en elmts simple-->syst. augm. vg1=ss2tf(vg(1)); vg2=clean(ss2tf(vg(2))); vg3=ss2tf(vg(3)); vg4=ss2tf(vg(4)); vg0=vg1+vg2; Ms=s+1;Ns=1/(s+1); Sys1=sysdiag(1,1,1,1,Ms);Sys2=sysdiag(1,Ns); w50=0.4; w51= 8; w52 = 29; Rg=[diag([w50,w51,w52]);[1,1,1]]*[vg(1)+vg(2);vg(3);vg(4)]; U=[0,-1;1,-1]; amin = 0; amax = 2; while (amax -amin)/amax > 1e-2, a = (amin + amax)/2; write(%io(2),a,'(f6.4)') w3=(1/ab)*horner((1+s^3),s/a)*w31*w33*w34*w35; P=sysdiag(tf2ss(w3),Rg)*U; Ptmp=Sys1*P*Sys2; [sk,mu]=H_inf(Ptmp,r,0.8,1.2,1); if mu == [] then amin = a; else amax = a; end end w3=(1/ab)*horner((1+s^3),s/amin)*w31*w33*w34*w35; P=sysdiag(tf2ss(w3),Rg)*U; //xbasc(); xset("window",1);gainplot([w3;errmul],.1,1,0.005); Ptmp=Sys1*P*Sys2; [Ktmp,mu]=H_inf(Ptmp,r,0.9,1.1,30); K=ss2tf(Ktmp)/s; ks=trfmod(K); olp=ks*proc; rep2 = repfreq(ks,frq); xbasc(2); xset("window",2);xselect();nyquist(olp,0.03,0.8,0.00015); m_circle(20*log(2.05)/log(10));xset("dashes",0); sensit = rep1 ./(rep3 + rep1.*rep2); xbasc(3); xset("window",3);xselect();gainplot(frq,[sensit;rep1;rep2],['G/(1+KG)';'G';'K']); www=lft(Ptmp,Ktmp); xbasc(5);xset("window",5);xselect(); gainplot(www,0.01,10); www1=lft(ss2tf(P),r,ks); xbasc(6);xset("window",6);xselect(); gainplot(www1,0.01,10,['W3G/(1+KG)';'W50G0/(1+KG)';'W51G1/(1+KG)';'W52G2/(1+KG)']);
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v=120; n=75/100; p=1.5*746; i=p/(n*v); disp("the current (in A) that must be supplied is"); disp(i);
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clc; clear; mprintf('MACHINE DESIGN \n Timothy H. Wentzell, P.E. \n EXAMPLE-10.1 Page No.195\n'); P=100; //[lb/in^2] Hydraulic pressure F=450; //[lb] Extension force Fr=400; //[lb] Retraction force A=F/P; //[in^2] Cross section area D=sqrt(4*A/%pi); //[in] Bore of cylinder mprintf('\n The bore of cylinder is %f in.',D); //Use 2.5in bore cylinder Dm=2.5; //[in] Bore of cylinder Dr=1; //[in] Diameter of rod A2=%pi*Dm^2/4-%pi*Dr^2/4; //[in^2] F2=P*A2; //[lb] Force if F2>=Fr then mprintf('\n The diameter of rod is %f in.',Dr); else mprintf('\n This would not meet requirement'); end //This would meet requirement Ab=%pi*Dm^2/4; //[in^2] Cross section area //Note-In the book V=180.7 is used instead of V=180.64158 d=20; //[in] stroke V=Ab*d+A2*d; //[in^3] Volume per cycle t=2; //[s] Cycle time FR=V/t; //[in^3/s] Flowrate FR=FR*7.48*60/1728; //[gal/min] Flowrate mprintf('\n Flow rate required is %f gal/min.',FR);
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exec("alaqiltest.start", -1); if typeof(CSP_ITERATION_FWD_get()) <> "constant" then alaqiltesterror(); end if typeof(CSP_ITERATION_BWD_get()) <> "constant" then alaqiltesterror(); end if typeof(ABCDE_get()) <> "constant" then alaqiltesterror(); end if typeof(FGHJI_get()) <> "constant" then alaqiltesterror(); end try bar1(CSP_ITERATION_FWD_get()) bar1(CSP_ITERATION_BWD_get()) bar1(1) bar1(int32(1)) bar2(ABCDE_get()) bar2(FGHJI_get()) bar2(1) bar2(int32(1)) bar3(ABCDE_get()) bar3(FGHJI_get()) bar3(1) bar3(int32(1)) catch alaqiltesterror() end if typeof(enumInstance_get()) <> "constant" then alaqiltesterror(); end if enumInstance_get() <> 2 then alaqiltesterror(); end if typeof(Slap_get()) <> "constant" then alaqiltesterror(); end if Slap_get() <> 10 then alaqiltesterror(); end if typeof(Mine_get()) <> "constant" then alaqiltesterror(); end if Mine_get() <> 11 then alaqiltesterror(); end if typeof(Thigh_get()) <> "constant" then alaqiltesterror(); end if Thigh_get() <> 12 then alaqiltesterror(); end exec("alaqiltest.quit", -1);
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clc // Given that lambda = 5.893e-7 // wavelength of light in meter V = 0.36 // stopping potential for emitted electron in eV h = 6.62e-34 // Planck constant in J-sec c = 3e8 // speed of light in m/sec e = 1.6e-19 // charge on an electron in C m = 9.1e-31 // mass of an electron in kg // Sample Problem 14 on page no. 14.25 printf("\n # PROBLEM 14 # \n") printf("Standard formula used \n ") printf(" E_k = h*mu - phi \n") E = h * c / lambda w = ((h * c) / lambda) * (1 / e) - V f = w * e / h printf("\n Maximum energy is %f eV.\n Work function is %f eV.\n Threshold frequency is %e Hz. ",E/e,w,f)
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@relation led7digit @attribute Led1 real[0.0,1.0] @attribute Led2 real[0.0,1.0] @attribute Led3 real[0.0,1.0] @attribute Led4 real[0.0,1.0] @attribute Led5 real[0.0,1.0] @attribute Led6 real[0.0,1.0] @attribute Led7 real[0.0,1.0] @attribute number{0,1,2,3,4,5,6,7,8,9} @inputs Led1,Led2,Led3,Led4,Led5,Led6,Led7 @outputs number @data 2 8 6 6 6 6 7 7 9 7 0 7 0 0 1 1 2 8 3 3 4 4 5 5 7 7 9 5 9 9 0 0 0 0 3 7 5 5 6 8 0 7 2 2 3 9 4 4 1 7 5 5 5 5 6 6 7 7 9 9 1 1 1 7 4 4 6 6 7 7 2 2 4 4 9 9 9 9 2 2 3 3 3 9 8 0 8 8 9 9 9 9 4 4 5 5 4 9 8 8
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function [x]=descente(A,b,n) x(1)=b(1)/A(1,1); for k=2:n, s=0; for i=1:(k-1), s=s+A(k,i)*x(i); end x(k)=(b(k)-s)/A(k,k); end endfunction
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mode(-1); warning('off'); z=0 w=1 leeg=-1 //6*6 eenvoudig (iOs "hitori") N1=[5 2 1 5 4 6 5 4 3 2 5 4 1 5 4 4 6 2 4 4 5 1 5 1 4 3 5 5 2 1 2 4 6 4 5 5] C1=[z w w w w w w z w w z w w w w z w w z w z w w z w w w z w w w z w w z w] //9*9 eenvoudig (iOs "Real Hitori") N2=[1 8 2 4 3 9 4 1 5 6 5 5 1 1 4 9 3 3 8 4 6 9 5 3 2 6 7 4 8 3 8 7 8 8 2 9 1 6 4 2 3 6 5 9 1 9 5 8 3 5 2 7 6 1 2 5 3 1 6 4 4 2 8 5 4 4 2 9 3 7 7 6 7 9 1 5 1 6 3 8 8] C2=[z w w w z w z w w w z w z w w w w z w w w w w z w z w w z w z w w z w w w w z w w z w w z w z w w z w w w w w w z w w z w z w w z w z w w z w w w w w w z w w w z] // 5*5 gemakkelijk (hitoriconquest.com) N3=[5 5 1 5 3 5 4 1 2 1 5 3 4 3 5 3 4 5 4 2 1 2 3 3 4] C3=[z w w z w w w z w w z w w z w w z w w w w w w z w] // 5*5 iets moeilijker (hitoriconquest.com) N4=[5 3 3 2 2 3 3 2 5 4 1 2 3 1 5 4 2 1 3 5 1 5 4 1 3] C4=[w w z w z w z w w w w w w z w w z w w z z w w w w] // 8*8 iets moeilijker (muren) (hitoriconquest.com) N5=[5 2 4 5 6 1 6 7 5 5 2 7 8 1 4 1 1 2 8 6 4 7 3 1 3 4 7 7 5 2 7 6 1 6 7 3 8 5 2 8 2 2 3 5 7 1 6 7 6 7 3 1 5 3 8 4 5 8 5 2 1 6 5 3] C5=[w w w z w w z w z w w w w z w w w z w w w w w z w w w z w w z w z w z w z w w w w z w w w z w z w w z w z w w w z w w w w w z w] //5*5 gemakkelijk (brainbashers) N6=[3 1 5 5 1 1 5 2 3 4 2 5 3 2 5 5 1 2 2 3 4 1 1 5 5] C6=[w z w z w w w w w w w z w z w w w z w w w z w w z] //7*7 gemakkelijk (brainbashers) N7=[4 2 1 2 6 6 5 7 2 6 2 1 5 3 7 7 2 5 5 2 6 1 1 7 5 2 6 6 2 6 5 6 3 5 1 4 5 2 1 4 2 7 5 1 4 6 4 3 5] C7=[w w w z w z w w z w w w w w z w w z w z w w z w w w w z w w w z w z w z w z w w w w w w w w z w z] //9*9 gemakkelijk (brainbashers) N8=[4 2 3 8 1 2 5 4 6 8 2 6 6 9 2 7 8 3 6 7 5 4 2 8 9 2 6 5 9 1 6 2 1 4 6 8 1 7 2 4 4 1 6 7 5 1 5 9 2 9 3 1 6 2 2 1 8 9 6 6 3 8 7 3 6 8 9 7 4 2 4 9 4 1 1 7 4 6 9 9 2] C8=[z w w w w z w w w w z w z w w w z w w w w w z w w w z w w z w w w w z w w z w z w z w w w z w w w z w w w z w w z w w z w w w w w w z w w w z w w z w w z w z w w()] //6*6 medium (muren!) (brainbashers) N9=[5 2 2 1 6 6 2 6 5 4 4 3 1 6 4 2 3 6 1 4 5 5 4 1 3 2 1 6 4 5 3 1 1 3 1 2] C9=[w z w w w z w w w w z w w z w w w w z w z w z w w w w w w w z w z w z w] //12*12 gemakkelijk (brainbashers) N10=[2 11 1 12 7 1 10 6 3 6 12 2 4 11 7 10 9 2 11 5 8 8 6 9 11 7 9 1 4 6 12 3 9 11 8 7 4 4 6 5 10 12 9 1 6 9 11 10 9 2 4 8 10 9 7 6 2 7 5 6 2 8 5 7 1 10 12 4 5 12 3 7 10 8 9 6 5 1 5 1 12 4 9 8 11 10 12 10 11 12 3 8 5 9 9 8 12 2 10 7 5 3 9 10 9 11 1 6 5 5 3 4 11 9 4 12 8 2 8 11 5 6 6 3 9 4 8 2 12 7 12 1 12 9 10 6 12 10 4 7 6 2 2 9] C10=[z w w w w z w z w w z w w z w w z w w w z w w w w w z w w w w w w z w z z w w w z w z w z w w w w z w w w z w w w z w z w w w z w w z w z w w w w z w w z w w z w w z w z w w z w z w w w z w z w w z w w w w w z w w w z w w w z w z w w w z w w w z w w w w w z w w w z w w z w z w w w z w z] //6*6 medium (brainbashers) N11=[5 2 2 1 6 6 2 6 5 4 4 3 1 6 4 2 3 6 1 4 5 5 4 1 3 2 1 6 4 5 3 1 1 3 1 2] C11=[w z w w w z w w w w z w w z w w w w z w z w z w w w w w w w z w z w z w] // speciaal geval: alle 2 in laatste kolom zwart N12=[3 4 2 5 2 4 2 4 1 4 2 2 1 4 2 1 5 4 2 3 4 5 5 3 3] C12=[w w w w z z w z w w w z w w z w w w w w w z w w z]
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function out=a(n) if (n==0) out=2*lambda/%pi; else out=-2/(n*%pi)*sin(n*(%pi-lambda)); end endfunction N=1000; t=linspace(0.01,5,4); lambda=%pi/2; theta=linspace(0,2*%pi,1000); p=100; for i=1:N somme=a(0)/2; for n=1:p somme=somme+a(n)*cos(n*theta)*exp(-n^2*t(i)); end drawlater; subplot(2,2,i); plot(theta,somme,'b'); set(gca(),'data_bounds',[0 2*%pi -0.2 1.2]); drawnow; end
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/* * By: Jatin Kumar Mandav * * ASK Modulation * * Inputs: Data or Digital Information Signal. * Carrier Signal Frequency, Carrier Frequency Amplitude * */ function [] = ask_mod(data, freq_carrier, amp_carrier) t = [0:0.001:1] carrier_signal = amp_carrier*sin(2*%pi*freq_carrier*t) zeroes = 0*t modulated_signal = [] for i = 1:length(data) if data(i) == 1 then modulated_signal = [modulated_signal, carrier_signal] else modulated_signal = [modulated_signal, zeroes] end end plot(modulated_signal) title("Modulated Signal") endfunction
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<Profile Name="ProfileEvStress"> <Module Name="EvStress"> <Suite Name="EvStress"> <Test Name="TestAll"/> </Suite> </Module> </Profile>
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exec("swigtest.start", -1); p = getnull(); checkequal(SWIG_this(p), 0, "SWIG_this(p)"); checkequal(funk(p), %T, "funk(p)"); exec("swigtest.quit", -1);
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//chapter13,Example13_2,pg 391 M235U=235//at.mass of 235U m=10^-3 N=6.023*10^23 Eperfi=200*10^6//energy per fission E=Eperfi*1.6*10^-19//energy per fission (in joules) T=10^-6 A=M235U P=((m*N)/A)*(E/T)//power output printf("power of explosion\n") printf("P=%.2f watt",P)
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function graph() a = [0 1 0 0 0 0 0 0; 0 0 1 1 0 0 0 0; 0 0 0 0 1 0 0 0; 0 0 0 0 0 1 0 0; 0 0 0 0 0 0 1 0; 0 0 0 0 0 0 1 0; 0 0 0 0 0 0 0 1; 0 0 0 0 0 0 0 0] disp(a, 'a') a = a + a' disp(a, 'a') [nl, nc] = size(a) n = nl teta = [0 : 2*%pi/n :(n-1)* 2*%pi/n] x = cos(teta) y = sin(teta) plot2d(x, y, -9) plot2d(-2, -2, 0) plot2d(2, 2, 0) for i = 1 : n xstring(x(i), y(i), string(i)) end k = 0 for i = 1 : n for j = i : n if a(i, j) == 1 k = k+1 b(k, 1) = i b(k, 2) = j end end end m = k for k = 1: m plot2d([x(b(k, 1)), x(b(k, 2))], [y(b(k, 1)), y(b(k, 2))], 1) end global('pre', 'pos', 'npre', 'npos', 'ordemdfs', 'ordem') pre = zeros(1, n) pos = zeros(1, n) ordem = zeros(1, n) npre = 1 npos = 1 dfs(a, 1) disp(ordem, 'ordem') endfunction function dfs(a, v) global('pre', 'pos', 'npre', 'npos', 'ordem') pre(v) = npre; ordem(npre) = v npre = npre+1 for i = 1: n if a(v, i) == 1 && pre(i) == 0 dfs(a, i) end end pos(v) = npos; npos = npos+1 endfunction
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(unwatch all) (clear) (dribble-on "Actual//gnrcerr.out") (batch "gnrcerr.bat") (dribble-off) (clear) (open "Results//gnrcerr.rsl" gnrcerr "w") (load "compline.clp") (printout gnrcerr "gnrcerr.bat differences are as follows:" crlf) (compare-files "Expected//gnrcerr.out" "Actual//gnrcerr.out" gnrcerr) (close gnrcerr)
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//Chapter 11 //page no 386 //given clc; clear all; q=4.9*10^-18; //in m/W.GHz raman gain slope f=100; //in GHz A=50*10^-6; //cross sectional area in micro meter square P0=3.5; //in mW Le=10*10^3; G=q*f*10^6/2/A; N=20; mprintf("\n G = %e ",G); CT=N*(N-1)*(P0*10^-3*G*Le)/2; printf("\n CT(L) = %0.2f ",CT);
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load DMux.hdl, output-file DMux.out, output-list in sel a b; set in 0, set sel 0, eval, output; set sel 1, eval, output; set in 1, set sel 0, eval, output; set sel 1, eval, output;
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function [] = kiks_gui_staticbtn() // Display mode mode(0); // Display warning for floating point exception ieee(1); // ----------------------------------------------------- // (c) 2000-2004 Theodor Storm <theodor@tstorm.se> // http://www.tstorm.se // ----------------------------------------------------- global("KIKS_GUI_HDL","KIKS_TIMESCALE","KIKS_updatelmp"); KIKS_updatelmp = -1; KIKS_TIMESCALE = -1; // !! L.12: Matlab function findobj not yet converted, original calling sequence used // L.12: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","update_frame"); // !! L.13: Matlab function set not yet converted, original calling sequence used // L.13: Name conflict: function name changed from set to %set set(H,"BackgroundColor",[0.3,0.3,0.3]); // !! L.14: Matlab function findobj not yet converted, original calling sequence used // L.14: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","update_text"); // !! L.15: Matlab function set not yet converted, original calling sequence used // L.15: Name conflict: function name changed from set to %set set(H,"BackgroundColor",[0.3,0.3,0.3]); // !! L.17: Matlab function findobj not yet converted, original calling sequence used // L.17: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","button_dynamic"); // !! L.18: Matlab function set not yet converted, original calling sequence used // L.18: Name conflict: function name changed from set to %set set(H,"Value",0); // !! L.19: Matlab function findobj not yet converted, original calling sequence used // L.19: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","button_real"); // !! L.20: Matlab function set not yet converted, original calling sequence used // L.20: Name conflict: function name changed from set to %set set(H,"Value",0); // !! L.21: Matlab function findobj not yet converted, original calling sequence used // L.21: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","button_static"); // !! L.22: Matlab function set not yet converted, original calling sequence used // L.22: Name conflict: function name changed from set to %set set(H,"Value",1); // !! L.24: Matlab function findobj not yet converted, original calling sequence used // L.24: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","step_popup"); // !! L.25: Matlab function set not yet converted, original calling sequence used // L.25: Name conflict: function name changed from set to %set set(H,"Enable","on"); // !! L.26: Matlab function findobj not yet converted, original calling sequence used // L.26: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","stat_popup"); // !! L.27: Matlab function set not yet converted, original calling sequence used // L.27: Name conflict: function name changed from set to %set set(H,"Enable","on"); // !! L.29: Matlab function findobj not yet converted, original calling sequence used // L.29: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","acc_popup"); // !! L.30: Matlab function set not yet converted, original calling sequence used // L.30: Name conflict: function name changed from set to %set set(H,"Enable","off"); // !! L.31: Matlab function findobj not yet converted, original calling sequence used // L.31: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","limit_popup"); // !! L.32: Matlab function set not yet converted, original calling sequence used // L.32: Name conflict: function name changed from set to %set set(H,"Enable","on"); // !! L.33: Matlab function findobj not yet converted, original calling sequence used // L.33: Name conflict: function name changed from findobj to %findobj H = findobj("Tag","int_check"); // !! L.34: Matlab function set not yet converted, original calling sequence used // L.34: Name conflict: function name changed from set to %set set(H,"Enable","on"); kiks_gui_getstatlistbox; endfunction
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// Exa 3.11 clc; clear; close; format('v',6) // Given data I_Z = 0.2;// in A R = 10;// in ohm V_Z = 8 + (R*I_Z);// in V I_Lmin = V_Z/R;// in A I_Zmax = 0.2;//in A Vimax = 15;// in V // The minimum value of R Rimin = (Vimax-V_Z)/(I_Zmax+I_Lmin);// in ohm disp(Rimin,"The minimum value of R in ohm is"); // Note: The calculation in the book is not accurate, So the answer in the book is not accurate.
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// Initilization of variables v_A=5 // m/s // speed of ship A v_B=2.5 // m/s // speed of ship B theta=135 // degree // angle between the two ships // Calculations // Here, OA=v_A // m/s OB=v_B // m/s // The magnitude of relative velocity is given by cosine law as, AB=sqrt((OA^2)+(OB^2)-(2*OA*OB*cosd(theta))) // m/s // where AB gives the relative velocity of ship B with respect to ship A // Applying sine law to find the direction, Let alpha be the direction of the reative velocity, then alpha=asind((OB*sind(theta))/(AB)) // degree // Results clc printf('The magnitude of relative velocity of ship B with respect to ship A is %f m/s \n',AB) printf('The direction of the relative velocity is %f degree \n',alpha)
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//Example 6.22 clc clear x = 3:8; y = [0.205 0.24 0.259 0.262 0.25 0.224]; n = length(x); del = %nan*ones(n,5); del(:,1) = y'; for j = 2:5 for i = 1:n-j+1 del(i,j) = del(i+1,j-1) - del(i,j-1); end end X = poly(0, "X"); x0 = x(1); y0 = y(1); h = x(2) - x(1); p = (X-x0)/h; del0 = del(1,:); del0 = round(del0*10^4)/10^4; del0 = del0(1:find(del0==0)-1); Y = 0; for i = 0:length(del0)-1 t = 1; for j = 1:i t = t * (p-j+1); end Y = Y + t*del0(i+1)/factorial(i); end disp(Y,"y = ") dydx = derivat(Y); minx = roots(dydx); miny = round(horner(Y,minx)*10^5)/10^5; disp(minx,"min_x = ") disp(miny,"min_y = ") //min_y value is incorrectly displayed in textbook as 0.25425 instead of 0.26278
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disp("Part a"); l=100; d=2*10^(-3); ro=1.72*10^(-8); a=%pi*(d^2)/4; r=ro*l/a; disp("the resistance (in Ω) of copper wire is"); disp(r); disp("Part b"); ro1=2.63*10^(-8); r1=r*ro1/ro; disp("the resistance (in Ω) of aluminium wire is"); disp(r1);
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clear; clc; //Example 7.9 r=2600; C1=2*10^-6; C2=0.1*10^-6; fB=1/(2*%pi*r*(C1+C2)); printf('\n3dB frequency=%.2f MHz\n',fB)
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// Scilab code Ex5.3: Pg.196-197 (2008) clc; clear; E_k = 150; // Kinetic energy of a cosmic ray proton, GeV h = 6.63e-034; // Plank's constant, J-s m = 1.67e-027; // Mass of proton, kg c = 3e+08; // Velocity of light, m/s E_0 = 0.938; // Rest energy of the proton, GeV lamda_c = h/(m*c); // Compton wavelength of proton, m r = E_k/E_0; // Ratio of kinetic energy to rest energy of proton // Since this value on the curve corresponds to about 6e-03 on the axis, therefore r_w = 6e-03; // Ratio of de broglie wavelength of proton to its compton wavelength lamda = r_w*lamda_c; // de Broglie wavelength of the proton, m printf("\nThe de-Broglie wavelength of cosmic ray proton = %3.1e m = %3.1e fm",lamda, lamda*1e+15); // Result // The de-Broglie wavelength of cosmic ray proton = 7.9e-018 m = 7.9e-003 fm
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//el algoritmo fue interpretado de la pagina http://www.mat.ucm.es/~fmacia/Docencia/MN/Matlab/root/hibrido.pdf function Hibrido(f,a,b,itx,e) //f es la función que se ingresara entre comillas //a es un punto //b es un punto //e es la tolerancia //itx es el numero maximo de iteraciones k=2; o(1)=a; o(2)=b; A(1)=0; A(2)=a; printf('+-----------+----------------------+----------------------+\n'); printf('| Iteracion | r | error |\n'); printf('+-----------+----------------------+----------------------+\n'); printf('| %9d | %20.15f | %20.15f |\n',1,o(1),e); while k<itx xn=o(k); x=xn fx=evstr(f); an=A(k); x=an fa=evstr(f); et=abs(an-xn); if(et>=e) xnm=o(k-1); x=xnm fmx=evstr(f); deltaB=(an-xn)/2; difdiv=(fx-fmx)/(xn-xnm) if (difdiv~=0)//aca va un ~= deltaS=-(fx/difdiv); if((deltaS*deltaB)>0)&(abs(deltaS)<abs(deltaB)) o(k+1)=xn+deltaS; printf('| %9d | %20.15f | %20.15f |\n',k,o(k+1),et); else o(k+1)=xn+deltaB; printf('| %9d | %20.15f | %20.15f |\n',k,o(k+1),et); end else o(k+1)=xn+deltaB; printf('| %9d | %20.15f | %20.15f |\n',k,o(k+1),et); end xmm=o(k+1);//esto es un x+1 segun el pseudo algoritmo x=xmm fxm=evstr(f); if(fa*fxm)<0 A(k+1)=an; else A(k+1)=xn; end k=k+1; Y(k)=k; else printf('no hay raiz, perdon'); k=itx; end end plot(Y,o); endfunction
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// Scilab Code Ex2.14 Ratio of masses of a proton and an electron: Pg:54 (2008) RH = 1.09678e+07; // Rydberg constant for hydrogen, per metre RHe = 1.09722e+07; // Rydberg constant for helium, per metre MH_m_ratio = (RH - 1/4*RHe)/(RHe - RH); // Ratio of mass of a proton to that of an electron printf("\nThe ratio of mass of a proton to that of an electron = %4d", MH_m_ratio); // Result // The ratio of mass of a proton to that of an electron = 1869
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load complemento.hdl, output-file complemento.out, compare-to complemento.cmp, output-list ah%B1.16.1 al%B1.16.1 sh%B1.16.1 sl%B1.16.1; set ah %B0000000000000000, set al %B0101101111101101, eval, output; set ah %B0000000000000000, set al %B1011011000110010, eval, output; set ah %B0000000000000000, set al %B0010111011110001, eval, output; set ah %B1111111111111111, set al %B1011011011010000, eval, output; set ah %B0000000000000000, set al %B0001011000010010, eval, output; set ah %B0000000000000000, set al %B0001110001011110, eval, output; set ah %B1111111111111111, set al %B0111011011001000, eval, output; set ah %B1111111111111111, set al %B1101011110111100, eval, output; set ah %B0000000000000000, set al %B1000111111100011, eval, output; set ah %B1111111111111111, set al %B0111001001011101, eval, output;
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//Ex6_10 : //Color Balancing. // Version : Scilab 5.4.1 // Operating System : Window-xp, Window-7 //Toolbox: Image Processing Design 8.3.1-1 //Toolbox: SIVP 0.5.3.1-2 //Reference book name : Digital Image Processing //book author: Rafael C. Gonzalez and Richard E. Woods clc; close; clear; xdel(winsid())//to close all currently open figure(s). ////////////////// Tonal Correction for the Flat Image //////////////////////// Color=imread("Ex6_10.tif"); Color=imresize(Color,0.25); [nr nc]=size(Color); figure,ShowColorImage(Color,'Gray Image'); title('Original Image','color','blue','fontsize',4); C=255-Color(:,:,1); M=255-Color(:,:,2); Y=255-Color(:,:,3); ///////////////////// Color Balance Correction in Cyan Component ////////////////////// D=0:1/256:1; H1=1*D^2.5; // Transfer Function (Design from the Gamma Funcetion). H2=1*D^0.5; // Transfer Function (Design from the Gamma Funcetion). figure,subplot(211),plot(H1); xlabel('Intensity'); ylabel('Magnitude'); title('HSI Intensity Transformation Function(Heavy in Cyan)'); subplot(212),plot(H2); xlabel('Intensity'); ylabel('Magnitude'); title('HSI Intensity Transformation Function (Weak in Cyan)','color','blue','fontsize',4); C_Modify=[]; for i=1:nr for j=1:nc C_Modify1(i,j,1)=H1(uint16(C(i,j,1))+1); C_Modify2(i,j,1)=H2(uint16(C(i,j,1))+1); end end Balance_Image1(:,:,1)=C_Modify1; Balance_Image1(:,:,2)=M; Balance_Image1(:,:,3)=Y; figure,ShowColorImage(Balance_Image1,'RGB Image'); title('Color Balanced image','color','blue','fontsize',4); Balance_Image2(:,:,1)=C_Modify2; Balance_Image2(:,:,2)=M; Balance_Image2(:,:,3)=Y; figure,ShowColorImage(Balance_Image2,'RGB Image'); title('Color Balanced image','color','blue','fontsize',4); ///////////////////// Color Balance Correction in Megenta Component ////////////////////// D=0:1/256:1; H1=1*D^2.5; // Transfer Function (Design from the Gamma Funcetion). H2=1*D^0.5; // Transfer Function (Design from the Gamma Funcetion). figure,subplot(211),plot(H1); xlabel('Intensity'); ylabel('Magnitude'); title('HSI Intensity Transformation Function(Heavy in Megenta)','color','blue','fontsize',4); subplot(212),plot(H2); xlabel('Intensity'); ylabel('Magnitude'); title('HSI Intensity Transformation Function (Weak in Megenta)','color','blue','fontsize',4); for i=1:nr for j=1:nc Y_Modify1(i,j,1)=H1(uint16(Y(i,j,1))+1); Y_Modify2(i,j,1)=H2(uint16(Y(i,j,1))+1); end end Balance_Image1(:,:,1)=255-C; Balance_Image1(:,:,2)=255-M; Balance_Image1(:,:,3)=255-Y_Modify1; figure,ShowColorImage(Balance_Image1,'RGB Image'); title('Color Balanced image','color','blue','fontsize',4); Balance_Image2(:,:,1)=255-C; Balance_Image2(:,:,2)=255-M; Balance_Image2(:,:,3)=255-Y_Modify2; figure,ShowColorImage(Balance_Image2,'RGB Image'); title('Color Balanced image','color','blue','fontsize',4); ///////////////////// Color Balance Correction in Yellow Component ////////////////////// D=0:1/256:1; H1=1*D^2.5; // Transfer Function (Design from the Gamma Funcetion). H2=1*D^0.5; // Transfer Function (Design from the Gamma Funcetion). figure,subplot(211),plot(H1); xlabel('Intensity'); ylabel('Magnitude'); title('HSI Intensity Transformation Function(Heavy in Yellow)','color','blue','fontsize',4); subplot(212),plot(H2); xlabel('Intensity'); ylabel('Magnitude'); title('HSI Intensity Transformation Function (Weak in Yellow)','color','blue','fontsize',4); for i=1:nr for j=1:nc M_Modify1(i,j,1)=H1(uint16(M(i,j,1))+1); M_Modify2(i,j,1)=H2(uint16(M(i,j,1))+1); end end Balance_Image1(:,:,1)=255-C; Balance_Image1(:,:,2)=255-M_Modify1; Balance_Image1(:,:,3)=255-Y; figure,ShowColorImage(Balance_Image1,'RGB Image'); title('Color Balanced image','color','blue','fontsize',4); Balance_Image2(:,:,1)=255-C; Balance_Image2(:,:,2)=255-M_Modify2; Balance_Image2(:,:,3)=255-Y; figure,ShowColorImage(Balance_Image2,'RGB Image'); title('Color Balanced image','color','blue','fontsize',4);
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clear; clc; // A Textbook on HEAT TRANSFER by S P SUKHATME // Chapter 7 // Heat Exchangers // Example 7.4(b) // Page 302 printf("Example 7.4(b), Page 302 \n \n"); // Using Mean Temperature Difference approach m_hot = 10 ; // [kg/min] m_cold = 25 ; // [kg/min] hh = 1600 ; // [W/m^2 K], Heat transfer coefficient on hot side hc = 1600 ; // [W/m^2 K], Heat transfer coefficient on cold side Thi = 70 ; // [C] Tci = 25 ; // [C] The = 50 ; // [C] // Heat Transfer Rate, q q = m_hot/60*4179*(Thi-The); // [W] // Heat gained by cold water = heat lost by the hot water Tce = 25 + q*1/(m_cold/60*4174); // [C] // Using equation 7.5.13 Tm = ((Thi-Tci)-(The-Tce))/log((Thi-Tci)/(The-Tce)); // [C] U = 1/(1/hh + 1/hc); // [W/m^2 K] A = q/(U*Tm); // Area, [m^2] m_hot = 20 ; // [kg/min] // Flow rate on hot side i.e. 'hh' is doubled hh = 1600*2^0.8 ; // [W/m^2 K] U = 1/(1/hh + 1/hc); // [W/m^2 K] m_hC_ph = m_hot/60*4179 ; // [W/K] m_cC_pc = m_cold/60*4174 ; // [W/K] // Therefore C = m_hC_ph/m_cC_pc ; NTU = U*A/m_hC_ph ; printf("NTU = %f \n",NTU); // From equation 7.6.8 e = [1 - exp(-(1+C)*NTU)]/(1+C) ; // Therefore (Thi - The)/(Thi - Tci) = e , we get The = Thi - e*(Thi - Tci); // [C] // Equating the heat lost by water to heat gained by cold water , we get Tce = Tci + [m_hC_ph*(Thi-The)]/m_cC_pc; printf("Exit temperature of cold and hot stream are %f C and %f C respectively.",Tce,The);
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// Modified by Minho Kim (9 Oct 2014) load Decoder4Way.hdl, output-file Decoder4Way.out, compare-to Decoder4Way.cmp, output-list in%B2.2.2 out%B1.4.1; set in %B00, eval, output; set in %B01, eval, output; set in %B10, eval, output; set in %B11, eval, output;
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//Chapter 9, Problem 6 clc; B=1.4; //flux density l=12*10^-2; //length N=80; //no of turns n=1200/60; //rotation in sec E1=90; //emf r=(8*10^-2)/2; Q90=%pi/2; //calculating velocity v=2*%pi*n*r; //calculating maximum emf E=2*N*B*v*l*sin(Q90); //calculating velocity with emf 90V v=E1/(2*N*B*l*sin(Q90)); //calculating speed of coil w=v/r; w1=(w*60)/(2*%pi); disp("(a)"); printf("Maximum emf induced = %f V",E); disp("(b)"); printf("Speed of coil in rev/min = %d rev/min",w1);
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clc e=1/10 // in link k= sqrt (100*e/1.5) printf('a)The slope in degrees is = %f\n',k) n=sqrt(50/e) printf(' b)Max slope is 1 in %f',n)
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//Testing for complex inputs(exception handling) a=2+1*%i; rc2is(a); //Output //--error 10000 //Input reflection coefficients are not real //at line 33 of function rc2is called by : //rc2is(a);
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clear; clc; close; Gdb = 100; Ratio_V2_by_V1 = 10^(Gdb/20); disp(Ratio_V2_by_V1,'Magnitude gain = ');
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//Variable declaration n=8; //number of atoms a=5.62*10**-10; //lattice constant(m) M=72.59; //atomic weight(kg) Na=6.02*10**26; //avagadro number //Calculation rho=n*M/(a**3*Na); //density(kg/m**3) //Result printf('density is %0.3f kg/m**3 \n',(rho))
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// chapter 5 // example 5.3 // Determine series resistance and safe highest frequency // page-175 clear; clc; // given I_T=120; // in A (total current) C_gs1=2200; // in pF (gate to source capacitance of MOSFET 1) C_gd1=390; // in pF (gate to drain capacitance of MOSFET 1) L_g1=2; // in nH (stray inductance of MOSFET 1) C_gs2=2700; // in pF (gate to source capacitance of MOSFET 2) C_gd2=330; // in pF (gate to drain capacitance of MOSFET 2) L_g2=2.3; // in nH (stray inductance of MOSFET 2) // calculate C_gs1=C_gs1*1E-12; // changing unit from pF to F C_gd1=C_gd1*1E-12; // changing unit from pF to F L_g1=L_g1*1E-9; // changing unit from nF to F C_gs2=C_gs2*1E-12; // changing unit from pF to F C_gd2=C_gd2*1E-12; // changing unit from pF to F L_g2=L_g2*1E-9; // changing unit from nF to F f1=1/(2*%pi*sqrt(L_g1*(C_gs1+C_gd1))); // calculation of oscillating frequency of MOSFET 1 f2=1/(2*%pi*sqrt(L_g2*(C_gs2+C_gd2))); // calculation of oscillating frequency of MOSFET 1 f_h=min(f1,f2)/10; // calculation of safe highest frequency Rg=1/(2*%pi*(C_gs1+C_gd1)*f_h); // calculation of series resistance in the gate f_h=f_h*1E-6; // changing unit from Hz to MHz printf("\nThe oscillating frequency of MOSFET 1 is \t f1=%.2E Hz",f1); printf("\nThe oscillating frequency of MOSFET 2 is \t f2=%.2E Hz",f2); printf("\n\n Since the safe highest frequency should be at least 1 decade lower than oscillating frequency, therefore the safe highest frequency is \t %.f MHz",f_h); printf("\n\nThe series resistance in the gate terminal of both MOSFET is \t Rg=%.2f ohm",Rg); // Note: The answer for the series resistance varies due to precise calculation
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//page 161 //Example 5.8 clc; clear; close; A = [1 2;3 4]; disp(A,'A = '); d = det(A); disp(d,'det A = ','Determinant of A is:'); ad = (det(A) * eye(2,2)) / A; disp(ad,'adj A = ','Adjoint of A is:'); disp('Thus, A is not invertible as a matrix over the ring of integers.'); disp('But, A can be regarded as a matrix over field of rational numbers.'); in = inv(A); //The A inverse matrix given in book has a wrong entry of 1/2. It should be -1/2. disp(in,'inv(A) = ','Then, A is invertible and Inverse of A is:'); //end
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function s = simp_comp(f,a,b,M) //intervalos equiespaciados h=(b-a)/M; sump=0; sumi=0; //sumatorias for (i=1:M-1) //calculamos el valor de f(xi) y=f(a+(i*h)); //verificamos si i es par o impar r=modulo(i,2); if (r==0) then //par sump=sump+y; else //impar sumi=sumi+y; end end s=(h/3)*(f(a)+f(b)+2*(sump)+4*(sumi)); endfunction
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<?xml version="1.0" encoding="utf-8"?> <test> <description>desc P=10</description> <executable>APESolver</executable> <parameters>APE_2DPulseAdv_WeakDG_MODIFIED.xml</parameters> <files> <file description="Session File">APE_2DPulseAdv_WeakDG_MODIFIED.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="p" tolerance="1e-4">6.77218</value> <value variable="u" tolerance="1e-7">0.00160109</value> <value variable="v" tolerance="1e-7">0.00163104</value> </metric> <metric type="Linf" id="2"> <value variable="p" tolerance="1e-4">30.1206</value> <value variable="u" tolerance="1e-7">0.00609606</value> <value variable="v" tolerance="1e-7">0.00607659</value> </metric> </metrics> </test>
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// calculate damping factor, time constant, error and time lag // calculate damping factor, natural frequency, time constant, error and time lag clc; Mp1=20/40; Mp2=10/40; Mp3=5/40; Eta=0.225; disp(Eta,'damping factor') Td=1.2; wd=2*%pi/Td; wn=wd/[(1-Eta^2)^0.5]; tc=1/wn; disp(tc,'time constant(s)') ess=2*Eta/wn; ess5=5*ess; disp(ess5,'error for 5mm/s ramp(mm)') Tlag=2*Eta*tc; disp(Tlag,'time lag(s)') Eta1=Eta*(0.5)^0.5; disp(Eta1,'New damping factor') Td=1.2; wn1 = wn*(0.5)^0.5; disp(wn1,'New natural frequency(rad/s)') tc1=1/wn; disp(tc1,'New time constant(s)') ess51=ess5; disp(ess51,'new error for 5mm/s ramp(mm)') Tlag1=Tlag; disp(Tlag1,'new time lag(s)');
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// Iintilization of variables r=250 // m // radius of the curved road a_t=0.6 // m/s^2 // tangential acceleration a=0.75 // m/s^2 // total acceleration attained by the car // Calculations a_n=sqrt(a^2-a_t^2) // m/s^2 v=sqrt(a_n*r) // m/s // Using v=u+a*t u=0 t=v/a_t // seconds // Now using v^2-u^2=2*a*s s=v^2/(2*a_t) // m // Results clc printf('The distance traveled by the car is %f m \n',s) printf('The time for which the car travels is %f seconds \n',t)
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//Example 8.2 // Numerical Aperture & acceptance angle clc; //given data : u1=1.62;//refractive index of core u2=1.52;// refractive index of clad A=asin(sqrt(u1^2-u2^2));// acceptance angle in radian NA=sin(A);// numerical aperture A=A*180/%pi;// to convert in degree disp(A,"Acceptance angle in degree") disp(NA,"Numerical Aperture")
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clc clear printf('example 1.6 page number 27 \n\n') //to find vapor pressre of ethyl alchohal pa1 = 23.6; //VP of ethyl alchohal at 10 degree C pa3=760 //VP of ethyl alchohal at 78.3 degree C in mm Hg pb1 = 9.2 //VP of ethyl water at 10 degree C in mm Hg pb3=332 //VP of ethyl water at 78.3 degree C in mm Hg C=(log10(pa1/pa3)/(log10(pb1/pb3))); pb2=149 //VP of water at 60 degree C in mm Hg pas=(pb3/pb2); pa=C*log10(pas); pa2=pa3/(10^pa); printf("vapor pressure of ethyl alcholoh at 60 degree C = %f mm Hg",pa2)
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clc; clear all; hb=input("Enter the height of base station antenna:") hm=input("Enter the height of mobile station antenna:") Gt=input("Gain of the transmitting antenna:") Gr=input("Gain of the receiving antenna:") dist=input("Enter the distance between transmitting and receiving antenna:") Amu=24 f1=input("Enter the first frequency value:") f2=input("Enter the second frequency value:") f3=input("Enter the third frequency value:") f4=input("Enter the fourth frequency value:") f5=input("Enter the fifth frequency value:") d=[1:1:dist]' //////OUTDOOR PROPAGATION MODEL HATA MODEL/////// d=[1:1:dist]' Ch=0.8 + (1.1*log10(f1)-0.7)*hm - 1.56*log10(f1) Lp1 = 69.55 + 26.16*log10(f1) - 13.82*log10(hb) - Ch + [44.9 - 6.55*log10(hb)]*log10(d) Ch=0.8 + (1.1*log10(f2)-0.7)*hm - 1.56*log10(f2) Lp2 = 69.55 + 26.16*log10(f2) - 13.82*log10(hb) - Ch + [44.9 - 6.55*log10(hb)]*log10(d) Ch=0.8 + (1.1*log10(f3)-0.7)*hm - 1.56*log10(f3) Lp3 = 69.55 + 26.16*log10(f3) - 13.82*log10(hb) - Ch + [44.9 - 6.55*log10(hb)]*log10(d) Ch=0.8 + (1.1*log10(f4)-0.7)*hm - 1.56*log10(f4) Lp4 = 69.55 + 26.16*log10(f4) - 13.82*log10(hb) - Ch + [44.9 - 6.55*log10(hb)]*log10(d) Ch=0.8 + (1.1*log10(f5)-0.7)*hm - 1.56*log10(f5) Lp5 = 69.55 + 26.16*log10(f5) - 13.82*log10(hb) - Ch + [44.9 - 6.55*log10(hb)]*log10(d) figure; plot(d,[Lp1 Lp2 Lp3 Lp4 Lp5]); xlabel('x--> D (distance in Km)','fontsize',4); ylabel('y--> Lp (path loss)','fontsize',4); title('Hata model','fontsize',7); hl=legend(["200MHZ","400MHZ","600MHZ","800MHZ","1000MHZ"],4);
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// 15.01.01 function Out=Bezier(varargin) Nargs=length(varargin); Ptlist=varargin(1); Ctrlist=varargin(2); Num=10; for J=3:Nargs Tmp=varargin(J); K=mtlb_findstr(Tmp,'='); Tmp1=strsplit(Tmp,[K-1,K]); Tmp2=ascii(Tmp1(1,1)); Lhs=char(Tmp2(1)); if Lhs=="N" then Num=evstr(Tmp1(3,1)); end; end; if length(Num)==1 Num=Num*ones(1:length(Ctrlist)) end; Out=[]; for ii=1:length(Ctrlist) Tmp1=[Ptlist(ii),Ptlist(ii+1)]; Tmp2=Ctrlist(ii); if ii==1 then St=0 else St=1 end; for J=St:Num(ii) Tmp=Bezierpt(J/Num(ii),Tmp1,Tmp2); Out=[Out;Tmp]; end; end; endfunction;
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//Controllers and Their Optimisation// //Example 12.5// G=6;//smaller time constant in ms// T1=80;//bigger time constant in ms// Tn=T1;//time constant of the controller in ms// printf('Time constant of the controller=Tn=%fms',Tn); V=T1/(2*G);//gain of the control system// printf('\nGain of the control system=V=%f',V); Wn=1/(sqrt(2)*G);//Natural frequency of the system in rad/ms// printf('\nNatural frequency of the system=Wn=%frad/ms',Wn); Tf=4.7*G;//time taken by the system to achiecve its desired output for firsttime// printf('\ntime taken by the system to achieve its desired value=Tf=%fms',Tf); printf('\nMaximum overshoot for a symmetrically optimised system is 4.3 percent'); Tmax=6.24*G;//time at which maximum overload will occur in ms// printf('\nTime at which maximum overload will occur=Tmax=%fms',Tmax);