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-chain [[2,2,1,0],[1,1,1,1],[1,2,2,0],[2,3,2,0]] [3,4,5,6] 3 1 [[2,2,1,0],[1,1,1,1],[1,2,2,0],[2,3,2,0]],det=-1 [3,4,5,6], chain 8 => [19,18,21,28] => [95,86,97,134] => [459,412,461,642] => [2203,1974,2205,3076] => [10559,9458,10561,14738] => [50595,45316,50597,70614] => [242419,217122,242421,338332] => [1161503,1040294,1161505,1621046]
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Wb = 10^-4; Vcb1 = 1; Vcb2 = 5; q = 1.6*10^-19; Db = 20; Vbe = 0.7; kT = 26*10^-3; //in eV ni = 1.5*10^10; Nab = 5*10^16; Nde = 5*10^15; eps0 = 8.84*10^-14; //in F/m eps = 11.9*eps0; Vbi = kT*log(Nab*Nde/ni^2) disp(Vbi,"Built in voltage (in V) = ") dW2 = 2*eps*(Vbi+Vcb1)*Nde/(q*Nab*(Nab+Nde)); dW = sqrt(dW2); disp(dW,"The extent of depletion into the base side (in cm) = ") Wbn = Wb - dW; disp(Wbn,"neutral base width (in cm) = ") dW1 = (2*eps*(Vbi+Vcb2)*Nde/(q*Nab*(Nab+Nde)))^0.5; disp(dW1,"When the collector-base voltage increases to 5 V, extent of depletion into the base side (in cm)") Wbn1 = Wb - dW1; disp(Wbn1,"neutral base width (in cm) = ") nbo = ni^2/Nab; disp(nbo,"base minority carrier concentrations (in per cm cube) = ") Jc1 = q*Db*nbo/Wbn*exp(Vbe/kT); disp(Jc1,"For the base-collector bias of 1 V, collector current density (in A/square cm)") Jc2 = q*Db*nbo/Wbn1*exp(Vbe/kT); disp(Jc2,"For the base-collector bias of 5 V, collector current density (in A/square cm)") slope = (Jc2-Jc1)/(Vcb2-Vcb1); disp(slope,"The slope of the Jc vs. VCE curve = ") Va = Jc2/slope - (Vcb2+Vbe); disp(Va, "Early voltage (in V) = ")
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clc; clear; m=1.67*10^-27 //mass of particle in kPP L=0.1*10^-9 //width in nm n=3 //quantum number h=6.63*10^-34 //Plancks constant in J-s //calculation //(1) E=(n^2*h^2)/(8*m*L^2) mprintf("The energy of the particle is = %2.2e Joules\n",E) //The answer provided in the textbook is wrong. //(2) lambda=(2*L)/n p=h/lambda mprintf("The momentum of the particle is = %1.2e kg-ms^-1\n",p) //(3) P=((1/L)*(L/3)) //after integration mprintf("The probability of finding particle between x=0 and x=L/3 is = %f",P)
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clear all; clc; funcprot(0); //function to calculate m and delta function [m,delta] = func(a_l,alpha2,theta) m = 0.23*(2*a_l)^2 + alpha2/500; delta = m*theta; endfunction //given data alpha1_ = 50;// in deg alpha2_ = 20;// in deg a_l = 0.5;//percentage s_l = 1.0; eps = 21;//in deg //Calculations theta = alpha1_ - alpha2_; alpha21 = 20;//in deg [m1,delta1] = func(a_l,alpha21,theta); alpha22 = 28.1;//in deg [m2,delta2] = func(a_l,alpha22,theta); alpha23 = 28.6;//in deg [m3,delta3] = func(a_l,alpha23,theta); alpha1 = eps + alpha23; i = alpha1 - alpha1_; alpham = (180/%pi)*atan(0.5*(tan(alpha1*%pi/180) + tan(alpha23*%pi/180))); CL = 2*(s_l)*cos(alpham*%pi/180)*(tan(alpha1*%pi/180) - tan(alpha23*%pi/180)); //Results printf('The fluid deflection = %d deg.',eps); printf('\n The fluid incidence = %.1f deg.',i); printf('\n The ideal lift coefficient at the design point = %.2f',CL);
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clc //initialisation of variables w= 15 //ft D= 15 //ft W= 62.4 //lb/ft^3 a= 120 //degrees h1= 15 //ft h2= 4 ///ft h3= 18 //ft //CALCULATIONS Pu= w*D*W*w/2 hu= ((w*D^3/12)/(w^2*D/2))+w/2 Pd= W*h2*w*h2/2 hd= ((w*h2^3/12)/(h2*h1*(h2/2)))+(h2/2) P= Pu-Pd h= (Pu*(h1-hu)-Pd*(h2-hd))/P F= P/(2*sind(a/4)) RT= F*(h3-(h1/10)-h)/(h3-(h1/5)) RB=F-RT //RESULTS printf ('RB = %.f lb ',RB)
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Syms t,s disp('given') disp('V=e^-t(sint) R1=1,R2=1,C=0.5,L=2') disp('laplace transforming the ckt elements') disp('Total impedance is') z=((2*s^2+5*s+4)/(2*s^2+s+2)) disp(z) disp('laplace transformed voltage is') v=laplace('%e^(-t)*sin(2*t)',t,s) disp(v) disp('The current can be found as v/z') i=v/z disp(i,"The total current in s domain")
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clc; s1=1.7189; v1=0.0978;//m^3 p1=2.01;//bar p2=10;//bar lamda=1.1; v2=v1*(p1/p2)^(1/lamda); s_1=1.7564;//kJ/kg K s_2=1.7847;//kJ/kg K v_1=0.0228;//m^3 v_2=0.0222;//m^3 v_3=0.0233;//m^3 s2=s_1+[(v_1-v_2)/(v_3-v_2)]*(s_2-s_1) disp("increase in entropy"); disp("kJ/kg K",s2-s1)
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//control systems by Nagoor Kani A //Edition 3 //Year of publication 2015 //Scilab version 6.0.0 //operating systems windows 10 // Example 6.15 clc; clear; s=poly(0,'s') //dominent pole sd=-zeta*w=%i*w*sqrt(1-zeta^2) zeta=0.9//damping ratio w=2.5//natural frequency of osciilation in rad/sec sd=(-zeta*w)+((%i*w)*sqrt(1-zeta^2)) disp(sd,'the dominennt pole is') d=abs(sd) disp(d,'the value of d is ') betaa=phasemag(sd) disp(betaa,'the value of betaa is;') h=syslin('c',4/(s+1)*(s+5))//given tranfer function G(s) //find magnitude and phase of G(s) at s=sd a=4/((1+sd)*(5+sd)) ad=abs(a) disp(ad,'the value of ad is') phid=phasemag(a) disp(phid,'the value of phid is') ki=-(d*sind(phid))/(ad*sind(betaa))//integral constant disp(ki,'the integral constant is') kp=(-sind(betaa+phid))/(ad*sind(betaa))-(2*ki*cosd(betaa))/d //proportional constant disp(kp,'the proportional constant is') hc=syslin('c', 2.02*(s+1.19)/s)//transfer function of PD controller is kpof +kd*s disp(hc,'transfer function of PI controller is') hcmp=syslin('c',h*hc)//transfer function compensated system disp(hcmp,'transfer function compensated system ')
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from elist.elist import * from xdict.jprint import pobj from xdict.jprint import pdir #1. __init__(alist) l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) #2. __repr__ l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) l ltree pobj(ltree.showlog) #3. tree(**kwargs) l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) pathlists = ltree.tree() pathlists pathlists = ltree.tree(leaf_only=True) pathlists pathlists = ltree.tree(leaf_only=True,from_lv=1,to_lv=2) pathlists pathlists = ltree.tree(non_leaf_only=True) pathlists #4 flatten l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) flat = ltree.flatten() flat ltree.flatWidth ltree.depth #5. dig l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) depthfirst = ltree.dig() depthfirst = ltree.dig(2) depthfirst = ltree.dig(5) #6. level l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) level = ltree.level(1) level = ltree.level(1,leaf_only=True) level = ltree.level(1,non_leaf_only=True) level = ltree.level(2) level = ltree.level(3) #7. include l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) l[3][1][0] ltree.include(3,1,0) l[3][1][2] ltree.include(pathlist = [3,1,2]) #8. __getitem__ l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) ltree[1,0] l[1][0] ltree[3,1,1] l[3][1][1] #9. search from xdict.TestLib.genrand import gen_random_recursive_only_list_data as randlist l = randlist() l = [ 'v_4', 'v_7', 'v_6', 'v_8', [ 'v_7', 'v_1', [ 'v_2', [ [ [ 'v_3', 'v_6', [ 'v_1', 'v_7', [], 'v_3', 'v_2', 'v_8', 'v_3', 'v_8', 'v_8', 'v_7', [], 'v_6', 'v_8', 'v_2' ], 'v_4', 'v_3', 'v_2', 'v_3', 'v_5', 'v_3', 'v_5', [ [], 'v_1' ], 'v_8', 'v_4', 'v_7', 'v_6', [ 'v_4', [], 'v_4', 'v_2', 'v_7', [], 'v_5', 'v_6', 'v_2', 'v_1', 'v_7', 'v_3', [] ], 'v_8', 'v_1', 'v_1', [ 'v_8', 'v_3', [], 'v_6', 'v_7', 'v_2', 'v_2', 'v_1', 'v_5', 'v_7', [], 'v_4', 'v_5', 'v_7', 'v_7', 'v_3', 'v_4', 'v_5', 'v_7', 'v_8' ] ], 'v_4', 'v_5', 'v_6', 'v_4', 'v_3', 'v_4', 'v_1', 'v_2', [ 'v_2', 'v_2', 'v_8', [ 'v_1', 'v_1', 'v_2', [], 'v_7', 'v_4', 'v_4', 'v_8', 'v_6', 'v_8', 'v_3', 'v_5', 'v_6', 'v_7' ], 'v_5', [ 'v_4', 'v_7', 'v_1', [], 'v_8', [], 'v_5', 'v_6', 'v_3', 'v_1', 'v_6', 'v_2', [], 'v_5' ], 'v_2', 'v_7' ], 'v_3', 'v_4', 'v_2', [ [ 'v_1', 'v_3', 'v_2', [], [] ], [ 'v_8', 'v_6', 'v_6', 'v_5' ], 'v_8', 'v_6', [ 'v_3', 'v_8', 'v_8', 'v_5', 'v_6', 'v_2', 'v_1', 'v_4', 'v_5', 'v_2', 'v_2', 'v_8', [], 'v_8', 'v_6' ], 'v_4', 'v_1', 'v_3', 'v_4', [ 'v_2', 'v_4', 'v_6', 'v_5', 'v_1' ], 'v_7', 'v_2', 'v_6', 'v_2', 'v_7', 'v_6', 'v_1', [ 'v_1', [], [], 'v_8', 'v_1' ], [ 'v_5', 'v_6', 'v_3', 'v_3', 'v_5', 'v_3', 'v_6', 'v_5' ] ], [ 'v_5', 'v_6', 'v_1', 'v_7', 'v_7', 'v_4', 'v_7', [ 'v_4', 'v_1', 'v_8', 'v_1', 'v_1', 'v_2', 'v_5', [] ], 'v_5' ], [ 'v_5', 'v_7', 'v_1', 'v_8' ], 'v_1', 'v_5', 'v_4' ], 'v_2', 'v_7', [ 'v_1', 'v_8', 'v_6', 'v_3', 'v_1', [ 'v_5', 'v_6', 'v_6', [ 'v_5', [], 'v_8', [], 'v_6', [], 'v_1', 'v_6', 'v_6', 'v_1', 'v_3', 'v_7', 'v_7', 'v_2', 'v_8', 'v_7', [], [], 'v_1', [] ], 'v_7', 'v_4', 'v_3', [ [], 'v_1', 'v_7', 'v_2', 'v_1', 'v_3', 'v_1', 'v_1', 'v_2', 'v_6', 'v_8', 'v_3' ] ], 'v_7', 'v_1', 'v_4', 'v_2', 'v_2', 'v_7', 'v_3', 'v_4', [ 'v_3', 'v_5', 'v_4', 'v_8', 'v_2', 'v_6', 'v_4', 'v_2', [ 'v_1' ], 'v_8', 'v_7', 'v_5', 'v_6', [ [], [], 'v_2', 'v_8', [], 'v_5', 'v_3', 'v_8', [], 'v_5' ], 'v_6', 'v_6', 'v_8', [ 'v_7', 'v_7', 'v_3', 'v_7', 'v_1', 'v_8', 'v_6', [], 'v_4', 'v_2', 'v_2', 'v_3' ], 'v_6' ] ], 'v_3', 'v_1', 'v_2', 'v_7', 'v_8', 'v_1', 'v_7', 'v_4' ], 'v_7', 'v_1', 'v_4', 'v_6' ], 'v_8', [ 'v_4', 'v_2', 'v_6', 'v_4' ], 'v_4', 'v_6', 'v_4', 'v_2', 'v_3', 'v_5', [ [ 'v_7', 'v_8', 'v_7', 'v_2', 'v_8', 'v_2', 'v_6', 'v_4', 'v_6', 'v_6', [ [ 'v_4', 'v_5', 'v_8', 'v_2', [ 'v_1', 'v_1', 'v_5', [], 'v_6', 'v_3', 'v_3', 'v_2', 'v_1', 'v_1', 'v_1', [], 'v_4', 'v_8', 'v_8' ] ], 'v_1', 'v_1', 'v_8', 'v_1', 'v_2', 'v_2', 'v_1', 'v_1', [ [ 'v_7' ], 'v_4', 'v_4', 'v_3', [ [], 'v_4', 'v_7', 'v_1', 'v_6', 'v_6' ], [ [], 'v_2', 'v_8', 'v_7', 'v_8', 'v_5', 'v_5', 'v_5', 'v_6', [], [], 'v_6', 'v_2', [], 'v_7', 'v_8', 'v_2' ], [ 'v_4', 'v_5', [], 'v_1', [], 'v_1', 'v_6', 'v_5', 'v_3', 'v_6', 'v_4', 'v_2', 'v_7', 'v_6', 'v_3', 'v_3', 'v_8', 'v_3', 'v_5', 'v_8' ], 'v_5', 'v_3', 'v_7', [ 'v_5', [], 'v_2', 'v_3', 'v_8', 'v_5', 'v_1', 'v_4', 'v_5', 'v_5', 'v_3', 'v_4', 'v_5', 'v_2', [], 'v_7', 'v_1', 'v_1', 'v_3', 'v_3' ], 'v_5', 'v_4', 'v_1', 'v_4', 'v_3', 'v_3', 'v_6' ], 'v_1', [ 'v_8', 'v_3', 'v_5', 'v_4', 'v_4', 'v_6', 'v_5', [ 'v_4', 'v_6', 'v_3', 'v_3' ], [ 'v_5', 'v_7', 'v_3', 'v_7', 'v_1', 'v_4', 'v_3', 'v_7', 'v_5', 'v_6', 'v_3', 'v_6', [], [], 'v_6' ], 'v_4', 'v_3', 'v_4' ], 'v_8', 'v_7', 'v_1', 'v_8', 'v_2', 'v_1', 'v_2', [ 'v_6', 'v_5', 'v_2', 'v_5', 'v_2', 'v_7', 'v_3', 'v_5', 'v_2', [ 'v_6', 'v_6', 'v_8', 'v_2', 'v_2', 'v_2', 'v_7', 'v_3', 'v_5', 'v_4', 'v_4', 'v_5' ], 'v_6' ] ], 'v_3', 'v_5', [ 'v_6', 'v_5', [ 'v_4', 'v_3', 'v_6', 'v_7' ], 'v_7', 'v_3', [ 'v_4', 'v_8', 'v_8', 'v_6', 'v_4', 'v_6', 'v_8', [ 'v_4', 'v_8' ], 'v_7', 'v_3', 'v_6', 'v_6', 'v_3', 'v_2', [ 'v_4', [], [], 'v_8', 'v_3', 'v_1', 'v_6', 'v_4', [], 'v_3', 'v_8', 'v_8', 'v_8', [], 'v_2', 'v_8' ] ], 'v_5', 'v_8', 'v_5', 'v_6', 'v_8', 'v_1', 'v_8', 'v_2', [ 'v_5' ] ], 'v_8' ], 'v_8', 'v_3', 'v_4', 'v_2', 'v_8', 'v_4', 'v_8', [ 'v_1', [ 'v_6', 'v_8', 'v_3', 'v_1', [ 'v_4', 'v_4', 'v_3', 'v_4', 'v_6', 'v_5', 'v_7', [ [], 'v_4', 'v_5', 'v_5', 'v_7', 'v_8', 'v_2', 'v_4', 'v_7', [], 'v_1', 'v_1', 'v_6', 'v_6' ], [ 'v_1', 'v_2', 'v_1', 'v_3', 'v_8', 'v_7', 'v_5', 'v_5', 'v_1', 'v_6' ], 'v_6' ], 'v_7', 'v_8', [ 'v_4', [ [], 'v_8', 'v_8', [], 'v_6', 'v_3', 'v_8', 'v_3', 'v_4', 'v_2', [], 'v_4', [] ], [ 'v_8', [], 'v_4', 'v_7', 'v_8', [], 'v_5' ], 'v_1', 'v_4', 'v_7', 'v_5', [ 'v_5', 'v_5', 'v_6', 'v_8', 'v_4', 'v_3', 'v_7', 'v_7', 'v_4', 'v_6', 'v_4', 'v_7', 'v_3', 'v_5', 'v_6' ], 'v_1', 'v_1', 'v_4', [ 'v_4', 'v_5', 'v_7', 'v_7', 'v_4', [], [], 'v_8', 'v_1', 'v_2', 'v_6', [], 'v_6', 'v_1' ], 'v_4' ], [ 'v_5', 'v_4', 'v_1', [ 'v_1', [], 'v_7', 'v_1', 'v_5', 'v_8', [], 'v_6', [], 'v_2', 'v_5', 'v_2', 'v_6', [] ], 'v_4', 'v_5', [ 'v_5', 'v_2', 'v_4', 'v_4' ], 'v_2', [ 'v_5', 'v_7', 'v_3' ], 'v_7', 'v_7', [ 'v_8', 'v_3' ], 'v_2', 'v_3', 'v_3', 'v_1', 'v_8', 'v_3', 'v_6' ], 'v_1', 'v_5', 'v_8', 'v_3', 'v_6', 'v_2' ], 'v_4', 'v_8', 'v_4', [ 'v_4' ], 'v_5', [ 'v_3', 'v_2', [ [ 'v_5', 'v_4', 'v_1', 'v_7', 'v_2', 'v_7', 'v_2', 'v_3', [], [], 'v_8', 'v_1', 'v_7' ], 'v_2', 'v_7', [ 'v_5', 'v_2', 'v_8', 'v_3', 'v_4', 'v_3', 'v_5', [] ], 'v_5', 'v_8', 'v_5', [ [], 'v_3', [], [], 'v_1', 'v_4', 'v_2', 'v_2', 'v_3', 'v_7', [] ], 'v_8', 'v_5', 'v_3' ], 'v_2', 'v_1', 'v_7', 'v_6', 'v_3' ], 'v_3', 'v_7', 'v_8', 'v_4', 'v_5', [ 'v_1', 'v_3', 'v_6', 'v_4', [ 'v_5', [ 'v_8', 'v_6', [], 'v_2' ], 'v_5', 'v_1', 'v_3', 'v_2', 'v_7', 'v_8', [ 'v_8', [], 'v_6', 'v_4', 'v_7' ] ] ], 'v_3', [ 'v_3', 'v_5', 'v_6', 'v_7', [ 'v_7', 'v_6', 'v_1', 'v_4', 'v_8' ] ], 'v_1' ], 'v_4', 'v_6', 'v_3', 'v_7', 'v_1', 'v_8', 'v_3', [ [ 'v_5', 'v_3', 'v_7', 'v_5', [ [ 'v_2', 'v_7', 'v_5', 'v_4' ], 'v_4', [ 'v_2', 'v_8', [], 'v_2', 'v_7', 'v_3', 'v_7' ], 'v_1' ], 'v_3', [ 'v_4', 'v_1', 'v_8', 'v_7', 'v_1', 'v_2', 'v_3', [ [], 'v_3', 'v_4', 'v_2', 'v_5', 'v_5', 'v_7', 'v_6', 'v_1', 'v_1', 'v_2', 'v_8', [], 'v_4' ], 'v_1', 'v_8', 'v_4', 'v_8', 'v_5', 'v_6', [ [], [], 'v_8', 'v_8', [], 'v_3', 'v_4', 'v_4', [], 'v_4', 'v_8' ], 'v_4', [ 'v_7', 'v_5', 'v_3', 'v_7', [], 'v_1' ], 'v_7' ], 'v_1', [ 'v_5', 'v_7', [ [], 'v_5', 'v_6', 'v_2', 'v_1', 'v_3', [], [], 'v_5' ], 'v_5', 'v_3', 'v_8', 'v_5', 'v_7', 'v_3', 'v_3', 'v_2' ], 'v_1', [ 'v_5', 'v_2', 'v_3', [ 'v_6', 'v_4', 'v_3', 'v_1', [], 'v_6', 'v_5', [], 'v_1', 'v_6', 'v_8', 'v_4', 'v_7', 'v_1', 'v_4' ], 'v_4', 'v_2', 'v_7', 'v_3', [ [], [] ], 'v_1', [ 'v_8', 'v_2', 'v_7', 'v_3', 'v_4', 'v_3', 'v_4', 'v_7', 'v_5', [], 'v_6', 'v_8', 'v_1', [] ], 'v_6', 'v_7', 'v_2', 'v_8' ], [ 'v_4', 'v_3', 'v_4', 'v_3', 'v_5', 'v_6', 'v_7', 'v_4', [ 'v_8', 'v_5' ], 'v_3', 'v_8', 'v_1', [ 'v_2', 'v_5', 'v_1', 'v_6', 'v_8', 'v_2', [], 'v_5', 'v_1', 'v_6', 'v_8', 'v_7', 'v_8', 'v_8', 'v_4', 'v_6' ], 'v_5', 'v_2', 'v_5', 'v_2', 'v_5' ], 'v_4', 'v_4', [ [ 'v_4', 'v_4', 'v_7' ], 'v_3', 'v_7', [ [] ], 'v_5', 'v_7', 'v_3', 'v_2', 'v_1', 'v_8', [ [], 'v_2', 'v_3', 'v_4', [], 'v_4', 'v_7', 'v_5', 'v_5', 'v_3', 'v_2' ], 'v_2', 'v_6', 'v_1', 'v_8', 'v_5', [ 'v_7', 'v_4', 'v_2', 'v_3', 'v_2', 'v_4', 'v_8', 'v_7', 'v_2' ] ], 'v_4' ], 'v_2' ], 'v_7', 'v_1' ], [ 'v_1', 'v_7', 'v_1', 'v_6', 'v_2', 'v_2', 'v_5', 'v_4', 'v_3', 'v_3', 'v_6', 'v_8' ], 'v_5' ], 'v_3', 'v_3', [ 'v_6' ], 'v_7', 'v_2', 'v_3', [ 'v_7', 'v_2', 'v_4', 'v_4', 'v_5', 'v_8', 'v_2', 'v_3', 'v_1', 'v_3', [ 'v_5', 'v_2', 'v_8' ] ] ] l = ['v_4', 'v_7', 'v_6', 'v_8', ['v_7', 'v_1', ['v_2', [ [ ['v_3', 'v_6', ['v_1', 'v_7', [], 'v_3', 'v_2', 'v_8', 'v_3', 'v_8', 'v_8', 'v_7', [], 'v_6', 'v_8', 'v_2'], 'v_4', 'v_3', 'v_2', 'v_3', 'v_5', 'v_3', 'v_5', [ [], 'v_1' ], 'v_8', 'v_4', 'v_7', 'v_6', ['v_4', [], 'v_4', 'v_2', 'v_7', [], 'v_5', 'v_6', 'v_2', 'v_1', 'v_7', 'v_3', []], 'v_8', 'v_1', 'v_1', ['v_8', 'v_3', [], 'v_6', 'v_7', 'v_2', 'v_2', 'v_1', 'v_5', 'v_7', [], 'v_4', 'v_5', 'v_7', 'v_7', 'v_3', 'v_4', 'v_5', 'v_7', 'v_8']], 'v_4', 'v_5', 'v_6', 'v_4', 'v_3', 'v_4', 'v_1', 'v_2', ['v_2', 'v_2', 'v_8', ['v_1', 'v_1', 'v_2', [], 'v_7', 'v_4', 'v_4', 'v_8', 'v_6', 'v_8', 'v_3', 'v_5', 'v_6', 'v_7'], 'v_5', ['v_4', 'v_7', 'v_1', [], 'v_8', [], 'v_5', 'v_6', 'v_3', 'v_1', 'v_6', 'v_2', [], 'v_5'], 'v_2', 'v_7'], 'v_3', 'v_4', 'v_2', [ ['v_1', 'v_3', 'v_2', [], [] ], ['v_8', 'v_6', 'v_6', 'v_5'], 'v_8', 'v_6', ['v_3', 'v_8', 'v_8', 'v_5', 'v_6', 'v_2', 'v_1', 'v_4', 'v_5', 'v_2', 'v_2', 'v_8', [], 'v_8', 'v_6'], 'v_4', 'v_1', 'v_3', 'v_4', ['v_2', 'v_4', 'v_6', 'v_5', 'v_1'], 'v_7', 'v_2', 'v_6', 'v_2', 'v_7', 'v_6', 'v_1', ['v_1', [], [], 'v_8', 'v_1' ], ['v_5', 'v_6', 'v_3', 'v_3', 'v_5', 'v_3', 'v_6', 'v_5'] ], ['v_5', 'v_6', 'v_1', 'v_7', 'v_7', 'v_4', 'v_7', ['v_4', 'v_1', 'v_8', 'v_1', 'v_1', 'v_2', 'v_5', []], 'v_5'], ['v_5', 'v_7', 'v_1', 'v_8'], 'v_1', 'v_5', 'v_4' ], 'v_2', 'v_7', ['v_1', 'v_8', 'v_6', 'v_3', 'v_1', ['v_5', 'v_6', 'v_6', ['v_5', [], 'v_8', [], 'v_6', [], 'v_1', 'v_6', 'v_6', 'v_1', 'v_3', 'v_7', 'v_7', 'v_2', 'v_8', 'v_7', [], [], 'v_1', [] ], 'v_7', 'v_4', 'v_3', [ [], 'v_1', 'v_7', 'v_2', 'v_1', 'v_3', 'v_1', 'v_1', 'v_2', 'v_6', 'v_8', 'v_3' ]], 'v_7', 'v_1', 'v_4', 'v_2', 'v_2', 'v_7', 'v_3', 'v_4', ['v_3', 'v_5', 'v_4', 'v_8', 'v_2', 'v_6', 'v_4', 'v_2', ['v_1'], 'v_8', 'v_7', 'v_5', 'v_6', [ [], [], 'v_2', 'v_8', [], 'v_5', 'v_3', 'v_8', [], 'v_5' ], 'v_6', 'v_6', 'v_8', ['v_7', 'v_7', 'v_3', 'v_7', 'v_1', 'v_8', 'v_6', [], 'v_4', 'v_2', 'v_2', 'v_3'], 'v_6']], 'v_3', 'v_1', 'v_2', 'v_7', 'v_8', 'v_1', 'v_7', 'v_4' ], 'v_7', 'v_1', 'v_4', 'v_6'], 'v_8', ['v_4', 'v_2', 'v_6', 'v_4'], 'v_4', 'v_6', 'v_4', 'v_2', 'v_3', 'v_5', [ ['v_7', 'v_8', 'v_7', 'v_2', 'v_8', 'v_2', 'v_6', 'v_4', 'v_6', 'v_6', [ ['v_4', 'v_5', 'v_8', 'v_2', ['v_1', 'v_1', 'v_5', [], 'v_6', 'v_3', 'v_3', 'v_2', 'v_1', 'v_1', 'v_1', [], 'v_4', 'v_8', 'v_8']], 'v_1', 'v_1', 'v_8', 'v_1', 'v_2', 'v_2', 'v_1', 'v_1', [ ['v_7'], 'v_4', 'v_4', 'v_3', [ [], 'v_4', 'v_7', 'v_1', 'v_6', 'v_6' ], [ [], 'v_2', 'v_8', 'v_7', 'v_8', 'v_5', 'v_5', 'v_5', 'v_6', [], [], 'v_6', 'v_2', [], 'v_7', 'v_8', 'v_2' ], ['v_4', 'v_5', [], 'v_1', [], 'v_1', 'v_6', 'v_5', 'v_3', 'v_6', 'v_4', 'v_2', 'v_7', 'v_6', 'v_3', 'v_3', 'v_8', 'v_3', 'v_5', 'v_8'], 'v_5', 'v_3', 'v_7', ['v_5', [], 'v_2', 'v_3', 'v_8', 'v_5', 'v_1', 'v_4', 'v_5', 'v_5', 'v_3', 'v_4', 'v_5', 'v_2', [], 'v_7', 'v_1', 'v_1', 'v_3', 'v_3'], 'v_5', 'v_4', 'v_1', 'v_4', 'v_3', 'v_3', 'v_6' ], 'v_1', ['v_8', 'v_3', 'v_5', 'v_4', 'v_4', 'v_6', 'v_5', ['v_4', 'v_6', 'v_3', 'v_3'], ['v_5', 'v_7', 'v_3', 'v_7', 'v_1', 'v_4', 'v_3', 'v_7', 'v_5', 'v_6', 'v_3', 'v_6', [], [], 'v_6' ], 'v_4', 'v_3', 'v_4' ], 'v_8', 'v_7', 'v_1', 'v_8', 'v_2', 'v_1', 'v_2', ['v_6', 'v_5', 'v_2', 'v_5', 'v_2', 'v_7', 'v_3', 'v_5', 'v_2', ['v_6', 'v_6', 'v_8', 'v_2', 'v_2', 'v_2', 'v_7', 'v_3', 'v_5', 'v_4', 'v_4', 'v_5'], 'v_6'] ], 'v_3', 'v_5', ['v_6', 'v_5', ['v_4', 'v_3', 'v_6', 'v_7'], 'v_7', 'v_3', ['v_4', 'v_8', 'v_8', 'v_6', 'v_4', 'v_6', 'v_8', ['v_4', 'v_8'], 'v_7', 'v_3', 'v_6', 'v_6', 'v_3', 'v_2', ['v_4', [], [], 'v_8', 'v_3', 'v_1', 'v_6', 'v_4', [], 'v_3', 'v_8', 'v_8', 'v_8', [], 'v_2', 'v_8' ]], 'v_5', 'v_8', 'v_5', 'v_6', 'v_8', 'v_1', 'v_8', 'v_2', ['v_5']], 'v_8'], 'v_8', 'v_3', 'v_4', 'v_2', 'v_8', 'v_4', 'v_8', ['v_1', ['v_6', 'v_8', 'v_3', 'v_1', ['v_4', 'v_4', 'v_3', 'v_4', 'v_6', 'v_5', 'v_7', [ [], 'v_4', 'v_5', 'v_5', 'v_7', 'v_8', 'v_2', 'v_4', 'v_7', [], 'v_1', 'v_1', 'v_6', 'v_6' ], ['v_1', 'v_2', 'v_1', 'v_3', 'v_8', 'v_7', 'v_5', 'v_5', 'v_1', 'v_6'], 'v_6' ], 'v_7', 'v_8', ['v_4', [ [], 'v_8', 'v_8', [], 'v_6', 'v_3', 'v_8', 'v_3', 'v_4', 'v_2', [], 'v_4', [] ], ['v_8', [], 'v_4', 'v_7', 'v_8', [], 'v_5'], 'v_1', 'v_4', 'v_7', 'v_5', ['v_5', 'v_5', 'v_6', 'v_8', 'v_4', 'v_3', 'v_7', 'v_7', 'v_4', 'v_6', 'v_4', 'v_7', 'v_3', 'v_5', 'v_6'], 'v_1', 'v_1', 'v_4', ['v_4', 'v_5', 'v_7', 'v_7', 'v_4', [], [], 'v_8', 'v_1', 'v_2', 'v_6', [], 'v_6', 'v_1' ], 'v_4' ], ['v_5', 'v_4', 'v_1', ['v_1', [], 'v_7', 'v_1', 'v_5', 'v_8', [], 'v_6', [], 'v_2', 'v_5', 'v_2', 'v_6', []], 'v_4', 'v_5', ['v_5', 'v_2', 'v_4', 'v_4'], 'v_2', ['v_5', 'v_7', 'v_3'], 'v_7', 'v_7', ['v_8', 'v_3'], 'v_2', 'v_3', 'v_3', 'v_1', 'v_8', 'v_3', 'v_6'], 'v_1', 'v_5', 'v_8', 'v_3', 'v_6', 'v_2' ], 'v_4', 'v_8', 'v_4', ['v_4'], 'v_5', ['v_3', 'v_2', [ ['v_5', 'v_4', 'v_1', 'v_7', 'v_2', 'v_7', 'v_2', 'v_3', [], [], 'v_8', 'v_1', 'v_7' ], 'v_2', 'v_7', ['v_5', 'v_2', 'v_8', 'v_3', 'v_4', 'v_3', 'v_5', []], 'v_5', 'v_8', 'v_5', [ [], 'v_3', [], [], 'v_1', 'v_4', 'v_2', 'v_2', 'v_3', 'v_7', [] ], 'v_8', 'v_5', 'v_3' ], 'v_2', 'v_1', 'v_7', 'v_6', 'v_3'], 'v_3', 'v_7', 'v_8', 'v_4', 'v_5', ['v_1', 'v_3', 'v_6', 'v_4', ['v_5', ['v_8', 'v_6', [], 'v_2'], 'v_5', 'v_1', 'v_3', 'v_2', 'v_7', 'v_8', ['v_8', [], 'v_6', 'v_4', 'v_7']]], 'v_3', ['v_3', 'v_5', 'v_6', 'v_7', ['v_7', 'v_6', 'v_1', 'v_4', 'v_8']], 'v_1'], 'v_4', 'v_6', 'v_3', 'v_7', 'v_1', 'v_8', 'v_3', [ ['v_5', 'v_3', 'v_7', 'v_5', [ ['v_2', 'v_7', 'v_5', 'v_4'], 'v_4', ['v_2', 'v_8', [], 'v_2', 'v_7', 'v_3', 'v_7'], 'v_1' ], 'v_3', ['v_4', 'v_1', 'v_8', 'v_7', 'v_1', 'v_2', 'v_3', [ [], 'v_3', 'v_4', 'v_2', 'v_5', 'v_5', 'v_7', 'v_6', 'v_1', 'v_1', 'v_2', 'v_8', [], 'v_4' ], 'v_1', 'v_8', 'v_4', 'v_8', 'v_5', 'v_6', [ [], [], 'v_8', 'v_8', [], 'v_3', 'v_4', 'v_4', [], 'v_4', 'v_8' ], 'v_4', ['v_7', 'v_5', 'v_3', 'v_7', [], 'v_1'], 'v_7'], 'v_1', ['v_5', 'v_7', [ [], 'v_5', 'v_6', 'v_2', 'v_1', 'v_3', [], [], 'v_5' ], 'v_5', 'v_3', 'v_8', 'v_5', 'v_7', 'v_3', 'v_3', 'v_2'], 'v_1', ['v_5', 'v_2', 'v_3', ['v_6', 'v_4', 'v_3', 'v_1', [], 'v_6', 'v_5', [], 'v_1', 'v_6', 'v_8', 'v_4', 'v_7', 'v_1', 'v_4'], 'v_4', 'v_2', 'v_7', 'v_3', [ [], [] ], 'v_1', ['v_8', 'v_2', 'v_7', 'v_3', 'v_4', 'v_3', 'v_4', 'v_7', 'v_5', [], 'v_6', 'v_8', 'v_1', []], 'v_6', 'v_7', 'v_2', 'v_8'], ['v_4', 'v_3', 'v_4', 'v_3', 'v_5', 'v_6', 'v_7', 'v_4', ['v_8', 'v_5'], 'v_3', 'v_8', 'v_1', ['v_2', 'v_5', 'v_1', 'v_6', 'v_8', 'v_2', [], 'v_5', 'v_1', 'v_6', 'v_8', 'v_7', 'v_8', 'v_8', 'v_4', 'v_6'], 'v_5', 'v_2', 'v_5', 'v_2', 'v_5'], 'v_4', 'v_4', [ ['v_4', 'v_4', 'v_7'], 'v_3', 'v_7', [ [] ], 'v_5', 'v_7', 'v_3', 'v_2', 'v_1', 'v_8', [ [], 'v_2', 'v_3', 'v_4', [], 'v_4', 'v_7', 'v_5', 'v_5', 'v_3', 'v_2' ], 'v_2', 'v_6', 'v_1', 'v_8', 'v_5', ['v_7', 'v_4', 'v_2', 'v_3', 'v_2', 'v_4', 'v_8', 'v_7', 'v_2'] ], 'v_4' ], 'v_2' ], 'v_7', 'v_1' ], ['v_1', 'v_7', 'v_1', 'v_6', 'v_2', 'v_2', 'v_5', 'v_4', 'v_3', 'v_3', 'v_6', 'v_8'], 'v_5' ], 'v_3', 'v_3', ['v_6'], 'v_7', 'v_2', 'v_3', ['v_7', 'v_2', 'v_4', 'v_4', 'v_5', 'v_8', 'v_2', 'v_3', 'v_1', 'v_3', ['v_5', 'v_2', 'v_8']]] from xdict.TestLib.genrand import gen_random_recursive_only_list_data as randlist l = randlist() ltree = ListTree(l) pathlists = ltree.search('v_4') pathlists.__len__() l[0] l[4][2][1][0][0][3] l[4][2][1][0][0][19][11] l[11][3] #cond_search pl1=ltree.search('v_4') pl1.__len__() #we found 125 match of "v_4" pl2=ltree.search('v_8') pl2.__len__() #we found 117 match of "v_8" #the next we need to found "v_4" or "v_8" whose pathlist includes <14>, and the <14> appears at index <4> in the pathlist def cond_func(ele_value,ele_pathlist,position): cond1 = ("4" in ele_value) | ("8" in ele_value) cond2 = (14 in ele_pathlist) cond3 = False if(cond2): cond3 = (ele_pathlist.index(14) == position) else: pass return(cond1 & cond2 & cond3) position = 4 pl = ltree.cond_search(cond_func=cond_func,cond_func_args=[position]) #lquery #ancestors l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) ltree ltree.ancestor_paths(3,1,0) ltree.ancestors(3,1,0) l[3] l[3][1] #parent l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) ltree ltree.parent_path(3,1,0) ltree.parent(3,1,0) l[3][1] #descendants l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) ltree ltree.descendant_paths(3) ltree.descendants(3) ltree.descendant_paths(3,leaf_only=True) ltree.descendants(3,leaf_only=True) ltree.descendant_paths(3,non_leaf_only=True) ltree.descendants(3,non_leaf_only=True) l[3][1] #prevSib l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) ltree # ltree.lsib_path ltree.prevSibPath(3,1,1) # ltree.lsib ltree.prevSibling(3,1,1) ltree.prevSibPath(3,1,0) == None #l[3][1][0] has no left sibling #nextSib l = [1, [4], 2, [3, [5, 6]]] ltree = ListTree(l) ltree # ltree.rsib_path ltree.nextSibPath(3,1,0) # ltree.rsib ltree.nextSibling(3,1,0) ltree.nextSibPath(3,1,1) == None #l[3][1][1] has no right sibling #sibs l = [1, [4], 2, [3, [5, 6],7,[8,9]]] ltree = ListTree(l) ltree ltree.sib_paths(3,1) ltree.sibs(3,1) ltree.sib_paths(3,1,leaf_only=True) ltree.sibs(3,1,leaf_only=True) ltree.sib_paths(3,1,non_leaf_only=True) ltree.sibs(3,1,non_leaf_only=True) #some_sibs l = [1, [4], 2, [3, [5, 6],7,[8,9]]] ltree = ListTree(l) ltree #ltree.some_sib_paths ltree.someSibPaths(3,1,some=[0,3]) #ltree.some_sibs ltree.someSibs(3,1,some=[0,3]) ltree.someSibPaths(3,1,some=[0,3],leaf_only=True) ltree.someSibs(3,1,some=[0,3],leaf_only=True) ltree.someSibPaths(3,1,some=[0,3],non_leaf_only=True) ltree.someSibs(3,1,some=[0,3],non_leaf_only=True) #whichSib l = [1, [4], 2, [3, [5, 6],7,[8,9]]] ltree = ListTree(l) ltree #ltree.which_sib_path ltree.whichSibPath(3,1,which=2) #ltree.which_sib ltree.whichSib(3,1,which=2) ltree.whichSibPath(3,1,which=1,leaf_only=True) ltree.whichSib(3,1,which=1,leaf_only=True) ltree.whichSibPath(3,1,which=1,non_leaf_only=True) ltree.whichSib(3,1,which=1,non_leaf_only=True) #precedingSibs l = [1, [4], 2, [3, [5, 6],7,[8,9]]] ltree = ListTree(l) ltree #ltree.preceding_sib_paths ltree.precedingSibPaths(3,1) #ltree.preceding_sibs ltree.precedingSibs(3,1) ltree.precedingSibPaths(3,1,leaf_only=True) ltree.precedingSibs(3,1,leaf_only=True) ltree.precedingSibPaths(3,1,non_leaf_only=True) ltree.precedingSibs(3,1,non_leaf_only=True) #followingSibs l = [1, [4], 2, [3, [5, 6],7,[8,9]]] ltree = ListTree(l) ltree #ltree.following_sib_paths ltree.followingSibPaths(3,1) #ltree.following_sibs ltree.followingSibs(3,1) ltree.followingSibPaths(3,1,leaf_only=True) ltree.followingSibs(3,1,leaf_only=True) ltree.followingSibPaths(3,1,non_leaf_only=True) ltree.followingSibs(3,1,non_leaf_only=True) # lcin l = [1, [4], 2, [3, [5, 6],[8,9],7]] ltree = ListTree(l) ltree ltree.lcin_path(3,2,0) l[3][1][1] ltree.lcin(3,2,0) l[3][2][0] #rcin l = [1, [4], 2, [3, [5, 6],[8,9],7]] ltree = ListTree(l) ltree ltree.rcin_path(3,1,1) l[3][2][0] ltree.rcin(3,1,1) l[3][1][1] #sons l = [1, [4], 2, [3, [5, 6],[8,9],7]] ltree = ListTree(l) ltree ltree.son_paths(3) ltree.sons(3) ltree.son_paths(3,leaf_only=True) ltree.sons(3,leaf_only=True) ltree.son_paths(3,non_leaf_only=True) ltree.sons(3,non_leaf_only=True) #PARAMS l = [1, [4], 2, [3, [5, 6],[8,9],7]] ltree = ListTree(l) ltree ltree.depth ltree.total ltree.flatWidth ltree.maxLevelWidth #cond_remove_seqs from elist.elist import * ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) def afterCH(ele,ch): cond = (ord(str(ele)) > ord(ch)) return(cond) new = cond_remove_seqs(ol,[0,2],cond_func=afterCH,cond_func_args=['B']) ol new id(ol) id(new) #### ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) rslt = cond_remove_seqs(ol,[0,2],cond_func=afterCH,cond_func_args=['B'],mode='original') ol rslt id(ol) id(rslt) #cond_remove_some from elist.elist import * ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) def afterCH(ele,ch): cond = (ord(str(ele)) > ord(ch)) return(cond) new = cond_remove_some(ol,0,2,cond_func=afterCH,cond_func_args=['B']) ol new id(ol) id(new) #### ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) rslt = cond_remove_some(ol,0,2,cond_func=afterCH,cond_func_args=['B'],mode='original') ol rslt id(ol) id(rslt) #cond_remove_all from elist.elist import * ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) def afterCH(ele,ch): cond = (ord(str(ele)) > ord(ch)) return(cond) new = cond_remove_all(ol,cond_func=afterCH,cond_func_args=['B']) ol new id(ol) id(new) #### ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) rslt = cond_remove_all(ol,cond_func=afterCH,cond_func_args=['B'],mode='original') ol rslt id(ol) id(rslt) #cond_replace_value_all from elist.elist import * ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) def afterCH(ele,ch): cond = (ord(str(ele)) > ord(ch)) return(cond) new = cond_replace_value_all(ol,"REPLACED",cond_func=afterCH,cond_func_args=['B']) ol new id(ol) id(new) #### ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) rslt = cond_replace_value_all(ol,"REPLACED",cond_func=afterCH,cond_func_args=['B'],mode="original") ol rslt id(ol) id(rslt) # >>> #cond_replace_value_all # ... # >>> from elist.elist import * # >>> ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] # >>> id(ol) # 139927002027016 # >>> def afterCH(ele,ch): # ... cond = (ord(str(ele)) > ord(ch)) # ... return(cond) # ... # >>> new = cond_replace_value_all(ol,"REPLACED",cond_func=afterCH,cond_func_args=['B']) # >>> ol # [1, 'X', 3, 'b', 5, 'c', 6, 'A', 7, 'b', 8, 'B', 9] # >>> new # [1, 'REPLACED', 3, 'REPLACED', 5, 'REPLACED', 6, 'A', 7, 'REPLACED', 8, 'B', 9] # >>> id(ol) # 139927002027016 # >>> id(new) # 139927014765896 # >>> #### # ... ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] # >>> id(ol) # 139927002026184 # >>> rslt = cond_replace_value_all(ol,"REPLACED",cond_func=afterCH,cond_func_args=['B'], mode="original") # >>> ol # [1, 'REPLACED', 3, 'REPLACED', 5, 'REPLACED', 6, 'A', 7, 'REPLACED', 8, 'B', 9] # >>> rslt # [1, 'REPLACED', 3, 'REPLACED', 5, 'REPLACED', 6, 'A', 7, 'REPLACED', 8, 'B', 9] # >>> id(ol) # 139927002026184 # >>> id(rslt) # 139927002026184 from elist.elist import * ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) def afterCH(ele,ch): cond = (ord(str(ele)) > ord(ch)) return(cond) new = cond_replace_value_seqs(ol,"REPLACED",[0,2],cond_func=afterCH,cond_func_args=['B']) ol new id(ol) id(new) #### ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) rslt = cond_replace_value_seqs(ol,"REPLACED",[0,2],cond_func=afterCH,cond_func_args=['B'],mode="original") ol rslt id(ol) id(rslt) # >>> # >>> from elist.elist import * # >>> ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] # >>> id(ol) # 139927002027016 # >>> def afterCH(ele,ch): # ... cond = (ord(str(ele)) > ord(ch)) # ... return(cond) # ... # >>> new = cond_replace_value_seqs(ol,"REPLACED",[0,2],cond_func=afterCH,cond_func_args=['B']) # id(new) # >>> ol # [1, 'X', 3, 'b', 5, 'c', 6, 'A', 7, 'b', 8, 'B', 9] # >>> new # [1, 'REPLACED', 3, 'b', 5, 'REPLACED', 6, 'A', 7, 'b', 8, 'B', 9] # >>> id(ol) # 139927002027016 # >>> id(new) # 139927002026312 # >>> #### # ... ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] # >>> id(ol) # 139927014765896 # >>> rslt = cond_replace_value_seqs(ol,"REPLACED",[0,2],cond_func=afterCH,cond_func_args=['B'],mode="original") # >>> ol # [1, 'REPLACED', 3, 'b', 5, 'REPLACED', 6, 'A', 7, 'b', 8, 'B', 9] # >>> rslt # [1, 'REPLACED', 3, 'b', 5, 'REPLACED', 6, 'A', 7, 'b', 8, 'B', 9] # >>> id(ol) # 139927014765896 # >>> id(rslt) # 139927014765896 # >>> from elist.elist import * ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) def afterCH(ele,ch): cond = (ord(str(ele)) > ord(ch)) return(cond) new = cond_replace_value_some(ol,"REPLACED",0,2,cond_func=afterCH,cond_func_args=['B']) ol new id(ol) id(new) #### ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] id(ol) rslt = cond_replace_value_some(ol,"REPLACED",0,2,cond_func=afterCH,cond_func_args=['B'],mode="original") ol rslt id(ol) id(rslt) # >>> # >>> from elist.elist import * # >>> ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] # >>> id(ol) # 139927002028680 # >>> def afterCH(ele,ch): # ... cond = (ord(str(ele)) > ord(ch)) # ... return(cond) # ... # >>> new = cond_replace_value_some(ol,"REPLACED",0,2,cond_func=afterCH,cond_func_args=['B']) # >>> ol # [1, 'X', 3, 'b', 5, 'c', 6, 'A', 7, 'b', 8, 'B', 9] # >>> new # [1, 'REPLACED', 3, 'b', 5, 'REPLACED', 6, 'A', 7, 'b', 8, 'B', 9] # >>> id(ol) # 139927002028680 # >>> id(new) # 139927002028168 # >>> #### # ... ol = [1,'X',3,'b',5,'c',6,'A',7,'b',8,'B',9] # >>> id(ol) # 139927002027784 # >>> rslt = cond_replace_value_some(ol,"REPLACED",0,2,cond_func=afterCH,cond_func_args=['B'],mode="original") # >>> ol # [1, 'REPLACED', 3, 'b', 5, 'REPLACED', 6, 'A', 7, 'b', 8, 'B', 9] # >>> rslt # [1, 'REPLACED', 3, 'b', 5, 'REPLACED', 6, 'A', 7, 'b', 8, 'B', 9] # >>> id(ol) # 139927002027784 # >>> id(rslt) # 139927002027784 # >>> # >>> #cond_value_indexes_mapping l = [('BIGipServer', 'rd19'), ('TS013d8ed5', '0105b6b0'), ('BIGipServer', 'rd19'), ('TS013d8ed5', '0105b6b0'), ('SID', '1'), ('SID', '2')] def cond_func(ele,*args): cond = ele[0] return(cond) desc = cond_value_indexes_mapping(l,cond_func=cond_func) pobj(desc) # >>> l = [('BIGipServer', 'rd19'), ('TS013d8ed5', '0105b6b0'), ('BIGipServer', 'rd19'), ('TS013d8ed5', '0105b6b0'), ('SID', '1'), ('SID', '2')] # >>> # >>> def cond_func(ele,*args): # ... cond = ele[0] # ... return(cond) # ... # >>> desc = cond_value_indexes_mapping(l,cond_func=cond_func) # >>> pobj(desc) # { # 'BIGipServer': # [ # 0, # 2 # ], # 'SID': # [ # 4, # 5 # ], # 'TS013d8ed5': # [ # 1, # 3 # ] # } # >>> from elist.elist import * l = [('BIGipServer', 'rd100'), ('TS013d8ed5', '00A0'), ('BIGipServer', 'rd200'), ('TS013d8ed5', '00B0'), ('SID', '1'), ('SID', '2')] def cond_func(ele,*args): cond = ele[0] return(cond) uniqualized = cond_uniqualize(l,cond_func=cond_func) pobj(uniqualized) l = [('BIGipServer', 'rd100'), ('TS013d8ed5', '00A0'), ('BIGipServer', 'rd200'), ('TS013d8ed5', '00B0'), ('SID', '1'), ('SID', '2')] reserved_mapping = {'BIGipServer':0,'TS013d8ed5':1,'SID':1} uniqualized = cond_uniqualize(l,cond_func=cond_func,reserved_mapping=reserved_mapping) pobj(uniqualized) # >>> # >>> # >>> from elist.elist import * # >>> l = [('BIGipServer', 'rd100'), ('TS013d8ed5', '00A0'), ('BIGipServer', 'rd200'), ('TS013d8ed5', '00B0'), ('SID', '1'), ('SID', '2')] # >>> # >>> def cond_func(ele,*args): # ... cond = ele[0] # ... return(cond) # ... # >>> uniqualized = cond_uniqualize(l,cond_func=cond_func) # >>> pobj(uniqualized) # [ # ( # 'BIGipServer', # 'rd100' # ), # ( # 'TS013d8ed5', # '00A0' # ), # ( # 'SID', # '1' # ) # ] # >>> # >>> l = [('BIGipServer', 'rd100'), ('TS013d8ed5', '00A0'), ('BIGipServer', 'rd200'), ('TS013d8ed5', '00B0'), ('SID', '1'), ('SID', '2')] # pobj(uniqualized) # >>> # >>> reserved_mapping = {'BIGipServer':0,'TS013d8ed5':1,'SID':1} # >>> uniqualized = cond_uniqualize(l,cond_func=cond_func,reserved_mapping=reserved_mapping) # >>> pobj(uniqualized) # [ # ( # 'BIGipServer', # 'rd100' # ), # ( # 'TS013d8ed5', # '00B0' # ), # ( # 'SID', # '2' # ) # ] # >>>
b70cdaca01ecedba267fc188cfe8e3afa9a2acf2
449d555969bfd7befe906877abab098c6e63a0e8
/551/CH15/EX15.14/14.sce
552989bdd6267634ec6b295c4b3b3a8435ff7678
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
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clc A=1*1.5; //m^2 ts=300; //0C tf=20; //0C h=20; //W/m^2 0C Q=h*A*(ts-tf)/10^3; //kW disp("Rate of heat transfer =") disp(Q) disp("kW")
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function x=%sp_l_s(a,b) // a\b , a sparse b full // Copyright INRIA [ma,na]=size(a) [mb,nb]=size(b) if mb*nb==1 then x=a\(b*speye(na,na)),return;end if ma<>mb then error(12),end if ma<>na then b=a'*b;a=a'*a;end if isreal(a)&isreal(b) then [h,rk]=lufact(a) if rk<mini(ma,na) then warning('deficient rank: rank = '+string(rk)),end x=[] for k=1:nb x=[x,lusolve(h,b(:,k))] end ludel(h) else [h,rk]=lufact([real(a) -imag(a);imag(a) real(a)]) if rk<2*mini(ma,na) then warning('deficient rank: rank = '+string(rk/2)),end x=[] for k=1:nb x=[x,lusolve(h,[real(b(:,k));imag(b(:,k))])] end x=x(1:$/2,:)+%i*x($/2+1:$,:) ludel(h) end
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Example9_7.sce
clear; clc; // Example: 9.7 // Page: 342 printf("Example: 9.7 - Page: 342\n\n"); // Solution //*****Data******// // Data = [X1 V*10^6(cubic m/mol)]; Data = [0 20;0.2 21.5;0.4 24.0;0.6 27.4;0.8 32.0;1 40]; //************// scf(1.1); plot(Data(:,1),Data(:,2)); title("Example 9.7"); xlabel("Mole fraction"); ylabel("Molar Volume*10^(6)"); xgrid(); // Solution (i) printf("For X1 = 0.5\n"); // A tangent is drawn to the curve at X1 = 0.5. // The intercept at X2 = 0 or X1 = 1, gives V1_bar. V1_bar1 = 33.8*10^(-6);// [cubic m/mol] // The intercept at X2 = 1 or X1 = 0, gives V2_bar. V2_bar1 = 17*10^(-6);// [cubic m/mol] printf("Partial molar volume of component 1 is %.2e cubic m/mol\n",V1_bar1); printf("Partial molar volume of component 2 is %.2e cubic m/mol\n",V2_bar1); printf("\n"); // Solution (ii) printf("For X2 = 0.75\n"); // A tangent is drawn to the curve at X1 = 0.75. // The intercept at X2 = 0 or X1 = 1, gives V1_bar. V1_bar2 = 36.6*10^(-6);// [cubic m/mol] // The intercept at X2 = 1 or X1 = 0, gives V2_bar. V2_bar2 = 12.4*10^(-6);// [cubic m/mol] point1 = [0 V1_bar1; 1 V2_bar1]; point2 = [0 V1_bar2;1 V2_bar2]; scf(2); plot(point1(:,1),point1(:,2),point2(:,1),point2(:,2)); legend("X1 = 0.5","X1 = 0.75"); xlabel("Mole fraction"); ylabel("Molar Volume"); printf("Partial molar volume of component 1 is %.2e cubic m/mol\n",V1_bar); printf("Partial molar volume of component 2 is %.2e cubic m/mol\n",V2_bar);
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clc s=10 //angle of slope in rad HA=100*(1/(cosd(s))-1) //Hypotenusal allowance in m HA1=HA*0.201 printf('a)Hypotenusl allowance = %f \n',HA1 ) k= atan(0.2) HA2=100*(1/(cos(k))-1) HA3=HA2*0.201 printf(' b)Hypotenusl allowance = %f m',HA3 )
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ex_1_20_1.sce
errcatch(-1,"stop");mode(2);//Example 1.20.1: Turn Off Time ; ; //given data : format('v',6) Vs=200;//in volts R1=10;// in ohm R2=R1; C=5;// in micro-farad Tc=(R1*C)/1.44; disp(Tc,"The Circuit Turn Off Time,Tc(micro-sec) = ") exit();
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clc; A=[0 1;-1/8 3/4]; B=[0;1]; q2=[0 ;0]; q0=[0;1]; //we know q2=A^2*q0+[B A*B]*X X=inv([B A*B])*[q2-A^2*q0]; disp(X,"therefore [x(1);x(0)]=")
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fir2.sci
function B = fir2(N, F, M, varargin) funcprot(0); rhs = argn(2) if(rhs<3 | rhs>6) error("Wrong number of input arguments."); end select(rhs) case 3 then B = callOctave("fir2", N, F, M); case 4 then B = callOctave("fir2", N, F, M, varargin(1)); case 5 then B = callOctave("fir2", N, F, M, varargin(1), varargin(2)); case 6 then B = callOctave("fir2", N, F, M, varargin(1), varargin(2), varargin(3)); end endfunction
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15_2.sce
clc //initialisation of variables v=2.5//fps N=0.015//fps a=(40+27)//in b=(40*27+27*19)/a c=0.440//cfs w=49*0.09/100//cfs g=0.008//percent Q=0.82//cfs r=0.795//cfs t=2.35*1.16//fps d1=113.20-113.03//ft d2=12//ft //CALCULATIONS R=r/Q//cfs D=g*r//in D2=d1*d2//in //RESULTS printf('The required capacity and find the slope size and hydraulic characteristics of the system=% f in',D2)
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fonk_alt_ust_sinirlama_hocanın_yaptigi.sce
function out=sat_u(x,l_lim,u_lim) s=length(x); for k=1:1:s; if x(k)<=l_lim then v(k)=l_lim; elseif x(k)>=u_lim then v(k)=u_lim; else v(k)=x(k); end end out=v; endfunction
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9_12.sce
clc //initialisation of variables kw= 10^-14 Ka= 1.8*10^-5 //CALCULATIONS Kb= Ka B= sqrt(kw/(Ka*Kb)) //RESULTS printf (' degree of hydrolysis = %.1e ',B)
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//chapter9 //example9.7 //page148 V=10 // V V_D=0.7 // V R_BC=2 // kilo ohm R=2 // kilo ohm // by Kirchoff voltage law we get // -V_D-I_D*R_BC-2*I_D*R+V=0 thus making I_D as subject we get I_D=(V-V_D)/(R_BC+2*R) V_Q=2*I_D*R printf("I_D = %.3f mA \n",I_D) printf("V_Q = %.3f V \n",V_Q)
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clear //Given h=6.62*10**-34 m=9*10**-31 v=10**5 mp=1.67*10**-27 //Calculation l=h/(m*v) lp=h/(mp*v) //Result printf("\n De-Broglie wavelength of electrons is %0.1f *10**-10 m",l*10**10) printf("\n De-Broglie wavelength of protons is %0.4f *10**-10 m",lp*10**10)
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Ex22_26.sce
clear //Given ap=60 //Degree u=3 //Calculation // a=1/sqrt(u) C=asin(a)*180/3.14 //Result printf("\n Critical angle for this medium is %0.2f Degree",C)
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Chapter2_Example34.sce
//Chapter-2, Example 2.34, Page 2.65 //============================================================================= clc clear //INPUT DATA Q=50000;//Rating of the transformer in VA Pi=500;//Constat losses in W Pcu=900;//Full load variable losses in W cosq=0.8;//Power factor //CALCULATIONS nFL=((Q*cosq)/((Q*cosq)+Pi+Pcu))*100;//Full load efficiency L=(Q*sqrt(Pi/Pcu))/1000;//Load at which transformer operates at maximum efficiency in KVA n=((L*1000)/((L*1000)+Pi+Pi))*100;//Maximum efficiency //OUTPUT mprintf('a)Full load efficiency is %3.2f percent \nb)Load at which transformer operates at maximum efficiency is %3.2f KVA \nc)Maximum efficiency is %3.2f percent',nFL,L,n) //=================================END OF PROGRAM==============================
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clear // n=1.25 //number of turns o=2*3.14*n //angle of contact u=0.3 //coefficient of friction t=600.0 //force at the other end of the rope //if the impending motion of the weight be downward. T2=t*%e**(u*o) W=T2 printf("Maximum weight is %f",W) printf("\n answer in textbook is wrong") //if the impending motion of weight be upwards T1=t*%e**(-1*u*o) W=T1 printf("\n Minimum weight is %f",W)
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clc T1 = 275 // Temperature of air at entrance to compressor in K T3 = 310 // Temperature of air at entrance to turbine in K P1 = 1 // Inlet pressure in bar P2 = 4 // Outlet pressure in bar nc = 0.8 // Compressor efficiency T2s = T1*(P2/P1)^(.286) // Ideal temperature after compression T2 = T1 + (T2s-T1)/nc // Actual temperature after compression pr1 = 0.1 // Pressure loss in cooler in bar pr2 = 0.08 //Pressure loss in condenser in bar P3 = P2-0.1 // Actual pressure in condenser P4 = P1+0.08 // Actual pressure in evaporator PR = P3/P4 // Pressure ratio T4s = T3*(1/PR)^(0.286) // Ideal temperature after expansion nt = 0.85 // turbine efficiency T4 = T3-(T3-T4s)*nt // Actual temperature after expansion COP = (T1-T4)/((T2-T3)-(T1-T4)) // Coefficient of performance printf("\n Example 14.11\n") printf("\n Pressure ratio for the turbine is %f ",PR) printf("\n COP is %f ",COP) //The answers vary due to round off error
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ScreenName String 'Confirm File Overwrite Dialog Screen' ImplName String 'Dialog Screen' ElementChunkArray Int 4 ScreenElementType Int 0 ImplName String 'Front End Dialog Screen Backdrop' TabIndex Int 1 Selectable Bool True Enabled Bool True ReferenceArea Rect( 61, 165, 603, 436 ) # left,top,right,bottom ScreenElementType Int 1 ImplName String 'Open Dialog Next Button' TabIndex Int 3 Selectable Bool True Enabled Bool True ReferenceArea Rect( 205, 300, 355, 344 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT02_YES' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Open Dialog Previous Button' TabIndex Int 4 Selectable Bool True Enabled Bool True ReferenceArea Rect( 439, 300, 589, 344 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT02_NO' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Center Justify Label' TabIndex Int 5 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 236, 800, 269 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT02_FILECHANGE_OVERWRITE' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1
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function y = primitive (f, t, x) //This function calculates the primitive of a given function supplied as input. //Calling Sequence //y = primitive(f, t) //y = primitive(f, t, x) //Parameters //f: //t: //x //Description //This is an Octave function. //This function calculates the primitive of a given function supplied as input. //The second parameter t is a vector at which the output is evaluated (at the points t). This vector should be ascending and ordered. //The function approximates the primitive (indefinite integral) of the univariate function handle f with constant of integration x. //Examples //primitive([1,4,5],3,9) //ans = // 9. funcprot(0); rhs = argn(2) if(rhs<2 | rhs>3) error("Wrong number of input arguments.") end select(rhs) case 2 then y = callOctave("primitive",f, t) case 3 then y = callOctave("primitive",f, t, x) end endfunction
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//Finding heat //Example 15.29(pg. 411) clc clear C=2*(10^-6)//capacitance of condenser in F V=10000//PD across condenser in Volts E=(1/2)*C*(V^2)//energy stored in condenser in Joules H=E/4.2//heat produced in the wire in calories printf('Thus heat produced in the wire is %2.2f calories',H)
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clear; M=10; p=0.7; nb_lancers = 5000; N_0 = 5; function y=F(x,K,U) y=x; if (K>x) &(U<=p) then y=x+1; elseif (K<=x)&(U>p) then y= x-1 else y=x end endfunction function r=Xstar() N=N_0; K = grand(1,N,"uin",1,M); U = grand(1,N,"unf",0,1); has_coalescence = %f while ~has_coalescence x_0 = 0; x_1 = M; for j=N:-1 :1 //Calcul de F_0(F_-1(...(x_0)..)) resp. x_1 x_0 = F(x_0,K(j),U(j)) x_1 = F(x_1,K(j),U(j)) end if x_0 == x_1 //S'il y a coalescence, on renvoie x_0 (=x_1) r = x_0 has_coalescence = %t else //Sinon, on double le tableau et on recommence K(N+1:2*N) = grand(1,N,"uin",1,M); U(N+1:2*N) = grand(1,N,"unf",0,1); N=2*N end end endfunction for i=1 : nb_lancers results(i)=Xstar(); end histplot(0.5:10.5,results,style=2)
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function [k,wh]=getobj(objs,pt) n=size(objs) wh=[]; x=pt(1);y=pt(2) data=[] k=[] for i=2:n o=objs(i) if o(1)=='Block' then graphics=o(2) [orig,sz]=graphics(1:2) data=[(orig(1)-x)*(orig(1)+sz(1)-x),(orig(2)-y)*(orig(2)+sz(2)-y)] if data(1)<0&data(2)<0 then k=i,break,end elseif o(1)=='Link' then [frect1,frect]=xgetech(); eps=0.01*min(abs(frect(3)-frect(1)),abs(frect(4)-frect(2))) xx=o(2);yy=o(3); x=x;y=y; n=prod(size(xx)) t=((yy(1:n-1)-yy(2:n))*x+(xx(2:n)-xx(1:n-1))*y+.. xx(1:n-1).*yy(2:n)-xx(2:n).*yy(1:n-1))... ./sqrt((xx(2:n)-xx(1:n-1))^2+.. (yy(2:n)-yy(1:n-1))^2) l=find(abs(t)<eps) for j=1:prod(size(l)) lj=l(j) if (x-xx(lj))*(x-xx(lj+1))<0 then wh=lj;k=i,break,end if (y-yy(lj))*(y-yy(lj+1))<0 then wh=lj;k=i,break,end end elseif o(1)=='Text' then graphics=o(2) [orig,sz]=graphics(1:2) data=[(orig(1)-x)*(orig(1)+sz(1)-x),(orig(2)-y)*(orig(2)+sz(2)-y)] if data(1)<0&data(2)<0 then k=i,break,end end end
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// Theory and Problems of Thermodynamics // Chapter 3 // Thermodynamic Properties of Fluids // Example 3 clear ;clc; //Given data N = 10000 // Number of moles of Methane T = 300 // Temperature of methane in K P = 6 // Pressure of Methane in Mpa Pc = 4.6 // Critical pressure constant of Methane in MPa Tc = 190.6 // critical Temperature constant of Methane in K R = 8.314 // Gas constant Pr = P/Pc // Residual Pressure Tr = T/Tc // Residual Temperature Z = 0.93 // From compressibility chart P = P*1e6 // Units conversion from MPa to Pa // for ideal gas V = Z*N*R*T/P mprintf('Volume calculated from generalized compresibility chart = %4.3f cubic meters' ,V)
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clc clear //INPUT DATA m=20;//calorimeter of water equivalent in gm n=1030;//weight of water in gm p=2;//no.of paddles a=10;//weight of each paddle in kg s=80;//distance between paddles in m g=980;//accelaration due to gravity in cm/sec^2 //CALCULATIONS E=(p*a*1000*g*s*100);//potential energy in dyne cm T=(E)/(1050*4.18*10^7);//rise in temperature in deg.C //if the rise in temp be T,then heat gained by the calorimeter and its contets is 1050T so J=(E)/(1050*T) where (j=4.18*10^7erg/cal) //OUTPUT mprintf('the rise in temperature of water is %3.2f deg.C',T)
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// This file is part of the materials accompanying the book // "The Elements of Computing Systems" by Nisan and Schocken, // MIT Press. Book site: www.idc.ac.il/tecs // File name: projects/08/FunctionCalls/SimpleFunction/SimpleFunctionVME.tst load SimpleFunction.vm, output-file SimpleFunction.out, compare-to SimpleFunction.cmp, output-list RAM[0]%D1.6.1 RAM[1]%D1.6.1 RAM[2]%D1.6.1 RAM[3]%D1.6.1 RAM[4]%D1.6.1 RAM[310]%D1.6.1; set sp 317, set local 317, set argument 310, set this 3000, set that 4000, set argument[0] 1234, set argument[1] 37, set argument[2] 9, set argument[3] 305, set argument[4] 300, set argument[5] 3010, set argument[6] 4010, repeat 10 { vmstep; } output;
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// Chapter 10_Fundamentals of the Metal Oxide Semiconductor Field Effect Transistor //Caption_Flat band voltage //Ex_3//page 442 Na=10^16 tox=500*10^-8 //oxide thickness Qss=10^11 //trapped charge per unit area e=1.6*10^-19 eps_ox=3.9*8.85*10^-14 Cox=eps_ox/tox QSS=Qss*e phi_ms=-1.1 Vfb=phi_ms-(QSS/Cox) printf('Flat band voltage for this MOS capacitor is %1.2f V',Vfb)
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//Crate resting on cart //refer fig. 15.7 (a),(b) and (c) //Applying equilibrium condition //N=W=750 N //Frictional force mu=0.3 N=750 F=mu*N a=(225*9.81)/(750) //m/sec^2 //Consider dynamic equilibrium of the system P=250+((1250*2.943)/(9.81)) //N printf("\nMaximum allowable P=%.2f N and a=%.3f m/sec^2",P,a)
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a = input("Informe o coeficiente a :"); b = input("Informe o coeficiente b :"); c = input("Informe o coeficiente c :"); if (a==0) & (b==0) printf("Equacao degenerada\n"); end if (a==0) & (b<>0) printf("Raiz única em %g.\n",-c/b); end if (a<>0) & (c==0) x = -b\a; printf("Raiz 1 = 0\n"); printf("Raiz 2 = %g\n",x); end if (a<>0) & (c<>0) d = b*b - 4*a*c; if disc >= 0 x1 = -b/(2*a) + sqrt(d)/(2*a); x2 = -b/(2*a) - sqrt(d)/(2*a); printf("Raiz1 = %g\n",x1); printf("Raiz2 = %g\n",x2); else pr = -b/(2*a); pi = sqrt(abs(d))/(2*a); printf("Parte real = %g\n",pr); printf("Parte imaginária = %g\n",pi); end end
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clear; clc; close; Vcc = 9; Vbe = 0.7; Vt = 26*(10^(-3)); Rf = 180*(10^(3)); Rc = 2.7*(10^(3)); Beta = 200; ro = %inf; disp("Values at ro=infinity are :-"); Ib = (Vcc-Vbe)/(Rf+(Beta*Rc)); Ie = (Beta+1)*Ib; re = Vt/Ie; disp(re,"Value of diode resistive element(re) :"); Zi = re/((1/Beta)+(Rc/Rf)); disp(Zi,"Input Impedance(Zi) :"); Zo = (Rc*Rf)/(Rc+Rf); disp(Zo,"Output Impedance(Zo) :"); Av = -Rc/re; disp(Av,"Voltage gain(Av) :"); disp("Values at ro=25kohm are :- "); ro_2 = 20*(10^(3)); Zi_2 = (1+((Rc*ro_2)/(Rc+ro_2))/Rf)/((1/(Beta*re))+(1/Rf)+(((Rc*ro_2)/(Rc+ro_2))/(Rf*re))); disp(Zi_2,"Input Impedance(Zi) :"); Zo_2 = (ro_2*Rc*Rf)/(ro_2*Rc+Rc*Rf+Rf*ro_2); disp(Zo_2,"Output Impedance(Zo) :"); Av_2 = -[1/Rf + 1/re]*[ro_2*Rc/(ro_2+Rc)]/[1+[(ro_2*Rc)/(ro_2+Rc)]/Rf]; disp(Av_2,"Voltage gain(Av) :");
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//chapter 1 Ex 22 clc; clear; close; //let value to be found is x numerator=658^3-328^3; denominator=658^2+658*328+328^2; x=(numerator/denominator); mprintf("x=%.0f",x);
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//clear// //Caption: Calculation of power budget for optical link //Example13.1 //page 464 clear; clc; close; N = [5,10,50]; //number stations alpha = 0.4;//attenuation in dB/Km L_tap = 10;// coupling loss in dB L_thru = 0.9;// coupler throughput in dB Li = 0.5;//Intrinsic coupler loss in dB Lc = 1.0; // coupler-to-fiber loss in dB L = 0.5; //link length in Km fiber_Loss = alpha*L; //fiber loss in dB Pbudget = N*(alpha*L+2*Lc+Li+L_thru)-alpha*L-2*L_thru+2*L_tap; disp(fiber_Loss,'fiber loss in dB for L =500 m') disp(Pbudget,'power budget in dB for optical link when N = 5,10 and 50 stations respectively =') //Result //fiber loss in dB for L =500 m // 0.2 //power budget in dB for optical link when N = 5,10 and 50 stations respectively = // 36. 54. 198.
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clear clc disp("example 10.10") b11=0.001 b12=-0.0005 b22=0.0024 q1=0.08 r1=16 q2=0.08 r2=12 lamda=20 p2=0 for x=1:4 p1=(1-(r1/lamda)-(2*p2*b12))/((q1/lamda)+2*b11) p2=(1-(r2/lamda)-(2*p1*b12))/((q2/lamda)+2*b22) end pl=b11*p1^2+2*b12*p1*p2+b22*p2^2 pr=p1+p2-pl printf("thus \t p1=%2.1fMW,p2=%2.1fMW\n pl=%1.1fMW\npower resevied %2.1fMW",p1,p2,pl,pr)
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// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/05/CPU-external.tst load CPU.hdl, output-file CPU-external.out, compare-to CPU-external.cmp, output-list time%S0.4.0 inM%D0.6.0 instruction%B0.16.0 reset%B2.1.2 outM%D1.6.0 writeM%B3.1.3 addressM%D0.5.0 pc%D0.5.0; set instruction %B0011000000111001, // @12345 tick, output, tock, output; set instruction %B1110110000010000, // D=A tick, output, tock, output; set instruction %B0101101110100000, // @23456 tick, output, tock, output; set instruction %B1110000111010000, // D=A-D tick, output, tock, output; set instruction %B0000001111101000, // @1000 tick, output, tock, output; set instruction %B1110001100001000, // M=D tick, output, tock, output; set instruction %B0000001111101001, // @1001 tick, output, tock, output; set instruction %B1110001110011000, // MD=D-1 tick, output, tock, output; set instruction %B0000001111101000, // @1000 tick, output, tock, output; set instruction %B1111010011010000, // D=D-M set inM 111, tick, output, tock, output; set instruction %B0000000000001110, // @14 tick, output, tock, output; set instruction %B1110001100000100, // D;jlt tick, output, tock, output; set instruction %B0000001111100111, // @999 tick, output, tock, output; set instruction %B1110110111100000, // A=A+1 tick, output, tock, output; set instruction %B1110001100001000, // M=D tick, output, tock, output; set instruction %B0000000000010101, // @21 tick, output, tock, output; set instruction %B1110011111000010, // D+1;jeq tick, output, tock, output; set instruction %B0000000000000010, // @2 tick, output, tock, output; set instruction %B1110000010010000, // D=D+A tick, output, tock, output; set instruction %B0000001111101000, // @1000 tick, output, tock, output; set instruction %B1110111010010000, // D=-1 tick, output, tock, output; set instruction %B1110001100000001, // D;JGT tick, output, tock, output; set instruction %B1110001100000010, // D;JEQ tick, output, tock, output; set instruction %B1110001100000011, // D;JGE tick, output, tock, output; set instruction %B1110001100000100, // D;JLT tick, output, tock, output; set instruction %B1110001100000101, // D;JNE tick, output, tock, output; set instruction %B1110001100000110, // D;JLE tick, output, tock, output; set instruction %B1110001100000111, // D;JMP tick, output, tock, output; set instruction %B1110101010010000, // D=0 tick, output, tock, output; set instruction %B1110001100000001, // D;JGT tick, output, tock, output; set instruction %B1110001100000010, // D;JEQ tick, output, tock, output; set instruction %B1110001100000011, // D;JGE tick, output, tock, output; set instruction %B1110001100000100, // D;JLT tick, output, tock, output; set instruction %B1110001100000101, // D;JNE tick, output, tock, output; set instruction %B1110001100000110, // D;JLE tick, output, tock, output; set instruction %B1110001100000111, // D;JMP tick, output, tock, output; set instruction %B1110111111010000, // D=1 tick, output, tock, output; set instruction %B1110001100000001, // D;JGT tick, output, tock, output; set instruction %B1110001100000010, // D;JEQ tick, output, tock, output; set instruction %B1110001100000011, // D;JGE tick, output, tock, output; set instruction %B1110001100000100, // D;JLT tick, output, tock, output; set instruction %B1110001100000101, // D;JNE tick, output, tock, output; set instruction %B1110001100000110, // D;JLE tick, output, tock, output; set instruction %B1110001100000111, // D;JMP tick, output, tock, output; set reset 1; tick, output, tock, output; set instruction %B0111111111111111, // @32767 set reset 0; tick, output, tock, output;
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example1.sce
clear; clc; printf("\n example 2.1"); // printing out values of the array . a=[31 40 57 46 97 84]; printf("\nvalues are :\n"); disp(a);
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PSO.sce
/* PSO ALGORITHM Functions Aviliable: ReportPSO PSO EvaluatePSO UpdatePSO */ function [Report,Table,RProm] = ReportPSO() Table=[]; tprom=0; Report=[]; Ixprom=zeros(1,10); for exper=1:10 tic();[B,Rep,miny]=PSO(100);a=toc(); tprom = tprom + a; Bprom=Ixprom+B'; Report=[Report; Rep']; end tprom = tprom / 10; //pause, //Execution time //Mean and standard deviation RProm=mean(Report,'r'); Table = [tprom RProm(100) Ixprom]; // clf // plot(Report'); // plot(RProm','*k'); endfunction function [B,Rep,miny]=PSO(TC) miny=100000000; maxy=-100000000; MR=zeros(10,2); MR(:,1)=10//LUB(1); MR(:,2)=-1//LUB(2); Rep=[]; //Poblacion inicial Ti=100; // Total de individuos P=Create(100,10, MR); B=P(1,:); //Mejor solución global PL=P; //Mejor posición local V=zeros(Ti,10); //Velocidad FEL=zeros(Ti,1); //Mejor evaluación local for cycles=1:TC //Evaluacion [FE,miny,maxy,B,PL,FEL]=EvaluationPSO(P,miny,maxy,B,PL,FEL); //Actualizacón de posición [P,V]=UpdatePSO(P,V); Rep=[Rep; miny]; disp(miny) end endfunction function [P,V]=UpdatePSO(P,V) w=0.3; beta1=0.35; beta2=0.35; [Ti, D] = size(P); PL=zeros(Ti,10); //Velocidad B=zeros(Ti,1); //Mejor evaluación local for k=1:Ti for d=1:D V(k,d) = V(k,d)*w + beta1*rand()*(PL(k,d)-P(k,d))+beta2*rand()*(B(d)-P(k,d)); P(k,d) = P(k,d) + V(k,d); end end endfunction function [FE,miny,maxy,B,PL,FEL]=EvaluationPSO(P,miny,maxy,B,PL,FEL) [TI, D] = size(P);FE=zeros(1,TI); for k=1:TI for d=1:D X(d)=P(k,d); end [y, MR] = TestFunction(X,2); if y>maxy then maxy=y; // Ix=X; //best solution found (maximization)) end if y<miny then miny=y; B=X; //best solution found (minimization) end //Minimization FE(k) = 1 - normalization(y,miny,maxy); if FE(k)>FEL(k) then disp(FE) pause() FEL(k)=FE(k); for d=1:D PL(k,d) = X(d); end end end endfunction
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eg7_2b.sce
function result= totalerror(n1, n2, n12) result = n1*n2/n12; endfunction
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2_19.sce
//convert dependent current source to dependent voltage source //Mesh Equations A=[14,-2,0;-2,18,3;2,-2,-1] O=inv(A)*[100;0;0] disp(O(3))
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// To determine the maximum safe working voltage clear clc; r=.5;//radius of conductor(cm) g1max=34; er=5; r1=1; R=7/2;//external dia(cm) g2max=(r*g1max)/(er*r1); V=((r*g1max*log(r1/r))+(r1*g2max*log(R/r1))); V=V/(sqrt(2)); mprintf("Maximum safe working volltage ,V =%.2f kV r.m.s\n",V);
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Ex4_7_4.sce
clear clc XA=0.70; YA=0.35; P=600;//in torr PA=(YA*P)/XA;//vapour pressure of pure A printf('PA=%.1d torr',PA) PB=((1-YA)*P)/(1-XA);//vapour pressure of pure B printf('\nPB=%.1f torr',PB) //page 145
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Exa2_55.sce
//Exa 2.55 clc; clear; close; //Given data : format('v',6); Output=3;//in H.P. Output=3*735.5;//in watts Efficiency=0.83;//unitless cosfi=0.8;//power factor Vl=500;//in volt Input=Output/Efficiency;//in watts //Formula : Input=sqrt(3)*Vl*Il*cosfi Il=Input/(sqrt(3)*Vl*cosfi);//in Ampere ISCbyIFL=3.5;//ratio of SC current to full load current ISC=ISCbyIFL*Il;//in Ampere LineCurrent=ISC/3;//in Ampere(for star delta starter) disp(LineCurrent,"Line Current(in Ampere) :"); //Note : Ans in the book is not accurate.
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Ex5_6.sce
//Example 5_6 clc(); clear; //To calculate the interplanar spacing and wavelength n1=1 theta1=23 //units in degrees n2=3 theta2=60 //units in degrees lamda1=97 //units in pm lamda2=(n2*lamda1*sin(theta1*(%pi/180)))/(sin(theta2*(%pi/180))) //units in pm d=(n2*lamda1)/(2*sin(theta2*(%pi/180))) //units in pm printf("Wavelength lamda=%dpm \n Interplanar spacing d=%dpm",lamda2,d)
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example5_57.sce
clear; clc; // Stoichiometry // Chapter 5 // Energy Balances // Example 5.57 // Page 314 printf("Example 5.57, Page 314 \n \n"); // solution To = 273.15 T1 = 308.15 H1 = 124.8*(T1-To) // kJ/kmol H2 = 134.9*(T1-To) // kJ/kmol HE1 = .1*.9*[542.4+55.4*(.9-.1)-132.8*(.9-.1)^2-168.9*(.9-.1)^3] // kJ/kmol of mix Ha = HE1+H1*.1+H2*.9 HE2 = .2*.8*[542.4+55.4*(.8-.2)-132.8*(.8-.2)^2-168.9*(.8-.2)^3] // kJ/kmol of mix Hb = HE2+H1*.2+H2*.8 HE3 = .3*.7*[542.4+55.4*(.7-.3)-132.8*(.7-.3)^2-168.9*(.7-.3)^3] // kJ/kmol of mix Hc = HE3+H1*.3+H2*.7 HE4 = .4*.6*[542.4+55.4*(.6-.4)-132.8*(.6-.4)^2-168.9*(.6-.4)^3] // kJ/kmol of mix Hd = HE4+H1*.4+H2*.6 HE5 = .5*.5*[542.4+55.4*(.5-.5)-132.8*(.5-.5)^2-168.9*(.5-.5)^3] // kJ/kmol of mix He = HE5+H1*.5+H2*.5 HE6 = .6*.4*[542.4+55.4*(.4-.6)-132.8*(.4-.6)^2-168.9*(.4-.6)^3] // kJ/kmol of mix Hf = HE6+H1*.6+H2*.4 HE7 = .7*.3*[542.4+55.4*(.3-.7)-132.8*(.3-.7)^2-168.9*(.3-.7)^3] // kJ/kmol of mix Hg = HE7+H1*.7+H2*.3 HE8 = .8*.2*[542.4+55.4*(.2-.8)-132.8*(.2-.8)^2-168.9*(.2-.8)^3] // kJ/kmol of mix Hh = HE8+H1*.8+H2*.2 HE9 = .9*.1*[542.4+55.4*(.1-.9)-132.8*(.1-.9)^2-168.9*(.1-.9)^3] // kJ/kmol of mix Hi = HE9+H1*.9+H2*.1 HE10 = .0*1.*[542.4+55.4*(.0-1.)-132.8*(.0-1.)^2-168.9*(.0-1.)^3] // kJ/kmol of mix Hj = HE10+H1+H2*0 x = linspace(0,1,100) y = linspace(4300,5000,100) y = 4721.5-57.4*x+1137.7*x^2-3993.6*x^3+3909.2*x^4-1351.2*x^5 plot(x,y) title("H vs x1") xlabel("x1") ylabel("H (kJ/kg sol.)") printf(" Enthalpy, kJ/kmol mix \n x1 HE H \n 0 0 "+string(H2)+" \n 0.1 "+string(HE1)+" "+string(Ha)+" \n 0.2 "+string(HE2)+" "+string(Hb)+" \n 0.3 "+string(HE3)+" "+string(Hc)+" \n 0.4 "+string(HE4)+" "+string(Hd)+" \n 0.5 "+string(HE5)+" "+string(He)+" \n 0.6 "+string(HE6)+" "+string(Hf)+" \n 0.7 "+string(HE7)+" "+string(Hg)+" \n 0.8 "+string(HE8)+" "+string(Hh)+" \n 0.9 "+string(HE9)+" "+string(Hi)+" \n 1.0 "+string(HE10)+" "+string(Hj)+"")
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B7_Plota_Dinamic_Deform.sce
if nao_calculado // A deformada é calculada somente no caso em que já não tenha // sido, pois esse processo (esse loop) é muito demorado DX = zeros(np,m,N1); DY = zeros(np,m,N1); CDX = zeros(np,m,N1); CDY = zeros(np,m,N1); d = zeros(6,1); winH = waitbar(0,"Calculando deformada . . ."); tot = m*N1*np; for i=1:m N = MN(Lx(i)); R2 = [c(i) -s(i); s(i) c(i)]; DxL = Lx(i)/(np-1); for k=1:N1 for j=1:6 d(j) = DJ(Des(i,j),k); end // O vetor 'd' é colocado em coordenadas nos eixos // locais, usando a equação XXX d = Rt(:,:,i)*d; // O campo de deslocamentos em eixos locais é obtido // usando a equação XXX fi = N*d; // A deformada é obtida para np pontos ao longo da barra xL = 0; for j=1:np des = horner(fi,xL); xL = xL + DxL; // Mudança de base executada com a equação XXX des = R2*des; DX(j,i,k) = des(1); DY(j,i,k) = des(2); waitbar((np*N1*(i-1)+np*(k-1)+np)/tot,winH) end end end close(winH); end // Informa que a deformada dinâmica já foi calculada ao menos // uma vez e delcara o fator de escala da deformada nao_calculado = 0; // Delcara o fator de escala da deformada e Tempo que se pretende rolar o filme resposta = evstr(x_mdialog("Fator de escala e tempo:", ... ["Fator de escala:" "Tempo do Filme (seg):"], ... ["100" "10"])); [fs,tempo] = (resposta(1),resposta(2)); if ~isempty(fs) then // Calcula as coordenadas da deformada para todos os instantes winH = waitbar(0,"Calculando deformada . . .") for k=1:N1 CDX(:,:,k) = CX + fs*DX(:,:,k); CDY(:,:,k) = CY + fs*DY(:,:,k); waitbar(k/N1,winH) end close(winH); BoundX = eixoEstr.data_bounds(2) BoundY = eixoEstr.data_bounds(4) delete(Deformada(1).parent) plot(eixoEstr,CDX(:,:,1),CDY(:,:,1),'r'); Deformada = gce().children eixoEstr.data_bounds = [0 BoundX 0 BoundY] for i=1:3 Axes(i).tight_limits(2) = "on" plot(Axes(i),[0;0],Axes(i).data_bounds(3:4)) TimeBar(i) = gce().children end for k=1:N1 for i=1:m Deformada(i).data = [CDX(:,i,k),CDY(:,i,k)]; end for i=1:3 TimeBar(i).data(:,1) = [t(k);t(k)] end sleep(tempo/N1,"s"); end delete(TimeBar) end
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clear clc //initialisation of variables b= 6 //in s= 12 //in d= 4 //in a1= 30 //degrees a2= 90 //degrees a3= 120 //degrees N= 120 //r.p.m n= 4 //calculations A= 2*%pi*N/60 V= %pi*(b/12)^2*n/4 v= (b/12)^2*A*(b/12)/(d/12)^2 Q1= v*%pi*(d/12)^2*sind(a1)/4 Q2= v*%pi*(d/12)^2*sind(a2)/4 Q3= v*%pi*(d/12)^2*sind(a3)/4 Q4= V-Q1 Q5= Q2-V Q6= Q3-V a4= asind(V/(v*%pi*(d/12)^2))+a1 A= 180-a4-a1 //RESULTS printf ('rate of flow at a1 = %.3f cuses',Q4) printf ('\n rate of flow at a2 = %.3f cuses',Q5) printf ('\n rate of flow at a3 = %.3f cuses',Q6) printf ('\n crak angle = %.1f degrees',a4) printf ('\n crak angle = %.1f degrees',A) //The answer is a bit different due to rounding off error in textbook
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clc //initialisation of variables B= 3 //ft Cd= 0.6 g= 32.2 //ft/sec^2 d1= 6 //in d2= 4 //in //CALCULATIONS Q2= 0.428 //cuses r= sqrt((((d1/12)^5)/((d2/12)^5))) Q1= r*Q2 Q= Q1+Q2 //RESULTS printf ('Total inflow = %.3f cuses',Q)
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clc; clear; close; Cload=200;//in fF Cin=2;//in fF Tnand=4; Tnor=5; Tinv=3; Fanout_d=(Tnand*Tnor*Tinv*Cload/Cin)^(1/3); Cj2=Tnor*Cload/Fanout_d;disp(Cj2,'Cj+2 (in fermifarad)='); Cj1=Tinv*Cj2/Fanout_d;disp(Cj1,'Cj+1 (in fermifarad)='); Cin1=Tnand*Cj1/Fanout_d;disp(Cin1,'Cin(in fermifarad)='); mprintf('\nfor nand gate:Cin=%ffF , so Wp=Wn=0.5um\n',Cin1); mprintf('\nfor inverter:Cin=%ffF , so Wp=3um & Wn=1.5um\n',Cj1); mprintf('\nfor nor gate:Cin=%ffF , so Wp=22um & Wn=5.5um\n',Cj2); //answers vary due to round off error
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function [L,U] = mylu2b(A) n=size(A,1) for k = 1 : n-1 for i = k + 1 : n A(i,k) = A(i, k)/A(k, k); end for i = k + 1 : n for j = k + 1 : n A(i,j)= A(i,j)- A(i,k)*A(k,j); end end end // expression de U U=triu(A); // expression de L L=tril(A) endfunction
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// Lineare Regression // TODO: clear all stuff before starting clc; clear; //close all; function [x,y]=generateXY(x_start,x_end,x_interval,G) x = x_start:x_interval:x_end; y = 2.*x.^2-G.*x+1; endfunction function [x_t,t] = generateTrainingsSet(x,y,G,my,Sigma) // Y=grand(m,n,'nor',Av,Sd) generates random variates from the normal distribution with mean Av (real) and standard deviation Sd (real >= 0) x_t = x(1:6:$); [m,n] = size(x_t); noise = grand(m,n,'nor',my, Sigma); y_t = 2*x_t.^2-G*x_t+1; t = y_t + noise; endfunction function plotData(x,y,x_t,t,y_star, y_star_II) clf; //set(gca(),"auto_clear","off"); plot(x,y,'ro-',x_t,t,'bo-',x,y_star,'go-',x,y_star_II,'co-'); //set(gca(),"auto_clear","on"); endfunction plotColors = ['r','g','b','c','m','y']; function plotDataY(x,Y) [m,n] = size(Y); [i,j] = size(plotColors); clf; set(gca(),"auto_clear","off"); for index=1:m plotArg = strcat([plotColors(modulo(index-1,j)+1),'-']); //plot(x,Y(index,:),'ro-'); plot(x,Y(index,:),plotArg); end set(gca(),"auto_clear","on"); endfunction //function A = createA(x) // // A = ([x x x].^[0 1 2])'; // x_1 = x.^0; // x_2 = x.^1; // x_3 = x.^2; // A = [x_1;x_2;x_3]; //endfunction function A = createA(x,d) // d ... dimension of polynom [m,n] = size(x); A = zeros(d,n); // transform x into a polynom of degree d for index=1:d+1 A(index,:) = x.^(index-1); end endfunction function w_star = compute_w_star(A,y,lamda) // create pseudo inverse and compute Aw=b // see UNDERSTANDING MACHINE LEARNING, page 94ff AAT = A*A'; b = A*y; succ = 0; A_plus = []; while ~succ try A_plus = inv(AAT); succ = 1; catch // check if above is not invertible [m,n] = size(AAT); AAT = lamda*eye(m,n) + AAT; end end w_star = A_plus*b; endfunction //function y = createPolynomValues(x,w) // [m,n]=size(x); // I=ones(m,n); // y = w(1).*I+w(2).*x+w(3).*x.*x; //endfunction function y = createPolynomValues(x,w) [m,n]=size(x); I=ones(m,n); y = w(1).*I; [m2,n2] = size(w); pol_degree = m2 - 1; for index=1:pol_degree y = y+w(index+1).*x.^index; end endfunction function Y = createPolynomValuesW(x,W) [m,n] = size(W); [i,j] = size(x); Y = zeros(n,j); for index=1:n Y(index,:) = createPolynomValues(x,W(:,index)); end endfunction function W_star = trans_x_comp_w_star(x, y, lamba, dimension_start, dimension_end) // w_star is a column vector // W_star is a list of column vectors A_i = createA(x,dimension_start); W_star = compute_w_star(A_i,y,lamda); for dimension_i=dimension_start+1:dimension_end A_i = createA(x,dimension_i); // add zero line at the bottom [m,n] = size(W_star) W_star = cat(1,W_star,zeros(1,n)) W_star = cat(2,W_star,compute_w_star(A_i,y,lamda)) end endfunction function w_n = onlineLMS(A,y,my, e_threshold) // implement online learn from formula // see http://de.wikipedia.org/wiki/LMS-Algorithmus //e(n) = y(n) - x(n)'*w(n); //w(n+1) = w(n) + my* e(n) * x(n); [m,n] = size(A); w_n = ones(m,1); cont = 1; while cont cont = 0; for n_index=1:n x_n = A(:,n_index); y_n = y(n_index); e_n = y_n - x_n'*w_n; // e_n ... error of equation n if e_n > e_threshold cont = 1; end w_n = w_n + my*e_n*x_n; end end endfunction x_start = 0; x_end = 5; x_interval = 0.1; G = 10; [x,y]=generateXY(x_start,x_end,x_interval,G); my = 0; Sigma = 0.7; [x_t,t]=generateTrainingsSet(x,y,G,my,Sigma); y_t = t'; lamda = 0.0001; ////A_3 = createA(x_t,3); ////w_star_3 = compute_w_star(A_3,y_t,lamda); ////y_star_3 = createPolynomValues(x,w_star_3); // ////A_4 = createA(x_t,4); ////w_star_4 = compute_w_star(A_4,y_t,lamda); ////y_star_4 = createPolynomValues(x,w_star_4); // ////plotData(x,y,x_t,t,y_star_3,y_star_4); // dimension_start = 3; dimension_end = 9; W_star = trans_x_comp_w_star(x_t,y_t,lamda,dimension_start, dimension_end); Y = createPolynomValuesW(x,W_star); plotDataY(x,Y); threshold = 0.01; my = 0.05; A_3 = createA(x_t,3); w_online_3 = onlineLMS(A_3, y_t ,my, threshold);
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clc //Initialization of variables N1=1 N2=1 N3=3 N4=1 //calculations N=N1+N2+N3+N4 sig=factorial(N) /(factorial(N1) *factorial(N2)*factorial(N3)*factorial(N4)) //results printf("No. of ways of arranging = %d ",sig)
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//example 3 //energy transport by mass clear clc vf=0.001053 //specific volume of saturated liquid water in m3/kg vg=1.1594 //specific volume of water vapour in m3/kg ug=2519.2 //specific internal energy of water vapour kJ/kg hg=2693.1 //specific enthalpy of water vapour kJ/kg disp('Saturation conditions exist in a pressure cooker at all times after the steady operating conditions are established') disp(' Therefore, the liquid has the properties of saturated liquid and the exiting steam has the properties of saturated vapor at the operating pressure.') m=0.6/(vf*1000) //reduction in mass of liquid in pressure cooker in kg M=m/(40*60) //mass flow rate of steam in kg/s A=8*10^-6 //exit area in m^2 V=M*vg/A //exit velocity in m/s e=hg-ug //flow energy of steam in kJ/kg TE=hg //total nergy of steam in kJ/kg E=M*hg //energy flow rate of steam leaving cooker in kW printf("\n Hence,The mass flow rate of the steam is = %.6f kg/s. \n",M); printf("\n The exit velocity is = %.1f m/s. \n",V); printf("\n The total energy of the steam is = %.1f kJ/kf. \n",TE); printf("\n The flow energy of the steam is = %.1f kJ/kg. \n",e); printf("\n The rate at which energy leaves the cooker by steam is = %.3f kW. \n",E);
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// 09.10.17 // 09.12.05 // 09.12.29 // 14.09.30 addition supported function Assignrep(varargin) global ASSIGNLIST; Nargs=length(varargin); for I=1:2:Nargs Vname=varargin(I); Val=varargin(I+1); Tmp=Assign('?'+Vname); if Tmp=='Not found' Tmp=length(ASSIGNLIST); ASSIGNLIST(Tmp+1)=Vname; ASSIGNLIST(Tmp+2)=Val; else I=Tmp(1); ASSIGNLIST(I+1)=Val; end; end endfunction;
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//Page Number: 238 //Example 4.20 clc; //Given vswr=2; D1=8; //mW D2=2; //mW //Reflection coefficient at arm 4 T=(vswr-1)/(vswr+1); //Powwe delivered to D1 P=(D1*100)/(1-T^2); P1=0.99*P; //Power reflected at D1 W1=(P/100)*T*T; //Power reflected at load W2=D2-W1; Tt=sqrt((W2*100)/(P1)); pt=(1+Tt)/(1-Tt); disp(pt,'VSWR:'); Pl=P1*(1-(Tt*Tt)); disp('mW',Pl,'Power delivered:'); //Answer for P1 should be 792 but it is given as 800
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Name=Paladins Androxys Dash Practice PlayerCharacters=Androxys BotCharacters=Viktor.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Androxys AddedBots=Viktor.bot;Viktor.bot PlayerMaxLives=0 BotMaxLives=0;0 PlayerTeam=0 BotTeams=0;0 MapName=kovaim1.map MapScale=1.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Fortnite WeaponHeroTag=pump, shotgun, training, real, train, jump DifficultyTag=3 AuthorsTag=LeCeuv BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Shotgun jumping training GameVersion=1.0.7.2 ScorePerDistance=0.0 [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=Viktor DodgeProfileNames=Long Strafes Jumping 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=Viktor Profile SeeThroughWalls=false NoDodging=false NoAiming=false [Character Profile] Name=Androxys MaxHealth=2100.0 WeaponProfileNames=Revolver;;;;;;; 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=600.0 MaxCrouchSpeed=500.0 Acceleration=16000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 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=Cylindrical MainBBHeight=90.0 MainBBRadius=32.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=Dash.abilmov;Float.abilmov;Nether Punch.abilmelee;Ultimate.abilwep HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.25 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 [Character Profile] Name=Viktor Profile MaxHealth=2100.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 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HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.25 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 [Dodge Profile] Name=Long Strafes Jumping MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=1.5 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=0.65 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Revolver Type=Hitscan ShotsPerClick=1 DamagePerShot=520.0 KnockbackFactor=4.0 TimeBetweenShots=0.85 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.67 MagazineMax=9 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=450.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=495.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=Gunshot BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=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 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=100.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=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=1.0 MinRecoilUp=0.2 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 [Weapon Profile] Name=Ultimate Weapon Andro Type=Projectile ShotsPerClick=1 DamagePerShot=4000.0 KnockbackFactor=0.0 TimeBetweenShots=0.5 Pierces=true 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=4 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=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=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=1 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=103.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=true Radius=1000.0 DamageAtCenter=4000.0 DamageAtEdge=880.0 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=1.0,1.0,-1.0,5.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=1.0,1.0,-1.0,5.0 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 [Movement Ability Profile] Name=Dash MaxCharges=3.0 ChargeTimer=2.95 ChargesRefundedOnKill=1.0 DelayAfterUse=0.25 FullyAuto=false AbilityDuration=0.25 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=2000.0 MainVelocityCanGoVertical=true MainVelocitySetToMovementKeys=false UpVelocity=0.0 EndVelocityFactor=0.2 Hurtbox=true HurtboxRadius=300.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=true AbilityBlocksMovement=true AbilityBlocksAttack=true AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=0.2 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=25.0 AIMinTargDist=0.0 AIMaxTargDist=1750.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.75 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=75.0 AIDamageReactionResetTimer=1.0 [Movement Ability Profile] Name=Float MaxCharges=1.0 ChargeTimer=4.0 ChargesRefundedOnKill=0.0 DelayAfterUse=0.25 FullyAuto=true AbilityDuration=3.0 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=200.0 MainVelocityCanGoVertical=true MainVelocitySetToMovementKeys=true UpVelocity=150.0 EndVelocityFactor=1.0 Hurtbox=true HurtboxRadius=50.0 HurtboxDamage=0.1 HurtboxGroundKnockbackFactor=0.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=false AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=0.0 AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=false AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Weapon Ability Profile] Name=Ultimate MaxCharges=1.0 ChargeTimer=60.0 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false WeaponProfile=Ultimate Weapon Andro BlockAttackTimer=0.0 AbilityBlockedWhenAttacking=false AmmoPerShot=0 AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Melee Ability Profile] Name=Nether Punch MaxCharges=1.0 ChargeTimer=1.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.15 HurtboxRadius=250.0 HurtboxDamage=450.0 HurtboxGroundKnockbackFactor=0.0 HurtboxAirKnockbackFactor=0.0 BlockAttackTimer=0.5 AbilityBlockedWhenAttacking=false AmmoPerShot=0 FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 AIUseInCombat=true AIUseOutOfCombat=false AIUseOnGround=true AIUseInAir=true AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -576.000000 0.000000 256.000000 448.000000 0.000000 256.000000 448.000000 0.000000 -768.000000 -576.000000 0.000000 -768.000000 -576.000000 -16.000000 256.000000 448.000000 -16.000000 256.000000 448.000000 -16.000000 -768.000000 -576.000000 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Vector3 position -64.000000 0.000000 -736.000000 entity type CameraPath UInt32 entityIdAttachedTo 5 UInt8 posLerp 2 UInt8 angleLerp 2 entity type Effect Vector3 position 0.000000 256.000000 0.000000 String64 effectName internal/misc/reflectionprobe entity type Target Vector3 position 320.000000 256.000000 320.000000 Vector3 angles -135.000000 30.000000 0.000000 String32 name end entity type PlayerSpawn Vector3 position -64.000000 0.000000 224.000000 Vector3 angles 180.000000 0.000000 0.000000 entity type PlayerSpawn Vector3 position 416.000000 0.000000 -256.000000 Vector3 angles 270.000000 0.000000 0.000000 entity type PlayerSpawn Vector3 position -544.000000 0.000000 -256.000000 Vector3 angles 90.000000 0.000000 0.000000
34695f5d74e5b16cece0c9849bfecf9c1c9a0974
449d555969bfd7befe906877abab098c6e63a0e8
/1727/CH10/EX10.2/10_2.sce
a1ed8d1ab02a3cc17316f5f6cb487118e1b5fcb6
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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clc //Initialization of variables u=2 //m/s x=0.15 //m nu=1.5e-5 //m^2/s B=0.5 //m rho=1.22 //kg/m^3 //calcualtions Rx=u*x/nu delta= 4.91*x/sqrt(Rx) deltas=1.729*x/sqrt(Rx) Cf=1.328/sqrt(Rx) Ff=Cf*0.5*rho*u^2 *2*B*x //results printf("Boundary layer thickness = %.2f cm",delta*100) printf("\n Displacement thickness = %.2f cm",deltas*100) printf("\n Average drag coeffcient = %.4f",Cf) printf("\n Drag force = %.4f N",Ff)
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//Variable declaration El=10**-2*50; //energy loss(J) H=El*60; //heat produced(J) d=7.7*10**3; //iron rod(kg/m**3) s=0.462*10**-3; //specific heat(J/kg K) //Calculation theta=H/(d*s); //temperature rise(K) //Result printf('temperature rise is %0.3f K \n',(theta))
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clc disp("Example 2.60") printf("\n") disp("Design a zener voltage regulator to meet following specification") printf("Given\n") printf("1 Resistance are in ohms \n 2 Current are in ampere \n 3 voltage sources are in volt\n") //DC input voltage(10V[+-]20%) Vimin=10-2 Vimax=10+2 //DC output voltage Vo=5 //Load current ILmax=20*10^-3 ILmin=0 //zener current Izmax=80*10^-3 Izmin=5*10^-3 //maximum Resistance Rmax=(Vimin-Vo)/(Izmin+ILmax) //minimum resistance Rmin=(Vimax-Vo)/(Izmax+ILmin) //Required resistance R=(Rmax+Rmin)/2 //load resistance RL=Vo/ILmax printf("minimum resistance %d ohm \n",Rmin) printf("maximum resistance %d ohm \n",Rmax) printf("required resistance %d ohm \n",R) printf("load resistance %d ohm \n",RL)
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//chapter 3 example 4 b// clc clear //core refractive index=n1,relative refractive index difference=d,operating wavelength=l,critical radius of curvature=Rc,cladding refractive index=n2// d=0.03; n1=1.500; n2=sqrt((n1^2)-(2*d*(n1^2))); l=0.8*(10^-6); Rc=((3*(n1^2)*l)/(4*%pi*((n1^2)-(n2^2))^1.5))*(10^6);//critical radius of curvature// printf("\n critical radius of curvature=%f*(10^-6).\n",Rc);
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//Problem 20.03: An ideal transformer has a turns ratio of 8:1 and the primary current is 3 A when it is supplied at 240 V. Calculate the secondary voltage and current. //initializing the variables: tr = 8/1; // turns ratio I1 = 3; // in Amperes V1 = 240; // in Volts //calculation: //A turns ratio of 8:1 means that the transformer has 28 turns on the primary for every 1turns on the secondary V2 = V1/tr //secondary current I2 = I1*tr printf("\n\n Result \n\n") printf("\n secondary voltage is %.0f V and secondary current is %.0f A",V2, I2)
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s = poly(0,'s'); t = 0:.001:10; // PART A h1 = 1/s^2; h2 = 50*s/(s^2+s+100); h3 = s-2; h4 = h1*h2*h3; Heq = syslin('c', h4/(1+h4)); // PART B h1 = s; h2 = 1/s; h3 = h1*h1+h2; // inner series + parallel connection h4 = h3/(h3+1)*h2; // taking care of upper feedback loop Heq_b = syslin('c', h1*h4/(1+h1*h4)); // very similar to a part (just there is additional multiplication in feedback loop), this Heq itslf works like a syslin object would //PART C h1 = s; h2 = 2*s; h3 = 1/(s+1); h4 = 4; G1 = h1+h2; G2 = h1/(1+h1); G3 = h1/(G1); // 1/s+2 G4 = G1*G2+ h2; G5 = 4*G3/(1+4*G3); G6 = G4*G5; Heq = syslin('c', G6/(1+G6));
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// Chapter9 // Page.No-387 // Example_9_1 // Second order inverting butterworth lowpass filter // Given clear;clc; dc_gain=5; f1=2*10^3; // Cutoff freq in Hz Q=10; // Figure of merit R2=(316*10^3)/10; // Resistance R2 printf("\n Resistance R2 is = %.1f ohm \n",R2) // Result R3=(100*10^3)/((3.16*Q)-1); printf("\n Resistance R3 is = %.1f ohm \n",R3) // Result printf("\n Resistance R1 is Open \n") // Result R4=(5.03*10^7)/f1; printf("\n Resistance R4 is = %.1f ohm \n",R4) // Result R5=R4; printf("\n Resistance R5 is = %.1f ohm \n",R5) // Result R6=1.8*10^3; // Assumption R7=dc_gain*R6; printf("\n Resistance R7 is = %.1f ohm \n",R7) // Result and its a potentiometer R8=(R6*R7)/(R6+R7); printf("\n Resistance R8 is = %.3f ohm \n",R8) // Result
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//Finding the Performance of a Dc-Dc converter //Example 5.1(Page No- 168) clc clear //given data pi = 3.141592 Vs = 220;//V k = 0.5; R = 10;//Ohm Vch = 2;//V //part(a) Va = (k*(Vs-Vch)); printf('(a)\t The average output voltage Va = %d V',Va); //part(b) Vo = sqrt(k)*(Vs-Vch); printf('\n (b)\t the rms output voltage %3.2fV',Vo) //part(c) Po = k*(Vs-Vch)^2/R; Pi = k*Vs*(Vs-Vch)/R; eta = Po/Pi; printf('\n (c)\t The converter efficiency %2.2f%%',eta*100) //part(d) Ri = R/k; printf('\n (d)\t The effective input resistance Ri of the converter %d Ohm',Ri) //part(e) Vm = ((Vs*2)/pi); Vrms = Vm/sqrt(2); printf('\n (e)\t RMS value of fundamental component: %2.2fV',Vrms)
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//Exa 8.6 clc; clear; close; //Given data : R1=50;//in kohm R1=R1*10^3;//in ohm C1=0.001;//in uF C1=C1*10^-6;//in F R2=1;//in kohm R2=R2*10^3;//in ohm C2=0.01;//in uF C2=C2*10^-6;//in F //Part (i) //Formula : f=1/(2*%pi*sqrt(C1*C2*R1*R2)) f=1/(2*%pi*sqrt(C1*C2*R1*R2));//in Hz disp(f/1000,"Frequency of oscillations in kHz : "); //Part (ii) CurrentGain=1+C2/C1+R1/R2;//unitless disp(CurrentGain,"Current Gain : ");
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clear //Given w=1000/60.0 r=0.3 B=0.5 //T //Calculation v=w*r vav=v/2.0 e=B*r*vav //Result printf("\n e.m.f induced is %0.3f V",e)
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main function test(); var x; var y; var z; { let x <- 0; let y <- 1; let z <- x + y; return z }; { call test() }.
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Title: TestName: < Type in smth>; Difficulty: < Type in >; FullTime: < Type in a number of seconds for the test >; Questions: < Type in a number of the question in the test>; EndTitle. StartTest: Question: 1; Weight: 1.0; BeginText: EndText; Choice: AtX: 8; AtY: 8; Width: 500; Height: 450; 1: endcase; 2: endcase; 3: endcase; 4: endcase; 5: endcase; Right: 1; Ask; Question: 2; Weight: 1.0; BeginText: EndText; MultiChoice: AtX: 8; AtY: 8; Width: 500; Height: 450; 1: endcase; 2: endcase; 3: endcase; 4: endcase; 5: endcase; Right: 1,3; Ask; Question: 1; Weight: 1; BeginText: EndText; Image: AtX: 8; AtY: 8; Width: 500; Height: 180; path : image.bmp; EndImage; MultiChoice: AtX: 510; AtY: 8; Width: 500; Height: 450; 1: endcase; 2: endcase; 3: endcase; 4: endcase; 5: endcase; Right: 1,3; Ask; Question: 1; Weight: 1; BeginText: EndText; Edit: AtX: 8; AtY: 8; Width: 100; Height: 20; 1: endcase; 2: endcase; 3: endcase; EndEdit; Ask; EndTest.
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//Chapter 29 Ex 1 clc; clear; close; //(a) facevalue=90; marketvalue=100; cost1=7200*(facevalue/marketvalue); mprintf("Cost of Rs.7200 stock is Rs %d",cost1); //(b) marketvalue=100; premium=4; facevalue=marketvalue+premium; cost2=4500*(facevalue/marketvalue); mprintf("\n Cost of Rs.4500 stock is Rs %d",cost2); //(c) marketvalue=100; discount=15; facevalue=marketvalue-discount; cost3=6400*(facevalue/marketvalue); mprintf("\n Cost of Rs.6400 stock is Rs %d",cost3);
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clear; //clc(); // Example 1.1 // Page: 9 printf("Example-1.1 Page no.-9\n\n"); //***Data***// m_i = 10;//[g] m_w = 990;//[g] M_i = 342.3;//[g] M_w = 18;//[g] // The mass fraction is // ( mass fraction of sucrose ) = x_i (by mass) = m_i/(sum of all substances) x_i = m_i/(m_i+m_w); x_i = x_i*100;// [in percentage] // This is also the weight fraction. // The mole fraction is // ( mole fraction of sucrose ) = x_j (by mole) = n_i/(sum of number moles of all the substances) n_i = m_i/M_i;// number of moles of sucrose n_w = m_w/M_w;// number of moles of water x_j = n_i/(n_i+n_w); x_j = x_j*100;// [in percentage] // The molality, a concentration unit is widely used in equilibrium calculations, is defined as // m (molality) = (moles of solute)/(kg of solvent) m = n_i/m_w*1000;//[molal] // For solutions of solids and liquids (but not gases) ppm almost always means ppm by mass, so x_ppm = x_i*10^(6)/100;//[ppm] printf(" sucrose concentration in terms of the mass fraction is %f%%\n",x_i); printf(" sucrose concentration in terms of the mole fraction is %f%%\n",x_j); printf(" sucrose concentration in terms of the molality is %f molal\n",m); printf(" sucrose concentration in terms of the ppm is %f ppm",x_ppm);
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//Fluid Systems - By Shiv Kumar //Chapter 12- Reciprocating Pumps //Example 12.5 //To Determine the Pressure Head on Piston at Begining, Middle and End of Suction Stroke. clc clear //Given Data:- L=150; //Length of Stroke, mm l_s=7; //Length of Suction Pipe, m ds_by_D=3/4; //Ratio of Suction Pipe Diameter to Piston Diameter, ds/D hs=2.5; //Suction Head, m ds=75; //Diameter of Suction Pipe, mm N=75; //Crank Speed, rpm f=0.01; //Co-efficient of Friction //Data Used:- g=9.81; //Acceleration due to gravity, m/s^2 h_atm=10.33; //Atmospheric Pressure Head, m of water //Computations:- L=L/1000; //m ds=ds/1000; //m r=L/2; //Crank radius, m A_by_as=(1/ds_by_D)^2; omega=2*%pi*N/60; //Angular Velocity, rad/s //At Begining of Suction Stroke, theta=0; //degrees h_as=(l_s/g)*A_by_as*omega^2*r*cosd(theta); //Acceleration Head, m of water h_fs=(4*f*l_s/(2*g*ds))*(A_by_as*omega*r*sind(theta))^2; //Head loss due to friction, m of water h_v=hs+h_fs+h_as; //Pressure Head on Piston, m of water Vaccum h_abs=h_atm-h_v; //Pressure Head on Piston, m of water Absolute //Result 1 printf("At Begining of Suction Stroke\n Pressure Head on Piston=%.2f m of water Vaccum \n\t\t\t =%.2f m of water Absolute\n\n",h_v,h_abs) //The answer vary due to round off error //At Mid of Suction Stroke, theta=90; //degrees h_as=(l_s/g)*A_by_as*omega^2*r*cosd(theta); //Acceleration Head, m of water h_fs=(4*f*l_s/(2*g*ds))*(A_by_as*omega*r*sind(theta))^2; //Head loss due to friction, m of water h_v=hs+h_fs+h_as; //Pressure Head on Piston, m of water Vaccum h_abs=h_atm-h_v; //Pressure Head on Piston, m of water Absolute //Result 2 printf("At Middle of Suction Stroke\n Pressure Head on Piston=%.4f m of water Vaccum \n\t\t\t =%.3f m of water Absolute\n\n",h_v,h_abs) //The answer vary due to round off error //At End of Suction Stroke, theta=180; //degrees h_as=(l_s/g)*A_by_as*omega^2*r*cosd(theta); //Acceleration Head, m of water h_fs=(4*f*l_s/(2*g*ds))*(A_by_as*omega*r*sind(theta))^2; //Head loss due to friction, m of water h_v=hs+h_fs+h_as; //Pressure Head on Piston, m of water Vaccum h_abs=h_atm-h_v; //Pressure Head on Piston, m of water Absolute //Result 3 printf("At End of Suction Stroke\n Pressure Head on Piston=%.2f m of water Vaccum \n\t\t\t =%.2f m of water Absolute\n\n",h_v,h_abs) //The answer vary due to round off error
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clc,clear exec('input1.sce',-1) clf //Making the histogram plot histplot(10,S,xlabel('----S---->'),ylabel('--Frequency-->'),title('Histogram of distribution of S'))
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// Exa 4.9 format('v',6) clc; clear; close; // Given data epsilon = 16/(36 * %pi * 10^11);// in F/cm A = 1 * 10^-2; W = 2 * 10^-4; // The barrier capacitance C_T = (epsilon * A)/W;// in F C_T= C_T*10^12;// in pF disp(C_T,"The barrier capacitance in pF is");
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//example3.11 clc disp("For the npn silicon transistors,") disp("V_CE(sat)=0.3 V and V_BE(sat)=0.7 V = V_rho") disp("While V_BE(cut-in)=0.5 V= V_gamma ...Referring Table 3.1") i=(12-0.3-0.7+0.5)/(2000+200) format(6) disp(i,"(I''_B)(in mA)=(V_CC-V_CE(sat)-V_rho-V_gamma)/(R_c+r''_bb)=") disp("Hence the overshoot in base voltage of Q2 is:") d=(5.227*200*10^-3)+0.7-0.5 format(7) disp(d,"delta(in V)=(I''_b*r''_bb)+(V_rho)-(V_gamma)=") v=12-(5.227*2) disp(v,"V_C1(in V)=(V_CC)-(I''_B*R_C)=") disp("These are the values of various voltages just after the circuit returns back to stable state i.e at t=T.") disp("The width of the output pulse") t=(0.69*20*10^3)*(1000*10^-12) format(11) disp(t,"T(in sec)=(0.69*20*10^-3)*(1000*10^-12)=") disp("The voltage waveforms at base of Q2, Q1 and collector of Q2, Q1 are shown in the fig 3.87 on previous page.") disp("The overshoot in V_C1 is (delta'') and is same as (delta) ") disp("Therefore, (delta'')=1.2454 V") f=(-(14.7*20*10^3)/(40*10^3))+((12*20*10^3)/(40*10^3)) format(5) disp(f,"V_F(in V)=((-V_BB*R1)/(R1+R2))+((V_CC*R2)/(R1+R2))= ") disp("V_C2=V_CE(sat)=0.3 in stable state") c=(((12*20000)/(40000))+((54.692*2000)/(22000))) format(7) disp(c,"V_C2(in V)[in quasi-stable state]=((V_CC*R1)/(R1+R2))+((V_delta*R_C)/(R1+R_C))= ")
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bfp-008-cvtfrlog.tst
*Testcase bfp-008-cvtfrlog.tst: CELFBR, CDLFBR, CXLFBR #Testcase bfp-008-cvtfrlog.tst: IEEE Convert From Logical #..Includes CONVERT FROM LOGICAL 32 (3). Also tests traps and exceptions #..and results from different rounding modes (CELFBR only). sysclear archmode esame # # Following suppresses logging of program checks. This test program, as part # of its normal operation, generates 2 program check messages that have no # value in the validation process. (The messages, not the program checks.) # ostailor quiet loadcore "$(testpath)/bfp-008-cvtfrlog.core" runtest 1.0 ostailor default # restore messages for subsequent tests # inputs converted to BFP short - result values *Compare r 1000.10 *Want "CELFBR result pairs 1-2" 3F800000 3F800000 40000000 40000000 r 1010.10 *Want "CELFBR result pairs 3-4" 40800000 40800000 4F800000 4F800000 r 1020.10 *Want "CELFBR result pairs 5-6" 4F7FFFFF 4F7FFFFF 4F800000 4F800000 # inputs converted to BFP short - FPCR contents *Compare r 1100.10 *Want "CELFBR FPC pairs 1-2" 00000000 F8000000 00000000 F8000000 r 1110.10 *Want "CELFBR FPC pairs 3-4" 00000000 F8000000 00080000 F8000C00 r 1120.10 *Want "CELFBR FPC pairs 5-6" 00000000 F8000000 00080000 F8000C00 # inputs converted to BFP short - rounding mode test results *Compare r 1200.10 *Want "CELFBR maxint-32 result FPC modes 1-3, 7" 4F7FFFFF 4F800000 4F7FFFFF 4F7FFFFF r 1210.10 *Want "CELFBR maxint-32 result M3 modes 1, 3-5" 4F800000 4F7FFFFF 4F800000 4F7FFFFF r 1220.08 *Want "CELFBR maxint-32 result M3 modes 6, 7" 4F800000 4F7FFFFF r 1230.10 *Want "CELFBR 0xFFFFFF00 result FPC modes 1-3, 7" 4F7FFFFF 4F7FFFFF 4F7FFFFF 4F7FFFFF r 1240.10 *Want "CELFBR 0xFFFFFF00 result M3 modes 1, 3-5" 4F7FFFFF 4F7FFFFF 4F7FFFFF 4F7FFFFF r 1250.08 *Want "CELFBR 0xFFFFFF00 result M3 modes 6, 7" 4F7FFFFF 4F7FFFFF r 1260.10 *Want "CELFBR 0xFFFFFF40 result FPC modes 1-3, 7" 4F7FFFFF 4F800000 4F7FFFFF 4F7FFFFF r 1270.10 *Want "CELFBR 0xFFFFFF40 result M3 modes 1, 3-5" 4F800000 4F7FFFFF 4F800000 4F7FFFFF r 1280.08 *Want "CELFBR 0xFFFFFF40 result M3 modes 6, 7" 4F800000 4F7FFFFF # inputs converted to BFP short - rounding mode test FPCR contents *Compare r 1500.10 *Want "CELFBR maxint-32 FPC modes 1-3, 7 FPCR" 00000001 00000002 00000003 00000007 r 1510.10 *Want "CELFBR maxint-32 M3 modes 1, 3-5 FPCR" 00080000 00080000 00080000 00080000 r 1520.08 *Want "CELFBR maxint-32 M3 modes 5-7" 00080000 00080000 r 1530.10 *Want "CELFBR 0xFFFFFF00 FPC modes 1-3, 7 FPCR" 00000001 00000002 00000003 00000007 r 1540.10 *Want "CELFBR 0xFFFFFF00 M3 modes 1, 3-5 FPCR" 00000000 00000000 00000000 00000000 r 1550.08 *Want "CELFBR 0xFFFFFF00 M3 modes 6-7" 00000000 00000000 r 1560.10 *Want "CELFBR 0xFFFFFF40 FPC modes 1-3, 7 FPCR" 00000001 00000002 00000003 00000007 r 1570.10 *Want "CELFBR 0xFFFFFF40 M3 modes 1, 3-5 FPCR" 00080000 00080000 00080000 00080000 r 1580.08 *Want "CELFBR 0xFFFFFF40 M3 modes 6-7" 00080000 00080000 # inputs converted to BFP long - result values *Compare r 2000.10 *Want "CDLFBR result pair 1" 3FF00000 00000000 3FF00000 00000000 r 2010.10 *Want "CDLFBR result pair 2" 40000000 00000000 40000000 00000000 r 2020.10 *Want "CDLFBR result pair 3" 40100000 00000000 40100000 00000000 r 2030.10 *Want "CDLFBR result pair 4" 41EFFFFF FFC00000 41EFFFFF FFC00000 r 2040.10 *Want "CDLFBR result pair 5" 41EFFFFF E0000000 41EFFFFF E0000000 r 2050.10 *Want "CDLFBR result pair 6" 41EFFFFF F0000000 41EFFFFF F0000000 # Inputs converted to BFP long - FPCR contents *Compare r 2100.10 *Want "CDLFBR FPC pairs 1-2" 00000000 F8000000 00000000 F8000000 r 2110.10 *Want "CDLFBR FPC pairs 3-4" 00000000 F8000000 00000000 F8000000 r 2120.10 *Want "CDLFBR FPC pairs 5-6" 00000000 F8000000 00000000 F8000000 # Inputs converted to BFP extended - result values *Compare r 3000.10 *Want "CXLFBR result 1a" 3FFF0000 00000000 00000000 00000000 r 3010.10 *Want "CXLFBR result 1b" 3FFF0000 00000000 00000000 00000000 r 3020.10 *Want "CXLFBR result 2a" 40000000 00000000 00000000 00000000 r 3030.10 *Want "CXLFBR result 2b" 40000000 00000000 00000000 00000000 r 3040.10 *Want "CXLFBR result 3a" 40010000 00000000 00000000 00000000 r 3050.10 *Want "CXLFBR result 3b" 40010000 00000000 00000000 00000000 r 3060.10 *Want "CXLFBR result 4a" 401EFFFF FFFC0000 00000000 00000000 r 3070.10 *Want "CXLFBR result 4b" 401EFFFF FFFC0000 00000000 00000000 r 3080.10 *Want "CXLFBR result 5a" 401EFFFF FE000000 00000000 00000000 r 3090.10 *Want "CXLFBR result 5b" 401EFFFF FE000000 00000000 00000000 r 30A0.10 *Want "CXLFBR result 6a" 401EFFFF FF000000 00000000 00000000 r 30B0.10 *Want "CXLFBR result 6b" 401EFFFF FF000000 00000000 00000000 # Inputs converted to BFP extended - FPCR contents *Compare r 3200.10 *Want "CXLFBR FPC pairs 1-2" 00000000 F8000000 00000000 F8000000 r 3210.10 *Want "CXLFBR FPC pairs 3-4" 00000000 F8000000 00000000 F8000000 r 3220.10 *Want "CXLFBR FPC pairs 5-6" 00000000 F8000000 00000000 F8000000 *Done
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clc clear //Input data l=537;//Latent heat of steam in cal/g V2=1674;//The specific volume of one gram of steam in cm^3 V1=1.000;//The specific volume of one gram of water in cm^3 p=2.712;//The increase in the pressure in cm of Hg t=100;//The boiling point of water in degree centigrade //Calculations T=t+273;//The boiling point of water in K P=p*13.6*980;//The increase in the pressure in dynes/cm^2 L=l*4.2*10^7;//Latent heat of steam in ergs T1=(P*T*(V2-V1))/L;//The change in the temperature of the boiling water when the pressure is increased in K //Output printf('The change in temperature of boiling water is %3.0f K (or) %3.0f degree centigrade ',T1,T1)
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clc clear //input e1=350//heat per second t=7+273 //teperature sig=5.7*10^-8//stephans constant //calculation e2=e1*4//stephans law E=sig*(t^4-t^4)//stephans law //output printf("the rate of emission is %3.3f W",e2) printf("\nthe rate of emission when outer temperature is increased is %d W",E)
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clear //Given u1=1 u2=1.5 R=1 //Calculation x=(u1+u2)/(u2-u1) //Result printf("\n Distance of the object is %0.3f R", x)
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//Finding the Performance of a Dc-Dc converter with RL load //Example 5.2(Page No- 174) clc clear //given data Vs = 220;//V R = 5;//Ohm L = 7.5*10^-3;//H E = 0;//V k = 0.5; f = 1000;//Hz //part(a) // I2 = I1*exp(-(kTR/L)+((Vs-E)/R*(1-exp((-(k*T*R/L)))))) // and I1 = I2*exp(-(1-k)*(T*R/L))-(E/R)*(1-exp(-(1-k)*TR/L)) //Solving these two equations to get I1 and I2 A = [0.7165 -1; 1 -0.7165]; b = [-12.473; 0]; x = A\b; I1 = x(1); I2 = x(2); printf('(a)\t Maximum instanteneous current I1: %.2f A',I1) //part(b) printf('\n (b)\t The peak instanteneous load current I2: %.2f A',I2) //part(c) del_I = I2-I1; //del_I del_I_max = (Vs/R)*(tanh(R/(4*f*L)));// the maximum peak to peak ripple current del_I_max_app = (Vs)/(4*f*L); // approximate maximum ripple current printf('\n (c)\t del_I (I2-I1) :%.3f A',del_I); printf('\n \t The maximum peak to peak ripple current :%0.2f A',del_I_max) printf('\n \t Approximate maximum ripple current :%.2f A',del_I_max_app); //part(d) Ia = (I2+I1)/2 ; printf('\n (d)\t The average load current is %f A',Ia); //part(e) Io = sqrt(I1^2 + (I2-I1)^2/3 + I1*(I2-I1)); printf('\n (e)\t rms value of load current is %.2f A',Io); //part(f) Is = k*Ia ; Ri = Vs/Is ; printf('\n (f)\t The average source current : %f A',Is); printf('\n \t the effective input Ri :%d A',Ri); //part(g) Ir = sqrt(k)*sqrt(I1^2+(I2-I1)^2/3+I1*(I2-I1)); printf('\n (g)\t The rms converter current :%.2f A',Ir)
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question(1, 'item 4-1', 'Als je van links af een lamp laat schijnen door de gaatjes van de L, wat is dan de vergroting die je vindt op het (scherpe) beeld rechts?', [ '2', '0,5', '1', 'weet niet' ], state(state, '', [ s1 = shield(pos_x(7.3), unit(1)), m1 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(17.3), show_gauge(true)), s2 = shield2(pos_x(27.25)), d1 = ruler(from(s1), to(m1), pos_y(1.5)), d2 = ruler(from(m1), to(s2), pos_y(3.4)) ])). question(2, 'item 4-2', 'Als we van links af een lamp laten schijnen, hoe ver moet dan een voorwerp van de lens af staan om een scherp beeld te krijgen?', [ '10 centimeter', '8 centimeter', '5 centimeter', 'weet niet' ], state(state, '', [ s4 = shield2(pos_x(25.5)), m3 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(15.5), show_gauge(true)), d14 = ruler(from(m3), to(s4), pos_y(6.2)) ])). question(3, 'item 4-3', 'Wat kun je in bovenstaande situatie zeggen over het beeld van het voorwerp?', [ 'In deze situatie is er geen beeld', 'In deze situatie is het beeld kleiner dan het voorwerp', 'In deze situatie is het beeld groter dan het voorwerp', 'weet niet' ], state(state, '', [ l1 = biglamp(instrument_name(biglamp)), m1 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(19.9), show_gauge(true), instrument_name(lens)), s1 = shield(pos_x(5.05), unit(1), instrument_name(shield)), d1 = ruler(from(m1), to(s1), pos_y(-6.7)), c1 = construction_line(pos_x(0), instrument_name(consline)), d2 = ruler(from(s1), to(c1), pos_y(5.95)) ])). question(4, 'item 4-4', 'Wat kun je in bovenstaande situatie zeggen over het beeld van het voorwerp?', [ 'In deze situatie is er geen beeld', 'In deze situatie is het beeld kleiner dan het voorwerp', 'In deze situatie is het beeld groter dan het voorwerp', 'weet niet' ], state(state, '', [ l1 = biglamp(instrument_name(biglamp)), m1 = lens(label(''), radius(5), thickness(0.1), focal_distance(5), sfere_left(*), sfere_right(*), breaking_index(1.51), pos_x(13.95), show_gauge(true), instrument_name(lens)), s1 = shield(pos_x(4.95), unit(1), instrument_name(shield)), d1 = ruler(from(m1), to(s1), pos_y(-6.7)), c1 = construction_line(pos_x(0), instrument_name(consline)), d2 = ruler(from(s1), to(c1), pos_y(5.95)) ])).
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clc //variable initialisation V=440 //Supply voltage in volts P=4 //number of poles f=50 //Supply frequency in Hz R=0.2 //rotor resistance in ohm X=0.35 //leakage reactance in ohm N1=1450 //speed in rpm N2=1200 //speed in rpm S2=0.2 //solution Vph=V/sqrt(3) Ns=(120*f)/P//Synchronous Speed Wms=2*%pi*Ns/60 S=(Ns-N1)/Ns T=(3/Wms)*(Vph^2)*(R/S)/((R/S)^2+(X)^2)//The answer provided in the textbook is wrong K=T/(1-S) T2=K*(1-S2) Vph2=sqrt(T2*((R/S)^2+(X)^2)/((3/Wms)*(R/S))) Vl=Vph2*sqrt(3) printf('\n\n Torque=%0.1f N-m\n\n',T)//The answer provided in the textbook is wrong printf('\n\n Line Voltage to be imposed=%0.1f Volts\n\n',Vph2)
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//Example 8_2 page no:297 clc; R=10;//resistance in ohm L=0.5*10^-3//inductance in henry; C=10*10^-6;//capacitance in farad; f=1/(2*%pi*sqrt(L*C)); f=f/1000;//converting to killoHertz disp(f,"the resonant frequency is (in kHz)");
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clear; clc; funcprot(0); //given data P = 20;//power required in kW cx1 = 7.5;//steady wind speed in m/s rho = 1.2;//density in kg/m^3 Cp = 0.35; eta_g = 0.75;//output electrical power eff_d = 0.85;//electrical generation efficiency //Calculations A2 = 2*P*1000/(rho*Cp*eta_g*eff_d*cx1^3); D2 = sqrt(4*A2/%pi); //Results printf('The diameter = %.1f m.',D2);
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errcatch(-1,"stop");mode(2);//caption:Find magnitude of limiting error fot R1 and R2 //Ex2.5 R1=36//resistance(in ohm) R2=75//resistance(in ohm) er=0.005//limiting error(in ohm) dR1=R1*er disp(dR1,'magnitude of limiting error for R1(in ohm)=') dR2=R2*er disp(dR2,'magnitude of limiting error for R2(in ohm)=') exit();
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//Caption: One-Sample Tests //One-sample Sign Test for small samples //Example9.2 //Page313 //Test 2: Ho: p =1/2, H1: p< 1/2 clear; clc; n = 8;//sample size p =0.5; q = 1-p; alpha = 0.05;//significance level plus_signs = 2; minus_signs = 7; //The binomial probability that the number of plus signs <=2 X =2; [P,Q]=cdfbin("PQ",X,n,p,q); disp(P,'The binomial probability that the number of plus signs P(X<=2)=') if (P>alpha) then disp('Sine it is greater than significance level, the binomial statistic falls') disp('in the acceptance region') else disp('Since it is less than significance level, the binomial statistic falls') disp('in the rejection region and the null hypothesis should be rejected') end //Result //The binomial probability that the number of plus signs P(X<=2)= // // 0.1445313 // // Sine it is greater than significance level, the binomial statistic falls // // in the acceptance region
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clc; //Example 4.6 //Page no 133 //Solution m=0.8; Aq=100; Fc=500; //kHz Vc=5*(10^-3); //mV Fm=1000; //Hz //(a) disp("(a)Substituting into equation 4-34(pgno 132), "); Am=Aq*(1+m); disp(Am," Amax = "); am=Aq*(1-m); disp(am,"Amin = "); //(b) Vom=Am*Vc; vom=am*Vc; disp('V',Vom,"(b)Vout(max) = "); disp('V',vom,"Vout(min) = ");
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// Initilization of Variables v_1=3 // m/s // uniform speed of the belt at top v_2=2 // m/s // uniform speed of the belt at the bottom r=0.4 // m // radius of the roller // Calculations // equating eq'ns 2 & 4 and solving for v_c & theta' (angular velocity). We use matrix to solve the eqn's A=[1 r;1 -r] B=[v_1;v_2] C=inv(A)*B // Results clc printf('The linear velocity (v_c) at point C is %f m/s \n',C(1)) printf('The angular velocity at point C is %f radian/seconds \n', C(2)) // NOTE: The answer of angular velocity is incorrect in the book
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clc // Given that lambda = 5000 // wavelength of light in angstrom theta = 30 // Central maximum spread out at on side // Sample Problem 3 on page no. 139 printf("\n # PROBLEM 3 # \n") printf(" Standard formula used \n") printf(" lambda = e*sin(theta) \n") e = lambda*1e-10 / sin(theta*%pi/180) // Calculation of width of slit printf("\n Width of slit is %ecm.",e*1e+2)
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//clear// clear; clc; //Example 15.2 //Given Tca = 70; //[C] Tcb = 130; //[C] Tha = 240; //[C] Thb = 120; //[C] //Solution //Using Eq.(15.7) and (15.8) neta_h = (Tcb-Tca)/(Tha-Tca); Z = (Tha-Thb)/(Tcb-Tca); //From Fig 15.7a, the correction factor is found Fg = 0.735; //the temperature drops are //At shell inlet: deltaT_i = Tha-Tcb; //[C] //At shell outlet: deltaT_o = Thb-Tca; //[C] Log_T = (deltaT_i-deltaT_o)/log(deltaT_i/deltaT_o); // the correct value of Log_T is Log_T = Fg*Log_T; //[C] disp('C',Log_T,'The correct mean emperature drop is') //Because of low value of Fg, a 1-2 heat exchanger is not suitable for this duty
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function [wt,a,f,scalo,wavescaled]=contwtmir(x,fmin,fmax,N,wave); // This Software is ( Copyright INRIA . 1998 1 ) // // INRIA holds all the ownership rights on the Software. // The scientific community is asked to use the SOFTWARE // in order to test and evaluate it. // // INRIA freely grants the right to use modify the Software, // integrate it in another Software. // Any use or reproduction of this Software to obtain profit or // for commercial ends being subject to obtaining the prior express // authorization of INRIA. // // INRIA authorizes any reproduction of this Software. // // - in limits defined in clauses 9 and 10 of the Berne // agreement for the protection of literary and artistic works // respectively specify in their paragraphs 2 and 3 authorizing // only the reproduction and quoting of works on the condition // that : // // - "this reproduction does not adversely affect the normal // exploitation of the work or cause any unjustified prejudice // to the legitimate interests of the author". // // - that the quotations given by way of illustration and/or // tuition conform to the proper uses and that it mentions // the source and name of the author if this name features // in the source", // // - under the condition that this file is included with // any reproduction. // // Any commercial use made without obtaining the prior express // agreement of INRIA would therefore constitute a fraudulent // imitation. // // The Software beeing currently developed, INRIA is assuming no // liability, and should not be responsible, in any manner or any // case, for any direct or indirect dammages sustained by the user. // // Any user of the software shall notify at INRIA any comments // concerning the use of the Sofware (e-mail : FracLab@inria.fr) // // This file is part of FracLab, a Fractal Analysis Software [nargout,nargin] = argn(0) ; // CHECK INPUT FORMATS [xr,xc] = size(x) ; if xr ~= 1 & xc ~= 1 error('1-D signals only') elseif xc == 1 x = conj(x') ; end // DEFAULT VALUES nt = length(x) ; if exists('wave') == 0 wave = 0 ; end if nargin == 1 XTF = fft(mtlb_fftshift(x),-1) ; sp = (abs(XTF(1:nt/2))).^2 ; f = linspace(0,0.5,nt/2+1) ; f = f(1:nt/2) ; plot(f,sp) ; fmin = input('lower frequency bound = ') ; fmax = input('upper frequency bound = ') ; N = input('Frequency samples = ') ; fmin_s = string(fmin) ; fmax_s = string(fmax) ; N_s = string(N) ; disp(['frequency runs from ',fmin_s,' to ',fmax_s,' over ',N_s,' points']) ; end if nargin == 5 if fmin >= fmax error('fmax must be greater to fmin') ; end end f = logspace(log10(fmax),log10(fmin),N) ; a = logspace(log10(1),log10(fmax/fmin),N) ; amax = max(a) ; if length(wave) == 1 if abs(wave) > 0 nh0 = abs(wave) ; for ptr = 1:N nha = round(nh0 * a(ptr)) ; ha = conj(morlet(f(ptr),nha,~mtlb_isreal(wave))) ; nbmir = min(nt,nha) ; x_mir = [x(nbmir:-1:2) x x(nt-1:-1:nt-nbmir+1)] ; detail = convol(ha,x_mir) ; wt(ptr,1:nt) = detail(nha + nbmir : nha + nbmir + nt -1 ) ; end elseif wave == 0 for ptr = 1:N ha = mexhat(f(ptr)) ; nha = (length(ha)-1)/2 ; nbmir = min(nt,nha) ; x_mir = [x(nbmir:-1:2) x x(nt-1:-1:nt-nbmir+1)] ; detail = convol(ha,x_mir) ; wt(ptr,1:nt) = detail(nha + nbmir : nha + nbmir + nt -1 ) ; end end wavescaled = wave ; elseif length(wave) > 1 wavef = fft(wave,-1) ; nwave = length(wave) ; f0 = find(abs(wavef(1:nwave/2)) == max(abs(wavef(1:nwave/2)))) ; f0 = mtlb_mean((f0-1).*(1/nwave)) ; disp(['mother wavelet centered at f0 = ',string(f0)]) ; f = logspace(log10(fmax),log10(fmin),N) ; a = logspace(log10(f0/fmax),log10(f0/fmin),N) ; amax = max(a) ; B = 0.99 ; R = B/((1.001)/2) ; nscale = max(128,round((B*nwave*(1+2/R)*log((1+R/2)/(1-R/2)))/2)) ; [wavescaled,nt_a] = dilate(wave,a,0.001,0.5,nscale) ; wavescaled = real(wavescaled) ; for ptr = 1:N ha = wavescaled(2:wavescaled(1,ptr),ptr) ; firstindice = (wavescaled(1,ptr)-mtlb_rem(wavescaled(1,ptr),2))/2 ; nbmir = min(nt,firstindice) ; x_mir = [x(nbmir:-1:2) x x(nt-1:-1:nt-nbmir+1)] ; detail = convol(ha,x_mir) ; detail = detail(firstindice + nbmir : firstindice + nbmir + nt -1 ) ; wt(ptr,1:nt) = conj(detail(:)') ; end end if nargout >= 4 scalo = real(wt.*conj(wt)) ; end
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////////////////////////////////////////////////////////////////////////////// // Author: Jia Wu // Version: 0.1 // Date: Dec. 2009 // // // Copyright (C) 2009 OpenPR // All rights reserved. // // Redistribution and use in source and binary forms, with or without // modification, are permitted provided that the following conditions are met: // // * Redistributions of source code must retain the above copyright // notice, this list of conditions and the following disclaimer. // * Redistributions in binary form must reproduce the above copyright // notice, this list of conditions and the following disclaimer in the // documentation and/or other materials provided with the distribution. // * Neither the name of OpenPR nor the names of its // contributors may be used to endorse or promote products derived // from this software without specific prior written permission. // // THIS SOFTWARE IS PROVIDED BY HOLDERS AND CONTRIBUTORS "AS IS" AND ANY // EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED // WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE // DISCLAIMED. IN NO EVENT SHALL HOLDER AND CONTRIBUTORS BE LIABLE FOR ANY // DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES // (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; // LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND // ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT // (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS // SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. //////////////////////////////////////////////////////////////////////////// /////////////////////////////////////////////////////////////////////////////// // Input: // data - dim*num data matrix; each column is a data point. // k - number of nearest neighbors. // b - b > 1 is a free parameter chosen to adjust the // ¡°blending¡± of different clusters // Output: // labels - labels of the input data. // centroids - cluster centroids /////////////////////////////////////////////////////////////////////////////// function [labels, centroids] = fuzzy_kmeans(data, k, b) if k<1, error('k should be a positive integer.'); end [dim, num] = size(data); labels = zeros(1, num); dist = zeros(k, num); //initialize means [val, idx] = sort(rand(1, num)); sel = idx(1:k); m = data(:, sel)+mean(data, 'c')*ones(1,k); o_m = zeros(dim, k); //initialize degrees p = rand(k, num); p = p./(ones(k,1)*sum(p,'r')); o_p = zeros(k, num); while((sum(abs(m-o_m))>1e-5)&(sum(abs(p-o_p))>1e-5)), o_m = m; o_p = p; for i=1:k, dist(i,:) = sum((data-m(:,i)*ones(1,num)).^2, 'r'); end //recompute degrees p = (dist.^(-1)).^(1/(b-1)); p = p./(ones(k,1)*sum(p,'r')); //recompute means p = p.^b; m = (data*p')./(ones(dim,1)*sum(p, 'c')'); end [maximun, labels] = max(p, 'r'); centroids = m; endfunction
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main(){ if(i<=0){ j=j+1; }}
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//Caption:Find the current in the coil //Exa:3.5 clc; clear; T=20;//torque exerted by spring (in Newton-meter) r=0.2;//radius of spring (in meter) F_s=T/r;//force exerted by spring on magnetic plate N=1000;//no. of turns in coil u_o=4*%pi*10^-7;//permablityof air A=9*10^-4;//area (in meter^2) function y = L ( x );//inductance y = (N^2)/ R ( x ); endfunction; function y = R ( x );//reluctance of air gap y = (2*x)/(u_o*A); endfunction; x = [0.001 ]'; // Points of interest t=[diag(derivative(L,x))];//t=dL/dx (at x=0.001m) //since t<o i.e,F_m is acting in opp direction that of weight //for equilibrium F_m=F_s I=sqrt((2*F_s)/(t*(-1)));//Refer to eqn3.23 disp(I,'current in the coil (in Amperes)=')