ASE 167M - Runge-Kutta step 4

ASE 167M - Runge-Kutta step 4 - hieght(i) = hieght(i-1) +

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clear all close all clc global g W Sw CDstar CLstar CD0 = 0.02; K = 0.07; h0 = 10000; g = 32.2; t0 = 0; W = 11000; CLstar = sqrt(CD0 / K); CDstar = 2 * CD0; Sw = 232; [temp, press, dens, sos] = atmos62(h0); V0 = sqrt(2 * W / (dens * Sw * CLstar)); gamma0 = -1 * CDstar / CLstar; x0 = 0; z0 = [x0; h0; V0; gamma0]; h = h0; t = t0; time(1) = t0; i = 0; dt = 2; htol = 1e-4; [Z] = RK4(@gf_derivs, [t t + dt], z0); h = Z(2); if(h < -htol) dt = 0.5 * dt; if (dt < 1e-9) break end elseif(h > htol) t = t + dt; i = i + 1; time(i) = t; z0 = Z; x(i) = Z(1); H(i) = Z(2); V(i) = Z(3); gamma(i) = Z(4); end end e hieght = h0; X = x0; Gamma = gamma0; v = V0; i = 2;
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Unformatted text preview: hieght(i) = hieght(i-1) + v(i-1)*Gamma(i-1)*dt; X(i) = X(i-1) + v(i-1)*dt; [temp, press, dens, sos] = atmos62(hieght(i)); v(i) = sqrt(2 * W / (dens * Sw * CLstar)); if (hieght(i) &lt; -htol) dt = 0.5 * dt; elseif (hieght &gt; htol) i = i + 1; end end e figure(2) hold on plot(x, H) plot( xlabel('Distance (ft)') ylabel('Altitude (ft)') title('Distance vs. Altitude') figure(3) hold on plot(x, V) xlabel('Time (sec)') ylabel('Velocity (ft/sec)') title('Time vs. Velocity') figure(4) hold on plot(x, gamma) xlabel('Time (sec)') ylabel('Flight Path Angle (rad)') title('Time vs. Flight Path Angle') t...
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ASE 167M - Runge-Kutta step 4 - hieght(i) = hieght(i-1) +

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