📄 c13l1.m
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X=200000.;
XD=-6000.;
BETA=500.;
XNOM=200000.;
XDNOM=-6000.;
BETANOM=800.;
TS=.1;
T=0.;
S=0.;
H=.001;
count=0;
while X>=0.
XOLD=X;
XDOLD=XD;
XNOMOLD=XNOM;
XDNOMOLD=XDNOM;
XDD=.0034*32.2*XD*XD*exp(-X/22000.)/(2.*BETA)-32.2;
XDDNOM=.0034*32.2*XDNOM*XDNOM*exp(-XNOM/22000.)/(2.*BETANOM)-32.2;
X=X+H*XD;
XD=XD+H*XDD;
XNOM=XNOM+H*XDNOM;
XDNOM=XDNOM+H*XDDNOM;
T=T+H;
XDD=.0034*32.2*XD*XD*exp(-X/22000.)/(2.*BETA)-32.2;
XDDNOM=.0034*32.2*XDNOM*XDNOM*exp(-XNOM/22000.)/(2.*BETANOM)-32.2;
X=.5*(XOLD+X+H*XD);
XD=.5*(XDOLD+XD+H*XDD);
XNOM=.5*(XNOMOLD+XNOM+H*XDNOM);
XDNOM=.5*(XDNOMOLD+XDNOM+H*XDDNOM);
S=S+H;
if S>=(TS-.00001)
S=0.;
DELXH=X-XNOM;
DELXDH=XD-XDNOM;
DELBETAH=BETA-BETANOM;
XH=XNOM+DELXH;
XDH=XDNOM+DELXDH;
BETAH=BETANOM+DELBETAH;
count=count+1;
ArrayT(count)=T;
ArrayX(count)=X;
ArrayXD(count)=XD;
ArrayDELXH(count)=DELXH;
ArrayDELXDH(count)=DELXDH;
end
end
figure
plot(ArrayT,ArrayX),grid
xlabel('Time (Sec)')
ylabel('Altitude (Ft)')
axis([0 50 0 200000])
figure
plot(ArrayT,ArrayXD),grid
xlabel('Time (Sec)')
ylabel('Velocity (Ft/Sec)')
axis([0 50 -7000 0])
figure
plot(ArrayT,ArrayDELXH),grid
xlabel('Time (Sec)')
ylabel('Error in Altitude (Ft)')
axis([0 50 0 15000])
figure
plot(ArrayT,ArrayDELXDH),grid
xlabel('Time (Sec)')
ylabel('Error in Velocity (Ft/Sec)')
axis([0 50 0 1000])
clc
output=[ArrayT',ArrayX',ArrayXD',ArrayDELXH',ArrayDELXDH'];
save datfil.txt output -ascii
disp 'simulation finished'
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