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% Fig. 6.46 Feedback Control of Dynamic Systems, 4e % Franklin, Powell, Emami % clear all; close all; num=1; den=[1 0 0]; w=logspace(-2,2,100); [m,p]=bode(num,den,w); loglog(w,m); grid; xlabel('\omega (rad/sec)'); ylabel('magnitude'); title('Fig. 6.46 Spacecraft frequency-response magnitude');
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