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controller structure & nonsmooth programming - Pierre Apkarian - Free

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challenges <strong>nonsmooth</strong> opt. MATLAB tools The End<br />

<strong>controller</strong> <strong>structure</strong><br />

• more complicated aircraft longitudinal law<br />

reference<br />

model<br />

R(s)<br />

z 1<br />

−<br />

feed<br />

forward<br />

F f (s)<br />

z 2<br />

r<br />

−<br />

K p + Ki<br />

s<br />

−<br />

roll−off<br />

filter<br />

F (s)<br />

aircraft<br />

G(s)<br />

N z<br />

q<br />

K q(s)<br />

w<br />

• tunable blocks often designed independently (suboptimal)<br />

<br />

<strong>controller</strong> <strong>structure</strong> & <strong>nonsmooth</strong> <strong>programming</strong> - http://pierre.apkarian.free.fr<br />

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