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148 CHAPTER 5. FEEDBACK SYSTEMS<br />

In our case<br />

a¢(xl )<br />

ax,<br />

avl<br />

-(1 + 2axi)<br />

=> O(xl, x2) = -(1 + 2ax1) [axi + x2] - x1 - [X2 + x1 + axi]<br />

where we have chosen k = 1. We now move on to the final step, in which we consider the<br />

third order system as a special case of (5.7)-(5.8) with<br />

x= I<br />

f<br />

x1<br />

x2 J J L 0 J<br />

L f(x1) Og(x1)x2<br />

From the results in the previous section we have that<br />

U = 090(x1, x2) [f (XI) + 9(xl)x2] + aO(xl, x2) X3 _ aV2<br />

axi 09x2 09x2<br />

is a stabilizing control law with associated Lyapunov function<br />

V +21<br />

5.3.2 Strict Feedback <strong>Sy</strong>stems<br />

We now consider systems of the form<br />

f (x) +CC 9(x)S1<br />

CC CC<br />

S1 = fl (x, Si) + 91(x, Sl)SCC2<br />

2 = f2(x,e1,6) + 92(x,6,6)e3<br />

9<br />

A,I,<br />

- k[x3 - W(xl, x2)], k > 0<br />

Sk-1 = A-1 (X, 6, S2, Sk-1) + 9k-1(x, SL 61- ' GAG<br />

6 = A(Xi61 2) ...7<br />

G)+A(xi6)6,.,Ck)U<br />

where x E R', Ct E R, and fi, g= are smooth, for all i = 1, , k. <strong>Sy</strong>stems of this form<br />

are called strict feedback systems because the nonlinearities f, fzf and gz depend only on<br />

the variables x, C1, that are fed back. Strict feedback systems are also called triangular<br />

0

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