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Nonlinear Control Sy.. - Free

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itrJ<br />

A.3. CHAPTER 6<br />

V<br />

315<br />

Thus,<br />

f If<br />

P = (DT(T,t)Q(T)a(D(T,t) dr+J<br />

4T(T,t)Q(T)41(T,t)<br />

dT - Q(t)<br />

J<br />

4pT<br />

(T, t)Q(T)4D (T, t) dTl - Q(t)<br />

-l A(t)-AT(t) 00<br />

which implies that<br />

A.3 Chapter 6<br />

P = -P(t)A(t) - AT(t)p(t) - Q(t).<br />

Theorem 6.1 Consider a function P(s) E R(s). Then F(s) E A if and only if (i) P(s) is<br />

proper, and (ii) all poles of F(s) lie in the left half of the complex plane.<br />

Proof: Assume first that P(s) satisfies (i) and (ii), and let n(s)andd(s) E R[s] respectively,<br />

be the numerator and denominator polynomials of F(s). Dividing n(s) by d(s), we can<br />

express F(s) as:<br />

F(s) = k + d s) = k + G(s) (A.9)<br />

where k E 1R and d(s) is strictly proper. Expanding G(s) in partial fractions and antitransforming<br />

(A.9), we have<br />

n<br />

f (t) = G-1{F(s)} = kb(t) + E g2(t)<br />

where n is the degree of d(s) and each g2 has one of the following forms [u(t) represents<br />

the unit step function : (i) ktii-1e)tu(t), if A < 0 is a real pole of multiplicity m; and<br />

(ii) ke(°+.3.+)tu(t), a < 0, if A = (v +,yw) is a complex pole. It follows that f (t) E A, and<br />

so F(s) E A. To prove the converse, notice that if (i) does not hold, then f (-) contains<br />

derivatives of impulses and so does not belong to A._Also, if (ii) does not hold, then, clearly,<br />

for some i, g2 ¢ G1 and then f (t) V A and F(s) il A, which completes the proof.<br />

Theorem 6.2 Consider a linear time-invariant system H, and let represent its impulse<br />

response. Then H is L stable if and only if hoo(t) + ha,(t) E A and moreover, if H<br />

is Gp stable, then JjHxjjr < jh11A11x11p.<br />

2=1<br />

J

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