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guidance, flight mechanics and trajectory optimization

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y<br />

2.4.11 Dynamic Programming <strong>and</strong> the Pontryagin Maximum Principle<br />

For the Bolza problem under consideration, the state system is given<br />

<strong>and</strong> the boundary conditions by<br />

ii = 4 cr, u)<br />

(2.4.148)<br />

x = x0 AT t =t, (2.4.149)<br />

7 C;r,,$)=O j .J=/,& pr r=+ (2.4.150)<br />

where t may or may not be specified. The control action u is to be selected<br />

so thatfan integral plus the function of the terminal state of the form<br />

G<br />

J ={ % (x,u)ort + +(X,9t,)= minimum<br />

0<br />

is a minimum. An application of the Pontryagin Max5mum Principle to this<br />

problem (Ref. 2.4.3) leads to the following requirements:<br />

(1) the control u is selected fromu so that at each instant the<br />

quantity H where<br />

(2.4.151)<br />

H = p’ f (x, u)- 7&t) = J; 3 5. (+.+ih%,U) (2.4.152)<br />

I<br />

is maximized.<br />

(2) the adjoint vector? satisfies the differential equations<br />

(2.4.153)

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