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guidance, flight mechanics and trajectory optimization

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2.4.8 The Problem of Bolza<br />

The preceding sections have delt with the Dynamic Programming formulation<br />

of the problem of Lagrange. In this section the Bolza Problem will be<br />

considered, since optimal <strong>trajectory</strong> <strong>and</strong> control problems are usually cast<br />

in this form. The Bellman equation for this case will be-developed <strong>and</strong><br />

some solutions presented. Also, some comparisons <strong>and</strong> parallels will be<br />

drawn between the Dynamic Programming approach <strong>and</strong> the Pontryagin Maximum<br />

Principle (Ref. 2.4.3).<br />

The problem of Bolza is usually stated in the following form: given<br />

the dynamical system<br />

ii = J(%,Lo ; L’=/,R (2.4.81A)<br />

or in the vector notation<br />

where the state x is a n-dimensional vector,<br />

<strong>and</strong> the control u is a r-dimensional vector,<br />

i= f(X) u) (2.4.81~)<br />

which is required to lie in some closed set u in the r-dimensional control<br />

space; determine the control history u(t) for which the functional<br />

J =s” $<br />

4<br />

(x,u)dt +$(x~,$) = minimum<br />

is minimized subject to the terminal constraints<br />

82<br />

(2.4.82)<br />

(2.4.83)<br />

(2.4.84)<br />

(2.4.85)

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