guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
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)