05.08.2013 Views

guidance, flight mechanics and trajectory optimization

guidance, flight mechanics and trajectory optimization

guidance, flight mechanics and trajectory optimization

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

(2.5.I.21)<br />

Thus, the control is to be selected to minimize the quantity inside the<br />

first set of brackets in Eq. (2.5.X1) (the quantity in the second bracket<br />

does not depend on U ), <strong>and</strong> the stochastic problem has been reduced to<br />

deterministic form.<br />

Then, using the Dynamic Programming approach, it follows that<br />

with the solution<br />

0 = ktlN ~‘Q~+LL~Q~u+~~ +<br />

u(t)<br />

-z<br />

The optimal control is given by<br />

(2.5.122)<br />

@.5.=3)<br />

(2.5.124)<br />

u=- Q;lGri 'ff rSi @.5.=5)<br />

To determine the value of h for which the terminal constraint is<br />

satisfied, note that<br />

142

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!