guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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I. -.<br />
In order to give an appreciation for the need for more sophisticated tech-<br />
niques, a sample problem will be worked by the Dynamic Programming techniques<br />
which have been discussed. The presentation will serve two purposes: first,<br />
it will illustrate the use of Dynamic Programming on a multi-dimensional<br />
allocation problem <strong>and</strong>, second,- it will demonstrate the rapid growth of<br />
storage requirements as a function of the dimension of the problem. The<br />
method of approximation in policy space will then be discussed in order to<br />
illustrate the savings in storage requirements <strong>and</strong> the increase in computa-<br />
tion time.<br />
Consider the problem of minimizing the function<br />
subject to the constraint that<br />
<strong>and</strong><br />
(2.3.4)<br />
z, + x2 + x3 = 3 (2.3.5)<br />
VJ + fi + $5 = 3 (2.3.6)<br />
Obviously, using Dynamic Programming to find a solution to this problem is<br />
not very efficient. The method of Lagrange multipliers is by far a more<br />
suitable method. However, the Dynamic Programming solution will be shobm<br />
for illustrative purposes.<br />
First, the problem i.s reduced to a series of simpler problem.<br />
53<br />
(2.3.7)<br />
(2.3.8)<br />
(2.3.9)