guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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2.2.2.2 Variational Problem with Movable Boundary<br />
Dynamic Progr amming will now be applied to the solution of a variational<br />
problem with a movable boundary. Consider the minimization of the functional<br />
subject to the constraint that<br />
L/co, = 0<br />
6<br />
= q-5<br />
(2.2.6)<br />
This problem appears as an example in Ref. 2.2.2 to illustrate the classical<br />
solution of a problem with a movable boundary. Note that this problem dif-<br />
fers in concept from the preceding problem in that the upper limit of<br />
integration is not explicitly specified. However, as would be suspected from<br />
previous problems, the Dynamic Programming approach still involves the divi-<br />
sion of the space into segments <strong>and</strong> the calculation of the cost of each<br />
transition. The set of end points is located on the line vr = )c~ -5. As<br />
mentioned earlier, there are two ways to perform the Dynamic Programming<br />
calculations in most problems. One method initiates the computation at the<br />
first stage <strong>and</strong> progresses to the last stage; the second method begins the<br />
computation at the end of the process <strong>and</strong> progresses to the first stage.<br />
Both methods are equivalent <strong>and</strong> yield the same answers as shown in an earlier<br />
example. The following example will be partially solved by using the second<br />
method. (The number of computations prohibits the complete manual solution.)<br />
The other problems in this section use the first method.<br />
To begin the Dynamic Programming solution, the space is divided as shown<br />
in the following sketch,<br />
23