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guidance, flight mechanics and trajectory optimization

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2.5<br />

DYNAMIC PROGRAMMING AND THE OPTIMIZATION OF STOCR$STIC~S$3Tl34S<br />

2.5.1 Introduction<br />

The previous sections of this report have dealt exclusively with the<br />

<strong>optimization</strong> of deterministic systems. In this section, some <strong>optimization</strong><br />

problems are considered in which the equations describing the system<br />

contain stochastic or r<strong>and</strong>om elements. This extension is considered<br />

desirable, if not necessary, since all phenomena occurring in nature are<br />

stochastic. That is, every physical process contains some parameters or<br />

elements which are not known exactly but which are known in some statistical<br />

sense. Fortunately, in many systems, the total effect of these r<strong>and</strong>om<br />

parameters on system behavior is negligible <strong>and</strong> the system can be approxi-<br />

mated by a deterministic model <strong>and</strong> analyzed using st<strong>and</strong>ard procedures. In<br />

other cases, however, the r<strong>and</strong>om elements are not negligible <strong>and</strong> may<br />

dominate those elements which are known precisely. The midcourse correction<br />

problem encountered in lunar <strong>and</strong> planetary transfer maneuvers is a case in<br />

point.<br />

Due to injection errors at the end of the boost phase of a planetary<br />

transfer, the vehicle's <strong>trajectory</strong> will differ slightly from the desired<br />

nominal condition, <strong>and</strong> hence, some correction maneuver will be required.<br />

To make such a maneuver, the <strong>trajectory</strong> error must be known;<br />

<strong>and</strong> so radar <strong>and</strong> optical measurement data are collected. This data will<br />

lead to a precise determination of the <strong>trajectory</strong> error only if the data<br />

itself are precise. Unfortunately, the measurements <strong>and</strong> measuring devices<br />

are not perfect. Hence, the midcourse maneuver which is made will not<br />

null the <strong>trajectory</strong> error. Rather, it will null some estimate of the error,<br />

for example, the most probable value of the error. The determination of when<br />

<strong>and</strong> how to make these corrections SO that the fuel consumed is a minimum is<br />

a problem of current interest in stochastic <strong>optimization</strong> theory. Note that<br />

if a deterministic model of the planetary transfer problem were used, the<br />

problem itself would cease to exist.<br />

At the present time, the area of optimal stochastic control is just<br />

beginning to be examined. Thus, there are no st<strong>and</strong>ard equations or<br />

st<strong>and</strong>ard approaches which can be applied to such systems. In fact, the<br />

literature on the subject contains very few problems which have been solved.<br />

One reason for this limited amount of literature is that the fundamental<br />

equations which are encountered are of the diffusion type; that is, they<br />

are second order partial differential equations, Hence, the method of<br />

characteristics, which is used in the deterministic case <strong>and</strong> which reduces<br />

the Bellman equation to a set of ordinary differential equation, can not be<br />

applied; rather, the partial differential equations must be utilized<br />

directly.<br />

A second factor contributing to the difficulty in h<strong>and</strong>ling stochastic<br />

problems is that the type of feedback being considered must be explicitly<br />

accounted for. This situation is just the opposite of that encountered<br />

in the deterministic case. If the initial state is known along with the<br />

control to be applied in a deterministic system, then all subsequent states<br />

108

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