guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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 />
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