guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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It is interesting to compare the value of the performance index for<br />
the perfectly, observable <strong>and</strong> perfectly inobservable cases. Since more<br />
information is available <strong>and</strong> is used in the perfectly observable case, the<br />
performance index for the perfectly observable case is the smaller of<br />
the two. Let the covariance of the initial state, V, is Eq. (2.5.31) be<br />
taken as zero. Hence, the initial state is known exactly in both the<br />
perfectly observable <strong>and</strong> inobservable cases <strong>and</strong> is given by<br />
4<br />
8-L = z. AT t-4<br />
From Eq. (2.5.28) <strong>and</strong> the expression for @ in (2.5.24) <strong>and</strong> (2.5.26),<br />
the performance index in the perfectly observable case is given by<br />
while from Equation (2.5.52)<br />
EfJ) = $5X0) Jo f ! tr (CS) dt (2.5.53A)<br />
OBSIiUVABLE<br />
4<br />
IN OBSEK?VABLP<br />
Since the matrix s satisfies<br />
both cases, it follows that<br />
ml<br />
-E/-i{<br />
4<br />
~'s&,);, +jtr(I/Q,)dt +tr&A) (2.5.53B)<br />
c<br />
the same equation <strong>and</strong> boundary condition in<br />
This difference can be shown to be positive by noting that s <strong>and</strong> V,from<br />
Eqs. (2.5.49) <strong>and</strong> (2.5.36),satisfy<br />
Integrating this expression with the condition that t/(f,)=O <strong>and</strong><br />
combining with (2.5.54) yields<br />
123<br />
(2-5=55)