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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)

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