guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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X@,rb) =<br />
where 7, is the 4 x 4(matrix fundamental matrix solution)<br />
\<br />
<strong>and</strong> wherep[&)is the initial value<br />
with (2.4.145).<br />
ofp <strong>and</strong> is to be selected consistent<br />
97<br />
(2.4.147)