guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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Alternately, for two neighboring points along the, curve<br />
sayxsndx-t6x<br />
where<br />
Thus, dividing by 6% <strong>and</strong> taking the limit provides<br />
But from (2.4.47)<br />
73<br />
(2.4.50)