MAXIMUM RANGE THREE-DIMENSIONAL LIFTING PLANETARY ENTRY.

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作者：
Dickmanns, E.D.
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来源：
NASA Technical Reports | 1972年 / TR R-387期
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V4 [航天（宇宙航行）];
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摘要：
Variational equations for maximum range three-dimensional quasisteady glide are given. Nonlinear oscillatory maximum range trajectories obtained with a refined gradient program are approximated by a superposition of quasisteady glide and linearized perturbation equation results. A ″basic″ control law is found which is closely followed for maximum cross-range trajectories. The effect of a reradiative heating constraint involving velocity, altitude and angle of attack on maximum cross-range trajectory for a Space Shuttle orbiter-type vehicle reentering the earth's atmosphere is investigated numerically.
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