This paper considers the minimum-time control of aeroassisted orbital transfer vehicle (AOTV) which arises in the study of coplanar HEO-LEO orbital transfer.
本文研究了在共面圆轨道HEO-LEO的过程中，气动辅助轨道转移飞行器（AOTV）在大气内飞行的极小时间控制问题。
Up to now the singular optimal control problems in the thrust synergetic orbital transfer have not been completely solved.
特别是由推力协同变轨所导致的奇异最优控制问题到目前尚没有完全解决。
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