常推力作用下飞行器固定时间最优交会

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常推力作用下飞行器固定时间最优交会

谌颖,陈祖贵,刘良栋

北京控制工程研究所

发布日期:1998-04-25

OPTIMAL BOUNDED THRUST TIME FIXED RENDEZVOUS OF SPACECRAFT

Chen Ying Chen Zugui Liu Liangdong (Beijing Institute of Control Engineering,Beijing 100080)

Published:1998-04-25
Supported by:
国家自然科学基金

摘要/Abstract

摘要： 研究了在常推力作用下，两个空间飞行器的固定时间最省燃料交会问题。通过对飞行器交会过程中最优推力弧段的研究，给出了关于飞行器的最优推力弧段的几个性质。这些结果为空间飞行器交会对接的工程设计提供了理论依据。

关键词: 常推力, 交会航天器

Abstract: The problem of optimal bounded thrust time fixed rendezvous of two spacecraft is investigated in this paper.Several properties on optimal thrust arcs are presented on the basis of the rendezvous process of spacecraft.These results have provided the theoretical fundamentals for the engineering design of rendezvous and docking of spacecraft.

谌颖,陈祖贵,刘良栋. 常推力作用下飞行器固定时间最优交会[J]. .

Chen Ying Chen Zugui Liu Liangdong (Beijing Institute of Control Engineering,Beijing 100080). OPTIMAL BOUNDED THRUST TIME FIXED RENDEZVOUS OF SPACECRAFT[J]. .