Design and Optimization of Return Orbit of Circumlunar Spacecraft

被引：0
|
作者：
Qiu S. [1 ]
Cao X.-B. [1 ]
Wang F. [1 ]
Zhang G. [1 ]
机构：
[1] School of Astronautics, Harbin Institute of Technology, Harbin
来源：
| 1600年 / China Spaceflight Society卷 / 41期
关键词：
Characteristic analysis; Circumlunar spacecraft; Function construction method; Return trajectory;
D O I：
10.3873/j.issn.1000-1328.2020.07.008
中图分类号：
学科分类号：
摘要：
A method for designing a lunar return orbit based on the Lambert problem is proposed according to the limitation of the traditional orbit design method. An orbital dynamic model is presented in three-dimensional space using new constrained parameters. The characteristics of the lunar return orbits based on this model are well studied. A function construction method is presented to deal with the optimal design with constraint conditions and an effective objective function is proposed. The orbital parameters of a certain circumlunar spacecraft are used as the initial values to design the return orbit. The results verify the effectiveness of the proposed return orbit design method and function construction method. © 2020, Editorial Dept. of JA. All right reserved.
引用
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页码：901 / 909
页数：8
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