Heuristic Planning Method of Spacecraft Zero Propellant Maneuver

被引：0
|
作者：
Wang Z. [1 ,2 ]
Xu R. [1 ,2 ]
Li Z.-Y. [1 ,2 ]
Zhu S.-Y. [1 ,2 ]
Chen D.-X. [3 ]
机构：
[1] School of Aerospace Engineering, Beijing Institute of Technology, Beijing
[2] Key Laboratory of Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing
[3] Shanghai Institute of Satellite Engineering, Shanghai
来源：
Yuhang Xuebao/Journal of Astronautics | 2021年 / 42卷 / 12期
关键词：
Attitude planning; Constraint evaluation function; Heuristic strategy; Zero propellant maneuver;
D O I：
10.3873/j.issn.1000-1328.2021.12.006
中图分类号：
学科分类号：
摘要：
Aiming at the problem of low planning efficiency caused by zero propellant maneuver (ZPM) constraint coupling, a constraint evaluation heuristic differential evolution algorithm is proposed. Based on the analysis of the ZPM constraints, a constraint evaluation function is established in the planning space to decouple the spacecraft constraints and control the moment gyroscope constraints. A heuristic strategy based on the evaluation function is designed to improve the population mutation of the differential evolution algorithm, actively control the planning process, guide the ZPM planning sequence to satisfy various constraints, and obtain the safe attitude maneuver path and control the moment gyroscope gimbal angle path. Finally, the results of numerical simulation show that this method can realize the ZPM planning of spacecraft. © 2021, Editorial Dept. of JA. All right reserved.
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页码：1532 / 1541
页数：9
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