宇航学报

宇航学报 ›› 2021, Vol. 42 ›› Issue (12): 1532-1541.doi: 10.3873/j.issn.1000-1328.2021.12.006

• 制导、导航、控制与电子 • 上一篇    下一篇

航天器零推进剂姿态机动启发式规划方法

王卓，徐瑞，李朝玉，朱圣英，陈德相   

  1. 1. 北京理工大学宇航学院，北京 100081；2. 深空自主导航与控制工业和信息部重点实验室，北京 100081；
    3.上海卫星工程研究所，上海 200240
  • 收稿日期:2021-02-05 修回日期:2021-04-07 出版日期:2021-12-15 发布日期:2021-12-15
  • 基金资助:
    国家重点研发计划资助(2019YFA0706500)；国家自然科学基金（61976020）

Heuristic Planning Method of Spacecraft Zero Propellant Maneuver

WANG Zhuo, XU Rui, LI Zhao yu, ZHU Sheng ying, CHEN De xiang   

  1. 1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2. Key Laboratory of Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 100081, China;3. Shanghai Institute of Satellite Engineering, Shanghai 200240, China
  • Received:2021-02-05 Revised:2021-04-07 Online:2021-12-15 Published:2021-12-15

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摘要： 针对零推进剂姿态机动约束耦合，导致规划效率低的问题，提出一种基于约束评价启发式的差分进化算法。基于零推进剂姿态机动约束分析，在规划空间中建立约束评价函数，对航天器约束和控制力矩陀螺约束进行解耦分类处理。设计基于约束评价函数的启发式策略，用于改进差分进化算法的种群变异，主动控制规划进程，引导零推进剂姿态机动规划序列满足多种约束，得到安全的姿态机动路径和控制力矩陀螺框架角路径。最后，数值仿真结果验证了该方法能够实现航天器零推进剂姿态机动规划。


关键词: 零推进剂姿态机动, 约束评价函数, 启发式策略, 姿态规划

Abstract: 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.


Key words: Zero propellant maneuver, Constraint evaluation function, Heuristic strategy;Attitude planning

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