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鹊桥二号中继星自主角动量管理设计及实现

郝策 王勇 关轶峰 王洪斌 胡少春 张迎发 郑永洁 韩沛宏

空间控制技术与应用2024,Vol.50Issue(6):42-49,8.
空间控制技术与应用2024,Vol.50Issue(6):42-49,8.DOI:10.3969/j.issn.1674-1579.2024.06.005

鹊桥二号中继星自主角动量管理设计及实现

Design and Application of Momentum Management for Queqiao-2 Relay Satellite

郝策 1王勇 2关轶峰 2王洪斌 3胡少春 2张迎发 2郑永洁 2韩沛宏2

作者信息

  • 1. 北京控制工程研究所,北京 100094||燕山大学,秦皇岛 066004
  • 2. 北京控制工程研究所,北京 100094
  • 3. 燕山大学,秦皇岛 066004
  • 折叠

摘要

Abstract

An autonomous momentum management strategy is proposed to solve the problems of the disturbance to the mission orbit and the influence on long-life of the Queqiao-2 relay satellite,which caused by the momentum wheel unloading under the control of thrust.Firstly,a momentum predictive model based on the satellite's attitude maneuver is established to predict the satellite's momentum changes,avoiding the problem of momentum wheel sat-uration during satellite maneuvering.Secondly,an event-triggering momentum management strategy is used to a-chieve autonomous management of the relay satellite on orbit momentum,increasing the jet unloading period effec-tively.In addition,the coupling jet unloading is adopted to improve the stability of obit maintenance.Finally,the experiments and flight results verify the effectiveness of the proposed momentum management strategy.

关键词

鹊桥二号中继星/预测模型/角动量管理/角动量卸载

Key words

Queqiao-2 relay satellite/predictive model/momentum management/momentum wheel unloading

分类

航空航天

引用本文复制引用

郝策,王勇,关轶峰,王洪斌,胡少春,张迎发,郑永洁,韩沛宏..鹊桥二号中继星自主角动量管理设计及实现[J].空间控制技术与应用,2024,50(6):42-49,8.

基金项目

国家重大专项工程探月四期 Major National Projects of China(The 4th Stage of China's Lunal Exploration) (The 4th Stage of China's Lunal Exploration)

空间控制技术与应用

OA北大核心CSTPCD

1674-1579

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