飞网抛射过程母卫星姿态干扰分析与姿态控制

高智杰; 孙富春; 闵海波; 王士星

doi:10.6052/0459-1879-12-249

飞网抛射过程母卫星姿态干扰分析与姿态控制

doi: 10.6052/0459-1879-12-249

1.
清华大学计算机科学与技术系, 北京100084
2. 第二炮兵装备研究院, 北京100085

基金项目: 国家自然科学基金资助项目(60904083,61203354).

详细信息

通讯作者:
高智杰,博士研究生,主要研究方向:智能控制理论与应用、卫星动力学分析与协同控制.E-mail:zjiegao@163.com

中图分类号: V423
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- 被引次数: 0
出版历程
- 收稿日期: 2012-09-13
- 修回日期: 2012-10-23
- 刊出日期: 2013-05-18

STUDY ON ATTITUDE DISTURBANCE AND CONTROL OF MOTHER SATELLITE DURING SPACE NET PROJECTING

1.
Department of Computer Science and Technology, Tsinghua University, Beijing 100084, China
2. The Second Artillery Equipment Academy, Beijing 100085, China

Funds: The project was supported by the National Natural Science Foundation of China (60904083, 61203354).

摘要

摘要: 空间飞网是一种新型的空间碎片或漂浮物回收装置. 飞网抛射过程会对母体卫星产生较大的干扰,影响卫星的姿态稳定,因此需要设计具有抗干扰能力的控制律来保证卫星姿态的稳定. 针对空间飞网直接抛射展开过程,分析了影响飞网抛射效果的主要因素,并建立了飞网发射所产生的干扰力矩模型. 针对卫星的控制要求,建立了卫星姿态控制系统的模型,设计了滑模变结构控制器,并给出数学推导过程. 最后,通过仿真对姿态干扰及控制器控制性能进行了分析研究,结果表明,设计的控制器能够保证卫星的稳定,满足设计指标要求.
- 飞网 /
- 母卫星 /
- 抛射 /
- 姿态控制 /
- 滑模控制
Abstract: Space net capturing is a novel technique for spacecraft capturing. In this paper, the disturbance imposed on the mother satellite, and the induced attitude control problem of the satellite, are investigated. Attention is focused on the dynamic process of mass ejection. The main factors affecting the performance of the net are analyzed and the model of the disturbance torque is developed. A sliding mode controller is developed to stabilize the attitude of the satellite and rigid mathematical proof is provided. Numerical simulation is conducted which demonstrates the effectiveness of the proposed algorithm.
- space net /
- mother satellite /
- projecting /
- attitude control /
- sliding mode

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参考文献(12)

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