卫星编队飞行轨道和姿态控制研究

张治国; 李俊峰

卫星编队飞行轨道和姿态控制研究

清华大学航天航空学院,北京 100084

基金项目: 国家自然科学基金资助项目(10672084);高等学校博士学科点专项科研基金资助项目(20060003097)

详细信息

作者简介:
张治国(1979- ),男,湖南常德人,博士生(联系人.Tel:+86-10-62773402;Fax:+86-10-62781824;E-mail:zzg7979@126.com).

中图分类号: V412.4
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出版历程
- 收稿日期: 2007-01-17
- 修回日期: 2007-11-12
- 刊出日期: 2008-01-15

Study on the Orbit and Attitude Control of Spacecraft Formation Flying

School of Aerospace, Tsinghua University, Beijing 100084, P. R. China

摘要

摘要: 卫星编队飞行是一种卫星应用的新概念，通过一系列造价更便宜的小卫星的分布式合作，代替大卫星实现复杂功能．在编队飞行一些应用中，要求受控卫星对目标卫星保持要求的相对位置和姿态以观察目标卫星的特定面，特别的，目标卫星可能是失效的．研究在近地轨道如何控制追踪星在失效的目标卫星附近飞行以追踪目标卫星特定面的问题，给出了相对姿态和一阶近似的相对轨道动力学方程．基于线性反馈和Liapunov稳定性理论设计了控制策略．进一步的，考虑目标卫星转动惯量的不确定性，通过自适应控制的方法，获得正确的转动惯量比率．数值仿真算例验证了该控制方法的有效性．
- 卫星编队飞行 /
- 相对轨道 /
- 相对姿态 /
- 动力学和控制
Abstract: Formation flying is a novel concept of distributing the functionality of large spacecraft among several smaller, less expensive, cooperative satellites. Some applications require that a controllable satellite keep relative position and attitude to observe a specific surface of another satellite among the cluster. Specially, the target space vehicle is malfunctioning. The problem of how to control a chaser satellite to fly around an outofwork target satellite closely in earth orbit and to track a specific surface is focused on. Relative attitude and first approximate relative orbital dynamics equations are presented. Control strategy is derived based on feedback linearization and Lyapunov theory of stability. Further, the uncertainty of inertia being considered, an adaptive control method is developed to obtain the correct inertial ratio. The numerical simulation is given to verify the validity of proposed control scheme.
- satellite formation flying /
- orbit /
- attitude /
- dynamics and control

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参考文献(28)

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卫星编队飞行轨道和姿态控制研究

作者简介:
张治国(1979- ),男,湖南常德人,博士生(联系人.Tel:+86-10-62773402;Fax:+86-10-62781824;E-mail:zzg7979@126.com).

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Study on the Orbit and Attitude Control of Spacecraft Formation Flying

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卫星编队飞行轨道和姿态控制研究

作者简介: 张治国(1979- ),男,湖南常德人,博士生(联系人.Tel:+86-10-62773402;Fax:+86-10-62781824;E-mail:zzg7979@126.com).

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Study on the Orbit and Attitude Control of Spacecraft Formation Flying

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出版历程

目录

作者简介:
张治国(1979- ),男,湖南常德人,博士生(联系人.Tel:+86-10-62773402;Fax:+86-10-62781824;E-mail:zzg7979@126.com).