## 留言板

 引用本文: 张治国, 李俊峰. 卫星编队飞行轨道和姿态控制研究[J]. 应用数学和力学, 2008, 29(1): 38-46.
ZHANG Zhi-guo, LI Jun-feng. Study on the Orbit and Attitude Control of Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(1): 38-46.
 Citation: ZHANG Zhi-guo, LI Jun-feng. Study on the Orbit and Attitude Control of Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(1): 38-46.

## 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).
• 中图分类号: V412.4

## Study on the Orbit and Attitude Control of Spacecraft Formation Flying

• 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．
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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

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