| 空间飞行器快速高精度姿态控制技术研究 |
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| 引用本文： | 樊会兵.空间飞行器快速高精度姿态控制技术研究[J].航天控制,2004,22(4):48-51. |
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| 作者姓名： | 樊会兵 |
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| 作者单位： | 北京航天自动控制研究所,北京,100854 |
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| 摘 要： | 针对空间飞行器在某些情况下对姿态偏差及姿态稳定度的严格要求 ,采用了超前网络校正和开关反馈控制的复合控制方法 ,同时从工程应用角度出发 ,对开关反馈的信号进行了调整 ,仿真结果表明这种复合控制在一定程度上解决了采用单一控制方式时控制精度与响应速度之间的矛盾。
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| 关 键 词： | 空间飞行器 姿控系统 开关反馈 极限环 |
| 文章编号： | 1006-3242(2004)04-0048-04 |
| 修稿时间： | 2004年4月9日 |
Study on High Precision Attitude Control System of Spacecraft |
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| Fan Huibing Beijing Aerospace Automatic Control Institute,Beijing.Study on High Precision Attitude Control System of Spacecraft[J].Aerospace Control,2004,22(4):48-51. |
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| Authors: | Fan Huibing Beijing Aerospace Automatic Control Institute Beijing |
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| Institution: | Fan Huibing Beijing Aerospace Automatic Control Institute,Beijing 100854 |
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| Abstract: | This paper makes use of leading control m et hod and switch feedback contrd method together to deal with the spacecraft attit ude nonlinear control problem in order to adjust to the strict reguirements of a ttitude stability,at the same time,adjusts the feedback signal according to the engineering need. The results of simulation shows that this kind of complex cont rol system could solve the contradiction between the precision and transient res ponse in high degree. |
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| Keywords: | Subject terms Spacecraft Attitude control system Switch feedback Limit cycle |
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