| 挠性卫星大角度机动变结构控制的全物理仿真实验研究 |
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| 引用本文： | 周军,周凤岐,李季苏,牟小刚.挠性卫星大角度机动变结构控制的全物理仿真实验研究[J].宇航学报,1999,20(1):66-70. |
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| 作者姓名： | 周军 周凤岐 李季苏 牟小刚 |
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| 作者单位： | 1. 西北工业大学航天工程学院·西安·710072
2. 中国空间技术研究院502所·北京·100080 |
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| 基金项目： | 国家高技术（863）航天领域研究计划资助项目 |
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| 摘 要： | 以具有大面积太阳帆板的卫星大角度机动为背景，针对常用的“飞轮－喷气”执行机械模式研究了变结构控制方案，考虑了控制精度和喷气消耗量问题，并成功地进行了国内首次挠性卫星大角度机动控制的全物理仿真实验，取得了显著的效果。
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| 关 键 词： | 挠性结构 大角度机动 变结构控制 卫星控制 |
EXPERIMENT RESEARCH FOR VARIABLE STRUCTURE CONTROL OF FLEXIBLE SATELLITES' LARGE ANGLE MANEUVERS |
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| Zhou Jun,Zhou Fengqi,Li Jisu,Mu Xiaogang.EXPERIMENT RESEARCH FOR VARIABLE STRUCTURE CONTROL OF FLEXIBLE SATELLITES'' LARGE ANGLE MANEUVERS[J].Journal of Astronautics,1999,20(1):66-70. |
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| Authors: | Zhou Jun Zhou Fengqi Li Jisu Mu Xiaogang |
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| Abstract: | The satellites with large solar panels taken as practical engineering background,a variable structure control scheme is studied for flexible satellite large angle maneuvers,and a simple control algorithem is also designed according to the "wheel thruster" actuator mode that is commonly used in satellite control,being considered emphatically the two problems of control precision and gas consumption.Based on the results above,the physical simulation experiments for the large angle maneuver control of flexible satellites are successfully completed in the first time of our country,and from that the remarkable effect is made. |
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| Keywords: | Flexible structure\ Large angle maneuver\ Variable structure control\ Satellite control\ Physical simulation experiment |
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