| 柔性空间飞行器的振动抑止控制 |
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| 引用本文： | 刘暾,常亚武,杨大明.柔性空间飞行器的振动抑止控制[J].航天控制,1992(2). |
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| 作者姓名： | 刘暾 常亚武 杨大明 |
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| 作者单位： | 哈尔滨工业大学，哈尔滨工业大学，哈尔滨工业大学 |
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| 摘 要： | 本文提出了一种带有柔性附件的卫星的振动主动抑止方法,给出了能抑止任意阶振动谐波的条件.作为举例,分析了太阳帆板的转动控制,在使帆板平稳旋转的同时,还使卫星姿态稳定无振.
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| 关 键 词： | 柔性 航天器 振动抑止 控制 |
The Vibration Suppression Control of Flexible Spacecrafts |
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| Liu Tun Chang Yawu Yang Daiming Harbin Institute of Technology.The Vibration Suppression Control of Flexible Spacecrafts[J].Aerospace Control,1992(2). |
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| Authors: | Liu Tun Chang Yawu Yang Daiming Harbin Institute of Technology |
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| Institution: | Liu Tun Chang Yawu Yang Daiming Harbin Institute of Technology |
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| Abstract: | This paper introduces a method of active vibration suppression control for spacecrafts with flexible appendages, and gives the conditions suppressing arbitrary numbers of harmonics. As an example, the angular control of satellite with a solar array is analysed. In this example, the solar array is not only rotated smoothly, but the satellite attitude can also be kept stable with sensible vibration |
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| Keywords: | Flexibility Spacecraft Vibration suppression Control |
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