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柔性空间飞行器的振动抑止控制
The Vibration Suppression Control of Flexible Spacecrafts
【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.
【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
- 【文献出处】 航天控制 ,Aerospace Control , 编辑部邮箱 ,1992年02期
- 【被引频次】18
- 【下载频次】169