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.
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
出处
《航天控制》
CSCD
北大核心
1992年第2期25-33,51,共10页
Aerospace Control
关键词
柔性
航天器
振动抑止
控制
Flexibility Spacecraft Vibration suppression Control
