Component synthesis vibration suppression method of two component forces for flexible spacecraft

被引：0
|
作者：
齐乃明 [1 ]
赵宝山 [1 ]
赵立军 [1 ,2 ]
赵志刚 [1 ]
莫丽东 [3 ]
机构：
[1] School of Astronautics, Harbin Institute of Technology
[2] State Key Laboratory of Robotics and System, Harbin Institute of Technology
来源：
Journal of Harbin Institute of Technology(New series) | 2012年 / 06期
基金：
中国国家自然科学基金;
关键词：
Vibration suppression; CSVS; Two component forces; Attitude maneuver; Jet control;
D O I：
暂无
中图分类号：
V414 [航天器结构力学];
学科分类号：
08 ; 0825 ;
摘要：
Considering the characteristics of two component forces on component synthesis vibration suppression(CSVS) method, two theorems on two component forces suppressing fractional multiple design frequency are given respectively. Meanwhile, the control force, which is composed by two arbitrary component forces with different initial time, can suppress certain frequencies for secondorder undamped vibration system. Using the above theorems, control moment of jet attitude maneuver on flexible spacecraft is designed on the basis principle of CSVS method. The simulations validate the correctness and effectiveness of the proposed method.
引用
收藏
页码：1 / 5
页数：5
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