Flexible spacecraft attitude maneuver planning based on variable amplitudes input shaping method

被引：0
|
作者：
Wang J. [1 ]
Wu J. [1 ]
Zou J. [1 ]
机构：
[1] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
来源：
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology | 2022年 / 44卷 / 01期
关键词：
Attitude maneuver; Flexible spacecraft with time-varying parameters; Residual vibration; Robustness; Variable amplitudes input shaping;
D O I：
10.11887/j.cn.202201011
中图分类号：
学科分类号：
摘要：
In order to solve the attitude maneuver problem for flexible spacecraft with time-varying parameters, the variable amplitudes zero vibration derivative shaper with stronger robustness was developed based on the variable amplitudes zero vibration shaper. The robust attitude maneuver strategy, in which its objective was to maneuver the spacecraft to the desired attitude state and cancel the residual vibration of the rotating flexible appendages at the same time, was proposed. Simulations were conducted by means of a spacecraft with rotating solar wings which undergoes three-axis maneuvers. The results indicate that this strategy is robust to frequency variations, uncertainties of damping coefficient and other uncertain factors. © 2022, NUDT Press. All right reserved.
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页码：68 / 76
页数：8
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