摘要
提出了一种分布式自适应振动抑制控制方法,有效抑制了卫星大挠性帆板在轨振动问题。考虑作动器和传感器的安装位置对控制效果的影响,通过分析邻接子模块之间振动和输出力的耦合影响,基于Lyapunov理论设计了完整的分布式自适应控制器。仿真结果表明,在外界持续干扰等情况下,本文设计的分布式控制系统与基于线性二次型调节器(LQR)的分布式控制方法相比抑振时间缩短了40%,与集中式控制方法相比抑振时间缩短了50%,得到了更良好的在轨抑振效果,对于卫星的稳定运行具有重要意义。
A distributed adaptive vibration suppression control method was investigated to effectively suppress the on-orbit vibration of large flexible satellite panels.Considering the influence of actuator and sensor installation position on the control effect,a complete distributed adaptive controller was designed based on Lyapunov theory by analyzing the coupling effect of vibration and output force between adjacent sub-modules.The simulation results show that the vibration suppression time of the proposed distributed control method is reduced by 40%compared with the distributed control method based on LQR control method and 50%compared with the centralized control method under the condition of continuous external interference.Furthermore,the proposed control method has an improved on-orbit vibration suppression effect and is of great significance for the stable operation of the satellite.
作者
张刘
曾庆铭
赵寰宇
范国伟
ZHANG Liu;ZENG Qing-ming;ZHAO Huan-yu;FAN Guo-wei(College of Instrumentation&Electrical Engineering,Jilin University,Changchun 130012,China)
出处
《吉林大学学报(工学版)》
EI
CAS
CSCD
北大核心
2023年第9期2676-2685,共10页
Journal of Jilin University:Engineering and Technology Edition
基金
国家自然科学基金项目(62073150,62073151,62001185)
吉林省科技厅项目(20210101177JC)。
关键词
分布式控制
自适应控制
大挠性航天器
李雅普诺夫理论
振动抑制
distributed control
adaptive control
large flexible spacecraft
Lyapunov theory
vibration suppression