Integral terminal sliding-mode robust vibration control of large space intelligent truss structures using a disturbance observer

被引:3
作者
Tian, Dalong [1 ]
Guo, Jianguo [1 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Inst Precis Guidance & Control, 127 West Youyi Rd, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
large space intelligent truss structure; forced vibration; piezoelectric actuator; active vibration control; integral terminal sliding-mode robust control; ACTIVE CONTROL; DESIGN; SUPPRESSION; PLACEMENT;
D O I
10.1177/09544100211029084
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This study aims to develop an advanced integral terminal sliding-mode robust control method using a disturbance observer (DO) to suppress the forced vibration of a large space intelligent truss structure (LSITS). First, the dynamics of the electromechanical coupling of the piezoelectric stack actuator and the LSITS, based on finite element and Lagrangian methods, are established. Subsequently, to constrict the vibration of the structure, a novel integral terminal sliding-mode control (ITSMC) law for the DO is used to estimate the parameter perturbation of the LSITS based on a continuous external disturbance. Simulation results show that, under a forced vibration and compared with the ITSMC system without a DO, the displacement amplitude of the ITSMC system with the DO is effectively reduced. In the case where the model parameters of the LSITS deviate by +/- 50%, and an unknown continuous external disturbance exists, the control system with the DO can adequately attenuate the structural vibration and realize robust control. Concurrently, the voltage of the employed piezoelectric stack actuator is reduced, and voltage jitter is alleviated.
引用
收藏
页码:1155 / 1165
页数:11
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