Attitude manoeuvre control and asymptotic disturbance rejection of flexible spacecraft

被引：1

作者：

Yu, Zhen ^{[1
]}

Guo, Yu ^{[1
]}

Zhong, Chenxing ^{[1
]}

Wu, Yifei ^{[1
]}

Guo, Jian ^{[1
]}

机构：

[1] Nanjing Univ Sci & Technol, Sch Automat, 200 Xiao Ling Wei, Nanjing 210094, Jiangsu, Peoples R China

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2019年 / 233卷 / 02期

基金：

中国国家自然科学基金;

关键词：

Attitude control; disturbance rejection; internal model; modal estimation; flexible spacecraft; ACTIVE VIBRATION SUPPRESSION; H-INFINITY CONTROL; ROBUST; TRACKING;

D O I：

10.1177/0954410017735127

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a novel approach to tackle the issues of attitude manoeuvre control and asymptotic disturbance rejection for a flexible spacecraft. The resulting attitude controller employs an internal model-based compensator to reject a class of persistent disturbances and a modal estimator for dynamic compensation of the rigid-flex coupling effect. The convergence of the modal variables can be guaranteed without the measures of them. The stability of the system is proved via the Lyapunov technique rigorously. Numerical results illustrate that improved attitude control performance and asymptotic disturbance rejection can both be achieved.

引用

页码：426 / 437

页数：12

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