Robust control for spacecraft rendezvous system with actuator unsymmetrical saturation: a gain scheduling approach

被引:28
作者
Wang, Qian [1 ]
Xue, Anke [1 ]
机构
[1] Hangzhou Dianzi Univ, Inst Informat & Control, Hangzhou, Zhejiang, Peoples R China
基金
中国国家自然科学基金;
关键词
Spacecraft rendezvous; robust; gain scheduling; LMI; unsymmetrical saturation; LINEAR-SYSTEMS; EQUATION APPROACH; FEEDBACK-CONTROL; PERFORMANCE; DESIGN;
D O I
10.1080/00207179.2017.1313451
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper has proposed a robust control for the spacecraft rendezvous system by considering the parameter uncertainties and actuator unsymmetrical saturation based on the discrete gain scheduling approach. By changing of variables, we transform the actuator unsymmetrical saturation control problem into a symmetrical one. The main advantage of the proposed method is improving the dynamic performance of the closed-loop system with a region of attraction as large as possible. By the Lyapunov approach and the scheduling technology, the existence conditions for the admissible controller are formulated in the form of linear matrix inequalities. The numerical simulation illustrates the effectiveness of the proposed method.
引用
收藏
页码:1241 / 1250
页数:10
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