Global Stabilization of Circular Orbit Rendezvous by Bounded Linear Feedback

被引：1
|
作者：
Luo, Weiwei [1 ]
Fu, Wenbo [1 ]
Zhu, Song [1 ]
Xu, Chuanchuan [2 ]
机构：
[1] China Univ Min & Technol, Jiangsu Ctr Appl Math CUMT, Sch Math, Xuzhou 221116, Jiangsu, Peoples R China
[2] Nanjing Res Inst Elect Engn, Nanjing, Peoples R China
来源：
2024 3RD CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, FASTA 2024 | 2024年
基金：
中国国家自然科学基金;
关键词：
Bounded linear feedback; Global stabilization; Spacecraft rendezvous; SYSTEMS SUBJECT;
D O I：
10.1109/FASTA61401.2024.10595259
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The global stabilization problem is revisited for the circular orbit spacecraft rendezvous system with actuator saturation. The linearized relative motion equation transformed into its Luenberger canonical form. It is noted that the system decomposed into a cascade of neutral stable linear systems, and bounded linear state feedback controllers for subsystems are designed respectively based on the absolute stability theory. The global stability of the closed-loop system is proved by providing explicit conditions on the parameters in the feedback gains. Optimal feedback gains are also discussed. Simulation results are given to show the effectiveness of the presented approaches.
引用
收藏
页码：1508 / 1512
页数：5
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