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
相关论文
共 50 条
  • [1] Global stabilization of circular orbit rendezvous by bounded linear feedback
    Luo, Weiwei
    Fu, Wenbo
    Zhu, Song
    Xu, Chuanchuan
    AEROSPACE SCIENCE AND TECHNOLOGY, 2025, 157
  • [2] Global Stabilization of the Spacecraft Rendezvous System by Delayed and Bounded Linear Feedback
    Luo, Weiwei
    Zhou, Bin
    He, Liang
    Duan, Guang-Ren
    IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2022, 52 (03): : 1373 - 1384
  • [3] Global Stabilization of Linearized Spacecraft Rendezvous System by Saturated Linear Feedback
    Zhou, Bin
    Lam, James
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2017, 25 (06) : 2185 - 2193
  • [4] Global Stabilization of Linear Systems with Bounded Controls by the Energy Function with Applications to the Spacecraft Rendezvous
    Zhou, Bin
    Liu, Yang
    2017 CHINESE AUTOMATION CONGRESS (CAC), 2017, : 2428 - 2435
  • [5] Global stabilization of linear discrete-time systems with bounded feedback
    Yang, YD
    Sontag, ED
    Sussmann, HJ
    SYSTEMS & CONTROL LETTERS, 1997, 30 (05) : 273 - 281
  • [6] Guidance for autonomous rendezvous in a circular orbit
    Yanushevsky, R
    Spaceflight Mechanics 2005, Vol 120, Pts 1 and 2, 2005, 120 : 1731 - 1737
  • [7] OPTIMAL RENDEZVOUS IN NEIGHBORHOOD OF A CIRCULAR ORBIT
    JONES, JB
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1976, 24 (01): : 55 - 90
  • [8] Global stabilization of linear systems via bounded controls
    Zhou, Bin
    Duan, Guang-Ren
    SYSTEMS & CONTROL LETTERS, 2009, 58 (01) : 54 - 61
  • [9] Global Stabilization of Multiple Oscillator Systems by Delayed and Bounded Feedback
    Yang, Xuefei
    Zhou, Bin
    Lam, James
    IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS II-EXPRESS BRIEFS, 2017, 64 (06) : 675 - 679
  • [10] Global stabilization of linear systems by bounded controls with guaranteed poles
    ZHOU Bin & DUAN GuangRen Center for Control Theory and Guidance Technology
    ScienceinChina(SeriesF:InformationSciences), 2008, (09) : 1256 - 1268
12345