Predictor-Based Control for a Flexible Satellite Subject to Output Time Delay

被引：11
|
作者：
Ma, Yonghao [1 ,2 ]
He, Xiuyu [1 ,2 ,3 ]
Chen, Mou [4 ]
He, Wei [1 ,2 ]
机构：
[1] Univ Sci & Technol Beijing, Inst Artificial Intelligence, Beijing 100083, Peoples R China
[2] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing 100083, Peoples R China
[3] Univ Sci & Technol Beijing, Shunde Grad Sch, Foshan 528399, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China
来源：
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY | 2022年 / 30卷 / 04期
基金：
中国博士后科学基金; 中国国家自然科学基金; 北京市自然科学基金;
关键词：
Satellites; Delay effects; Vibrations; Solar panels; Observers; Mathematical model; Delays; Flexible satellite; output time delay; predictor-based control; vibration control; VIBRATION CONTROL; NONLINEAR-SYSTEMS; ATTITUDE TRACKING; BOUNDARY CONTROL; MARINE RISERS; ACTUATOR; APPENDAGES; SPACECRAFT; DESIGN;
D O I：
10.1109/TCST.2021.3109270
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 article investigates a flexible satellite consisting of a central hub and two flexible solar panels. Different from previous control works, the output time delay is considered in vibration control for the satellite, whose model is more complex and strongly coupled. For dealing with output time delay, a compensated strategy based on a Luenberger observer and a predictor is developed to obtain the estimation of the current state. Then, a predictor-based control law is proposed to eliminate the vibration of flexible solar panels. Finally, the stability of the closed-loop system is analyzed by Lyapunov's direct method, and simulation results are given to demonstrate the efficiency of the developed method.
引用
收藏
页码：1420 / 1432
页数：13
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