Spacecraft Attitude Tracking Control Based On High-Order Fully Actuated System Approach

被引：4
|
作者：
Jin, Dongyan [1 ]
Jia, Shixiang [1 ]
Wang, Tong [1 ]
Qiu, Jianbin [1 ]
机构：
[1] Harbin Inst Technol, Res Inst Intelligent Control & Syst, Harbin 150001, Peoples R China
来源：
2023 2ND CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, CFASTA | 2023年
关键词：
High-order fully actuated system approach; Spacecraft attitude tracking; modified Rodrigues parameters;
D O I：
10.1109/CFASTA57821.2023.10243176
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 focuses on the attitude tracking control of spacecraft. Firstly, the modified Rodrigues parameters are selected to characterize the spacecraft's attitude, whose mathematical model is then established by considering the uncertainties of the spacecraft parameters and the bounded disturbances. The mathematical model of the spacecraft is transformed into a type of high-order fully actuated (HOFA) system with uncertainties. Then, based on the HOFA system approach, a robust controller for a type of HOFA system with uncertainties is designed, which can ensure that the system states converge to an arbitrary ellipsoidal region. Finally, the validness of the designed controller is verified by simulation.
引用
收藏
页码：1040 / 1044
页数：5
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