An spacecraft attitude maneuver method based on ADRC

被引：0

作者：

Yao Yao ^{[1
]}

Liu Lei ^{[1
]}

Wang Yong-ji ^{[1
]}

机构：

[1] Huazhong Univ Sci & Technol, Natl Key Lab Sci & Technol Multispectral Informat, Wuhan 430074, Peoples R China

来源：

2015 27TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2015年

关键词：

attitude maneuver; state-feedback; active disturbance rejection control;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Spacecraft attitude control problem of a class of MIMO control systems, and there is a strong coupling between channels. The ADRC method shows showed some deficiencies. This study proposes an integrated procedure to design the state-feedback decoupling controller to dynamically reduce the coupling effect, and then the non-linear SISO ADRC is designed to ensure the stability of the closed-loop system for each decoupling subject. Finally, the simulation results of a bank-to-turn vehicle model control show that the designed controller has good decoupling performance, with good robustness and adaptability.

引用

页码：3032 / 3037

页数：6