Active Disturbance Rejection Control of Satellite Attitude Based on High-Order Fully Actuated System Approach
Author:
Affiliation:
1. North China University of Water Resources and Electric Power,Zhengzhou,450045
2. Henan University of Technology,Zhengzhou,450001
3. Henan University of Engineering,Zhengzhou,451191
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10606543/10606546/10606888.pdf?arnumber=10606888
Reference28 articles.
1. Quasi-linear system approaches for flight vehicle control-part 1: an overview and problems;Duan;Journal of Astronautics,2020
2. Variable Structure Sliding Mode Control Method for Satellite Attitude Maneuver;Li;Journal of XiAn Jiaotong University,2020
3. Attitude control of large truss structure satellite with uncertainty;Zhu;Harbin: Harbin Institute of Technology,2019
4. Inverse optimal adaptive control for attitude tracking of spacecraft
5. Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
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