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Applied Mathematics and Nonlinear Sciences
Volume 8 (2023): Issue 1 (January 2023)
Open Access
Attitude control for the rigid spacecraft with the improved extended state observer
Yuteng Cao
Yuteng Cao
,
Qi Liu
Qi Liu
,
Guiqin He
Guiqin He
,
Qiuling Zhao
Qiuling Zhao
and
Fang Liu
Fang Liu
| Apr 27, 2023
Applied Mathematics and Nonlinear Sciences
Volume 8 (2023): Issue 1 (January 2023)
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Published Online:
Apr 27, 2023
Page range:
121 - 134
Received:
Nov 06, 2020
Accepted:
Nov 15, 2020
DOI:
https://doi.org/10.2478/amns.2021.1.00024
Keywords
rigid spacecraft
,
rotating solar array
,
disturbance
,
improved extended state observer
,
sliding mode control
© 2021 Cao et al., published by Sciendo.
This work is licensed under the Creative Commons Attribution 4.0 International License.
Yuteng Cao
School of Mechanical Electrical Engineering, Beijing Information Science and Technology University
Beijing, China
Qi Liu
Beijing Research Institute of Precise Mechatronics and Controls
Beijing, China
Guiqin He
School of Astronautics, Harbin Institute of Technology
Harbin, China
Qiuling Zhao
School of Mechanical Electrical Engineering, Beijing Information Science and Technology University
Beijing, China
Fang Liu
School of Mechanical Electrical Engineering, Beijing Information Science and Technology University
Beijing, China