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Applied Mathematics and Nonlinear Sciences
Volume 8 (2023): Numero 1 (Gennaio 2023)
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Attitude control for the rigid spacecraft with the improved extended state observer
Yuteng Cao
Yuteng Cao
School of Mechanical Electrical Engineering, Beijing Information Science and Technology University
Beijing, China
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Cao, Yuteng
,
Qi Liu
Qi Liu
Beijing Research Institute of Precise Mechatronics and Controls
Beijing, China
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Liu, Qi
,
Guiqin He
Guiqin He
School of Astronautics, Harbin Institute of Technology
Harbin, China
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He, Guiqin
,
Qiuling Zhao
Qiuling Zhao
School of Mechanical Electrical Engineering, Beijing Information Science and Technology University
Beijing, China
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Zhao, Qiuling
e
Fang Liu
Fang Liu
School of Mechanical Electrical Engineering, Beijing Information Science and Technology University
Beijing, China
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Liu, Fang
27 apr 2023
Applied Mathematics and Nonlinear Sciences
Volume 8 (2023): Numero 1 (Gennaio 2023)
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Pubblicato online:
27 apr 2023
Pagine:
121 - 134
Ricevuto:
06 nov 2020
Accettato:
15 nov 2020
DOI:
https://doi.org/10.2478/amns.2021.1.00024
Parole chiave
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.