Attitude control for the rigid spacecraft with the improved extended state observer
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27 apr 2023
INFORMAZIONI SU QUESTO ARTICOLO
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
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© 2021 Cao et al., published by Sciendo.
This work is licensed under the Creative Commons Attribution 4.0 International License.
Cao, Yuteng
School of Mechanical Electrical Engineering, Beijing Information Science and Technology UniversityBeijing, China
Liu, Qi
Beijing Research Institute of Precise Mechatronics and ControlsBeijing, China
He, Guiqin
School of Astronautics, Harbin Institute of TechnologyHarbin, China
Zhao, Qiuling
School of Mechanical Electrical Engineering, Beijing Information Science and Technology UniversityBeijing, China
Liu, Fang
School of Mechanical Electrical Engineering, Beijing Information Science and Technology UniversityBeijing, China