Open Access
ARTICLE
Adaptive Quasi Fixed-Time Orbit Control Around Asteroid with Performance Guarantees
1Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, Beijing, 100094, China.
2 School of Aeronautics and Astronautics, Central South University, Changsha, 410083, China.
3 School of Astronautics, Northwestern Polytechnical University, Xi’an, 710072, China.
* Corresponding Authors: Caisheng Wei. Email: ;
Zeyang Yin. Email: .
(This article belongs to this Special Issue: Nonlinear Computational and Control Methods in Aerospace Engineering)
Computer Modeling in Engineering & Sciences 2020, 122(1), 89-107. https://doi.org/10.32604/cmes.2020.07985
Received 17 July 2019; Accepted 25 August 2019; Issue published 01 January 2020