Fully actuated system approach to attitude control of flexible spacecraft with nonlinear time-varying inertia
Crossref DOI link: https://doi.org/10.1007/s11432-021-3349-3
Published Online: 2022-10-21
Published Print: 2022-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zhao, Tianyi
Duan, Guang-Ren
Text and Data Mining valid from 2022-10-21
Version of Record valid from 2022-10-21
Article History
Received: 27 July 2021
Revised: 13 September 2021
Accepted: 8 October 2021
First Online: 21 October 2022