Rigid spacecraft nonlinear robust $$H_\infty $$ attitude controller design under actuator misalignments
Crossref DOI link: https://doi.org/10.1007/s11071-023-08620-6
Published Online: 2023-06-29
Published Print: 2023-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Wang, Zhong
Li, Yan http://orcid.org/0000-0002-0163-6006
Text and Data Mining valid from 2023-06-29
Version of Record valid from 2023-06-29
Article History
Received: 14 August 2022
Accepted: 3 May 2023
First Online: 29 June 2023
Declarations
:
: The authors declare that they have no conflict of interest concerning the publication of this manuscript.