Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
Crossref DOI link: https://doi.org/10.1007/s11424-022-1515-8
Published Online: 2022-04-18
Published Print: 2022-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Liu, Gaoqi
Zhang, Kai
Li, Bin
Text and Data Mining valid from 2022-04-01
Version of Record valid from 2022-04-01
Article History
Received: 30 December 2021
Revised: 27 January 2022
First Online: 18 April 2022