Robust Finite-time Attitude Tracking Control of Rigid Spacecraft Under Actuator Saturation
Crossref DOI link: https://doi.org/10.1007/s12555-016-0768-1
Published Online: 2018-03-02
Published Print: 2018-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Chen, Hai-Tao
Song, Shen-Min
Zhu, Zhi-Bin
Text and Data Mining valid from 2018-02-01
Article History
Received: 9 December 2016
Revised: 11 May 2017
Accepted: 11 June 2017
First Online: 2 March 2018