Model predictive control of rigid spacecraft with two variable speed control moment gyroscopes
Crossref DOI link: https://doi.org/10.1007/s10483-017-2278-9
Published Online: 2017-10-26
Published Print: 2017-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Wu, Pengcheng
Wen, Hao
Chen, Ti
Jin, Dongping
License valid from 2017-10-26