Application of hybrid robust three-axis attitude control approach to overactuated spacecraft—A quaternion based model
Crossref DOI link: https://doi.org/10.1007/s11771-016-3228-4
Published Online: 2016-07-16
Published Print: 2016-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Mazinan, A. H.
License valid from 2016-07-01