H ∞ inverse optimal adaptive fault-tolerant attitude control for flexible spacecraft with input saturation
Crossref DOI link: https://doi.org/10.1007/s12204-015-1659-y
Published Online: 2015-10-29
Published Print: 2015-10
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Long, Hai-hui
Zhao, Jian-kang
Lai, Jian-qing
Text and Data Mining valid from 2015-10-01
