Finite-time H ∞ adaptive fault-tolerant control for wing flutter of reentry vehicle subject to input saturation
Crossref DOI link: https://doi.org/10.1007/s12555-015-0311-9
Published Online: 2017-01-19
Published Print: 2017-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Gao, Ming-Zhou
Cai, Guo-Ping
License valid from 2017-01-19