A guaranteed transient performance-based adaptive neural control scheme with low-complexity computation for flexible air-breathing hypersonic vehicles
Crossref DOI link: https://doi.org/10.1007/s11071-016-2637-0
Published Online: 2016-02-04
Published Print: 2016-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Bu, Xiangwei
Wu, Xiaoyan
Huang, Jiaqi
Wei, Daozhi
Funding for this research was provided by:
Aeronautical Science Foundation of China (20130196004)
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