Modified adaptive neural dynamic surface control for morphing aircraft with input and output constraints
Crossref DOI link: https://doi.org/10.1007/s11071-016-3196-0
Published Online: 2016-11-16
Published Print: 2017-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Wu, Zhonghua
Lu, Jingchao
Zhou, Qing
Shi, Jingping
Funding for this research was provided by:
National Natural Science Foundation of China (61374032, 61573286)
Aeronautical Science Foundation of China (20140753012)
License valid from 2016-11-16