Adaptive neural network dynamic surface control of hypersonic vehicle with variable geometry inlet
Author:
Affiliation:
1. Northwestern Polytechnical University,School of Aerospace,Xi’an,China,710072
2. Qian Xuesen Laboratory,China Academy of Space Technology,Beijing,China,100094
3. Xi’an Aerospace Propulsion Institute,Xi’an,China,710072
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10023546/10022325/10023696.pdf?arnumber=10023696
Reference15 articles.
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3. Adaptive Control for Hypersonic Vehicles With Time-Varying Faults
4. Robust backstepping decentralized tracking control for hypersonic flight vehicle with nonlinear uncertainties[J];qing;IEEE Control Theory and Applications,2018
5. Adaptive Sliding Mode Control Design for a Hypersonic Flight Vehicle
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