Fuzzy disturbance observer‐based dynamic surface control for air‐breathing hypersonic vehicle with variable geometry inlets
Author:
Affiliation:
1. School of Electrical and Information Engineering, Tianjin University92 Weijin RoadTianjin300072People's Republic of China
2. School of Electrical and Electronic Engineering, University of ManchesterManchesterM13 9PLUK
Funder
National Natural Science Foundation of China
Natural Science Foundation of Tianjin City
Publisher
Institution of Engineering and Technology (IET)
Subject
Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2017.0742
Reference43 articles.
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2. ClarksA.WuC. andMirmiranitM.et al.: ‘Development of an airframe‐propulsion integrated generic hypersonic vehicle model’.44 th AIAA Aerospace Sciences Meeting and Exhibit 2006
3. Hyper‐X flight engine ground testing for flight risk reduction;Huebner L.D.;J. Spacecr. Rockets,2001
4. KojimaT.TanatsuguN. andSatoT.et al.: ‘Development study on axisymmetric air inlet for Atrex engine’.10th AIAA/NAL‐NASDA‐ISAS Int. Space Planes and Hypersonic Systems and Technologies Conf. 2001
5. KuranovA. andSheikinE.: ‘Mhd control by external and internal flows in scramjet under Ajax concept’.41st Aerospace Sciences Meeting and Exhibit 2003
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