DocumentCode
1795218
Title
Fuzzy switched H∞ control for flexible air-breathing hypersonic vehicles
Author
Changhua Hu ; Xiaoxiang Hu ; Shipeng Fang
Author_Institution
302 Unit, Xi´an Res. Inst. of High-Technol., Xi´an, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
1895
Lastpage
1899
Abstract
The modeling, guidance and control of flexible air-breathing hypersonic vehicles (FAHVs) is highly challenging and still an open problem because of the complex inherent couplings, the strong flexibility effects, the big flight envelope, the varied parameters and external disturbance. A fuzzy switched H∞ control design method is addressed for FAHVs in this paper. The big flight envelope of FAHVs is divided into several regions with respect to the chosen switching signals, and the switched H∞ controller design method is presented. Fuzzy smooth switching condition is also introduced to avoid chattering of the plant at the switching boundaries. A numerical simulation is carried on the FAHVs´ original nonlinear dynamics to show the availability of the design methods.
Keywords
H∞ control; aircraft control; control system synthesis; flexible structures; fuzzy control; nonlinear dynamical systems; time-varying systems; FAHV control; FAHV guidance; FAHV modeling; FAHV original nonlinear dynamics; external disturbance; flexibility effects; flexible air-breathing hypersonic vehicles; flight envelope; fuzzy smooth switching condition; fuzzy switched H∞ control design method; numerical simulation; plant chattering; switching boundaries; switching signals; Atmospheric modeling; Control design; Design methodology; Nonlinear dynamical systems; Switches; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007470
Filename
7007470
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