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
Link To Document :
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