DocumentCode
2844220
Title
Design of nearspace vehicle based on fuzzy control
Author
Feng, Yuan ; He, Naibao ; Gao, Qian ; Gong, Chenglong ; Jiang, Changsheng
Author_Institution
Huaihai Inst. of Techology, Lianyungang, China
fYear
2010
fDate
26-28 May 2010
Firstpage
3263
Lastpage
3265
Abstract
With the assumption that NSV suffers the violent changes of aerodynamic paameters and the outside disturbance in hypersonic condition, to achieve high precision, an (fuzzy disturbance observer)FDO is designed which improves the approximation ability of the observer on-line. The strict proof of the Lyapunov stability is provided simutanously.
Keywords
Lyapunov methods; aircraft; approximation theory; fuzzy control; observers; space vehicles; Lyapunov stability; aerodynamic parameters; approximation ability; fuzzy control; fuzzy disturbance observer; hypersonic condition; nearspace vehicle; observer online; Aerodynamics; Automotive engineering; Control systems; Design engineering; Educational institutions; Fuzzy control; Helium; Lyapunov method; Robust control; Space vehicles; fuzzy disturbance observer; nearspace vehicle; robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location
Xuzhou
Print_ISBN
978-1-4244-5181-4
Electronic_ISBN
978-1-4244-5182-1
Type
conf
DOI
10.1109/CCDC.2010.5498616
Filename
5498616
Link To Document