DocumentCode :
1794920
Title :
Detection and diagnosis method study of the civil aircraft surface fault based on LS-SVM
Author :
Li Zhengqiang ; Qiao Wenfeng ; Tu Xiangzheng
Author_Institution :
State key Lab. of Civil Aircraft Flight Simulation, Shanghai Aircraft Design & Res. Inst., Shanghai, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
676
Lastpage :
679
Abstract :
Large civil aircraft control surface failure occurred in flight will directly affect the handling and safety of the aircraft, so the flight control system needs to have an online surface fault diagnosis function. For large civil aircraft control surfaces and more features, this paper proposes online fault diagnosis algorithm control surfaces based on the use of least squares support vector machine (LS-SVM), using the Internet to search and cross-validation method to select SVM parameters identified online aircraft effectors fault parameters change, and to overcome the weak signal due to noise input to bring the problem of inaccurate identification. In this paper the application of the a large civil aircraft made publicly available flight data, the algorithm simulation results show that the method has strong generalization ability and higher recognition results.
Keywords :
aerospace computing; aerospace safety; aircraft control; fault diagnosis; least mean squares methods; support vector machines; Internet; LS-SVM; aircraft control surface failure; aircraft safety; civil aircraft surface fault; detection method; flight control system; least squares method; online surface fault diagnosis function; support vector machine; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Fault diagnosis; Simulation; Support vector machines;
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.2014.7007296
Filename :
7007296
Link To Document :
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