DocumentCode :
1727324
Title :
Integrated model-based and grey-relational-analyzed diagnosis of wheel speed sensor for aircraft antilock braking
Author :
Dai Zhiyong ; Lin Hui ; Guo Hao
Author_Institution :
Sch. of Autom., Northwestern Polytech. Univ., Xi´an, China
fYear :
2013
Firstpage :
6077
Lastpage :
6082
Abstract :
The wheel speed sensor fault diagnosis for aircraft antilock braking system (ABS) is a difficult problem due to its poor working conditions and strongly nonlinear. To overcome this difficulty, a novel integrated model-based and grey-relational-analyzed diagnosis strategy is proposed. Due to its strong robustness, a sliding mode observer based on the aircraft braking model is employed to generate the residuals of the wheel speed. And grey-relational-analyzed diagnosis, which is known as its diagnostic accuracy and few computing requirement, is used for sensor failure diagnosis. Four different sensor states, namely normal state, gain variation failure, stuck failure, constant deviation failure, are simulated on an aircraft braking model and compared. The results presented indicate that this diagnosis strategy is capable of handing difficult wheel speed sensor failure.
Keywords :
aircraft control; aircraft instrumentation; angular velocity measurement; brakes; fault diagnosis; grey systems; observers; sensors; variable structure systems; wheels; aircraft antilock braking; aircraft braking model; constant deviation failure; fault diagnosis; gain variation failure; grey relational analysis; model based analysis; normal state; sensor failure diagnosis; sliding mode observer; stuck failure; wheel speed sensor diagnosis; Aerospace control; Aircraft; Atmospheric modeling; Fault diagnosis; Gears; Observers; Wheels; Antilock Braking System (ABS); Grey-relational-analyzed Diagnosis; Model-base Diagnosis; Nonlinear System; Sliding Mode Observer;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6640502
Link To Document :
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