DocumentCode :
128316
Title :
Modeling and simulation of switched reluctance machine based aircraft electric brake system by BP neural network
Author :
Zhang Zhihui ; Li Yuren
Author_Institution :
Northwestern Polytech. Univ., Xi´an, China
fYear :
2014
fDate :
9-11 June 2014
Firstpage :
338
Lastpage :
341
Abstract :
Based on the electromagnetic characteristics of switched reluctance machine (SRM) obtained by finite element method (FEM), two nonlinear mapping relations, namely i(ψ,θ) and T(i,θ), are modeled by BP neural network (BPNN) with Levenberg-Marquardt(LM) algorithm. On this basis, the dynamic simulation model of SRM based aircraft electric brake system (SRM-EBS) is built in Matlab. The performance of SRM-EBS is simulated with dry runway, and many results including brake torque and distance are presented. The simulation process shows that the BPNN model of SRM has advantages including fast learning speed, small convergent error, strong generalization ability and small network size. The simulation results indicate that SRM is suitable for application in aircraft electric brake system.
Keywords :
aircraft; backpropagation; brakes; finite element analysis; mathematics computing; neural nets; simulation; BP neural network; BPNN; FEM; Levenberg-Marquardt algorithm; Matlab; SRM-EBS; aircraft electric brake system; electromagnetic characteristics; finite element method; modeling; nonlinear mapping relations; simulation; switched reluctance machine; Aircraft; Atmospheric modeling; Mathematical model; Reluctance motors; Torque; Training; BP neural network; aircraft; electric brake system; modeling and simulation; switched reluctance machine;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industrial Electronics and Applications (ICIEA), 2014 IEEE 9th Conference on
Conference_Location :
Hangzhou
Print_ISBN :
978-1-4799-4316-6
Type :
conf
DOI :
10.1109/ICIEA.2014.6931184
Filename :
6931184
Link To Document :
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