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