• 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