• DocumentCode
    2496636
  • Title

    Identification model of aeroengine based on improved LS-SVM

  • Author

    Cai, Kailong ; Yao, Wuwen ; Lv, Boping

  • Author_Institution
    First Aeronaut. Inst. of the Air Force, Xinyang
  • fYear
    2008
  • fDate
    25-27 June 2008
  • Firstpage
    7368
  • Lastpage
    7373
  • Abstract
    Because of aeroengine properties such as the strong nonlinearity and time-varying uncertainty, a new identification algorithm of aeroengine model based on improved LS-SVM was brought forward. In the method, LS-SVM robustness was improved by adding weighed values to errors and its sparseness was improved by clipping algorithm. In terms of the recorded flight data on some turbofan engine, improved LS-SVM identification model of aeroengine was set up. Through the identification of the recorded flight data, the results show that the improved LS-SVM identification model has the advantages of high identification precision, good self-adaptability and strong robustness. It is effective that the improved LS-SVM identification model is used in aeroengine.
  • Keywords
    aerospace computing; jet engines; support vector machines; LS-SVM robustness; aeroengine identification model; aeroengine nonlinearity; clipping algorithm; time-varying uncertainty; turbofan engine; Automation; Electronic mail; Engines; Intelligent control; Lagrangian functions; Least squares methods; Nonlinear systems; Robustness; Support vector machines; Uncertainty; Aeroengine; Identification Model; Improved LS-SVM; Nonlinear System;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation, 2008. WCICA 2008. 7th World Congress on
  • Conference_Location
    Chongqing
  • Print_ISBN
    978-1-4244-2113-8
  • Electronic_ISBN
    978-1-4244-2114-5
  • Type

    conf

  • DOI
    10.1109/WCICA.2008.4594065
  • Filename
    4594065