• DocumentCode
    2828589
  • Title

    Identify flight control system based on least squares support vector machine

  • Author

    Zhong-jian Li ; Yin, De-Yi

  • Author_Institution
    Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
  • Volume
    4
  • fYear
    2010
  • fDate
    22-24 Oct. 2010
  • Abstract
    As flight control system is highly non-linear, it´s difficult to get desired results using traditional identification ways. And based on statistical learning theory, support vector machine, is considered a kind of new and feasible nonlinear system identification approach. In this paper, applied least square support vector regression machines and Series - Parallel identification model of system identification to identify flight control system model Through the simulation, the model of flight control system is successfully identified The simulation results show that: the design of the identification model predicted a good performance, with very high accuracy, at the same time; it also can be very good to reflect the characteristics of flight control systems.
  • Keywords
    aerospace control; identification; least mean squares methods; nonlinear control systems; statistical analysis; support vector machines; flight control system; least square method; nonlinear system identification; series-parallel identification model; statistical learning theory; support vector machine; Elevators; Kernel; Statistical learning theory; Support vector machine; flight control system; identification;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Application and System Modeling (ICCASM), 2010 International Conference on
  • Conference_Location
    Taiyuan
  • Print_ISBN
    978-1-4244-7235-2
  • Electronic_ISBN
    978-1-4244-7237-6
  • Type

    conf

  • DOI
    10.1109/ICCASM.2010.5620099
  • Filename
    5620099