• DocumentCode
    2476664
  • Title

    Modeling for landing process of a helicopter with rotator self-rotating based on support vector machine

  • Author

    Wang, Shuzhou ; San, Ye ; Zhang, Yunchang

  • Author_Institution
    Control & Simulation Centre, Harbin Inst. of Technol., Harbin
  • fYear
    2008
  • fDate
    25-27 June 2008
  • Firstpage
    645
  • Lastpage
    649
  • Abstract
    As a system identification method, neural network can be applied to build the simulation model of a helicopter. But it has some difficulties such as the hardness of selecting network structure, slow convergence speed, local minimum, and generalization ability question. To avoid the question above, the support vector machine (SVM) method is introduced to the field of flight simulation for the first time, and the rotator speed model for landing process of a helicopter with rotator self-rotating is built. Compared with the neural network model, the SVM simulation model of a helicopter owns some advantages such as simple structure, fast convergence speed and high generalization ability. It is shown by theoretic analysis and simulation result that the SVM method is feasible.
  • Keywords
    helicopters; identification; neurocontrollers; support vector machines; helicopter landing process; neural network; rotator speed model; selecting network structure hardness; support vector machine; system identification method; Aerospace simulation; Automation; Convergence; Electronic mail; Force control; Helicopters; Intelligent control; Neural networks; Support vector machines; System identification; generalization ability; helicopter; simulation model; support vector machine;
  • 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.2008.4592998
  • Filename
    4592998