• DocumentCode
    3226602
  • Title

    Modeling and active vibration control of rigid-flexible coupled system on vehicle

  • Author

    Liang, Qing ; Wu, Xinfeng ; Wang, Yong

  • Author_Institution
    Dept. of Autom., Univ. of Sci. & Technol. of China, Hefei, China
  • fYear
    2011
  • fDate
    22-24 April 2011
  • Firstpage
    4226
  • Lastpage
    4229
  • Abstract
    When the missile is carried by vehicle, vibration caused by the road surface environment can lead to the missile fatigue damage. To investigate the active vibration isolation method of vehicle-mounted flexible missile system, a rigid-flexible coupled model is built. The vehicle and the flexible missile are respectively simplified as a quarter suspension system and a flexible beam fixed on a mass. A robust H∞, controller is then designed for active vibration control. Simulation results verify that the proposed active vibration isolation method can reduce the vibration level more effectively compared with the passive isolation.
  • Keywords
    H∞ control; beams (structures); fatigue; flexible structures; robust control; shear modulus; suspensions (mechanical components); vibration control; active vibration control; active vibration isolation method; flexible beam; missile fatigue damage; quarter suspension system; rigid-flexible coupled system; road surface environment; robust H∞ controller; vehicle-mounted flexible missile system; Missiles; Robustness; Suspensions; Vehicles; Vibration control; Vibrations; Zirconium; active vibration isolation; flexible missile; rigid-flexible coupled; vehicle-mounted missile;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electric Technology and Civil Engineering (ICETCE), 2011 International Conference on
  • Conference_Location
    Lushan
  • Print_ISBN
    978-1-4577-0289-1
  • Type

    conf

  • DOI
    10.1109/ICETCE.2011.5774774
  • Filename
    5774774