• DocumentCode
    3041497
  • Title

    Application of magneto-rheological (MR) damper in landing gear shimmy

  • Author

    Chen Da-wei ; Gu Hong-bin ; Wu Hao

  • Author_Institution
    Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    1212
  • Lastpage
    1216
  • Abstract
    In order to study the semi-active control of landing gear shimmy, expressions of MR damper equivalent damping coefficient with voltage and amplitude was set up firstly. And then, the mathematical model for semi-active control of landing gear shimmy was constructed and maximum energy dissipation approach based on MR was proposed to suppress shimmy. Finally, the critical shimmy velocity varying with the vertical force during taxiing was investigated in different caster lengths. The simulation results show that the performance of MR to suppress shimmy is greatly superior to hydraulic shimmy damper during taxiing, and MR not only suppresses shimmy completely but also exhibits good robustness about some system parameters.
  • Keywords
    aerospace control; hydraulic control equipment; magnetorheology; robust control; shock absorbers; vibration control; caster length; critical shimmy velocity; damping coefficient; hydraulic shimmy damper; landing gear shimmy; magnetorheological damper; mathematical model; maximum energy dissipation; semiactive control; taxiing; vertical force; Aircraft; Damping; Force; Gears; Mathematical model; Shock absorbers; Wheels; magneto-rheological (MR) damper; maximum energy dissipation; robustness; semi-active; shimmy;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5633047
  • Filename
    5633047