• DocumentCode
    486901
  • Title

    An Optimized Yaw Damper for Enhanced Passenger Ride Comfort

  • Author

    Goslin, T.J. ; Ansari, F.H. ; Chakravarty, A.

  • Author_Institution
    Boeing Commercial Airplane Company
  • fYear
    1987
  • fDate
    10-12 June 1987
  • Firstpage
    395
  • Lastpage
    396
  • Abstract
    The primary purpose of any yaw damper is to suppress the dutch roll response of the airplane in turbulence. Large lateral accelerations at the aft end of the aircraft are especially degrading to ride quality. These lateral accelerations are due to higher frequency structural modes of the aircraft in addition to the low frequency dutch roll mode. Here we will present an optimized yaw damper to enhance passenger ride comfort. Because of the limited scope of this analysis, only the rigid body effects, or dutch roll mode, will be considered.
  • Keywords
    Acceleration; Aircraft; Airplanes; Damping; Degradation; Delay; Feeds; Filters; Frequency; Shock absorbers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1987
  • Conference_Location
    Minneapolis, MN, USA
  • Type

    conf

  • Filename
    4789350