• DocumentCode
    2761266
  • Title

    The design of LQG and H∞ controllers for use in active vibration control and narrow band disturbance rejection

  • Author

    Connolly, Allan J. ; Green, Michael ; Chicharo, Joe F. ; Bitmead, Robert R.

  • Author_Institution
    Dept. of Syst. Eng., Australian Nat. Univ., Canberra, ACT, Australia
  • Volume
    3
  • fYear
    1995
  • fDate
    13-15 Dec 1995
  • Firstpage
    2982
  • Abstract
    This paper develops an H∞ design method for narrow band disturbance rejection. The method is based on the LQG approach via disturbance modelling given in De Nicolao (1992). These LQG and H∞ approaches to the narrow band disturbance rejection problem are then applied to a helicopter active vibration control problem
  • Keywords
    H∞ control; aircraft control; control system synthesis; helicopters; linear quadratic Gaussian control; vibration control; H∞ controllers; LQG control; active vibration control; disturbance modelling; helicopter; narrow band disturbance rejection; Australia; Damping; Delta modulation; Frequency; H infinity control; Helicopters; Narrowband; Servomechanisms; Strips; Vibration control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
  • Conference_Location
    New Orleans, LA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-2685-7
  • Type

    conf

  • DOI
    10.1109/CDC.1995.478598
  • Filename
    478598
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2761266