• DocumentCode
    330427
  • Title

    Application of H∞ control to a vibration system using air jet propulsion

  • Author

    Ichihara, Hiroyuki ; Abe, Naoto ; Kanoh, Hideaki

  • Author_Institution
    Dept. of Precision Eng., Meiji Univ., Kanagawa, Japan
  • Volume
    1
  • fYear
    1998
  • fDate
    1-4 Sep 1998
  • Firstpage
    604
  • Abstract
    This paper deals with a vibration control using air jet propulsion. To study its effect, a two links pendulum with a pair of air jet actuators is used as control object. The purpose of the control design is to reject disturbances. We use a simple one link pendulum as a design model. By using identification result of an unmodeled dynamics, we design an H∞ controller to suppress its vibration. In the experiment, we show the effect of air jet propulsion and robust control
  • Keywords
    H∞ control; actuators; control system synthesis; dynamics; identification; pendulums; pneumatic control equipment; robust control; vibration control; H∞ control; air jet actuators; air jet propulsion; dynamics; identification; pendulum; robust control; vibration control; Actuators; Control design; Control systems; Propulsion; Pulse width modulation; Resonance; Robust control; Springs; Uncertainty; Vibration control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1998. Proceedings of the 1998 IEEE International Conference on
  • Conference_Location
    Trieste
  • Print_ISBN
    0-7803-4104-X
  • Type

    conf

  • DOI
    10.1109/CCA.1998.728545
  • Filename
    728545
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=330427