• DocumentCode
    783129
  • Title

    Active damping control of vibrational systems

  • Author

    Song, Y.D. ; Mitchell, T.L.

  • Author_Institution
    Dept. of Electr. Eng., North Carolina A&T State Univ., Greensboro, NC, USA
  • Volume
    32
  • Issue
    2
  • fYear
    1996
  • fDate
    4/1/1996 12:00:00 AM
  • Firstpage
    569
  • Lastpage
    577
  • Abstract
    The problem of vibration suppression in large flexible space structure (LFSS) is investigated. Based on the structure property of LFSS, an active damping strategy is proposed to effectively attenuate the critical vibrations of the structure subject to modeling uncertainty and external disturbance. Control algorithms are derived with the aim of suppressing both the vibrating magnitude and vibrating rate to an acceptable level. It is shown that the strategy exhibits robust and adaptive properties and is truly model-independent. The novelty of the proposed approach lies in the fact that it is fairly easy to set up the strategy and the overall computation involved is much less than any other strategies available to date. A two-bay truss is used to verify the validity of the proposed approach.
  • Keywords
    aerospace control; damping; flexible structures; vibration control; active damping control; critical vibrations; external disturbance; large flexible space structure; model-independent strategy; modeling uncertainty; two-bay truss; vibrating magnitude; vibrating rate; vibration suppression; vibrational systems; Actuators; Agriculture; Control systems; Damping; Flexible structures; Fuels; Modal analysis; NASA; Robustness; Uncertainty; Vibration control; Weight control;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.489501
  • Filename
    489501