• DocumentCode
    3593982
  • Title

    Robust Control of An Active Precision Truss Structure

  • Author

    Chu, C.C. ; Smith, R.S. ; Fanson, J.L.

  • Author_Institution
    Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109
  • fYear
    1990
  • Firstpage
    2490
  • Lastpage
    2495
  • Abstract
    Stringent pointing and shape accuracy requirements necessitate advances in the control of flexible structures. These precision truss structures will be flexible in the micron regime, and their vibration modes will be densely spaced throughout the frequency range of interest. Such attributes pose a great challenge for the control design to attenuate vibration in one frequency range while not destabilizing other flexible modes outside this range. The problem is further compounded by the inaccuracy of models which requires the control law to be robust to a variety of modeling uncertainties. This paper describes the efforts in control of an active precision truss structure experiment at JPL. The control objective is to provide vibration suppression to selected modes of the structure subject to a band-limited disturbance and modeling errors. Based on performance requirements and uncertainty description, several control laws using H¿ optimization method are synthesized. These controllers are implemented on the experimental facility. Preliminary experimental results are also presented.
  • Keywords
    Actuators; Control system synthesis; Control systems; Damping; Feedback control; Frequency; Robust control; Shape control; Uncertainty; Vibration control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1990
  • Type

    conf

  • Filename
    4791175