• DocumentCode
    488513
  • Title

    Modeling and Stabilization of Rotating Flexible Structures

  • Author

    Posbergh, T.A.

  • Author_Institution
    Aerospace Engineering and Mechanics, University of Minnesota, Minneapolis, MN 55455
  • fYear
    1990
  • fDate
    23-25 May 1990
  • Firstpage
    2452
  • Lastpage
    2453
  • Abstract
    The design of control systems for flexible spacecraft continues to be an important problem. In the case of spacecraft undergoing large rotations one needs to consider the underlying nonlinear model if we are to adequately model such a system for the purpose of control system design. In this paper we outline the derivation of a linear model for a rotating system and its stabilization.
  • Keywords
    Aerospace control; Capacitive sensors; Control system synthesis; Deformable models; Equations; Flexible structures; Nonlinear control systems; Solid modeling; Space vehicles; Symmetric matrices;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1990
  • Conference_Location
    San Diego, CA, USA
  • Type

    conf

  • Filename
    4791168
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=488513