• DocumentCode
    1673922
  • Title

    Fuzzy control based on H∞ output feedback for attitude stabilization of flexible satellite

  • Author

    Nam, Sae Kyu ; Kim, Kyung Kern

  • Author_Institution
    Agency for Defense Dev., Taejon, South Korea
  • Volume
    1
  • fYear
    2001
  • fDate
    6/23/1905 12:00:00 AM
  • Firstpage
    159
  • Lastpage
    162
  • Abstract
    This paper focuses on designing a robust fuzzy multivariable controller for the attitude stabilization system of a flexible satellite. Fuzzy control is combined with LMI-based H∞ output feedback methods to suppress the interaction of rigid-elastic coupling modes. The proposed method can afford to reinforce the precise pointing capability of satellites under parameter varying space missions, because its control structure reformulated on fuzzy cells offers the blending of sub-optimal control laws
  • Keywords
    H∞ control; artificial satellites; attitude control; control system synthesis; feedback; flexible structures; fuzzy control; multivariable control systems; robust control; stability; suboptimal control; H∞ output feedback; LMI-based H∞ output feedback methods; attitude stabilization; flexible satellite; fuzzy cells; fuzzy control; parameter varying space missions; pointing capability; rigid-elastic coupling mode interaction suppression; robust fuzzy multivariable controller design; sub-optimal control law blending; Attitude control; Control systems; Distributed control; Equations; Fuzzy control; Fuzzy systems; Lyapunov method; Matrices; Output feedback; Shape control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Fuzzy Systems, 2001. The 10th IEEE International Conference on
  • Conference_Location
    Melbourne, Vic.
  • Print_ISBN
    0-7803-7293-X
  • Type

    conf

  • DOI
    10.1109/FUZZ.2001.1007271
  • Filename
    1007271
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1673922