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Article Navigation> JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY> 2005> 14(2): 140-144
GUAN Ping, LIU Xiang-dong, CHEN Jia-bin, LIU Xiao-he. Flexible Satellite Attitude Control via Adaptive Fuzzy Linearization[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2005, 14(2): 140-144.
Citation: GUAN Ping, LIU Xiang-dong, CHEN Jia-bin, LIU Xiao-he. Flexible Satellite Attitude Control via Adaptive Fuzzy Linearization[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2005, 14(2): 140-144.
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Flexible Satellite Attitude Control via Adaptive Fuzzy Linearization

  • 1.

    School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China; Department of Automation, Beijing Institute of Machinery, Beijing 100085, China

  • 2.

    School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China

  • 3.

    Department of Automation, Beijing Institute of Machinery, Beijing 100085, China

Funds:SponsoredbytheNationalNaturalScienceFoundation(50277032)
  • Received Date:2003-11-23
    Abstract
  • The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite. The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.
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    • References (5)
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