• DocumentCode
    1366476
  • Title

    Adaptive fuzzy control of satellite attitude by reinforcement learning

  • Author

    van Buijtenen, Walter M. ; Schram, Gerard ; Babuska, Robert ; Verbruggen, Henk B.

  • Author_Institution
    Dept. of Electr. Eng., Delft Univ. of Technol., Netherlands
  • Volume
    6
  • Issue
    2
  • fYear
    1998
  • fDate
    5/1/1998 12:00:00 AM
  • Firstpage
    185
  • Lastpage
    194
  • Abstract
    The attitude control of a satellite is often characterized by a limit cycle, caused by measurement inaccuracies and noise in the sensor output. In order to reduce the limit cycle, a nonlinear fuzzy controller was applied. The controller was tuned by means of reinforcement learning without using any model of the sensors or the satellite. The reinforcement signal is computed as a fuzzy performance measure using a noncompensatory aggregation of two control subgoals. Convergence of the reinforcement learning scheme is improved by computing the temporal difference error over several time steps and adapting the critic and the controller at a lower sampling rate. The results show that an adaptive fuzzy controller can better cope with the sensor noise and nonlinearities than a standard linear controller
  • Keywords
    adaptive control; artificial satellites; attitude control; convergence; fuzzy control; learning (artificial intelligence); limit cycles; neurocontrollers; nonlinear control systems; adaptive fuzzy control; limit cycle; measurement inaccuracies; noncompensatory aggregation; nonlinear fuzzy controller; reinforcement learning; satellite attitude control; sensor noise; temporal difference error; Adaptive control; Attitude control; Control nonlinearities; Fuzzy control; Learning; Limit-cycles; Noise measurement; Programmable control; Satellites; Sensor phenomena and characterization;
  • fLanguage
    English
  • Journal_Title
    Fuzzy Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1063-6706
  • Type

    jour

  • DOI
    10.1109/91.669012
  • Filename
    669012