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Flexible Satellite Attitude Control via Adaptive Fuzzy Linearization

Flexible Satellite Attitude Control via Adaptive Fuzzy Linearization
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摘要 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. 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.
出处 《Journal of Beijing Institute of Technology》 EI CAS 2005年第2期140-144,共5页 北京理工大学学报(英文版)
基金 SponsoredbytheNationalNaturalScienceFoundation(50277032)
关键词 adaptive fuzzy control input-output linerization attitude maneuver flexible satellite adaptive fuzzy control input-output linerization attitude maneuver flexible satellite
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参考文献3

  • 1Sahjendra N S,Ashok I.Nonlinear decoupling sliding mode control and attitude control of spacecraft[].IEEE Transactions on Aerospace and Electronic Systems.1989
  • 2Elmali H,Olgac N.Robust output tracking of MIMO nonlinear systems via sliding mode technique[].Automatica.1992
  • 3Sahjendra N S,Woosoon Y.Feedback linearization and solar pressure satellite attitude control[].IEEE Trans on Aerospace and Electronic Systems.1996

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