Volume 40 Issue 3
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WANG Hongwei, SONG Xiaojuan, LI Changjie. Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft[J]. Journal of Space Science, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408
Citation: WANG Hongwei, SONG Xiaojuan, LI Changjie. Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft[J]. Journal of Space Science, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408
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Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft

doi: 10.11728/cjss2020.03.408

  • College of Mechanical Engineering, Inner Mongolia University of Technology, Hohhot 010051

  • Received Date: 2019-03-06
  • Rev Recd Date: 2020-02-11
  • Publish Date: 2020-05-15
    Abstract
  • In this paper, the large-angle attitude maneuver of three-axis stabilized liquid-filled spacecraft based on adaptive passive control is studied. The liquid sloshing is equivalent to the viscous spherical pendulum model, and the dynamic model of the coupled system is established by using the law of conservation of angular momentum. In view of the fact that gyroscope faults or gyroscope-free configuration lead to no angular velocity measurement of spacecraft attitude, considering the characteristics of unknown external disturbance, the moment of inertia uncertainty and the un-measurable characteristics of liquid sloshing displacement, the adaptive output feedback passive control law is designed for large angel attitude maneuver of spacecraft. The adaptive update laws are used to compensate for external disturbances and estimate state variables for liquid sloshing. The Lyapunov method and LaSalle invariant lemma prove that the control law can not only ensure the asymptotic stability of the closed-loop system but also ensure the two desired equilibrium positions are stable. Finally, simulation results verify the effectiveness of the proposed control method.

     

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