This article investigates the control allocation problem for attitude stabilization of an over-actuated spacecraft. A Stackelberg differential game framework is established to describe the bidirectional interactivity and decision-making mechanism between attitude control and control allocation, based on which the optimal attitude control law and the optimal control allocation strategy are designed integratedly and constitute a Stackelberg equilibrium to realize their overall stabilization and optimization. Simulation and experiment results demonstrate the effectiveness of the proposed approach.


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    Title :

    Control Allocation of Spacecraft Revisited: A Stackelberg Differential Game Approach


    Contributors:
    Ni, Yuan (author) / Yang, Hao (author) / Jiang, Bin (author)


    Publication date :

    2024-10-01


    Size :

    1693086 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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