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    The hybrid attitude maneuver control of the three-axis stable liquid-filled spacecraft with large-deformation appendage

    In this paper, the dynamic model of a three-axis stable liquid-filled spacecraft with a nonlinear appendage is developed. The flexible appendage is assumed to be a cantilever beam, and considering the geometri...

    Yunfeng Shen, Haoxiang Shi, Zhiwen Fan in International Journal of Dynamics and Cont… (2024)