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A consensus control framework for the rotational dynamics of multiple spacecraft is developed. The approach is energy based and guarantees asymptotic convergence of relative states between the spacecraft. Since the proposed control law emulates internal forces between the spacecraft, the overall angular momentum is kept constant. Furthermore, it is shown that the angular velocities of each spacecraft...
A consensus control framework for rotation dynamics of multiple underactuated spacecraft is developed. Following the results by Bullo et al. (2000), we propose a control law that achieves asymptotic consensus between the spacecraft. Finally, we present a numerical example to show efficacy of the proposed approach.
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