Distributed Approximate Optimal Attitude Control of Combined Spacecraft With Parameters Identification
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DOI: 10.1109/taes.2023.3341058
Abstract: The distributed attitude takeover control problem of a target spacecraft with unknown inertia matrix by using multiple service satellites is investigated in this article. Based on the time-interval integration model of the attitude dynamics, an… read more here.
Keywords: attitude control; control; inertia matrix; approximate optimal ... See more keywords