Spin-to-spin slew maneuvers under spherically constrained angular acceleration
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DOI: 10.1016/j.asr.2019.06.026
Abstract: Abstract This paper addresses a three-axis time-optimal attitude-control problem of rigid spacecraft. In this problem, an angular-acceleration vector lies within a spherically constrained space, and spin-to-spin boundary conditions are considered. The problem is converted into… read more here.
Keywords: spin spin; spherically constrained; angular acceleration; slew maneuvers ... See more keywords