Coupled orbital and attitude control in spacecraft rendezvous and soft docking
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DOI: 10.1177/0954410018792991
Abstract: This paper discusses coupled orbital and attitude control in spacecraft rendezvous and soft docking. The target spacecraft orbit can be either circular or elliptic. The high-fidelity model for this problem is intrinsically a nonlinear system… read more here.
Keywords: coupled orbital; control; orbital attitude; attitude control ... See more keywords