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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.11.026
Abstract: Abstract This work presents a closed-loop guidance algorithm for six-degrees of freedom spacecraft rendezvous with a passive target flying in an eccentric orbit. The main assumption is that the chaser vehicle has an attitude control…
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Keywords:
predictive controller;
six degrees;
degrees freedom;
spacecraft rendezvous ... See more keywords