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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.10.028
Abstract: Abstract The aim of this paper is to propose a distributed control architecture for a solar sail-based formation, flying around an L 2 -type artificial equilibrium point in the Sun-[Earth + Moon] circular restricted three-body problem. Two…
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Keywords:
formation flying;
solar sail;
formation;
flying around ... See more keywords