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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2020.07.010
Abstract: Abstract The aim of this paper is to evaluate the effect of a maximum admissible value of the sail cone angle on the transfer performance of a solar sail-based spacecraft in an interplanetary mission scenario.…
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Keywords:
attitude constraints;
solar sail;
sail;
effects attitude ... See more keywords