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Published in 2018 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2018.05.015
Abstract: Abstract Lunisat represents a next-generation microsatellite aimed at orbiting the Moon, and equipped with dispensers for the release of nanosatellites. This research is focused on the orbital dynamics of both the main microsatellite and the…
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Keywords:
dynamics maneuvers;
lunar orbit;
orbit dynamics;
maneuvers lunisat ... See more keywords
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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2020.07.046
Abstract: Abstract Chandrayaan-2, being the sequel of Indian Lunar Mission, differs with Chandrayaan-1 in targeting a specific lunar orbit. The primary ground trajectory design objective is to achieve the desired lunar orbit, from which the lander…
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Keywords:
moon;
lunar;
trajectory design;
lunar orbit ... See more keywords
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Published in 2022 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/09544100221138131
Abstract: To satisfy the requirement of contingency rescue in the lunar orbit insertion phase for crewed lunar exploration missions, this paper designs the contingency point return trajectory. First, according to different failure situations of the main…
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Keywords:
contingency;
point return;
insertion phase;
orbit insertion ... See more keywords