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Optimization of low-thrust transfers to libration point orbits

Autor: Weipeng Li, Hai Huang

Publikováno v: Aircraft Engineering and Aerospace Technology: An International Journal, 2016, Vol. 88, Issue 1, pp. 16-23.

Externí odkaz: http://www.emeraldinsight.com/doi/10.1108/AEAT-12-2013-0233

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A stable heliocentric disposal strategy for LPO missions, inspired by the natural co-orbital motion of Saturn's moons

Autor: A. Pousse and E.M. Alessi

Publikováno v: 72th International Astronautical Congress (IAC), Dubai, UAE, 25-29 October 2021, Dubai, UAE, 25-29/10/2021
info:cnr-pdr/source/autori:A. Pousse and E.M. Alessi/congresso_nome:72th International Astronautical Congress (IAC), Dubai, UAE, 25-29 October 2021/congresso_luogo:Dubai, UAE/congresso_data:25-29%2F10%2F2021/anno:2021/pagina_da:/pagina_a:/intervallo_pagine

In this work, we present a disposal strategy for Sun-Earth LPO missions, based on stable heliocentric graveyard trajectories that do not approach the Earth-Moon system in the long term. Previous studies analyzed the possibility of reentering to the E

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=cnr_________::0668e4f8938a2ce1bf857a4c8e5efc96
http://www.cnr.it/prodotto/i/458193

Trajectory Optimization in the Three-Body Problem for a Lunar Transportation System

Autor: Segura, Sergi, Viturro, Mauro, Lizy-Destrez, Stéphanie, Dumont, Etienne

Lunar missions and their design are in the agenda of most main space agencies around the world. With the goal of regular lunar missions, many of them manned, both time and fuel efficiency are currently being considered as key aspects of space mission

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::e0144447af91b6572e8ce51a5bfcf169
https://elib.dlr.de/132866/