@inproceedings{74d486f347844d839d80e89ea682d45c,
title = "Global search for low-thrust transfers to the moon in the planar circular restricted three-body problem",
abstract = "The present study globally searches for low-thrust transfers to the Moon in the planar, circular, restricted, three-body problem. To reduce the dimensionality of parameters for determining initial costates, we narrow down candidates of solutions to those satisfying the necessary conditions for optimality based on the indirect method and use an analogy with the two-body dynamics for the initial periodic orbit around the Earth. We obtain a wide range of Pareto solutions in terms of time of flight and mass consumption. Several solutions exploit resonant lunar gravity assists to reduce fuel consumption.",
author = "Kenta Oshima and Stefano Campagnola and Tomohiro Yanao",
note = "Funding Information: This study has been partially supported by Grant-in-Aid for JSPS Fellows No. 15J07090, and by JSPS Grant-in-Aid, No. 26800207. Copyright: Copyright 2017 Elsevier B.V., All rights reserved.; 26th AAS/AIAA Space Flight Mechanics Meeting, 2016 ; Conference date: 14-02-2016 Through 18-02-2016",
year = "2016",
language = "English",
isbn = "9780877036333",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "415--433",
editor = "Ozimek, {Martin T.} and Renato Zanetti and Bowes, {Angela L.} and Russell, {Ryan P.} and Ozimek, {Martin T.}",
booktitle = "Spaceflight Mechanics 2016",
}