@inproceedings{fa4c697d76b24da699484e7ab7017403,
title = "Low energy escape using tube dynamics associated with quasi-halo orbit",
abstract = "Analysis of tube dynamics under two dimensions has been analyzed by Koon et al.2 However, analysis in three dimensions has not been done sufficiently. In this work, we discuss on designing Mars escape trajectory in the three-body system via invariant manifolds. In contrast with the conventional methods, we propose to use invariant manifolds from quasi-periodic invariant tori and investigate quasi-halo orbits and their associated tubes. Finally, we show how the invariant manifolds of quasi-periodic orbits can provide new escape trajectories from the Martian system in the circular restricted three-body problem.",
author = "Kazutoshi Takemura and Nicola Baresi and Yasuhiro Kawakatsu and Hiroaki Yoshimura",
note = "Funding Information: H.Y. is partially supported by JSPS Grant-in-Aid for Scientific Research (16KT0024, 24224004), the MEXT? Top Global University Project ?and Waseda University (SR 2018K-195). Publisher Copyright: {\textcopyright} 2019, Univelt Inc. All rights reserved.; 29th AAS/AIAA Space Flight Mechanics Meeting, 2019 ; Conference date: 13-01-2019 Through 17-01-2019",
year = "2019",
language = "English",
isbn = "9780877036593",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "701--711",
editor = "Francesco Topputo and Sinclair, {Andrew J.} and Wilkins, {Matthew P.} and Renato Zanetti",
booktitle = "Spaceflight Mechanics 2019",
}