@inproceedings{72eb486db7e84e18a3176ea3f2c8d347,
title = "On the stability of approximate displaced lunar orbits",
abstract = "In a prior study, a methodology was developed for computing approximate large displaced orbits in the Earth-Moon circular restricted three-body problem (CRTBP) by the Moon-Sail two-body problem. It was found that far from the L(1) and L(2) points, the approximate two-body analysis for large accelerations matches well with the dynamics of displaced orbits in relation to the three-body problem. In the present study, the linear stability characteristics of the families of approximate periodic orbits are investigated.",
keywords = "restricted 3-body problem, points , periodic-orbits, solar-sail",
author = "Jules Simo and Colin McInnes",
year = "2010",
month = feb,
day = "14",
language = "English",
isbn = "9780877035602",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc",
number = "1-3",
pages = "1229--1238",
editor = "D. Mortari and T.F. Starchville and A.J. Trask and J.K. Miller",
booktitle = "Spaceflight mechanics 2010",
note = "20th Spaceflight Mechanics Meeting, Spaceflight Mechanics 2010 ; Conference date: 14-02-2011 Through 17-02-2011",
}