On the stability of approximate displaced lunar orbits
Simo, Jules and McInnes, Colin; Mortari, D. and Starchville, T.F. and Trask, A.J. and Miller, J.K., eds. (2010) On the stability of approximate displaced lunar orbits. In: Spaceflight mechanics 2010. Advances in the Astronautical Sciences . Univelt Inc, USA, pp. 1229-1238. ISBN 9780877035602
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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.
Creators(s): |
Simo, Jules ![]() | Item type: | Book Section |
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ID code: | 32600 |
Keywords: | restricted 3-body problem, points , periodic-orbits, solar-sail, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering, Control and Systems Engineering |
Subjects: | Technology > Mechanical engineering and machinery Technology > Motor vehicles. Aeronautics. Astronautics |
Department: | Faculty of Engineering > Mechanical and Aerospace Engineering |
Depositing user: | Pure Administrator |
Date deposited: | 20 Jan 2012 09:44 |
Last modified: | 01 Jan 2021 13:59 |
Related URLs: | |
URI: | https://strathprints.strath.ac.uk/id/eprint/32600 |
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