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 ORCID logoORCID: https://orcid.org/0000-0002-1489-5920 and McInnes, Colin; Mortari, D., Starchville, T.F., Trask, A.J. and Miller, J.K.
    Item type:Book Section
    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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