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  • Periodic and quasi-periodic motions for a Solar sail in the Earth-Moon system

    Paper number

    IAC-16,C1,7,10,x32976

    Coauthor

    Mr. Marc Jorba-Cuscó, University of Barcelona, Spain

    Coauthor

    Dr. Ariadna Farrés, University of Barcelona, Spain

    Coauthor

    Prof. Angel Jorba, University of Barcelona, Spain

    Year

    2016

    Abstract
    Solar sailing is an emerging way of spacecraft propulsion with a
    number of singularities with respect to traditional chemical
    thrusters. While the acceleration achieved by the sail is much
    smaller, it is continuous and limited only by the lifespan of the
    sail. In this work we perform a comprehensive numerical study of the natural motion of a solar sail in the Earth-Moon system. Models for the motion of a solar sail in the Earth-Moon system are not as well studied as in the Sun-Earth case, and, despite there are a few interesting works, none of them takes into account 
    Sun's gravity.\newline
    
    Hence, a model taking into account the Solar radiation pressure plus the gravitational attraction of Earth, Moon and Sun is proposed. In this (restricted) model, we prescribe the motion of Earth, Moon and Sun and focus on the motion of a spacecraft endowed with a solar sail. The described is a dynamical system depending on several parameters representing the efficiency and the orientation of the sail. It is of particular interest the motion near the (Earth-Moon) Lagrangian points.\newline
    
    This model may be regarded as a time-dependent periodic perturbation of the Restricted Three Body problem. Therefore the Lagrangian points are no longer equilibria but they are replaced by periodic orbits with the same period as the periodic perturbation. In a similar manner, the (non-resonant) periodic orbits are replaced by two dimensional invariant tori.
    Based on the computation of these invariant objects, we present a
    detailed description of the skeleton of the dynamics, and how it
    depends of the parameters of the system. This information is very
    useful for the design of space missions.
    Abstract document

    IAC-16,C1,7,10,x32976.brief.pdf

    Manuscript document

    IAC-16,C1,7,10,x32976.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.