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  • A study on the effect of solar radiation pressure on the stability region near the Earth-Moon triangular points

    Paper number

    IAC-15,C1,3,8,x29323

    Author

    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

    2015

    Abstract
    The Solar Radiation Pressure (SRP) is the pressure exerted by the electromagnetic radiation emitted by the Sun upon a body. It is known that this physical phenomenon plays an important role on the description of the motion of certain bodies. For instance, SRP has a significant impact on the motion of space dust and it is the underlying physical phenomenon that allows
    spatial navigation with a Solar Sail.\newline
    The purpose of this work is to study the existence of a stability region near the triangular point, $L_{4}$, of the Earth-Moon system when both, Sun's gravitational potential and SRP effects are considered. The model we use is the Bicircular Problem with an extra term corresponding to the SRP, which
    we call SRPBCP. Both the Bicircular Problem and the SRPBCP can be seen as a time dependent perturbation (due to the Sun) of the Earth-Moon Restricted Three Body Problem (RTBP).\newline
    It is well known that the RTBP has five equilibrium points ($L_{i}$, $i=1,\dots, 5$). We focus on $L_{4}$ (and $L_{5}$) which are linearly stable. When the periodic perturbation corresponding to the Sun is added, the Lagrangian points are no longer equilibria, they are replaced by periodic orbits with the same period as the Sun. If the SRP effect is neglected and we
    only consider the perturbation due to the gravitational field of the Sun, there are three periodic orbits with the same period as the Sun in the vicinity of the geometrical $L_{4}$. Analogously, in the Bicircular Problem, the vertical families of periodic orbits of the RTBP are replaced by $2$-dimensional
    invariant tori with two basic frequencies: one of the corresponding vertical orbit and the other corresponding to the periodic motion of the Sun. These invariant tori lead to an effective stability region located at some distance
    from the triangular point, that seems to persist in the real model.\newline
    We will investigate how these invariant tori vary when we include the effect of the SRP in our model, and show how this affects the stability region. We will consider different area-to-mass ratios to understand what kind of objects
    are expected to be found in these regions.
    Abstract document

    IAC-15,C1,3,8,x29323.brief.pdf

    Manuscript document

    IAC-15,C1,3,8,x29323.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.