Abstract Trajectory design in chaotic regimes allows for the exploitation of system dynamics to achieve certain behaviors. For example, for the Transiting Exoplanet Survey Satellite (TESS) mission, the selected science orbit represents a stable option well-suited to meet the mission objectives. Extended analysis of particular solutions nearby in the phase space reveals transitions into desirable terminal modes induced by natural dynamics. This investigation explores the trajectory behavior and borrows from flow-based analysis strategies to characterize modes of such a motion. Perturbed initial states from a TESS-like orbit are evolved to supply motion suitable for contingency analysis. Through the associated analysis, mechanisms are identified that drive the spacecraft into particular modes and supply conditions necessary for such transitions.


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    Titel :

    Mode Analysis for Long-Term Behavior in a Resonant Earth–Moon Trajectory


    Beteiligte:
    Short, Cody (Autor:in) / Howell, Kathleen (Autor:in) / Haapala, Amanda (Autor:in) / Dichmann, Donald (Autor:in)


    Erscheinungsdatum :

    2016




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.60 Raumfahrttechnik
    Lokalklassifikation TIB:    770/7040





    Mode Analysis for Long-Term Behavior in a Resonant Earth–Moon Trajectory

    Short, Cody / Howell, Kathleen / Haapala, Amanda et al. | Springer Verlag | 2016



    High-Accuracy Moon to Earth Escape Trajectory Optimization

    Yan, Hui / Gong, Qi / Park, Chan et al. | AIAA | 2010