The HelioSwarm mission will fly a multi-satellite observatory in a P/2 lunar resonant orbit to study plasma turbulence in the solar wind. Lunar resonant orbits enable long-term access to high Earth altitudes. The relative dynamics of a multi-satellite observatory introduce novel considerations for lunar resonant orbit design. Additional maneuvers in the post lunar encounter transfer enable heightened control of the lunar resonant orbit initial state compared to previous missions. Adjusting the mission orbit’s initial conditions enables refinement of the orbit design based on requirements imposed by the relative dynamics of the observatory. refinement of the orbit design based on requirements imposed by the relative dynamics of the observatory.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    HelioSwarm: Transfer Trajectory and P/2 Lunar Resonant Orbit Design for a Multi-Satellite Observatory


    Beteiligte:
    Paul Levinson-Muth (Autor:in) / Maxwell Joyner (Autor:in) / Laura Plice (Autor:in)

    Kongress:

    34th AIAA/AAS Space Flight Mechanics Meeting ; 2024 ; Orlando, FL, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    HelioSwarm: Relative Orbit Maintenance in Eccentric P/2 Lunar Resonant Orbit

    Paul Levinson Muth / Laura Plice / Jose Alvarellos | NTRS


    HelioSwarm: Relative Orbit Maintenance in Eccentric P/2 Lunar Resonant Orbit

    Paul Levinson-Muth / Laura Plice / Jose Alvarellos | NTRS


    HelioSwarm: Swarm Design Methods in Eccentric P/2 Lunar Resonant Orbit

    P. Levinson-Muth / S. West / L. Plice | NTIS | 2022


    HelioSwarm: Swarm Design Methods in Eccentric P/2 Lunar Resonant Orbit

    Paul Levinson-Muth / Stephen West / Laura Plice | NTRS