A low-cost orbit control strategy addressed only to control the orbit subtrack (latitude and longitude of the operational loop of the orbit) and to control the apogee passage time-shift, which impacts on the synchronization between the satellites, is studied. This control strategy, exclusively based on in plane maneuvers, consist of adjusting the apogee radius by perigee burns obtaining a semiaxis variation which cancels the total subtrack shift or puts the subtrack on the other side with respect to the nominal position.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Orbit Control Strategy for a Constellation of Three Satellites in Tundra Orbits


    Beteiligte:
    G. Rondinelli (Autor:in) / A. Cramarossa (Autor:in) / F. Graziani (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Low Cost Station Keeping Maneuvers for a Small-Satellites Constellation in Tundra Orbits

    A. Cramarossa / G. Barresi / G. Rondinelli et al. | NTIS | 1990


    Molniya/Tundra Orbit Constellation Considerations for Commercial Applications (AAS 01-215)

    Turner, A. E. / American Astronautical Society | British Library Conference Proceedings | 2001



    Molniya/Tundra Orbit Constellation Considerations for Commercial Applications (AAS 01-215)

    Turner, A. E. / AAS / AIAA | British Library Conference Proceedings | 2001


    Tundra Constellation Design and Stationkeeping

    Bruno, M.J. | Online Contents | 2005