IMAN is a Python tool that provides inertial sensor-based estimates of spacecraft trajectories within an atmospheric influence. It provides Kalman filter-derived spacecraft state estimates based upon data collected onboard, and is shown to perform at a level comparable to the conventional methods of spacecraft navigation in terms of accuracy and at a higher level with regard to the availability of results immediately after completion of an atmospheric drag pass.


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    Titel :

    Inertial Measurements for Aero-assisted Navigation (IMAN)


    Beteiligte:
    Jah, Moriba (Autor:in) / Lisano, Michael (Autor:in) / Hockney, George (Autor:in)


    Erscheinungsdatum :

    01.09.2007


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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