This presentation applies a covariance realism technique to the National Aeronautics and Space Administration (NASA) Earth Observation System (EOS) Aqua and Aura spacecraft based on inferential statistics. The technique consists of three parts: collection calculation of definitive state estimates through orbit determination, calculation of covariance realism test statistics at each covariance propagation point, and proper assessment of those test statistics.


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    Titel :

    Earth Observation System Flight Dynamics System Covariance Realism


    Beteiligte:

    Kongress:

    International Earth Science Constellation Mission Operations Working Group ; 2016 ; Boulder, CO, United States


    Erscheinungsdatum :

    01.03.2016


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






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