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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    Title :

    Earth Observation System Flight Dynamics System Covariance Realism


    Contributors:

    Conference:

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


    Publication date :

    2016-03-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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