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.
Earth Observation System Flight Dynamics System Covariance Realism
International Earth Science Constellation Mission Operations Working Group ; 2016 ; Boulder, CO, United States
2016-03-01
Miscellaneous
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English
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