AIAA-2003-5393 Prediction of Re-Entry of Space Debris Objects: Constant Gain Kalman Filter Approach
Conference, Atmospheric flight mechanics ; 2003 ; Austin, TX
2003-01-01
11 pages
Contains paper nos AIAA-2003-5300 to AIAA-2003-5707 with gaps
Conference paper
English
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A constant gain Kalman filter approach for the prediction of re-entry of risk objects
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