Orbit determination and thrust force modeling for a maneuvered GEO satellite 
using two-way adaptive Kalman filtering

Xu, T.; He, Kaifei; Xu, Guochang

doi:10.1007/s11433-012-4670-4

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Orbit determination and thrust force modeling for a maneuvered GEO satellite using two-way adaptive Kalman filtering

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Xu, T.
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He, Kaifei
1.2 Global Geomonitoring and Gravity Field, 1.0 Geodesy and Remote Sensing, Departments, GFZ Publication Database, Deutsches GeoForschungsZentrum;

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Xu, Guochang
1.2 Global Geomonitoring and Gravity Field, 1.0 Geodesy and Remote Sensing, Departments, GFZ Publication Database, Deutsches GeoForschungsZentrum;

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Xu, T., He, K., Xu, G. (2012): Orbit determination and thrust force modeling for a maneuvered GEO satellite using two-way adaptive Kalman filtering. - Science China Physics, Mechanics and Astronomy, 55, 4, 738-745.
https://doi.org/10.1007/s11433-012-4670-4

https://gfzpublic.gfz-potsdam.de/pubman/item/item_246541

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