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

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

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Xu, T.¹, Author
He, Kaifei², Author
Xu, Guochang², Author

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1External Organizations, ou_persistent22
21.2 Global Geomonitoring and Gravity Field, 1.0 Geodesy and Remote Sensing, Departments, GFZ Publication Database, Deutsches GeoForschungsZentrum, ou_146026

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DDC: 550 - Earth sciences

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Dates: Finally published : 2012

Publication Status: Finally published

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Identifiers: eDoc: 19971
GFZPOF: PT1 Planet Earth: Global Processes and Change
DOI: 10.1007/s11433-012-4670-4

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Title: Science China Physics, Mechanics and Astronomy

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Pages: - Volume / Issue: 55 (4) Sequence Number: - Start / End Page: 738 - 745 Identifier: CoNE: https://gfzpublic.gfz-potsdam.de/cone/journals/resource/journals443