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Orbit determination and thrust force modeling for a maneuvered GEO satellite using two-way adaptive Kalman filtering
TianHe Xu, KaiFei He, GuoChang XuVolume:
55
Language:
english
DOI:
10.1007/s11433-012-4670-4
Date:
April, 2012
File:
PDF, 680 KB
english, 2012