Orbit determination and thrust force modeling for a...

SCIENCE CHINA Physics, Mechanics & Astronomy 2012 / 04 Vol. 55; Iss. 4

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

TianHe Xu, KaiFei He, GuoChang Xu
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Volume:
55
Language:
english
DOI:
10.1007/s11433-012-4670-4
Date:
April, 2012
File:
PDF, 680 KB
english, 2012
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