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

✍ Scribed by TianHe Xu; KaiFei He; GuoChang Xu


Book ID
118814471
Publisher
Science in China Press (SCP)
Year
2012
Tongue
English
Weight
680 KB
Volume
55
Category
Article
ISSN
1672-1799

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