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Application of unscented Kalman filter in satellite orbit simulation

โœ Scribed by Zhao Dongming; Cai Zhiwu


Book ID
105623307
Publisher
Springer
Year
2006
Tongue
English
Weight
327 KB
Volume
9
Category
Article
ISSN
1009-5020

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## a b s t r a c t In the normal operation conditions of a pico satellite, a conventional Unscented Kalman Filter (UKF) gives sufficiently good estimation results. However, if the measurements are not reliable because of any kind of malfunction in the estimation system, UKF gives inaccurate result