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Autonomous satellite navigation via kalman filtering of magnetometer data

โœ Scribed by Matthias Wiegand


Publisher
Elsevier Science
Year
1996
Tongue
English
Weight
832 KB
Volume
38
Category
Article
ISSN
0094-5765

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Pico satellite attitude estimation via R
โœ Halil Ersin Soken; Chingiz Hajiyev ๐Ÿ“‚ Article ๐Ÿ“… 2010 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 430 KB

## 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