Pico satellite attitude estimation via R
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Halil Ersin Soken; Chingiz Hajiyev
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Article
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2010
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Elsevier Science
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English
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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