Two-stage unscented Kalman filter algorithm for fault estimation in spacecraft attitude control system

Published 2018 View Full Article

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Title
Two-stage unscented Kalman filter algorithm for fault estimation in spacecraft attitude control system
Authors
Keywords
-
Journal
IET Control Theory and Applications
Volume -, Issue -, Pages -
Publisher
Institution of Engineering and Technology (IET)
Online
2018-04-11
DOI
10.1049/iet-cta.2017.1369

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