Pico satellite attitude estimation via Robust Unscented Kalman Filter in the presence of measurement faults.
作者： Halil Ersin Soken , Chingiz Hajiyev
DOI: 10.1016/J.ISATRA.2010.04.001
关键词: Discrete time and continuous time 、 Scale factor 、 Engineering 、 Noise 、 Signal-to-noise ratio 、 System identification 、 Extended Kalman filter 、 Attitude control 、 Control theory 、 Kalman filter
摘要: … Kalman Filter (RUKF) algorithms with single and multiple measurement noise scale factors are introduced and applied for the attitude parameter estimation … satellite attitude estimation. …
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