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UKF-Based Reconfigurable Attitude Parameters Estimation and Magnetometer Calibration
Date
2012-07-01
Author
Söken, Halil Ersin
Hacızade, Cengiz
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This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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A reconfigurable unscented Kalman filter (UKF)-based estimation algorithm for magnetometer biases and scale factors is proposed as a part of the attitude estimation scheme of a pico satellite. Unlike existing algorithms, in this paper, scale factors are not treated, together with other parameters, as part of the state vector; they are estimated separately. After satisfying the conditions of the proposed stopping rule for bias estimation, UKF reconfigures itself for estimation of attitude parameters alone.
URI
https://hdl.handle.net/11511/69774
Journal
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
DOI
https://doi.org/10.1109/taes.2012.6237612
Collections
Department of Aerospace Engineering, Article