Quaternion invariant extended Kalman filtering for spacecraft attitude estimation

H Gui, AHJ de Ruiter - Journal of Guidance, Control, and Dynamics, 2018 - arc.aiaa.org
The spacecraft attitude estimation is addressed in the framework of invariant Kalman
filtering, which rests on invariance of the system dynamics and output map with respect to …
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[引用][C] Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation

H Gui, AHJ de Ruiter - Journal of Guidance Control …, 2018 - ui.adsabs.harvard.edu
Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation - NASA/ADS
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[PDF][PDF] Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation

H Gui, AHJ de Ruiter - researchgate.net
Among the existing methods, the multiplicative EKF (MEKF) in terms of quaternions has
achieved broad applications because it is nonsingular and involves fewer parameters than …