Four classical and invariant error-state Kalman filters for global aided INS are derived in full, with system matrices, Jacobians and reset rules presented for direct comparison.
Equivalence of Left- and Right-Invariant Extended Kalman Filters on Matrix Lie Groups
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abstract
This paper derives the extended Kalman filter (EKF) for continuous-time systems on matrix Lie groups observed through discrete-time measurements. By modeling the system noise on the Lie algebra and adopting a Stratonovich interpretation for the stochastic differential equation (SDE), we ensure that solutions remain on the manifold. The derivation of the filter follows classical EKF principles, naturally integrating a necessary full-order covariance reset post-measurement update. A key contribution is proving that this full-order covariance reset guarantees that the Lie-group-valued state estimate is invariant to whether a left- or right-invariant error definition is used in the EKF. Monte Carlo simulations of the aided inertial navigation problem validate the invariance property and confirm its absence when employing reduced-order covariance resets.
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2026 1verdicts
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Derivations of Error-State Kalman Filter Kinematics for Globally Applicable Aided Inertial Navigation Systems
Four classical and invariant error-state Kalman filters for global aided INS are derived in full, with system matrices, Jacobians and reset rules presented for direct comparison.