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This research proposes a Dual Quaternion-Based Unscented Kalman Filter integrated with Visual Inertial Odometry to improve state estimation in GPS-denied scenarios. Simulation results on the EuRoC MAV dataset demonstrate that the method achieves a position RMSE of 0.2584m under high initialization uncertainty, outperforming benchmark filters. The approach offers a robust mathematical framework combining unit dual quaternions with twistor parameterization for sigma point generation, relevant for robotics and autonomous vehicle navigation.
Dual Quaternion-Based Unscented Kalman Filter with Visual Inertial Odometry for Navigation in GPS-Denied Environments
arXiv:2606.09292v1 Announce Type: new Abstract: Reliable navigation in GPS-denied environments remains a fundamental challenge in robotics, aerospace, and autonomous vehicle applications. This paper presents a Dual Quaternion-Based Unscented Kalman Filter (DQUKF) equipped with a Visual Inertial Odometry (VIO) algorithm for accurate state estimation enabling navigation in GPS denied locations. The proposed framework formulates the DQUKF in an error state manner, where the nominal pose is represented by a unit dual quaternion and the local pose error is represented by a 6-dimensional twistor parameterization used for sigma point generation, covariance propagation, and measurement correction. In parallel, the VIO algorithm tracks features across image frames, synchronizes measurements between the IMU and camera, and provides visual constraints that complement inertial propagation. Simulation results on the EuRoC MAV dataset show that the proposed DQUKF converges under high initialization uncertainty and achieves a position RMSE of 0.2584~m in the difficult flight sequence, outperforming the benchmark filters.
Abstract:Reliable navigation in GPS-denied environments remains a fundamental challenge in robotics, aerospace, and autonomous vehicle applications. This paper presents a Dual Quaternion-Based Unscented Kalman Filter (DQUKF) equipped with a Visual Inertial Odometry (VIO) algorithm for accurate state estimation enabling navigation in GPS denied locations. The proposed framework formulates the DQUKF in an error state manner, where the nominal pose is represented by a unit dual quaternion and the local pose error is represented by a 6-dimensional twistor parameterization used for sigma point generation, covariance propagation, and measurement correction. In parallel, the VIO algorithm tracks features across image frames, synchronizes measurements between the IMU and camera, and provides visual constraints that complement inertial propagation. Simulation results on the EuRoC MAV dataset show that the proposed DQUKF converges under high initialization uncertainty and achieves a position RMSE of 0.2584~m in the difficult flight sequence, outperforming the benchmark filters.
Robotics (cs.RO); Systems and Control (eess.SY)
arXiv:2606.09292 [cs.RO]
(or arXiv:2606.09292v1 [cs.RO] for this version)
https://doi.org/10.48550/arXiv.2606.09292 Focus to learn more arXiv-issued DOI via DataCite (pending registration)
https://doi.org/10.1016/j.measurement.2026.121964 Focus to learn more DOI(s) linking to related resources
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