2020 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) 2020
DOI: 10.1109/iros45743.2020.9341216
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A real-time unscented Kalman filter on manifolds for challenging AUV navigation

Abstract: We consider the problem of localization and navigation of Autonomous Underwater Vehicles (AUV) in the context of high performance subsea asset inspection missions in deep water. We propose a solution based on the recently introduced Unscented Kalman Filter on Manifolds (UKF-M) for onboard navigation to estimate the robot's location, attitude and velocity, using a precise round and rotating Earth navigation model. Our algorithm has the merit of seamlessly handling nonlinearity of attitude, and is far simpler to… Show more

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Cited by 11 publications
(4 citation statements)
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“…Here, H 1 , H 2 , and H 3 are the Earth's magnetic field vector components in the orbit frame as a function of time given as where M e is the magnetic dipole moment of the Earth, 𝜖 is the magnetic dipole tilt, i is the orbit inclination, and 𝜔 e is the spin rate of the Earth. In (11), v mag,C ∈ R 3 is the magnetometer measurement noise which follows N(0, 𝜎 2 mag,C ⋅ I 3 ). The rate gyros measurement model is given as follows:…”
Section: Simulationmentioning
confidence: 99%
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“…Here, H 1 , H 2 , and H 3 are the Earth's magnetic field vector components in the orbit frame as a function of time given as where M e is the magnetic dipole moment of the Earth, 𝜖 is the magnetic dipole tilt, i is the orbit inclination, and 𝜔 e is the spin rate of the Earth. In (11), v mag,C ∈ R 3 is the magnetometer measurement noise which follows N(0, 𝜎 2 mag,C ⋅ I 3 ). The rate gyros measurement model is given as follows:…”
Section: Simulationmentioning
confidence: 99%
“…This is the stably embedded version (7) of the satellite system model (10), that is, S 3 × R 3 is an invariant manifold of the modified system and is exponentially stable for the modified system; refer to Lemma 1 in Ko et al's paper. 24 Then, we may apply the standard UKF derived in Euclidean space directly to the system model ( 13) and the measurement models given in (11) and (12). Since the satellite system in nature is a continuous-time system, we generate a continuous-time trajectory of the satellite using (10).…”
Section: Simulationmentioning
confidence: 99%
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“…The principal difficulty stems from the unavailability of the traditional global localization sensors, such as the global positioning system (GPS), due to the reduced propagation of radio frequency signals in the underwater domain. To reach a satisfactory navigation accuracy, most of the navigation filters for AUVs exploit Bayesian estimators, such as the Kalman filter (KF) or its variants applied to nonlinear systems, as the extended Kalman filter (EKF) [1] or the unscented Kalman filter (UKF) [2]. As reported in [3], three different categories can be defined to collect the navigation and localization techniques, as the dead reckoning (DR) strategies, the transponder-based strategies, or the geophysical data based strategies.…”
Section: Introductionmentioning
confidence: 99%