2019
DOI: 10.1109/jsen.2019.2935324
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A Novel Design Framework for Tightly Coupled IMU/GNSS Sensor Fusion Using Inverse-Kinematics, Symbolic Engines, and Genetic Algorithms

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Cited by 14 publications
(7 citation statements)
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“…The errors of the accelerometer and gyroscope in inertial navigation (IMU) can be divided into deterministic errors and random errors. Deterministic errors can be obtained through prior calibration, which mainly includes bias errors, scale errors, and axis misalignments [ 21 ]. For random error, it is assumed that the noise obeys Gaussian distribution, including Gaussian white noise and bias random walk.…”
Section: Core Algorithm Design Of Binocular Vision and Interval Navig...mentioning
confidence: 99%
“…The errors of the accelerometer and gyroscope in inertial navigation (IMU) can be divided into deterministic errors and random errors. Deterministic errors can be obtained through prior calibration, which mainly includes bias errors, scale errors, and axis misalignments [ 21 ]. For random error, it is assumed that the noise obeys Gaussian distribution, including Gaussian white noise and bias random walk.…”
Section: Core Algorithm Design Of Binocular Vision and Interval Navig...mentioning
confidence: 99%
“…To address this challenge, S. S Kourabbaslou [ 22 ] presents a flexible design framework utilizing symbolic engines to represent and linearize system and measurement models. A robust fixed−lag smoothing approach is proposed in case there is a mismatch between the nominal model and the actual model [ 23 , 24 ].…”
Section: Introductionmentioning
confidence: 99%
“…The integrated navigation system based on inertial navigation system (INS) and global navigation satellite system (GNSS) is one of the most valuable navigation modes, especially the tightly coupled navigation utilizing INS outputs and GNSS raw measurements. [1][2][3][4][5][6] In the navigation mode, even when the currently visible satellites are not enough to perform GNSS calculation alone, the limited GNSS measurement data and INS outputs can still be effectively used to obtain reliable navigation information through state estimation. However, unlike INS/GNSS loosely coupled navigation, due to the nonlinear nature of the GNSS raw measurements, the tightly coupled navigation incorporates nonlinearity in the system, enabling the classical Kalman filter (KF) unsuitable.…”
Section: Introductionmentioning
confidence: 99%
“…The integrated navigation system based on inertial navigation system (INS) and global navigation satellite system (GNSS) is one of the most valuable navigation modes, especially the tightly coupled navigation utilizing INS outputs and GNSS raw measurements 1–6 . In the navigation mode, even when the currently visible satellites are not enough to perform GNSS calculation alone, the limited GNSS measurement data and INS outputs can still be effectively used to obtain reliable navigation information through state estimation.…”
Section: Introductionmentioning
confidence: 99%