A magnetometer error compensation method based on external attitude assistance

Abstract The magnetic field serves as a crucial source of navigational information, typically measured by magnetometers in practical applications. However, magnetometers are inherently unstable instruments that require error compensation before formal use. Drawing inspiration from the system-level calibration approach of gyroscopes, this paper proposes a system-level error compensation method for magnetometers. By leveraging high-precision external attitude information, this method effectively measures the installation errors between the magnetometer’s three axes and the carrier coordinate system. It simultaneously calibrates sensitivity errors, non-orthogonality errors, and bias errors. The problem is formulated as a state estimation task and solved using an extended Kalman filter. Based on the estimation results, the compensation of the magnetometer was completed. The improvement of the magnetometer modulus and heading angle before and after compensation demonstrated the superior performance of the proposed method.

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Publication Details

Journal
Journal of Physics Conference Series
Published
2025-04-01
DOI
https://doi.org/10.1088/1742-6596/2996/1/012019
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
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article

A magnetometer error compensation method based on external attitude assistance

Di Yang, Shenglong Li, Yueyang Ben, Zhengfeng Chen et al.
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Journal of Physics Conference Series
Inertial Sensor and Navigation
article

A magnetometer error compensation method based on external attitude assistance

Di Yang, Shenglong Li, Yueyang Ben, Zhengfeng Chen, H. T. Peng
article en

Abstract

Abstract The magnetic field serves as a crucial source of navigational information, typically measured by magnetometers in practical applications. However, magnetometers are inherently unstable instruments that require error compensation before formal use. Drawing inspiration from the system-level calibration approach of gyroscopes, this paper proposes a system-level error compensation method for magnetometers. By leveraging high-precision external attitude information, this method effectively measures the installation errors between the magnetometer’s three axes and the carrier coordinate system. It simultaneously calibrates sensitivity errors, non-orthogonality errors, and bias errors. The problem is formulated as a state estimation task and solved using an extended Kalman filter. Based on the estimation results, the compensation of the magnetometer was completed. The improvement of the magnetometer modulus and heading angle before and after compensation demonstrated the superior performance of the proposed method.

Journal of Physics Conference SeriesVol. 2996(1)
Harbin Engineering University (CN), Huazhong Agricultural University (CN), Shanghai Power Equipment Research Institute (CN), Wuhan National Laboratory for Optoelectronics (CN), Huazhong University of Science and Technology (CN)
Openalex Percentile: Top 90%
Inertial Sensor and Navigation
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A magnetometer error compensation method based on external attitude assistance — Di Yang, Shenglong Li, et al. · Journal of Physics Conference Series (2025) | TGRS Research Map | TGRS