Bionic polarized light compass and micro-inertial assisted three-axis magnetometer calibration method and device
Through the bionic polarized light compass and micro-inertial sensor-assisted three-axis magnetometer calibration method, the problem of degradation of geomagnetic heading accuracy in the prior art is solved, and the high-precision calibration of the three-axis magnetometer and the overall accuracy of the navigation system are improved.
Patent Information
- Application Number
- CN202510065032.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-15
- Publication Date
- 2025-03-18
- Estimated Expiration
- 2045-01-15
AI Technical Summary
When obtaining the heading information of the carrier, the prior art has the problem of decreasing orientation accuracy, especially when the electromagnetic environment changes, the accuracy of the heading direction of the geomagnetic will significantly decrease, and magnetometer calibration is required, but the commonly used elliptical calibration methods require high maneuverability of large carriers.
The calibration method of bionic polarized light compass and micro-inertial sensor assists the three-axis magnetometer. The heading angle information provided by the bionic polarized light compass assists the micro-inertial sensor to complete the initial alignment. The attitude change and acceleration obtained by the micro-inertial sensor are used to solve the horizontal attitude angle, and the horizontal attitude information is provided for the bionic polarized light compass and three-axis magnetometers. A model of polarized light heading assisted three-axis magnetometer calibration is established, and the compensation coefficient is determined based on the polarized light heading and the measured value of the three-axis magnetometer to realize the calibration of the three-axis magnetometer.
High-precision calibration of three-axis magnetometers is realized, the overall accuracy of the navigation system is improved, the requirements for maneuverability of large platforms are reduced, and the applicability of the combined navigation system is improved in different application environments.
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Figure CN119469209B_ABST
Abstract
Citation Information
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