A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range

The micro-electro-mechanical inertial measurement unit (MEMS-IMU) has gradually become a research hotspot in the field of mid-low navigation, because of its advantages of low cost, small size, light weight, and low power consumption (CSWap). However, the performance of MEMS-IMUs can be severely degr...

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Main Authors: Haotian Yang, Bin Zhou, Lixin Wang, Haifeng Xing, Rong Zhang
Format: Article
Language:English
Published: MDPI AG 2018-09-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/18/9/3004
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spelling doaj-a943fb9f301f4f6094a4b05fb76a24852020-11-25T02:16:54ZengMDPI AGSensors1424-82202018-09-01189300410.3390/s18093004s18093004A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature RangeHaotian Yang0Bin Zhou1Lixin Wang2Haifeng Xing3Rong Zhang4Department of Precision Instrument, Tsinghua University, Beijng 100084, ChinaDepartment of Precision Instrument, Tsinghua University, Beijng 100084, ChinaXi’an Research Institute of High Technology, Xi’an 710025, ChinaDepartment of Precision Instrument, Tsinghua University, Beijng 100084, ChinaDepartment of Precision Instrument, Tsinghua University, Beijng 100084, ChinaThe micro-electro-mechanical inertial measurement unit (MEMS-IMU) has gradually become a research hotspot in the field of mid-low navigation, because of its advantages of low cost, small size, light weight, and low power consumption (CSWap). However, the performance of MEMS-IMUs can be severely degraded when subjected to temperature changes, especially gyroscopes. In order to make full use of the navigation accuracy, this paper proposes an optimized error calibration method for a tri-axial MEMS gyroscope across a full temperature range. First of all, a calibration error model is established which includes package misalignment error, sensor-to-sensor non-orthogonality error, scale factor, and bias. Then, a simple three-position positive/reversed test is undertaken by carrying out a single-axis temperature-controlled turntable at different reference temperature points. Lastly, the error compensation vector is obtained using the least squares method to establish an error matrix. It is worth mentioning that the error compensation vector at a known temperature point can be calculated through Lagrange interpolation; then, the outputs of the tri-axial MEMS gyroscope can be well compensated, eliminating the need for a recalibration step. The experimental results confirm the effectiveness of the proposed method, which is feasible and operational in engineering applications, and has a certain reference value.http://www.mdpi.com/1424-8220/18/9/3004thermal calibrationerror compensationtri-axial MEMS gyroscopeLagrange interpolation
collection DOAJ
language English
format Article
sources DOAJ
author Haotian Yang
Bin Zhou
Lixin Wang
Haifeng Xing
Rong Zhang
spellingShingle Haotian Yang
Bin Zhou
Lixin Wang
Haifeng Xing
Rong Zhang
A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range
Sensors
thermal calibration
error compensation
tri-axial MEMS gyroscope
Lagrange interpolation
author_facet Haotian Yang
Bin Zhou
Lixin Wang
Haifeng Xing
Rong Zhang
author_sort Haotian Yang
title A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range
title_short A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range
title_full A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range
title_fullStr A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range
title_full_unstemmed A Novel Tri-Axial MEMS Gyroscope Calibration Method over a Full Temperature Range
title_sort novel tri-axial mems gyroscope calibration method over a full temperature range
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2018-09-01
description The micro-electro-mechanical inertial measurement unit (MEMS-IMU) has gradually become a research hotspot in the field of mid-low navigation, because of its advantages of low cost, small size, light weight, and low power consumption (CSWap). However, the performance of MEMS-IMUs can be severely degraded when subjected to temperature changes, especially gyroscopes. In order to make full use of the navigation accuracy, this paper proposes an optimized error calibration method for a tri-axial MEMS gyroscope across a full temperature range. First of all, a calibration error model is established which includes package misalignment error, sensor-to-sensor non-orthogonality error, scale factor, and bias. Then, a simple three-position positive/reversed test is undertaken by carrying out a single-axis temperature-controlled turntable at different reference temperature points. Lastly, the error compensation vector is obtained using the least squares method to establish an error matrix. It is worth mentioning that the error compensation vector at a known temperature point can be calculated through Lagrange interpolation; then, the outputs of the tri-axial MEMS gyroscope can be well compensated, eliminating the need for a recalibration step. The experimental results confirm the effectiveness of the proposed method, which is feasible and operational in engineering applications, and has a certain reference value.
topic thermal calibration
error compensation
tri-axial MEMS gyroscope
Lagrange interpolation
url http://www.mdpi.com/1424-8220/18/9/3004
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