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...
Main Authors: | , , , , |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2018-09-01
|
Series: | Sensors |
Subjects: | |
Online Access: | http://www.mdpi.com/1424-8220/18/9/3004 |
id |
doaj-a943fb9f301f4f6094a4b05fb76a2485 |
---|---|
record_format |
Article |
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 |
work_keys_str_mv |
AT haotianyang anoveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT binzhou anoveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT lixinwang anoveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT haifengxing anoveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT rongzhang anoveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT haotianyang noveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT binzhou noveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT lixinwang noveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT haifengxing noveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange AT rongzhang noveltriaxialmemsgyroscopecalibrationmethodoverafulltemperaturerange |
_version_ |
1724888241504518144 |