A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation
Compensation of gravity disturbance can improve the precision of inertial navigation, but the effect of compensation will decrease due to the accelerometer bias, and estimation of the accelerometer bias is a crucial issue in gravity disturbance compensation. This paper first investigates the effect...
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doaj-85476bceced84247a746fa51c9db704d2020-11-24T22:00:42ZengMDPI AGSensors1424-82202018-03-0118388310.3390/s18030883s18030883A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance CompensationJunbo Tie0Juliang Cao1Lubing Chang2Shaokun Cai3Meiping Wu4Junxiang Lian5College of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, ChinaCollege of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, ChinaDepartment of Navigation Engineering, Naval University of Engineering, Wuhan 430000, ChinaCollege of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, ChinaCollege of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, ChinaCollege of Mechatronics and Automation, National University of Defense Technology, Changsha 410073, ChinaCompensation of gravity disturbance can improve the precision of inertial navigation, but the effect of compensation will decrease due to the accelerometer bias, and estimation of the accelerometer bias is a crucial issue in gravity disturbance compensation. This paper first investigates the effect of accelerometer bias on gravity disturbance compensation, and the situation in which the accelerometer bias should be estimated is established. The accelerometer bias is estimated from the gravity vector measurement, and a model of measurement noise in gravity vector measurement is built. Based on this model, accelerometer bias is separated from the gravity vector measurement error by the method of least squares. Horizontal gravity disturbances are calculated through EGM2008 spherical harmonic model to build the simulation scene, and the simulation results indicate that precise estimations of the accelerometer bias can be obtained with the proposed method.http://www.mdpi.com/1424-8220/18/3/883inertial navigationgravity disturbance compensationestimationaccelerometer bias |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Junbo Tie Juliang Cao Lubing Chang Shaokun Cai Meiping Wu Junxiang Lian |
spellingShingle |
Junbo Tie Juliang Cao Lubing Chang Shaokun Cai Meiping Wu Junxiang Lian A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation Sensors inertial navigation gravity disturbance compensation estimation accelerometer bias |
author_facet |
Junbo Tie Juliang Cao Lubing Chang Shaokun Cai Meiping Wu Junxiang Lian |
author_sort |
Junbo Tie |
title |
A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation |
title_short |
A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation |
title_full |
A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation |
title_fullStr |
A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation |
title_full_unstemmed |
A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation |
title_sort |
model of gravity vector measurement noise for estimating accelerometer bias in gravity disturbance compensation |
publisher |
MDPI AG |
series |
Sensors |
issn |
1424-8220 |
publishDate |
2018-03-01 |
description |
Compensation of gravity disturbance can improve the precision of inertial navigation, but the effect of compensation will decrease due to the accelerometer bias, and estimation of the accelerometer bias is a crucial issue in gravity disturbance compensation. This paper first investigates the effect of accelerometer bias on gravity disturbance compensation, and the situation in which the accelerometer bias should be estimated is established. The accelerometer bias is estimated from the gravity vector measurement, and a model of measurement noise in gravity vector measurement is built. Based on this model, accelerometer bias is separated from the gravity vector measurement error by the method of least squares. Horizontal gravity disturbances are calculated through EGM2008 spherical harmonic model to build the simulation scene, and the simulation results indicate that precise estimations of the accelerometer bias can be obtained with the proposed method. |
topic |
inertial navigation gravity disturbance compensation estimation accelerometer bias |
url |
http://www.mdpi.com/1424-8220/18/3/883 |
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