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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Main Authors: Junbo Tie, Juliang Cao, Lubing Chang, Shaokun Cai, Meiping Wu, Junxiang Lian
Format: Article
Language:English
Published: MDPI AG 2018-03-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/18/3/883
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spelling 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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