Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System

In order to improve the precision of Strapdown Inertial Navigation System (SINS) and reduce the complexity of the traditional calibration method, a novel calibration and compensation scheme is proposed. An optimization calibration method with four-direction rotations is designed to calculate all err...

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Main Authors: Jianli Li, Yanhai Ma, Chen Xiyuan
Format: Article
Language:English
Published: Wiley 2013-01-01
Series:Abstract and Applied Analysis
Online Access:http://dx.doi.org/10.1155/2013/359675
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author Jianli Li
Yanhai Ma
Chen Xiyuan
author_facet Jianli Li
Yanhai Ma
Chen Xiyuan
author_sort Jianli Li
collection DOAJ
description In order to improve the precision of Strapdown Inertial Navigation System (SINS) and reduce the complexity of the traditional calibration method, a novel calibration and compensation scheme is proposed. An optimization calibration method with four-direction rotations is designed to calculate all error coefficients of Ring Laser Gyroscope (RLG) SINS in a series of constant temperatures. According to the actual working environment, the temperature errors of RLG SINS are compensated by a nonlinear interpolation compensation algorithm. The experimental results show that the inertial navigation errors of the proposed method are reduced.
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institution Kabale University
issn 1085-3375
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language English
publishDate 2013-01-01
publisher Wiley
record_format Article
series Abstract and Applied Analysis
spelling doaj-art-85dc8737fa7f44459d19dbcff407bf5c2025-02-03T01:02:39ZengWileyAbstract and Applied Analysis1085-33751687-04092013-01-01201310.1155/2013/359675359675Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation SystemJianli Li0Yanhai Ma1Chen Xiyuan2Fundamental Science on Novel Inertial Instrument & Navigation System Technology Laboratory, School of Instrumentation Science & Optoelectronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, ChinaFundamental Science on Novel Inertial Instrument & Navigation System Technology Laboratory, School of Instrumentation Science & Optoelectronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, ChinaSchool of Instrumentation Science & Engineering, Southeast University, Nanjing 211100, ChinaIn order to improve the precision of Strapdown Inertial Navigation System (SINS) and reduce the complexity of the traditional calibration method, a novel calibration and compensation scheme is proposed. An optimization calibration method with four-direction rotations is designed to calculate all error coefficients of Ring Laser Gyroscope (RLG) SINS in a series of constant temperatures. According to the actual working environment, the temperature errors of RLG SINS are compensated by a nonlinear interpolation compensation algorithm. The experimental results show that the inertial navigation errors of the proposed method are reduced.http://dx.doi.org/10.1155/2013/359675
spellingShingle Jianli Li
Yanhai Ma
Chen Xiyuan
Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System
Abstract and Applied Analysis
title Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System
title_full Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System
title_fullStr Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System
title_full_unstemmed Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System
title_short Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System
title_sort error modeling calibration and nonlinear interpolation compensation method of ring laser gyroscope inertial navigation system
url http://dx.doi.org/10.1155/2013/359675
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AT chenxiyuan errormodelingcalibrationandnonlinearinterpolationcompensationmethodofringlasergyroscopeinertialnavigationsystem