An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System

In order to suppress the error caused by the drift of the gyroscope and further improve accuracy of the navigation system, combined with the method of measuring attitude by using the three-axis components of geomagnetic, a new scheme, consisting of Strapdown Inertial Navigation System (SINS)/Geomagn...

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Main Authors: Feng Xie, Minzhou Dong
Format: Article
Language:English
Published: Hindawi Limited 2021-01-01
Series:Journal of Sensors
Online Access:http://dx.doi.org/10.1155/2021/5525481
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spelling doaj-0e1194f9a79f4fe9b8fc293838c6f4312021-05-03T00:01:25ZengHindawi LimitedJournal of Sensors1687-72682021-01-01202110.1155/2021/5525481An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation SystemFeng Xie0Minzhou Dong1School of AstronauticsSchool of AstronauticsIn order to suppress the error caused by the drift of the gyroscope and further improve accuracy of the navigation system, combined with the method of measuring attitude by using the three-axis components of geomagnetic, a new scheme, consisting of Strapdown Inertial Navigation System (SINS)/Geomagnetic Navigation System (GNS), is designed for autonomous integrated navigation systems. The principle of this SINS/GNS integrated navigation system is explored, and the corresponding mathematical model is established. Furthermore, a Marginalized Particle Filter (MPF) is designed for this autonomous integrated navigation system. The simulation experiments are conducted, and the results show that the improved SINS/GNS autonomous integrated navigation system possesses strong robustness and high reliability, thus providing a new reference solution for autonomous navigation technology.http://dx.doi.org/10.1155/2021/5525481
collection DOAJ
language English
format Article
sources DOAJ
author Feng Xie
Minzhou Dong
spellingShingle Feng Xie
Minzhou Dong
An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System
Journal of Sensors
author_facet Feng Xie
Minzhou Dong
author_sort Feng Xie
title An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System
title_short An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System
title_full An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System
title_fullStr An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System
title_full_unstemmed An Improved Attitude Compensation Algorithm for SINS/GNS Integrated Navigation System
title_sort improved attitude compensation algorithm for sins/gns integrated navigation system
publisher Hindawi Limited
series Journal of Sensors
issn 1687-7268
publishDate 2021-01-01
description In order to suppress the error caused by the drift of the gyroscope and further improve accuracy of the navigation system, combined with the method of measuring attitude by using the three-axis components of geomagnetic, a new scheme, consisting of Strapdown Inertial Navigation System (SINS)/Geomagnetic Navigation System (GNS), is designed for autonomous integrated navigation systems. The principle of this SINS/GNS integrated navigation system is explored, and the corresponding mathematical model is established. Furthermore, a Marginalized Particle Filter (MPF) is designed for this autonomous integrated navigation system. The simulation experiments are conducted, and the results show that the improved SINS/GNS autonomous integrated navigation system possesses strong robustness and high reliability, thus providing a new reference solution for autonomous navigation technology.
url http://dx.doi.org/10.1155/2021/5525481
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