An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS

This paper investigates the attitude estimation errors caused by the deflections of vertical (DOV) in the case of a rotational inertial navigation system (INS) integrated with a global satellite navigation system (GNSS). It has been proved theoretically and experimentally that the DOV can introduce...

Full description

Bibliographic Details
Main Authors: Hao Xiong, Dongkai Dai, Yingwei Zhao, Xingshu Wang, Jiaxing Zheng, Dejun Zhan
Format: Article
Language:English
Published: MDPI AG 2019-04-01
Series:Sensors
Subjects:
Online Access:https://www.mdpi.com/1424-8220/19/7/1721
id doaj-bba65c1313ac4cdca87dca3caf5d567f
record_format Article
spelling doaj-bba65c1313ac4cdca87dca3caf5d567f2020-11-25T01:06:05ZengMDPI AGSensors1424-82202019-04-01197172110.3390/s19071721s19071721An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSSHao Xiong0Dongkai Dai1Yingwei Zhao2Xingshu Wang3Jiaxing Zheng4Dejun Zhan5College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaCollege of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaCollege of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaCollege of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaCollege of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaCollege of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaThis paper investigates the attitude estimation errors caused by the deflections of vertical (DOV) in the case of a rotational inertial navigation system (INS) integrated with a global satellite navigation system (GNSS). It has been proved theoretically and experimentally that the DOV can introduce a tilt error to the INS/GNSS integration, whereas less attention has been given to its effect to the heading estimation. In fact, due to the intercoupling characteristic of attitude errors, the heading estimation of an INS/GNSS integrated navigation system can also be affected. In this paper, first, the attitude estimation errors caused by DOV were deduced based on the INS’s error propagation functions. Then, the corresponding simulations were conducted and the results were well consistent with the theoretical analysis. Finally, a real shipborne marine test was organized with the aimed to verify the effect of DOV on attitude estimation in the rotational INS/GNSS integration, whereas the global gravity model was used for DOV compensation. The results with DOV compensation were compared with the corresponding results where the compensation was not used and showed that the heading estimation errors caused by DOV could exceed 20 arcsecs, which must be considered in high-precision application cases.https://www.mdpi.com/1424-8220/19/7/1721deflections of verticalattitude estimation errorsrotational INSINS/GNSS integrationglobal gravity model
collection DOAJ
language English
format Article
sources DOAJ
author Hao Xiong
Dongkai Dai
Yingwei Zhao
Xingshu Wang
Jiaxing Zheng
Dejun Zhan
spellingShingle Hao Xiong
Dongkai Dai
Yingwei Zhao
Xingshu Wang
Jiaxing Zheng
Dejun Zhan
An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS
Sensors
deflections of vertical
attitude estimation errors
rotational INS
INS/GNSS integration
global gravity model
author_facet Hao Xiong
Dongkai Dai
Yingwei Zhao
Xingshu Wang
Jiaxing Zheng
Dejun Zhan
author_sort Hao Xiong
title An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS
title_short An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS
title_full An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS
title_fullStr An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS
title_full_unstemmed An Analysis of the Attitude Estimation Errors Caused by the Deflections of Vertical in the Integration of Rotational INS and GNSS
title_sort analysis of the attitude estimation errors caused by the deflections of vertical in the integration of rotational ins and gnss
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2019-04-01
description This paper investigates the attitude estimation errors caused by the deflections of vertical (DOV) in the case of a rotational inertial navigation system (INS) integrated with a global satellite navigation system (GNSS). It has been proved theoretically and experimentally that the DOV can introduce a tilt error to the INS/GNSS integration, whereas less attention has been given to its effect to the heading estimation. In fact, due to the intercoupling characteristic of attitude errors, the heading estimation of an INS/GNSS integrated navigation system can also be affected. In this paper, first, the attitude estimation errors caused by DOV were deduced based on the INS’s error propagation functions. Then, the corresponding simulations were conducted and the results were well consistent with the theoretical analysis. Finally, a real shipborne marine test was organized with the aimed to verify the effect of DOV on attitude estimation in the rotational INS/GNSS integration, whereas the global gravity model was used for DOV compensation. The results with DOV compensation were compared with the corresponding results where the compensation was not used and showed that the heading estimation errors caused by DOV could exceed 20 arcsecs, which must be considered in high-precision application cases.
topic deflections of vertical
attitude estimation errors
rotational INS
INS/GNSS integration
global gravity model
url https://www.mdpi.com/1424-8220/19/7/1721
work_keys_str_mv AT haoxiong ananalysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT dongkaidai ananalysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT yingweizhao ananalysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT xingshuwang ananalysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT jiaxingzheng ananalysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT dejunzhan ananalysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT haoxiong analysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT dongkaidai analysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT yingweizhao analysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT xingshuwang analysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT jiaxingzheng analysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
AT dejunzhan analysisoftheattitudeestimationerrorscausedbythedeflectionsofverticalintheintegrationofrotationalinsandgnss
_version_ 1725191585919926272