High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation

A high-precision image-aided inertial navigation system (INS) is proposed as an alternative to the carrier-phase-based differential Global Navigation Satellite Systems (CDGNSSs) when satellite-based navigation systems are unavailable. In this paper, the image/INS integrated algorithm is modeled by a...

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Main Authors: Weiping Jiang, Li Wang, Xiaoji Niu, Quan Zhang, Hui Zhang, Min Tang, Xiangyun Hu
Format: Article
Language:English
Published: MDPI AG 2014-10-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/14/10/19371
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spelling doaj-17d51ee40f0f437da06aa669908cae0f2020-11-24T21:44:35ZengMDPI AGSensors1424-82202014-10-011410193711940110.3390/s141019371s141019371High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance EvaluationWeiping Jiang0Li Wang1Xiaoji Niu2Quan Zhang3Hui Zhang4Min Tang5Xiangyun Hu6GNSS Research Center, Wuhan University, Wuhan 430079, ChinaGNSS Research Center, Wuhan University, Wuhan 430079, ChinaGNSS Research Center, Wuhan University, Wuhan 430079, ChinaGNSS Research Center, Wuhan University, Wuhan 430079, ChinaGNSS Research Center, Wuhan University, Wuhan 430079, ChinaSchool of Remote Sensing and Information Engineering, Wuhan University, Wuhan 430079, ChinaSchool of Remote Sensing and Information Engineering, Wuhan University, Wuhan 430079, ChinaA high-precision image-aided inertial navigation system (INS) is proposed as an alternative to the carrier-phase-based differential Global Navigation Satellite Systems (CDGNSSs) when satellite-based navigation systems are unavailable. In this paper, the image/INS integrated algorithm is modeled by a tightly-coupled iterative extended Kalman filter (IEKF). Tightly-coupled integration ensures that the integrated system is reliable, even if few known feature points (i.e., less than three) are observed in the images. A new global observability analysis of this tightly-coupled integration is presented to guarantee that the system is observable under the necessary conditions. The analysis conclusions were verified by simulations and field tests. The field tests also indicate that high-precision position (centimeter-level) and attitude (half-degree-level)-integrated solutions can be achieved in a global reference.http://www.mdpi.com/1424-8220/14/10/19371image-aided inertial navigationtightly coupledobservability analysishigh precision
collection DOAJ
language English
format Article
sources DOAJ
author Weiping Jiang
Li Wang
Xiaoji Niu
Quan Zhang
Hui Zhang
Min Tang
Xiangyun Hu
spellingShingle Weiping Jiang
Li Wang
Xiaoji Niu
Quan Zhang
Hui Zhang
Min Tang
Xiangyun Hu
High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation
Sensors
image-aided inertial navigation
tightly coupled
observability analysis
high precision
author_facet Weiping Jiang
Li Wang
Xiaoji Niu
Quan Zhang
Hui Zhang
Min Tang
Xiangyun Hu
author_sort Weiping Jiang
title High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation
title_short High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation
title_full High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation
title_fullStr High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation
title_full_unstemmed High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation
title_sort high-precision image aided inertial navigation with known features: observability analysis and performance evaluation
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2014-10-01
description A high-precision image-aided inertial navigation system (INS) is proposed as an alternative to the carrier-phase-based differential Global Navigation Satellite Systems (CDGNSSs) when satellite-based navigation systems are unavailable. In this paper, the image/INS integrated algorithm is modeled by a tightly-coupled iterative extended Kalman filter (IEKF). Tightly-coupled integration ensures that the integrated system is reliable, even if few known feature points (i.e., less than three) are observed in the images. A new global observability analysis of this tightly-coupled integration is presented to guarantee that the system is observable under the necessary conditions. The analysis conclusions were verified by simulations and field tests. The field tests also indicate that high-precision position (centimeter-level) and attitude (half-degree-level)-integrated solutions can be achieved in a global reference.
topic image-aided inertial navigation
tightly coupled
observability analysis
high precision
url http://www.mdpi.com/1424-8220/14/10/19371
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AT quanzhang highprecisionimageaidedinertialnavigationwithknownfeaturesobservabilityanalysisandperformanceevaluation
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