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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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 |
work_keys_str_mv |
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