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Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing
Direct geo-referencing is an efficient methodology for the fast acquisition of 3D spatial data. It requires the fusion of spatial data acquisition sensors with navigation sensors, such as Global Navigation Satellite System (GNSS) receivers. In this contribution, we consider an integrated GNSS naviga...
Autores principales: | , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2014
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4168486/ https://www.ncbi.nlm.nih.gov/pubmed/25036330 http://dx.doi.org/10.3390/s140712715 |
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author | Nadarajah, Nandakumaran Paffenholz, Jens-André Teunissen, Peter J. G. |
author_facet | Nadarajah, Nandakumaran Paffenholz, Jens-André Teunissen, Peter J. G. |
author_sort | Nadarajah, Nandakumaran |
collection | PubMed |
description | Direct geo-referencing is an efficient methodology for the fast acquisition of 3D spatial data. It requires the fusion of spatial data acquisition sensors with navigation sensors, such as Global Navigation Satellite System (GNSS) receivers. In this contribution, we consider an integrated GNSS navigation system to provide estimates of the position and attitude (orientation) of a 3D laser scanner. The proposed multi-sensor system (MSS) consists of multiple GNSS antennas rigidly mounted on the frame of a rotating laser scanner and a reference GNSS station with known coordinates. Precise GNSS navigation requires the resolution of the carrier phase ambiguities. The proposed method uses the multivariate constrained integer least-squares (MC-LAMBDA) method for the estimation of rotating frame ambiguities and attitude angles. MC-LAMBDA makes use of the known antenna geometry to strengthen the underlying attitude model and, hence, to enhance the reliability of rotating frame ambiguity resolution and attitude determination. The reliable estimation of rotating frame ambiguities is consequently utilized to enhance the relative positioning of the rotating frame with respect to the reference station. This integrated (array-aided) method improves ambiguity resolution, as well as positioning accuracy between the rotating frame and the reference station. Numerical analyses of GNSS data from a real-data campaign confirm the improved performance of the proposed method over the existing method. In particular, the integrated method yields reliable ambiguity resolution and reduces position standard deviation by a factor of about 0.8, matching the theoretical gain of [Formula: see text] for two antennas on the rotating frame and a single antenna at the reference station. |
format | Online Article Text |
id | pubmed-4168486 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2014 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-41684862014-09-19 Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing Nadarajah, Nandakumaran Paffenholz, Jens-André Teunissen, Peter J. G. Sensors (Basel) Article Direct geo-referencing is an efficient methodology for the fast acquisition of 3D spatial data. It requires the fusion of spatial data acquisition sensors with navigation sensors, such as Global Navigation Satellite System (GNSS) receivers. In this contribution, we consider an integrated GNSS navigation system to provide estimates of the position and attitude (orientation) of a 3D laser scanner. The proposed multi-sensor system (MSS) consists of multiple GNSS antennas rigidly mounted on the frame of a rotating laser scanner and a reference GNSS station with known coordinates. Precise GNSS navigation requires the resolution of the carrier phase ambiguities. The proposed method uses the multivariate constrained integer least-squares (MC-LAMBDA) method for the estimation of rotating frame ambiguities and attitude angles. MC-LAMBDA makes use of the known antenna geometry to strengthen the underlying attitude model and, hence, to enhance the reliability of rotating frame ambiguity resolution and attitude determination. The reliable estimation of rotating frame ambiguities is consequently utilized to enhance the relative positioning of the rotating frame with respect to the reference station. This integrated (array-aided) method improves ambiguity resolution, as well as positioning accuracy between the rotating frame and the reference station. Numerical analyses of GNSS data from a real-data campaign confirm the improved performance of the proposed method over the existing method. In particular, the integrated method yields reliable ambiguity resolution and reduces position standard deviation by a factor of about 0.8, matching the theoretical gain of [Formula: see text] for two antennas on the rotating frame and a single antenna at the reference station. MDPI 2014-07-17 /pmc/articles/PMC4168486/ /pubmed/25036330 http://dx.doi.org/10.3390/s140712715 Text en © 2014 by the authors; licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution license (http://creativecommons.org/licenses/by/3.0/). |
spellingShingle | Article Nadarajah, Nandakumaran Paffenholz, Jens-André Teunissen, Peter J. G. Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing |
title | Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing |
title_full | Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing |
title_fullStr | Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing |
title_full_unstemmed | Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing |
title_short | Integrated GNSS Attitude Determination and Positioning for Direct Geo-Referencing |
title_sort | integrated gnss attitude determination and positioning for direct geo-referencing |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4168486/ https://www.ncbi.nlm.nih.gov/pubmed/25036330 http://dx.doi.org/10.3390/s140712715 |
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