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A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System
Traditional attitude determination using global navigation satellite system (GNSS) carrier phases is mostly applied on geodetic-grade receivers with sufficient baseline length. However, for some special applications such as mobile communication base station smart antenna attitude determination, only...
Autores principales: | , , , , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2018
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6069076/ https://www.ncbi.nlm.nih.gov/pubmed/29966398 http://dx.doi.org/10.3390/s18072114 |
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author | Li, Wenyi Fan, Peirong Cui, Xiaowei Zhao, Sihao Ma, Tianyi Lu, Mingquan |
author_facet | Li, Wenyi Fan, Peirong Cui, Xiaowei Zhao, Sihao Ma, Tianyi Lu, Mingquan |
author_sort | Li, Wenyi |
collection | PubMed |
description | Traditional attitude determination using global navigation satellite system (GNSS) carrier phases is mostly applied on geodetic-grade receivers with sufficient baseline length. However, for some special applications such as mobile communication base station smart antenna attitude determination, only low-cost receivers with ultra-short baselines can be employed, and the environments are more challenging. When solving the ambiguity resolution (AR) problem with low-cost receivers, it is hard for the traditional methods in ambiguity domain to estimate float ambiguities accurately due to the large code pseudorange noises; thus, such systems fail to determine the correct ambiguities. Aiming at improving the AR success rate for ultra-short baselines attitude determination with low-cost receivers, we provide an objective function named Mean Square Residual (MSR) based on the geometrical relationship among the position spherical search space, the fractional carrier phases, and the possible ambiguities. The method can be calculated without code pseudoranges, and thus, can provide a higher AR success rate when using low-cost receivers. The corresponding analysis and acceptance test method are discussed in this contribution, and further, as an extension for more complicated urban dynamic applications, a GNSS/Inertial Navigation System (INS) integrated system is introduced. Several experiments have been conducted to verify performance. |
format | Online Article Text |
id | pubmed-6069076 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2018 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-60690762018-08-07 A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System Li, Wenyi Fan, Peirong Cui, Xiaowei Zhao, Sihao Ma, Tianyi Lu, Mingquan Sensors (Basel) Article Traditional attitude determination using global navigation satellite system (GNSS) carrier phases is mostly applied on geodetic-grade receivers with sufficient baseline length. However, for some special applications such as mobile communication base station smart antenna attitude determination, only low-cost receivers with ultra-short baselines can be employed, and the environments are more challenging. When solving the ambiguity resolution (AR) problem with low-cost receivers, it is hard for the traditional methods in ambiguity domain to estimate float ambiguities accurately due to the large code pseudorange noises; thus, such systems fail to determine the correct ambiguities. Aiming at improving the AR success rate for ultra-short baselines attitude determination with low-cost receivers, we provide an objective function named Mean Square Residual (MSR) based on the geometrical relationship among the position spherical search space, the fractional carrier phases, and the possible ambiguities. The method can be calculated without code pseudoranges, and thus, can provide a higher AR success rate when using low-cost receivers. The corresponding analysis and acceptance test method are discussed in this contribution, and further, as an extension for more complicated urban dynamic applications, a GNSS/Inertial Navigation System (INS) integrated system is introduced. Several experiments have been conducted to verify performance. MDPI 2018-07-01 /pmc/articles/PMC6069076/ /pubmed/29966398 http://dx.doi.org/10.3390/s18072114 Text en © 2018 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 (CC BY) license (http://creativecommons.org/licenses/by/4.0/). |
spellingShingle | Article Li, Wenyi Fan, Peirong Cui, Xiaowei Zhao, Sihao Ma, Tianyi Lu, Mingquan A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System |
title | A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System |
title_full | A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System |
title_fullStr | A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System |
title_full_unstemmed | A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System |
title_short | A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System |
title_sort | low-cost ins-integratable gnss ultra-short baseline attitude determination system |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6069076/ https://www.ncbi.nlm.nih.gov/pubmed/29966398 http://dx.doi.org/10.3390/s18072114 |
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