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Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite
A low Earth orbiter (LEO)-based navigation signal augmentation system is considered as a complementary of current global navigation satellite systems (GNSS), which can accelerate precise positioning convergence, strengthen the signal power, and improve signal quality. Wuhan University is dedicated t...
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/PMC6263488/ https://www.ncbi.nlm.nih.gov/pubmed/30441781 http://dx.doi.org/10.3390/s18113919 |
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author | Wang, Lei Chen, Ruizhi Li, Deren Zhang, Guo Shen, Xin Yu, Baoguo Wu, Cailun Xie, Song Zhang, Peng Li, Ming Pan, Yuanjin |
author_facet | Wang, Lei Chen, Ruizhi Li, Deren Zhang, Guo Shen, Xin Yu, Baoguo Wu, Cailun Xie, Song Zhang, Peng Li, Ming Pan, Yuanjin |
author_sort | Wang, Lei |
collection | PubMed |
description | A low Earth orbiter (LEO)-based navigation signal augmentation system is considered as a complementary of current global navigation satellite systems (GNSS), which can accelerate precise positioning convergence, strengthen the signal power, and improve signal quality. Wuhan University is dedicated to LEO-based navigation signal augmentation research and launched one scientific experimental satellite named Luojia-1A. The satellite is capable of broadcasting dual-frequency band ranging signals over China. The initial performance of the Luojia-1A satellite navigation augmentation system is assessed in this study. The ground tests indicate that the phase noise of the oscillator is sufficiently low to support the intended applications. The field ranging tests achieve 2.6 m and 0.013 m ranging precision for the pseudorange and carrier phase measurements, respectively. The in-orbit test shows that the internal precision of the ephemeris is approximate 0.1 m and the clock stability is 3 × 10(−10). The pseudorange and carrier phase measurement noise evaluated from the geometry-free combination is about 3.3 m and 1.8 cm. Overall, the Luojia-1A navigation augmentation system is capable of providing useable LEO navigation augmentation signals with the empirical user equivalent ranging error (UERE) no worse than 3.6 m, which can be integrated with existing GNSS to improve the real-time navigation performance. |
format | Online Article Text |
id | pubmed-6263488 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2018 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-62634882018-12-12 Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite Wang, Lei Chen, Ruizhi Li, Deren Zhang, Guo Shen, Xin Yu, Baoguo Wu, Cailun Xie, Song Zhang, Peng Li, Ming Pan, Yuanjin Sensors (Basel) Article A low Earth orbiter (LEO)-based navigation signal augmentation system is considered as a complementary of current global navigation satellite systems (GNSS), which can accelerate precise positioning convergence, strengthen the signal power, and improve signal quality. Wuhan University is dedicated to LEO-based navigation signal augmentation research and launched one scientific experimental satellite named Luojia-1A. The satellite is capable of broadcasting dual-frequency band ranging signals over China. The initial performance of the Luojia-1A satellite navigation augmentation system is assessed in this study. The ground tests indicate that the phase noise of the oscillator is sufficiently low to support the intended applications. The field ranging tests achieve 2.6 m and 0.013 m ranging precision for the pseudorange and carrier phase measurements, respectively. The in-orbit test shows that the internal precision of the ephemeris is approximate 0.1 m and the clock stability is 3 × 10(−10). The pseudorange and carrier phase measurement noise evaluated from the geometry-free combination is about 3.3 m and 1.8 cm. Overall, the Luojia-1A navigation augmentation system is capable of providing useable LEO navigation augmentation signals with the empirical user equivalent ranging error (UERE) no worse than 3.6 m, which can be integrated with existing GNSS to improve the real-time navigation performance. MDPI 2018-11-14 /pmc/articles/PMC6263488/ /pubmed/30441781 http://dx.doi.org/10.3390/s18113919 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 Wang, Lei Chen, Ruizhi Li, Deren Zhang, Guo Shen, Xin Yu, Baoguo Wu, Cailun Xie, Song Zhang, Peng Li, Ming Pan, Yuanjin Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite |
title | Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite |
title_full | Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite |
title_fullStr | Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite |
title_full_unstemmed | Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite |
title_short | Initial Assessment of the LEO Based Navigation Signal Augmentation System from Luojia-1A Satellite |
title_sort | initial assessment of the leo based navigation signal augmentation system from luojia-1a satellite |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6263488/ https://www.ncbi.nlm.nih.gov/pubmed/30441781 http://dx.doi.org/10.3390/s18113919 |
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