Improving positioning accuracy of aircraft using SPP method in GLONASS system
The paper presents the results of a study showing the accuracy of the determination of aircraft position coordinates based on the SPP (Single Point Positioning) solution in the GLONASS (Globalnaja Navigatsionnaya Sputnikovaya Sistema) system. For this purpose, the paper develops and implements an a...
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Format: | Article |
Language: | English |
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Faculty of Transport, Warsaw University of Technology
2024-03-01
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Series: | Archives of Transport |
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Online Access: | https://www.archivesoftransport.com/index.php/aot/article/view/391 |
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author | Kamil Krasuski Adam Ciećko Grzegorz Grunwald Małgorzata Kirschenstein |
author_facet | Kamil Krasuski Adam Ciećko Grzegorz Grunwald Małgorzata Kirschenstein |
author_sort | Kamil Krasuski |
collection | DOAJ |
description |
The paper presents the results of a study showing the accuracy of the determination of aircraft position coordinates based on the SPP (Single Point Positioning) solution in the GLONASS (Globalnaja Navigatsionnaya Sputnikovaya Sistema) system. For this purpose, the paper develops and implements an algorithm for the correction of position errors as parameters describing positioning accuracy. The proposed algorithm uses position error values determined for a single GNSS (Global Navigation Satellite Systems) receiver, which are joined in a linear combination to determine the positioning accuracy of the aircraft. The algorithm uses linear coefficients as an inverse function of the number of GLONASS satellites being tracked by the GNSS receiver. The developed algorithm was tested for GLONASS satellite data recorded by Topcon HiPer Pro and Javad Alpha geodetic receivers, during a flight test carried out with a Cessna 172 aircraft around the military airport in Dęblin. Navigation calculations were carried out using RTKLIB v.2.4.3 and Scilab v.6.0.0 software. On the basis of the tests carried out, it was found that for single Topcon HiPer Pro and Javad Alpha receivers, position errors were up to ±11.4 m. However, by using the position error correction algorithm for both receivers, GLONASS positioning accuracy is up to ±3.6 m. The developed algorithm reduces position errors by 60-80% for all BLh (B- Latitude, L- Longitude, h- ellipsoidal height) coordinates. The paper shows the possibility of testing and implementing the proposed mathematical algorithm for the SPP solution in a GPS (Global Positioning System) navigation system. In this case the position errors from the GPS SPP solution range from -0.9 m to +0.9 m for all BLh coordinates. The obtained results showed that application the GLONASS and GPS system in air transport is important. The algorithm used in this work can also be applied to other global GNSS navigation systems (e.g. Galileo (European Navigation Satellite system) or BeiDou (Chinese Navigation Satellite System)) in air transport and navigation.
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first_indexed | 2024-04-25T00:12:58Z |
format | Article |
id | doaj.art-fccbf7e280564786bcfd510c9c013b95 |
institution | Directory Open Access Journal |
issn | 0866-9546 2300-8830 |
language | English |
last_indexed | 2024-04-25T00:12:58Z |
publishDate | 2024-03-01 |
publisher | Faculty of Transport, Warsaw University of Technology |
record_format | Article |
series | Archives of Transport |
spelling | doaj.art-fccbf7e280564786bcfd510c9c013b952024-03-13T10:19:25ZengFaculty of Transport, Warsaw University of TechnologyArchives of Transport0866-95462300-88302024-03-0169110.61089/aot2024.v0s1gv25Improving positioning accuracy of aircraft using SPP method in GLONASS systemKamil Krasuski0https://orcid.org/0000-0001-9821-4450Adam Ciećko1https://orcid.org/0000-0002-3984-0846Grzegorz Grunwald2https://orcid.org/0000-0001-9252-7624Małgorzata Kirschenstein3https://orcid.org/0000-0002-4817-083XInstitute of Navigation, Polish Air Force University, Dęblin, PolandFaculty of Geoengineering, University of Warmia and Mazury in Olsztyn, Olsztyn, PolandFaculty of Geoengineering, University of Warmia and Mazury in Olsztyn, Olsztyn, PolandInstitute of Navigation, Polish Air Force University, Dęblin, Poland The paper presents the results of a study showing the accuracy of the determination of aircraft position coordinates based on the SPP (Single Point Positioning) solution in the GLONASS (Globalnaja Navigatsionnaya Sputnikovaya Sistema) system. For this purpose, the paper develops and implements an algorithm for the correction of position errors as parameters describing positioning accuracy. The proposed algorithm uses position error values determined for a single GNSS (Global Navigation Satellite Systems) receiver, which are joined in a linear combination to determine the positioning accuracy of the aircraft. The algorithm uses linear coefficients as an inverse function of the number of GLONASS satellites being tracked by the GNSS receiver. The developed algorithm was tested for GLONASS satellite data recorded by Topcon HiPer Pro and Javad Alpha geodetic receivers, during a flight test carried out with a Cessna 172 aircraft around the military airport in Dęblin. Navigation calculations were carried out using RTKLIB v.2.4.3 and Scilab v.6.0.0 software. On the basis of the tests carried out, it was found that for single Topcon HiPer Pro and Javad Alpha receivers, position errors were up to ±11.4 m. However, by using the position error correction algorithm for both receivers, GLONASS positioning accuracy is up to ±3.6 m. The developed algorithm reduces position errors by 60-80% for all BLh (B- Latitude, L- Longitude, h- ellipsoidal height) coordinates. The paper shows the possibility of testing and implementing the proposed mathematical algorithm for the SPP solution in a GPS (Global Positioning System) navigation system. In this case the position errors from the GPS SPP solution range from -0.9 m to +0.9 m for all BLh coordinates. The obtained results showed that application the GLONASS and GPS system in air transport is important. The algorithm used in this work can also be applied to other global GNSS navigation systems (e.g. Galileo (European Navigation Satellite system) or BeiDou (Chinese Navigation Satellite System)) in air transport and navigation. https://www.archivesoftransport.com/index.php/aot/article/view/391GLONASSGPSaccuracyposition errorsSPP code method |
spellingShingle | Kamil Krasuski Adam Ciećko Grzegorz Grunwald Małgorzata Kirschenstein Improving positioning accuracy of aircraft using SPP method in GLONASS system Archives of Transport GLONASS GPS accuracy position errors SPP code method |
title | Improving positioning accuracy of aircraft using SPP method in GLONASS system |
title_full | Improving positioning accuracy of aircraft using SPP method in GLONASS system |
title_fullStr | Improving positioning accuracy of aircraft using SPP method in GLONASS system |
title_full_unstemmed | Improving positioning accuracy of aircraft using SPP method in GLONASS system |
title_short | Improving positioning accuracy of aircraft using SPP method in GLONASS system |
title_sort | improving positioning accuracy of aircraft using spp method in glonass system |
topic | GLONASS GPS accuracy position errors SPP code method |
url | https://www.archivesoftransport.com/index.php/aot/article/view/391 |
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