Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system

Multilateration estimates aircraft position using the Time Difference Of Arrival (TDOA) with a lateration algorithm. The Position Estimation (PE) accuracy of the lateration algorithm depends on several factors which are the TDOA estimation error, the lateration algorithm approach, the number of depl...

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Main Authors: Yaro, A. S., Sha’Ameri, A. Z., Kamel, N.
Format: Article
Language:English
Published: VSB-Technical University of Ostrava 2017
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Online Access:http://eprints.utm.my/id/eprint/75301/1/NidalKamel2017_GroundReceivingStationReferencePair.pdf
http://eprints.utm.my/id/eprint/75301/
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spelling my.utm.753012018-03-27T06:10:52Z http://eprints.utm.my/id/eprint/75301/ Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system Yaro, A. S. Sha’Ameri, A. Z. Kamel, N. TK Electrical engineering. Electronics Nuclear engineering Multilateration estimates aircraft position using the Time Difference Of Arrival (TDOA) with a lateration algorithm. The Position Estimation (PE) accuracy of the lateration algorithm depends on several factors which are the TDOA estimation error, the lateration algorithm approach, the number of deployed GRSs and the selection of the GRS reference used for the PE process. Using the minimum number of GRSs for 3D emitter PE, a technique based on the condition number calculation is proposed to select the suitable GRS reference pair for improving the accuracy of the PE using the lateration algorithm. Validation of the proposed technique was performed with the GRSs in the square and triangular GRS configuration. For the selected emitter positions, the result shows that the proposed technique can be used to select the suitable GRS reference pair for the PE process. A unity condition number is achieved for GRS pair most suitable for the PE process. Monte Carlo simulation result, in comparison with the fixed GRS reference pair lateration algorithm, shows a reduction in PE error of at least 70 % for both GRS in the square and triangular configuration. VSB-Technical University of Ostrava 2017 Article PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/75301/1/NidalKamel2017_GroundReceivingStationReferencePair.pdf Yaro, A. S. and Sha’Ameri, A. Z. and Kamel, N. (2017) Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system. Advances in Electrical and Electronic Engineering, 15 (3). pp. 391-399. ISSN 1336-1376 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85030571722&doi=10.15598%2faeee.v15i3.2254&partnerID=40&md5=8cf144b025959ffdd1a672f486d2403c DOI:10.15598/aeee.v15i3.2254
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic TK Electrical engineering. Electronics Nuclear engineering
spellingShingle TK Electrical engineering. Electronics Nuclear engineering
Yaro, A. S.
Sha’Ameri, A. Z.
Kamel, N.
Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system
description Multilateration estimates aircraft position using the Time Difference Of Arrival (TDOA) with a lateration algorithm. The Position Estimation (PE) accuracy of the lateration algorithm depends on several factors which are the TDOA estimation error, the lateration algorithm approach, the number of deployed GRSs and the selection of the GRS reference used for the PE process. Using the minimum number of GRSs for 3D emitter PE, a technique based on the condition number calculation is proposed to select the suitable GRS reference pair for improving the accuracy of the PE using the lateration algorithm. Validation of the proposed technique was performed with the GRSs in the square and triangular GRS configuration. For the selected emitter positions, the result shows that the proposed technique can be used to select the suitable GRS reference pair for the PE process. A unity condition number is achieved for GRS pair most suitable for the PE process. Monte Carlo simulation result, in comparison with the fixed GRS reference pair lateration algorithm, shows a reduction in PE error of at least 70 % for both GRS in the square and triangular configuration.
format Article
author Yaro, A. S.
Sha’Ameri, A. Z.
Kamel, N.
author_facet Yaro, A. S.
Sha’Ameri, A. Z.
Kamel, N.
author_sort Yaro, A. S.
title Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system
title_short Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system
title_full Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system
title_fullStr Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system
title_full_unstemmed Ground receiving station reference pair selection technique for a minimum configuration 3D emitter position estimation multilateration system
title_sort ground receiving station reference pair selection technique for a minimum configuration 3d emitter position estimation multilateration system
publisher VSB-Technical University of Ostrava
publishDate 2017
url http://eprints.utm.my/id/eprint/75301/1/NidalKamel2017_GroundReceivingStationReferencePair.pdf
http://eprints.utm.my/id/eprint/75301/
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85030571722&doi=10.15598%2faeee.v15i3.2254&partnerID=40&md5=8cf144b025959ffdd1a672f486d2403c
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score 13.211869