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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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/ 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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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 |
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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 |
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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 |
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VSB-Technical University of Ostrava |
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2017 |
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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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