Sensors for lightning measurements on aircraft

V. Stelmashuk, A.P.J. Deursen, van

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

6 Citations (Scopus)
65 Downloads (Pure)

Abstract

Lightning strikes a commercial airliner on the average once a year. The European project ldquoIn-flight Lightning Strike Damage Assessment System (ILDAS)rdquo [1] aims to develop and validate a prototype of a system capable to 1) reconstruct the current intensity and wave form, 2) determine of the region of impact on the aircraft, 3) build a maintenance database. Suitable sensors rely on determination of the magnetic field during a strike. Probes considered are inductive coils and solid state sensors, combined in such a way that these cover the full dynamic range in amplitudes (1 A/m up to 40 kA/m) and the full bandwidth (approx. 1 Hz up to 20 MHz). External sensors should be avoided if possible.
Original languageEnglish
Title of host publicationSensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy
Place of PublicationPiscataway
PublisherInstitute of Electrical and Electronics Engineers
Pages1035-1039
ISBN (Print)978-1-4244-2580-8
DOIs
Publication statusPublished - 2008

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Lightning
Aircraft
Solid-state sensors
Sensors
Magnetic fields
Bandwidth

Cite this

Stelmashuk, V., & Deursen, van, A. P. J. (2008). Sensors for lightning measurements on aircraft. In Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy (pp. 1035-1039). Piscataway: Institute of Electrical and Electronics Engineers. https://doi.org/10.1109/ICSENS.2008.4716620
Stelmashuk, V. ; Deursen, van, A.P.J. / Sensors for lightning measurements on aircraft. Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy. Piscataway : Institute of Electrical and Electronics Engineers, 2008. pp. 1035-1039
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title = "Sensors for lightning measurements on aircraft",
abstract = "Lightning strikes a commercial airliner on the average once a year. The European project ldquoIn-flight Lightning Strike Damage Assessment System (ILDAS)rdquo [1] aims to develop and validate a prototype of a system capable to 1) reconstruct the current intensity and wave form, 2) determine of the region of impact on the aircraft, 3) build a maintenance database. Suitable sensors rely on determination of the magnetic field during a strike. Probes considered are inductive coils and solid state sensors, combined in such a way that these cover the full dynamic range in amplitudes (1 A/m up to 40 kA/m) and the full bandwidth (approx. 1 Hz up to 20 MHz). External sensors should be avoided if possible.",
author = "V. Stelmashuk and {Deursen, van}, A.P.J.",
year = "2008",
doi = "10.1109/ICSENS.2008.4716620",
language = "English",
isbn = "978-1-4244-2580-8",
pages = "1035--1039",
booktitle = "Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy",
publisher = "Institute of Electrical and Electronics Engineers",
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}

Stelmashuk, V & Deursen, van, APJ 2008, Sensors for lightning measurements on aircraft. in Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy. Institute of Electrical and Electronics Engineers, Piscataway, pp. 1035-1039. https://doi.org/10.1109/ICSENS.2008.4716620

Sensors for lightning measurements on aircraft. / Stelmashuk, V.; Deursen, van, A.P.J.

Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy. Piscataway : Institute of Electrical and Electronics Engineers, 2008. p. 1035-1039.

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

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AU - Deursen, van, A.P.J.

PY - 2008

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N2 - Lightning strikes a commercial airliner on the average once a year. The European project ldquoIn-flight Lightning Strike Damage Assessment System (ILDAS)rdquo [1] aims to develop and validate a prototype of a system capable to 1) reconstruct the current intensity and wave form, 2) determine of the region of impact on the aircraft, 3) build a maintenance database. Suitable sensors rely on determination of the magnetic field during a strike. Probes considered are inductive coils and solid state sensors, combined in such a way that these cover the full dynamic range in amplitudes (1 A/m up to 40 kA/m) and the full bandwidth (approx. 1 Hz up to 20 MHz). External sensors should be avoided if possible.

AB - Lightning strikes a commercial airliner on the average once a year. The European project ldquoIn-flight Lightning Strike Damage Assessment System (ILDAS)rdquo [1] aims to develop and validate a prototype of a system capable to 1) reconstruct the current intensity and wave form, 2) determine of the region of impact on the aircraft, 3) build a maintenance database. Suitable sensors rely on determination of the magnetic field during a strike. Probes considered are inductive coils and solid state sensors, combined in such a way that these cover the full dynamic range in amplitudes (1 A/m up to 40 kA/m) and the full bandwidth (approx. 1 Hz up to 20 MHz). External sensors should be avoided if possible.

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Stelmashuk V, Deursen, van APJ. Sensors for lightning measurements on aircraft. In Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy. Piscataway: Institute of Electrical and Electronics Engineers. 2008. p. 1035-1039 https://doi.org/10.1109/ICSENS.2008.4716620