Sensors for lightning measurements on aircraft

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

doi:10.1109/ICSENS.2008.4716620

Sensors for lightning measurements on aircraft

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

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

6 Citations (Scopus)

141 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 language	English
Title of host publication	Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy
Place of Publication	Piscataway
Publisher	Institute of Electrical and Electronics Engineers
Pages	1035-1039
ISBN (Print)	978-1-4244-2580-8
DOIs	https://doi.org/10.1109/ICSENS.2008.4716620
Publication status	Published - 2008

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10.1109/ICSENS.2008.4716620

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Cite this

@inproceedings{1e1a8c61bfb94604904ee4e2f1c40e58,

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",

address = "United States",

}

TY - GEN

T1 - Sensors for lightning measurements on aircraft

AU - Stelmashuk, V.

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

PY - 2008

Y1 - 2008

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.

U2 - 10.1109/ICSENS.2008.4716620

DO - 10.1109/ICSENS.2008.4716620

M3 - Conference contribution

SN - 978-1-4244-2580-8

SP - 1035

EP - 1039

BT - Sensors 2008 IEEE, 26-29 Oct. 2008, Lecce Italy

PB - Institute of Electrical and Electronics Engineers

CY - Piscataway

ER -

Sensors for lightning measurements on aircraft

Abstract

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