This paper focuses on the localization of impacts applied on a composite aircraft by using low sampling frequency accelerometers. A new vibration-based approach using a modal model of the aircraft on ground is described to localize the impact on the cylindrical fuselage. Axial localization is achieved by estimating the contributions of specific vibration modes to the response. Angular localization is achieved by estimating the impact force direction. An impact test campaign is performed on an Airbus A350-900 equipped with only six accelerometers. Fifty percent of the applied impacts are localized within 2 m and more than 90% within 3 m.
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@article{CRMECA_2020__348_3_191_0,
author = {Dimitri Goutaudier and Guillaume Osmond and Didier Gendre},
title = {Impact localization on a composite fuselage with a sparse network of accelerometers},
journal = {Comptes Rendus. M\'ecanique},
pages = {191--209},
publisher = {Acad\'emie des sciences, Paris},
volume = {348},
number = {3},
year = {2020},
doi = {10.5802/crmeca.12},
language = {en},
}
TY - JOUR AU - Dimitri Goutaudier AU - Guillaume Osmond AU - Didier Gendre TI - Impact localization on a composite fuselage with a sparse network of accelerometers JO - Comptes Rendus. Mécanique PY - 2020 SP - 191 EP - 209 VL - 348 IS - 3 PB - Académie des sciences, Paris DO - 10.5802/crmeca.12 LA - en ID - CRMECA_2020__348_3_191_0 ER -
%0 Journal Article %A Dimitri Goutaudier %A Guillaume Osmond %A Didier Gendre %T Impact localization on a composite fuselage with a sparse network of accelerometers %J Comptes Rendus. Mécanique %D 2020 %P 191-209 %V 348 %N 3 %I Académie des sciences, Paris %R 10.5802/crmeca.12 %G en %F CRMECA_2020__348_3_191_0
Dimitri Goutaudier; Guillaume Osmond; Didier Gendre. Impact localization on a composite fuselage with a sparse network of accelerometers. Comptes Rendus. Mécanique, Volume 348 (2020) no. 3, pp. 191-209. doi : 10.5802/crmeca.12. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.5802/crmeca.12/
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