Detail publikace
Optimized Automatic Fault Electrode Management of Structural Health Monitoring of Aircraft Composites
PHAM, N. LEUCHTER, J. BLASCH, E.
Originální název
Optimized Automatic Fault Electrode Management of Structural Health Monitoring of Aircraft Composites
Typ
článek v časopise ve Web of Science, Jimp
Jazyk
angličtina
Originální abstrakt
Detecting the structural integrity of composite material used in an airframe includes passive nondestructive testing (NDT) and active electrical impendence tomography (EIT). EIT benefits enhance real-time response and accuracy but require pragmatic approaches to analyze the electrode errors from faulty or nonresponsive readings. The nonfunctional connections of measuring electrodes often occur during onboard aircraft operations for various reasons, such as deterioration. The deterioration of the electrode impedance impacts the quality of the EIT reconstructed image. This article compares different EIT methods and proposes surface fault detection EIT (SURFEIT). The proposed SURFEIT techniques that detect and compensate for faults are verified and evaluated using models with different locations of inside damages. Results prove the effectiveness of SURFEIT techniques, when the number of faulty electrodes is up to one-fourth of the total electrodes. The biggest benefit of the SURFEIT techniques is that they do not require any additional simulation work, lead to significant reduction of computation time, and afford very fast indications of damage locations.
Klíčová slova
Data compensation; electrical impedance tomography (EIT); manage faulty electrodes
Autoři
PHAM, N.; LEUCHTER, J.; BLASCH, E.
Vydáno
18. 9. 2024
Nakladatel
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
Místo
PISCATAWAY
ISSN
1558-1748
Periodikum
IEEE SENSORS JOURNAL
Ročník
24
Číslo
21
Stát
Spojené státy americké
Strany od
35686
Strany do
35699
Strany počet
14
URL
Plný text v Digitální knihovně
BibTex
@article{BUT193473,
author="Ngoc Nam {Pham} and Jan {Leuchter} and Erik {Blasch}",
title="Optimized Automatic Fault Electrode Management of Structural Health Monitoring of Aircraft Composites",
journal="IEEE SENSORS JOURNAL",
year="2024",
volume="24",
number="21",
pages="35686--35699",
doi="10.1109/JSEN.2024.3459614",
issn="1558-1748",
url="https://ieeexplore.ieee.org/document/10684087"
}