Publication detail
Optimized Automatic Fault Electrode Management of Structural Health Monitoring of Aircraft Composites
PHAM, N. LEUCHTER, J. BLASCH, E.
Original Title
Optimized Automatic Fault Electrode Management of Structural Health Monitoring of Aircraft Composites
Type
journal article in Web of Science
Language
English
Original Abstract
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.
Keywords
Data compensation; electrical impedance tomography (EIT); manage faulty electrodes
Authors
PHAM, N.; LEUCHTER, J.; BLASCH, E.
Released
18. 9. 2024
Publisher
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
Location
PISCATAWAY
ISBN
1558-1748
Periodical
IEEE SENSORS JOURNAL
Year of study
24
Number
21
State
United States of America
Pages from
35686
Pages to
35699
Pages count
14
URL
Full text in the Digital Library
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"
}