TY - JOUR
T1 - Development and experimental validation of a prototype system for Machine Learning based SHM in composite aerostructures
AU - Spiliotopoulos, P. E.
AU - Fera, F. T.
AU - Saramantas, I. E.
AU - Sakellariou, J. S.
AU - Fassois, S. D.
AU - Ofir, Y.
AU - Kressel, I.
AU - Tur, M.
AU - Papadopoulos, P.
AU - Giannopoulos, F.
AU - Spandonidis, C.
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2024
Y1 - 2024
N2 - The development and experimental validation of a Machine Learning (ML) vibration based Structural Health Monitoring (SHM) prototype system for composite aerostructures operating under uncertainty is presented. Following initial training, it is intended to operate autonomously, in almost real-time, without interrupting normal operation, relying on a limited number of acceleration and strain measurements from properly selected locations on the aerostructure. It is equipped with a multi-level information fusion methodology comprising multiple sensor technologies and diagnostic algorithms for optimized SHM performance in terms of damage detection and characterization. Through its flexible software, the system provides multiple options of ML based SHM methods targeting wide applicability to various types of structures. The system is validated based on numerous experiments with healthy and damaged full-scale composite bonded spars operating under multiple uncertainty factors. Its diagnostic performance indicates that the current progress in hardware and robust vibration-based Machine Learning algorithms may lead to compact, effective, and low cost SHM systems for composite aerostructures under normal operating conditions.
AB - The development and experimental validation of a Machine Learning (ML) vibration based Structural Health Monitoring (SHM) prototype system for composite aerostructures operating under uncertainty is presented. Following initial training, it is intended to operate autonomously, in almost real-time, without interrupting normal operation, relying on a limited number of acceleration and strain measurements from properly selected locations on the aerostructure. It is equipped with a multi-level information fusion methodology comprising multiple sensor technologies and diagnostic algorithms for optimized SHM performance in terms of damage detection and characterization. Through its flexible software, the system provides multiple options of ML based SHM methods targeting wide applicability to various types of structures. The system is validated based on numerous experiments with healthy and damaged full-scale composite bonded spars operating under multiple uncertainty factors. Its diagnostic performance indicates that the current progress in hardware and robust vibration-based Machine Learning algorithms may lead to compact, effective, and low cost SHM systems for composite aerostructures under normal operating conditions.
UR - http://www.scopus.com/inward/record.url?scp=85185550775&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/2692/1/012025
DO - 10.1088/1742-6596/2692/1/012025
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AN - SCOPUS:85185550775
SN - 1742-6588
VL - 2692
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012025
T2 - 7th International Conference of Engineering Against Failure, ICEAF 2023
Y2 - 21 June 2023 through 23 June 2023
ER -