Abstract
Damages to the aircraft body must be identified in order to avoid unforeseen events that could result in catastrophes if not examined properly. As most of these damages are provoked under normal working conditions, such as in this case during aircraft flight operations, rectifying these damages is nearly impractical. This work veils through a compiled report of Structural Health Monitoring (SHM) of an aircraft wing aiming at the deterioration caused throughout the entire structure of the wing which is subjected to numerous aerodynamics and mechanical constraints. The SHM report provides data which is used to study intramural Damages. Based on the investigation, the Convolutional Neural network (CNN), which is a typical algorithm of deep learning along with Recurrence graph, was chosen as the appropriate Methodology. The structural response recurrence graph can reveal details about the damage, similarity, and underlying structure. Wavelet packets are used to filter and recreate the initial structural response signal, considering the vibrational coupling between the aircraft and wing. Then, as a novel kind of damage feature, the recurrence graph of distinct damages is taken as input picture of the CNN. The findings show that this method provides added information about damage than traditional statistical pattern recognition techniques. These outcomes confirmed the proposed CNN-based model’s suitability for use with additional aircraft components.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Sohn, H., Farrar, C.R., Hemez, F.M., Shunk, D.D., Stinemates, D.W., Nadler, B.R., Czarnecki, J.J.: A Review of Structural Health Monitoring Literature: 1996–2001, p. 1. Los Alamos National Laboratory, USA (2003)
Sohn, H., Farrar, C.R., Hemez, F.M., Czarnecki, J.J.: A Review of Structural Health Review of Structural Health Monitoring Literature 1996–2001 (2002)
Lynch, J.P., Loh, K.J.: A summary review of wireless sensors and sensor networks for structural health monitoring. Shock Vibr. Dig. 38(2), 91–130 (2006)
Farrar, C.R., Worden, K.: An introduction to structural health monitoring. Philos. Trans. Royal Soc. A Math. Phys. Eng. Sci. 365(1851), 303–315 (2007)
Diamanti, K., Soutis, C.: Structural health monitoring techniques for aircraft composite structures. Prog. Aerosp. Sci. 46(8), 342–352 (2010)
Qing, X., Li, W., Wang, Y., Sun, H.: Piezoelectric transducer-based structural health monitoring for aircraft applications. Sensors 19(3), 545 (2019)
Wang, S.C.: Artificial neural network. In: Interdisciplinary Computing in Java Programming, pp. 81–100. Springer, Boston, MA (2003)
Abiodun, O.I., Jantan, A., Omolara, A.E., Dada, K.V., Mohamed, N.A., Arshad, H.: State-of-the-art in artificial neural network applications: a survey. Heliyon 4(11), e00938 (2018)
Momoh, J.A., Button, R.: Design and analysis of aerospace DC arcing faults using fast Fourier transformation and artificial neural network. In: 2003 IEEE Power Engineering Society General Meeting (IEEE Cat. No. 03CH37491), vol. 2, pp. 788–793. IEEE (2003, July)
Raol, J.R.: Neural network based parameter estimation of unstable aerospace dynamic systems. IEE Proc.-Control Theor. Appl. 141(6), 385–388 (1994)
Berke, L.: Application of Artificial Neural Networks to the Design Optimization of Aerospace Structural Components, vol. 4389. NASA (1993)
Ye, L., Su, Z., Yang, C., He, Z., Wang, X.: Hierarchical development of training database for artificial neural network-based damage identification. Compos. Struct. 76(3), 224–233 (2006)
Bakhary, N., Hao, H., Deeks, A.J.: Damage detection using artificial neural network with consideration of uncertainties. Eng. Struct. 29(11), 2806–2815 (2007)
Nick, H., Aziminejad, A., Hosseini, M.H., Laknejadi, K.: Damage identification in steel girder bridges using modal strain energy-based damage index method and artificial neural network. Eng. Fail. Anal. 119, 105010 (2021)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2024 The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Sucharitha, M., Sesha Talpa Sai, P.H.V., Thazha, S.K., Thomas, M., Hunagund, B., Krishna Anand, V.G. (2024). Damage Identification on Aircraft Wing Using Convolutional Neural Network Based Pattern Recognition. In: Talpa Sai, P.H.V.S., Potnuru, S., Avcar, M., Ranjan Kar, V. (eds) Intelligent Manufacturing and Energy Sustainability. ICIMES 2023. Smart Innovation, Systems and Technologies, vol 372. Springer, Singapore. https://doi.org/10.1007/978-981-99-6774-2_16
Download citation
DOI: https://doi.org/10.1007/978-981-99-6774-2_16
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-99-6773-5
Online ISBN: 978-981-99-6774-2
eBook Packages: EngineeringEngineering (R0)