Time series analysis and sparse sensor network-based impact monitoring for aircraft complex structures

被引:12
作者
Wang, Yishou [1 ]
Wang, Minghua [1 ]
Wu, Di [2 ]
Wang, Geng [1 ]
Yan, Jiajia [1 ]
Wang, Yue [2 ]
Qing, Xinlin [1 ]
机构
[1] Xiamen Univ, Sch Aerosp Engn, 422 Siming South Rd, Xiamen 361005, Fujian, Peoples R China
[2] China Acad Launch Vehicle Technol, 1 South Dahongmen Rd,Donggaodi St, Beijing 100000, Peoples R China
来源
STRUCTURAL HEALTH MONITORING-AN INTERNATIONAL JOURNAL | 2023年 / 22卷 / 06期
基金
中国国家自然科学基金;
关键词
Aircraft; composite structures; impact monitoring; time series analysis; sparse sensor network; LOCALIZATION; IDENTIFICATION; VELOCITY; PANEL; SKIN;
D O I
10.1177/14759217231166119
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
An impact monitoring method based on time series analysis and a sparse sensor network is proposed to identify the location of the impact event that occurs on aircraft complex structures and estimate the impact energy. Generally, a high-density sensor network is required for high localization accuracy of the impact event, but with the trade-off of high deployment costs. A sparse piezoelectric sensor network together with a coarse and fine two-step localization method is designed to balance accuracy and cost. The stress wave signals caused by impact are measured by the sensor network and regarded as time series. The impact localization problem is converted into a classification problem of time series, and the strategy of combining coarse localization (impact zone identification) and fine localization (impact localization within a zone) is used to achieve accurate identification of the impact locations. The zone where the impact event is located is first identified by the coarse localization algorithm based on K-nearest neighbor and dynamic time warping (DTW) and one-dimensional convolutional neural networks, respectively. Furthermore, the high accuracy identification of the impact location within the zone is achieved by the fine localization algorithm based on DTW and centroid localization. In terms of the impact energy estimation, the zone correction compensation algorithm is given to sufficiently reduce the estimation error of the impact energy. The low-velocity impact tests are performed on the composite stiffened panel and the aluminum alloy aircraft fuselage structure to verify the effectiveness of the proposed methods.
引用
收藏
页码:4069 / 4088
页数:20
相关论文
共 36 条
[1]   A nonlinear ultrasonic SHM method for impact damage localisation in composite panels using a sparse array of piezoelectric PZT transducers [J].
Andreades, Christos ;
Fierro, Gian Piero Malfense ;
Meo, Michele .
ULTRASONICS, 2020, 108
[2]   Numerical/experimental evaluation of buckling behaviour and residual tensile strength of composite aerospace structures after low velocity impact [J].
Cestino, E. ;
Romeo, G. ;
Piana, P. ;
Danzi, F. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 54 :1-9
[3]   Impact detection in anisotropic materials using a time reversal approach [J].
Ciampa, F. ;
Meo, M. .
STRUCTURAL HEALTH MONITORING-AN INTERNATIONAL JOURNAL, 2012, 11 (01) :43-49
[4]   A passive monitoring technique based on dispersion compensation to locate impacts in plate-like structures [J].
De Marchi, L. ;
Marzani, A. ;
Speciale, N. ;
Viola, E. .
SMART MATERIALS AND STRUCTURES, 2011, 20 (03)
[5]   Experimental Study on Impact Force Identification Using Output Response of Polyvinylidene Fluoride Sensor [J].
Dung, Cao Vu ;
Sasaki, Eiichi .
SENSORS AND MATERIALS, 2018, 30 (01) :7-21
[6]   An Event-Triggered Energy-Efficient Wireless Structural Health Monitoring System for Impact Detection in Composite Airframes [J].
Fu, Hailing ;
Khodaei, Zahra Sharif ;
Aliabadi, M. H. Ferri .
IEEE INTERNET OF THINGS JOURNAL, 2019, 6 (01) :1183-1192
[7]   Identification of impact force for smart composite stiffened panels [J].
Ghajari, M. ;
Sharif-Khodaei, Z. ;
Aliabadi, M. H. ;
Apicella, A. .
SMART MATERIALS AND STRUCTURES, 2013, 22 (08)
[8]  
Gholizadeh S., 2019, International Journal of Mechanical and Production Engineering, V7, P35
[9]   Probability based impact localization in plate structures using an error index [J].
Gorgin, Rahim ;
Wang, Ziping ;
Wu, Zhanjun ;
Yang, Yu .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2021, 157
[10]   Long-range impact localization with a frequency domain triangulation technique: Application to a large aircraft composite panel [J].
Goutaudier, Dimitri ;
Gendre, Didier ;
Kehr-Candille, Veronique ;
Ohayon, Roger .
COMPOSITE STRUCTURES, 2020, 238