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16 pages, 8780 KiB  
Article
Soil Mapping of Small Fields with Limited Number of Samples by Coupling EMI and NIR Spectroscopy
by Leonardo Pace, Simone Priori, Monica Zanini and Valerio Cristofori
Soil Syst. 2024, 8(4), 128; https://doi.org/10.3390/soilsystems8040128 - 7 Dec 2024
Viewed by 493
Abstract
Precision agriculture relies on highly detailed soil maps to optimize resource use. Proximal sensing methods, such as EMI, require a certain number of soil samples and laboratory analysis to interpolate the characteristics of the soil. NIR diffuse reflectance spectroscopy offers a rapid, low-cost [...] Read more.
Precision agriculture relies on highly detailed soil maps to optimize resource use. Proximal sensing methods, such as EMI, require a certain number of soil samples and laboratory analysis to interpolate the characteristics of the soil. NIR diffuse reflectance spectroscopy offers a rapid, low-cost alternative that increases datapoints and map accuracy. This study tests and optimizes a methodology for high-detail soil mapping in a 2.5 ha hazelnut grove in Grosseto, Southern Tuscany, Italy, using both EMI sensors (GF Mini Explorer, Brno, Czech Republic) and a handheld NIR spectrometer (Neospectra Scanner, Si-Ware Systems, Menlo Park, CA, USA). In addition to two profiles selected by clustering, another 35 topsoil augerings (0–30 cm) were added. Laboratory analyses were performed on only five samples (two profiles + three samples from the augerings). Partial least square regression (PLSR) with a national spectral library, augmented by the five local samples, predicted clay, sand, organic carbon (SOC), total nitrogen (TN), and cation exchange capacity (CEC). The 37 predicted datapoints were used for spatial interpolation, using the ECa map, elevation, and DEM derivatives as covariates. Kriging with external drift (KED) was used to spatialize the results. The errors of the predictive maps were calculated using five additional validation points analyzed by conventional methods. The validation showed good accuracy of the predictive maps, particularly for SOC and TN. Full article
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Figure 1
<p>Framework for the study area.</p>
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<p>Pretreatments applied to the spectral library with local samples (n = 377): on the left the Savitzky–Golay filter; on the right, the application of the standard normal variate.</p>
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<p>Maps of electrical conductivity (ECa) measured at different depths by EMI sensor. The black dots show the soil profiles (P24 and P25), whereas the polygons show the two STUs delineated by k-means clustering.</p>
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<p>Digital elevation model (DEM) with selected profiles.</p>
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<p>Profile P24.</p>
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<p>Profile P25.</p>
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<p>Total random augerings. The blue dots are the points selected for the local calibration set.</p>
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<p>Maps of clay (g·100 g<sup>−1</sup>), sand (g·100 g<sup>−1</sup>) and SOC (g·100 g<sup>−1</sup>), interpolated by KED, using the values of the sampling datapoints predicted by NIR spectroscopy and the most related covariates according to Pearson’s correlation index.</p>
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<p>Maps of TN (g·kg<sup>−1</sup>), CEC (meq·100 g<sup>−1</sup>) and CaCO<sub>3</sub> (g·100 g<sup>−1</sup>), interpolated by KED, using the values of the sampling datapoints predicted by NIR spectroscopy and the most related covariates according to Pearson’s correlation index.</p>
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<p>Error map of clay (g·100 g<sup>−1</sup>), sand (g·100 g<sup>−1</sup>), SOC (g·100 g<sup>−1</sup>)<sub>,</sub> TN (g·kg<sup>−1</sup>), CEC (meq·100 g<sup>−1</sup>), and CaCO<sub>3</sub> (g·100 g<sup>−1</sup>), interpolated by KED, using the values of the sampling datapoints predicted by NIR spectroscopy and the most related covariates according to Pearson’s index.</p>
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<p>Total random augerings. Blue dots are the points selected for the local calibration set; red dots are the points collected for the local validation set.</p>
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28 pages, 10795 KiB  
Article
Advanced Structural Technologies Implementation in Designing and Constructing RC Elements with C-FRP Bars, Protected Through SHM Assessment
by Georgia M. Angeli, Maria C. Naoum, Nikos A. Papadopoulos, Parthena-Maria K. Kosmidou, George M. Sapidis, Chris G. Karayannis and Constantin E. Chalioris
Fibers 2024, 12(12), 108; https://doi.org/10.3390/fib12120108 - 5 Dec 2024
Viewed by 382
Abstract
The need to strengthen the existing reinforced concrete (RC) elements is becoming increasingly crucial for modern cities as they strive to develop resilient and sustainable structures and infrastructures. In recent years, various solutions have been proposed to limit the undesirable effects of corrosion [...] Read more.
The need to strengthen the existing reinforced concrete (RC) elements is becoming increasingly crucial for modern cities as they strive to develop resilient and sustainable structures and infrastructures. In recent years, various solutions have been proposed to limit the undesirable effects of corrosion in RC elements. While C-FRP has shown promise in corrosion-prone environments, its use in structural applications is limited by cost, bonding, and anchorage challenges with concrete. To address these, the present research investigates the structural performance of RC beams reinforced with C-FRP bars under static loading using Structural Health Monitoring (SHM) with an Electro-Mechanical Impedance (EMI) system employing Lead Zirconate Titanate (PZT) piezoelectric transducers which are applied to detect damage development and enhance the protection of RC elements and overall, RC structures. This study underscores the potential of C-FRP bars for durable tensile reinforcement in RC structures, particularly in hybrid designs that leverage steel for compression strength. The study focuses on critical factors such as stiffness, maximum load capacity, deflection at each loading stage, and the development of crack widths, all analyzed through voltage responses recorded by the PZT sensors. Particular emphasis is placed on the bond conditions and anchorage lengths of the tensile C-FRP bars, exploring how local confinement conditions along the anchorage length influence the overall behavior of the beams. Full article
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<p>Cross-section, geometry, reinforcement details, spiral anchorage configuration, notations and positioning of PZTs for beams CFRP10-C and CFRP10-R.</p>
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<p>Four-point bending experimental setup, instrumentation, and SHM devices.</p>
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<p>Experimental behavior of specimens CFRP10-R and CFRP10-C.</p>
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<p>Voltage-frequency response of the PZT transducers of Beam CFRP-C; (<b>a</b>) PZT 3 and (<b>b</b>) PZT 2, (<b>c</b>) PZT C, and (<b>d</b>) PZT B.</p>
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<p>Voltage-frequency response of the PZT transducers of Beam CFRP-C; (<b>a</b>) PZT 1 and (<b>b</b>) PZT 4, (<b>c</b>) PZT A, and (<b>d</b>) PZT D.</p>
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<p>Voltage-frequency response of the PZT transducers of Beam CFRP-C; (<b>a</b>) PZT 1 and (<b>b</b>) PZT 4, (<b>c</b>) PZT A, and (<b>d</b>) PZT D.</p>
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<p>Voltage-frequency response of the PZT transducers of Beam CFRP-R; (<b>a</b>) PZT 1 and (<b>b</b>) PZT 2, (<b>c</b>) PZT A, and (<b>d</b>) PZT B.</p>
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<p>Voltage-frequency response of the PZT transducers of Beam CFRP-R; (<b>a</b>) PZT 1 and (<b>b</b>) PZT 2, (<b>c</b>) PZT A, and (<b>d</b>) PZT B.</p>
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<p>Voltage-frequency response of the PZT transducers of Beam CFRP-R; (<b>a</b>) PZT 3 and (<b>b</b>) PZT 4, (<b>c</b>) PZT C, and (<b>d</b>) PZT D.</p>
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<p>Cracking pattern of Beam CFRP10-C.</p>
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<p>RMSD index values of (<b>a</b>) PZT A, and (<b>b</b>) PZT 1 of Beam CFRP10-C.</p>
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<p>RMSD index values of (<b>a</b>) PZT B, and (<b>b</b>) PZT 2 of Beam CFRP10-C.</p>
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<p>RMSD index values of (<b>a</b>) PZT C, and (<b>b</b>) PZT 3 of Beam CFRP10-C.</p>
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<p>RMSD index values of (<b>a</b>) PZT D, and (<b>b</b>) PZT 4 of Beam CFRP10-C.</p>
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<p>Cracking pattern of Beam CFRP10-R.</p>
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<p>RMSD index values of (<b>a</b>) PZT A, and (<b>b</b>) PZT 1 of Beam CFRP10-R.</p>
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<p>RMSD index values of (<b>a</b>) PZT B, and (<b>b</b>) PZT 2 of Beam CFRP10-R.</p>
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<p>RMSD index values of (<b>a</b>) PZT C, and (<b>b</b>) PZT 3 of Beam CFRP10-R.</p>
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<p>RMSD index values of (<b>a</b>) PZT D, and (<b>b</b>) PZT 4 of Beam CFRP10-R.</p>
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16 pages, 5306 KiB  
Article
Electromagnetic Imaging for Breathing Monitoring
by Ivan Vassilyev and Zhassulan Mendakulov
Sensors 2024, 24(23), 7722; https://doi.org/10.3390/s24237722 - 3 Dec 2024
Viewed by 523
Abstract
The search for new non-invasive methods of investigating the functioning of human internal organs is an urgent task. One of these methods for assessing the functioning of the human respiratory system is electromagnetic sensing, which is based on a significant difference in the [...] Read more.
The search for new non-invasive methods of investigating the functioning of human internal organs is an urgent task. One of these methods for assessing the functioning of the human respiratory system is electromagnetic sensing, which is based on a significant difference in the dielectric permittivity of muscle tissue and air. During breathing, when the lungs are filled with air, the dielectric permittivity of the lungs decreases, which leads to a change in the level of the electromagnetic signal passing through the body. The results of experiments on recording changes in the level of electromagnetic radiation passing through the human body performed on an experimental device consisting of eight transmitting and receiving antennas located on opposite sides of the chest have been presented in the article. The possibility of visualizing the measured “pulmonograms” in the form of dynamic two-dimensional images showing the process of filling various parts of the lungs with air has been demonstrated. Full article
(This article belongs to the Special Issue Sensors for Breathing Monitoring)
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<p>Model of the electromagnetic wave propagation medium. Breathing process is accompanied by a change in the dielectric permittivity <math display="inline"><semantics> <mrow> <mi>ε</mi> </mrow> </semantics></math> and the distance <math display="inline"><semantics> <mrow> <mi>d</mi> </mrow> </semantics></math> of the second capacitor, changing the impedance of the medium.</p>
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<p>Block diagram of the device for microwave investigation of bronchopulmonary system, in particular, human respiration [<a href="#B2-sensors-24-07722" class="html-bibr">2</a>].</p>
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<p>Dimensions of the array of transmitting antennas “Tx antenna matrix” and the array of receiving antennas “Rx antenna matrix” before the beginning of a series of experiments.</p>
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<p>The patient examination process. Photo on the left was taken from [<a href="#B18-sensors-24-07722" class="html-bibr">18</a>].</p>
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<p>Pulmonograms of a man.</p>
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<p>Pulmonograms of a woman.</p>
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<p>The result of accumulation and averaging of a man’s pulmonogram.</p>
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<p>The result of accumulation and averaging of a woman’s pulmonogram.</p>
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<p>Representation of a man’s pulmonogram in decibels [<a href="#B18-sensors-24-07722" class="html-bibr">18</a>,<a href="#B19-sensors-24-07722" class="html-bibr">19</a>].</p>
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<p>Representation of a woman’s pulmonogram in decibels.</p>
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<p>Setting the boundary values of the image matrix. The size of the display area is <math display="inline"><semantics> <mrow> <mn mathvariant="bold">1441</mn> <mo>×</mo> <mn mathvariant="bold">1153</mn> </mrow> </semantics></math> pixels. The background image was taken from [<a href="#B20-sensors-24-07722" class="html-bibr">20</a>]. The spatial measurement points correspond to the following elements in the image matrix: Ch1 (193, 897); Ch2 (449, 897); Ch3 (705, 897); Ch4 (961, 897); Ch5 (193, 257); Ch6 (449, 257); Ch7 (705, 257), and Ch8 (961, 257).</p>
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<p>The result of imaging of a man’s pulmonograms.</p>
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<p>The result of imaging of a woman’s pulmonograms.</p>
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15 pages, 567 KiB  
Article
AI-Driven Electrical Fast Transient Suppression for Enhanced Electromagnetic Interference Immunity in Inductive Smart Proximity Sensors
by Silvia Giangaspero, Gianluca Nicchiotti, Philippe Venier, Laurent Genilloud and Lorenzo Pirrami
Sensors 2024, 24(22), 7372; https://doi.org/10.3390/s24227372 - 19 Nov 2024
Viewed by 509
Abstract
Inductive proximity sensors are relevant in position-sensing applications in many industries but, in order to be used in harsh industrial environments, they need to be immune to electromagnetic interference (EMI). The use of conventional filters to mitigate these perturbations often compromises signal bandwidth, [...] Read more.
Inductive proximity sensors are relevant in position-sensing applications in many industries but, in order to be used in harsh industrial environments, they need to be immune to electromagnetic interference (EMI). The use of conventional filters to mitigate these perturbations often compromises signal bandwidth, ranging from 100 Hz to 1.6 kHz. We have exploited recent advances in the field of artificial intelligence (AI) to study the ability of neural networks (NNs) to automatically filter out EMI features. This study offers an analysis and comparison of possible NN models (a 1D convolutional NN, a recurrent NN, and a hybrid convolutional and recurrent approach) for denoising EMI-perturbed signals and proposes a final model, which is based on gated recurrent unit (GRU) layers. This network is compressed and optimised to meet memory requirements, so that in future developments it could be implemented in application-specific integrated circuits (ASICs) for inductive sensors. The final RNN manages to reduce noise by 70% (MSEred) while occupying 2 KB of memory. Full article
(This article belongs to the Section Electronic Sensors)
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<p>Overview of the main stages of the study.</p>
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<p>Data set production procedure. (<b>a</b>) Signals generated according to IEC 61000-4-4 [<a href="#B1-sensors-24-07372" class="html-bibr">1</a>], representative of the analogue voltage output to Contrinex M30 inductive sensors, disturbed in 15 ms windows by bursts at frequencies of 1 kHz, 2.5 kHz, 5 kHz, and 10 kHz, respectively. (<b>b</b>) Extraction of noise and burst information from real signals: to obtain an estimate of the amount of noise in the signals, the standard deviation (<math display="inline"><semantics> <msub> <mi>σ</mi> <mi>noise</mi> </msub> </semantics></math>) of the four signals in the window prior to the start of burst generation was extracted. The average <math display="inline"><semantics> <msub> <mi>σ</mi> <mi>noise</mi> </msub> </semantics></math> value of the four signals was taken as a reference value for the simulated signals. The waveforms of the bursts were extracted by moving a window on the signals. (<b>c</b>) The voltage (V) as a function of the displacement of the target (x) was calculated according to the response diagram provided by the data sheet of M30 inductive sensor [<a href="#B23-sensors-24-07372" class="html-bibr">23</a>]. (<b>d</b>) The diagram describes the procedure used for the simulation of new signals. A signal indicative of x was generated. V was calculated as f(x), where f was found in (<b>c</b>). AWGN was added to the clean signal with a <math display="inline"><semantics> <mi>σ</mi> </semantics></math> of ±50% of the reference value found in (<b>b</b>). Bursts were added to the signal with a random frequency between 1 and 10 kHz. The signals were finally low-pass filtered at a random frequency between 5 and 100 kHz to simulate more real-world situations where disturbances are more attenuated. The signal thus obtained was the noisy signal. (<b>e</b>) Examples of simulated signals, representing, respectively, a target moving forward and backward relative to the sensor, an object moving away, and harmonic motion with an increase in frequency.</p>
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<p>The 1D-CNN approach’s architecture.</p>
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<p>RNN approach’s architecture.</p>
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<p>The 1D-CNN-GRU hybrid approach’s architecture.</p>
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<p>Cumulative explained variance plot for the three approaches.</p>
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<p>Example of a signal from the test set denoised by the different DNN approaches.</p>
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32 pages, 17953 KiB  
Article
Integrated Estimation of Stress and Damage in Concrete Structure Using 2D Convolutional Neural Network Model Learned Impedance Responses of Capsule-like Smart Aggregate Sensor
by Quoc-Bao Ta, Ngoc-Lan Pham and Jeong-Tae Kim
Sensors 2024, 24(20), 6652; https://doi.org/10.3390/s24206652 - 15 Oct 2024
Viewed by 851
Abstract
Stress and damage estimation is essential to ensure the safety and performance of concrete structures. The capsule-like smart aggregate (CSA) technique has demonstrated its potential for detecting early-stage internal damage. In this study, a 2 dimensional convolutional neural network (2D CNN) model that [...] Read more.
Stress and damage estimation is essential to ensure the safety and performance of concrete structures. The capsule-like smart aggregate (CSA) technique has demonstrated its potential for detecting early-stage internal damage. In this study, a 2 dimensional convolutional neural network (2D CNN) model that learned the EMI responses of a CSA sensor to integrally estimate stress and damage in concrete structures is proposed. Firstly, the overall scheme of this study is described. The CSA-based EMI damage technique method is theoretically presented by describing the behaviors of a CSA sensor embedded in a concrete structure under compressive loadings. The 2D CNN model is designed to learn and extract damage-sensitive features from a CSA’s EMI responses to estimate stress and identify damage levels in a concrete structure. Secondly, a compression experiment on a CSA-embedded concrete cylinder is carried out, and the stress–damage EMI responses of a cylinder are recorded under different applied stress levels. Finally, the feasibility of the developed model is further investigated under the effect of noises and untrained data cases. The obtained results indicate that the developed 2D CNN model can simultaneously estimate stress and damage status in the concrete structure. Full article
(This article belongs to the Section State-of-the-Art Sensors Technologies)
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<p>Scheme of CSA-based concrete damage monitoring by 2D CNN model.</p>
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<p>Prototype of capsule-like smart aggregate (CSA).</p>
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<p>Behaviors of EMI responses of CSA embedded in concrete structure under applied stress in z-direction: (<b>a</b>) CSA in structure under compression; (<b>b</b>) Section B-B; (<b>c</b>) changes in EMI responses.</p>
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<p>Data configuration of stress–damage EMI data for 2D CNN model.</p>
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<p>Architecture of 2D CNN deep regression and classification model.</p>
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<p>Fabrication of CSA-embedded concrete cylinder.</p>
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<p>Experimental setup: (<b>a</b>) stress–damage EMI measurement in CSA-embedded cylinder under compressive load; (<b>b</b>) compressive loading scenario.</p>
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<p>Measured stress–damage EMI responses of z-CSA under applied stresses: (<b>a</b>) S<sub>0</sub>; (<b>b</b>) S<sub>1</sub>; (<b>c</b>) S<sub>2</sub>; (<b>d</b>) S<sub>3</sub>; (<b>e</b>) S<sub>4</sub>; (<b>f</b>) S<sub>5</sub>.</p>
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<p>Stress–damage EMI responses of z-CSA under applied stresses S<sub>0–5</sub>.</p>
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<p>Visual observation of test specimen under applied stresses S<sub>0–5</sub>.</p>
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<p>Stress–damage EMI features of CSA under applied stresses S<sub>1–5</sub>: (<b>a</b>) RMSD; (<b>b</b>) CCD.</p>
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<p>EMI responses (in average of ensembles) CSA in cylinder under applied stresses S<sub>1–5</sub>.</p>
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<p>Example of noise-contaminated stress–damage EMI signals under applied stress level S<sub>1</sub> in testing set: (<b>a</b>) 4% noise; (<b>b</b>) 10% noise; (<b>c</b>) 16% noise.</p>
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<p>Loss values of 2D CNN model after 100 epochs.</p>
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<p>Stress prediction by 2D CNN model: (<b>a</b>) 0% noise; (<b>b</b>) 4% noise; (<b>c</b>) 10% noise; (<b>d</b>) 16% noise.</p>
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<p>RMSE comparison of 2D CNN model for stress estimation. (<b>a</b>) Trained levels of noise (0–5%); (<b>b</b>) untrained levels of noise (6–16%).</p>
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<p>Damage identification of 2D CNN model under noise levels: (<b>a</b>) 0% noise; (<b>b</b>) 4% noise; (<b>c</b>) 10% noise; (<b>d</b>) 16% noise.</p>
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<p>Accuracy of damage identification by 2D CNN model: true positive rate. (<b>a</b>) Trained levels of noise (0–5%); (<b>b</b>) untrained levels of noise (6–16%).</p>
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<p>Accuracy of damage identification by 2D CNN model: false negative rate. (<b>a</b>) Trained levels of noise (0–5%); (<b>b</b>) untrained levels of noise (6–16%).</p>
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<p>Accuracy of damage identification by 2D CNN model: false discovery rate. (<b>a</b>) Trained levels of noise (0–5%); (<b>b</b>) untrained levels of noise (6–16%).</p>
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<p>Visualization of labeled stress–damage EMI signals in training set for 2D CNN model: (<b>a</b>) Case 1 (untrained S<sub>2</sub>); (<b>b</b>) Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>); (<b>c</b>) Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>); (<b>d</b>) Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>).</p>
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<p>Loss values of 2D CNN model for untrained cases: (<b>a</b>) Case 1 (untrained S<sub>2</sub>); (<b>b</b>) Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>); (<b>c</b>) Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>); (<b>d</b>) Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>).</p>
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<p>Stress estimation of 2D CNN model for Case 1 (untrained S<sub>2</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Stress estimation of 2D CNN model for Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Stress estimation of 2D CNN model for Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Stress estimation of 2D CNN model for Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>RMSE comparison of 2D CNN model for stress estimation: (<b>a</b>) Case 1 (untrained S<sub>2</sub>); (<b>b</b>) Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>); (<b>c</b>) Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>); (<b>d</b>) Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>).</p>
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<p>Damage identification of 2D CNN model for Case 1 (untrained S<sub>2</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Damage identification of 2D CNN model for Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Damage identification of 2D CNN model for Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Damage identification of 2D CNN model for Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 5% noise.</p>
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<p>Accuracy of damage identification by 2D CNN model: true positive rate. (<b>a</b>) Case 1 (untrained S<sub>2</sub>); (<b>b</b>) Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>); (<b>c</b>) Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>); (<b>d</b>) Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>).</p>
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<p>Accuracy of damage identification by 2D CNN model: false negative rate. (<b>a</b>) Case 1 (untrained S<sub>2</sub>); (<b>b</b>) Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>); (<b>c</b>) Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>); (<b>d</b>) Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>).</p>
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<p>Accuracy of damage identification by 2D CNN model: false discovery rate. (<b>a</b>) Case 1 (untrained S<sub>2</sub>); (<b>b</b>) Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>); (<b>c</b>) Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>); (<b>d</b>) Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>).</p>
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<p>Probability assessment of damage identification results: Case 1 (untrained S<sub>2</sub>).</p>
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<p>Probability assessment of damage identification results: Case 2 (untrained S<sub>2</sub>, S<sub>4</sub>). (<b>a</b>) Untrained “DL0” (partially); (<b>b</b>) untrained “DL2”.</p>
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<p>Probability assessment of damage identification results: Case 3 (untrained S<sub>2</sub>, S<sub>3</sub>). (<b>a</b>) Untrained “DL0” (partially); (<b>b</b>) untrained “DL1”.</p>
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<p>Probability assessment of damage identification results: Case 4 (untrained S<sub>1</sub>, S<sub>3</sub>, S<sub>5</sub>). (<b>a</b>) Untrained “DL0” (partially); (<b>b</b>) untrained “DL1”; (<b>c</b>) untrained “DL3”.</p>
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<p>Training and validation loss of three 2D CNN architectures: (<b>a</b>) M1; (<b>b</b>) M2; (<b>c</b>) M3.</p>
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29 pages, 15583 KiB  
Article
Advanced Structural Monitoring Technologies in Assessing the Performance of Retrofitted Reinforced Concrete Elements
by Maria C. Naoum, Nikos A. Papadopoulos, George M. Sapidis and Constantin E. Chalioris
Appl. Sci. 2024, 14(20), 9282; https://doi.org/10.3390/app14209282 - 12 Oct 2024
Viewed by 962
Abstract
Climate change induces extreme effects with lower-than-designed restoration periods, imposing the necessity of strengthening the structural integrity of existing and mainly older RC structures, which are often demonstrated to be under-reinforced in terms of the shear capacity, mainly due to outdated and old [...] Read more.
Climate change induces extreme effects with lower-than-designed restoration periods, imposing the necessity of strengthening the structural integrity of existing and mainly older RC structures, which are often demonstrated to be under-reinforced in terms of the shear capacity, mainly due to outdated and old design codes/standards. Thus, finding cost-effective and feasible methods to strengthen RC elements is becoming increasingly important. Thin RC layers for jacketing represent a modern advancement in repairing and retrofitting RC members. In this context, U-shaped mortar jackets were employed to strengthen three shear-critical beams. In addition, a critical aspect in the success of any jacketing method is the degree of bonding and interaction between the original member and the new jacket. Additionally, the performance of these U-shaped jackets was assessed using an Electro-Mechanical-Impedance-based (EMI-based) method using a Piezoelectric-Transducer-enabled (PZT-enabled) technique. The integration of advanced monitoring technologies in retrofitting applications offers valuable insights into the performance and longevity of the retrofit system. Therefore, this study aims to experimentally investigate the cohesion between construction materials and assess the effectiveness of U-shaped jackets. Through the proposed Structural Health Monitoring (SHM) technique, any degradation at the interface or slippage of the retrofitting jacket can be promptly detected, restraining further damage development and potential failure of the structure. Full article
(This article belongs to the Collection Nondestructive Testing (NDT))
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<p>Geometrical and reinforcement details of initial and retrofitted beams.</p>
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<p>Preparation of the surface.</p>
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<p>Retrofitting process for beams “B-J”.</p>
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<p>Test setup and instrumentation.</p>
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<p>Positions and notations of the PZTs of beam “B500-J”.</p>
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<p>Positions and notations of the PZTs of beam “B200a-J”.</p>
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<p>Positions and notations of the PZTs of beam “B200b-J”.</p>
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<p>Schematic illustration of the monitoring process.</p>
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<p>Comparative mechanical responses for beams “B” and (<b>a</b>) “B-500-J”, (<b>b</b>) “B-200a-J”, and (<b>c</b>) “B200b-J”.</p>
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<p>Mechanical response for beam “B500-J”, EMI measurements, and crack meters.</p>
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<p>Cracking pattern of beam “B500-J”.</p>
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<p>Voltage responses for beam “B500-J”.</p>
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<p>Mechanical response for beam “B200a-J”, EMI measurements, and crack meters.</p>
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<p>Cracking pattern of beam “B200a-J”.</p>
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<p>Voltage responses for beam “B200a-J”.</p>
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<p>Mechanical response for beam “B200b-J”, EMI measurements, and crack meters.</p>
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<p>Cracking pattern of beam “B200b-J”.</p>
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<p>Voltage responses for beam “B200b-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “J” PZTs’ notation and position for “B500-J”, and (<b>b</b>) RMSD index values for “J” of “B500-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “SA” PZTs’ notation and position for “B500-J”, and (<b>b</b>) RMSD index values for “SA” of “B500-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “X” PZTs’ notation and position for “B500-J”, and (<b>b</b>) RMSD index values for “X” of “B500-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “J” PZTs’ notation and position for “B200a-J”, and (<b>b</b>) RMSD index values for “J” of “B200a-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “SA” PZTs’ notation and position for “B200a-J”, and (<b>b</b>) RMSD index values for “SA” of “B200a-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “X” PZTs’ notation and position for “B200a-J”, and (<b>b</b>) RMSD index values for “X” of “B200a-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “J” PZTs’ notation and position for “B200b-J”, and (<b>b</b>) RMSD index values for “J” of “B200b-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “SA” PZTs’ notation and position for “B200b-J”, and (<b>b</b>) RMSD index values for “SA” of “B200b-J”.</p>
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<p>(<b>a</b>) Cracking at failure and “X” PZTs’ notation and position for “B200b-J”, and (<b>b</b>) RMSD index values for “X” of “B200b-J”.</p>
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17 pages, 11505 KiB  
Article
Retrieval and Comparison of Multi-Satellite Polar Ozone Data from the EMI Series Instruments
by Kaili Wu, Ziqiang Xu, Yuhan Luo, Qidi Li, Kai Yu and Fuqi Si
Remote Sens. 2024, 16(19), 3619; https://doi.org/10.3390/rs16193619 - 28 Sep 2024
Viewed by 610
Abstract
The Environmental Trace Gases Monitoring Instrument (EMI) series are second-generation Chinese spectrometers on board the GaoFen-5 (GF-5) and DaQi-1 (DQ-1) satellites. In this study, a comparative analysis of EMI series data was conducted to determine the daily trend of ozone concentration changes owing [...] Read more.
The Environmental Trace Gases Monitoring Instrument (EMI) series are second-generation Chinese spectrometers on board the GaoFen-5 (GF-5) and DaQi-1 (DQ-1) satellites. In this study, a comparative analysis of EMI series data was conducted to determine the daily trend of ozone concentration changes owing to different transit times and to improve the overall quality and reliability of EMI series datasets. The daily EMI total ozone column (TOC) obtained using the Differential Optical Absorption Spectroscopy (DOAS) method were compared to vertical column density (VCD) gathered by the TROPOspheric Monitoring Instrument (TROPOMI). The results from October to November 2023 indicated a fine correlation (R = 0.98) between the daily EMI series data and a fine correlation (R ≥ 0.95) and spatial distribution closely resembling that of the TROPOMI TOCs. Furthermore, the EMI series data fusion results were highly correlated with TROPOMI TOCs (R = 0.99). Since the EMI series instruments had two different overpass times and the volume of available data at same pixel was increased by approximately three-fold, the temporal and spatial resolution was improved a lot. The results indicated that, compared to a single sensor, the EMI series DOAS TOCs generated more accurate and stable global TOC results and also enabled looking at the changes in the intraday TOCs. These outcomes highlight the potential of the EMI instruments for reliably monitoring the ozone variations in polar regions. Full article
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<p>A selected example of ozone DOAS fitting from EMI-DQ01 data on 10 December 2023. (<b>a</b>) Measured (red) and reference (blue) spectra; (<b>b</b>) measured and fitted ozone optical densities; and (<b>c</b>) EMI-DQ01 RMS values of the DOAS fitting.</p>
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<p>(<b>a</b>) Spatial distribution of the monthly mean global TOCs for the November 2023 EMI-GF5(01A) data; (<b>b</b>) spatial distribution of the monthly mean global TOCs for the November 2023 EMI-GF5(02) data; (<b>c</b>) spatial distribution of the monthly mean global TOCs for the November 2023 EMI-DQ01 data; (<b>d</b>) spatial distribution of the monthly mean global TOCs for the November 2023 TROPOMI data.</p>
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<p>(<b>a</b>–<b>c</b>) Global maps of relative differences between EMI-GF5(01A), EMI-DQ01, and EMI-GF5(02) with TROPOMI TOC.</p>
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<p>(<b>a</b>) Spatial distribution of the monthly mean Antarctic TOCs for the November 2023 EMI-GF5(01A) data; (<b>b</b>) spatial distribution of the monthly mean Antarctic TOCs for the November 2023 EMI-GF5(02) data; (<b>c</b>) spatial distribution of the monthly mean Antarctic TOC values for the November 2023 EMI-DQ01 data; (<b>d</b>) spatial distribution of the monthly mean Antarctic TOC values for the November 2023 TROPOMI data.</p>
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<p>(<b>a</b>) Linear fit between global EMI-GF5(01A) and TROPOMI TOCs for 30 November 2023; (<b>b</b>) linear fit between global EMI-GF5(02) and TROPOMI TOCs for 30 November 2023; (<b>c</b>) linear fit between global EMI-DQ01 and TROPOMI TOCs for 30 November 2023; (<b>d</b>) fit between global EMI-GF5(01A) and EMI-DQ01 TOCs for 30 November 2023.</p>
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<p>Analysis of the changes in the TOCs at several ground-based stations in the morning and afternoon from 20 November 2023 to 24 December 2023.</p>
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<p>Relative differences between the ground-based TOCs and those of the (<b>a</b>) EMI-GF5(02), (<b>b</b>) EMI-DQ01, and (<b>c</b>) EMI-GF5(01A) datasets.</p>
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<p>Comparison of time series of EMI-GF5 (01A), EMI-GF5 (02), and EMI-DQ01 and ground-based TOCs for several selected stations worldwide.</p>
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<p>(<b>a</b>) Spatial distributions of monthly average TOC fusion results for the EMI series datasets for November 2023; (<b>b</b>) linear fit between TOC fusion results for the EMI datasets and TROPOMI TOCs for November 2023; (<b>c</b>) differences between the TOC fusion results for the EMI datasets and TROPOMI TOCs for November 2023.</p>
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<p>The daily Antarctic TOCs on 30 November 2023 are derived from the EMI series and TROPOMI.</p>
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23 pages, 5748 KiB  
Article
Efficacy of PZT Sensors Network Different Configurations in Damage Detection of Fiber-Reinforced Concrete Prisms under Repeated Loading
by Maria C. Naoum, Nikos A. Papadopoulos, George M. Sapidis and Maristella E. Voutetaki
Sensors 2024, 24(17), 5660; https://doi.org/10.3390/s24175660 - 30 Aug 2024
Cited by 1 | Viewed by 710
Abstract
Real-time structural health monitoring (SHM) and accurate diagnosis of imminent damage are critical to ensure the structural safety of conventional reinforced concrete (RC) and fiber-reinforced concrete (FRC) structures. Implementations of a piezoelectric lead zirconate titanate (PZT) sensor network in the critical areas of [...] Read more.
Real-time structural health monitoring (SHM) and accurate diagnosis of imminent damage are critical to ensure the structural safety of conventional reinforced concrete (RC) and fiber-reinforced concrete (FRC) structures. Implementations of a piezoelectric lead zirconate titanate (PZT) sensor network in the critical areas of structural members can identify the damage level. This study uses a recently developed PZT-enabled Electro-Mechanical Impedance (EMI)-based, real-time, wireless, and portable SHM and damage detection system in prismatic specimens subjected to flexural repeated loading plain concrete (PC) and FRC. Furthermore, this research examined the efficacy of the proposed SHM methodology for FRC cracking identification of the specimens at various loading levels with different sensor layouts. Additionally, damage quantification using values of statistical damage indices is included. For this reason, the well-known conventional static metric of the Root Mean Square Deviation (RMSD) and the Mean Absolute Percentage Deviation (MAPD) were used and compared. This paper addresses a reliable monitoring experimental methodology in FRC to diagnose damage and predict the forthcoming flexural failure at early damage stages, such as at the onset of cracking. Test results indicated that damage assessment is successfully achieved using RMSD and MAPD indices of a strategically placed network of PZT sensors. Furthermore, the Upper Control Limit (UCL) index was adopted as a threshold for further sifting the scalar damage indices. Additionally, the proposed PZT-enable SHM method for prompt damage level is first established, providing the relationship between the voltage frequency response of the 32 PZT sensors and the crack propagation of the FRC prisms due to the step-by-step increased imposed load. In conclusion, damage diagnosis through continuous monitoring of PZTs responses of FRC due to flexural loading is a quantitative, reliable, and promising application. Full article
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<p>Fresh SFRC, including fibers.</p>
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<p>(<b>a</b>) Test set up, (<b>b</b>) loading sequence, and (<b>c</b>) WiAMS devices.</p>
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<p>Experimental behavior of the (<b>a</b>) PC and (<b>b</b>) SFRC specimens.</p>
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<p>Cracking pattern of tested specimens at failure: (<b>a</b>) Specimen 1; (<b>b</b>) Specimen 2; (<b>c</b>) Specimen 3; (<b>d</b>) Specimen 4.</p>
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<p>Cracking pattern of tested specimens at failure: (<b>a</b>) Specimen 1; (<b>b</b>) Specimen 2; (<b>c</b>) Specimen 3; (<b>d</b>) Specimen 4.</p>
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<p>Configuration and positions of the used PZT patches mounted to the FRC prisms: (<b>a</b>) Specimen 1; (<b>b</b>) Specimen 2; (<b>c</b>) Specimen 3; (<b>d</b>) Specimen 4.</p>
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<p>Specimen 1: Typical voltage frequency response of the PZT sensor BL.</p>
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<p>Damage assessment measurements considering (<b>a</b>) RMSD and (<b>b</b>) MAPD indices values of all PZTs of Specimen 1, and (<b>c</b>) cracking pattern of Specimen 1.</p>
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<p>Damage assessment measurements considering (<b>a</b>) RMSD and (<b>b</b>) MAPD indices values of all PZTs of Specimen 1, and (<b>c</b>) cracking pattern of Specimen 1.</p>
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<p>Specimen 2: Typical voltage frequency response of the PZT sensor BL.</p>
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<p>Damage assessment measurements considering (<b>a</b>) RMSD and (<b>b</b>) MAPD indices values of all PZTs of Specimen 2, and (<b>c</b>) cracking pattern of Specimen 2.</p>
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<p>Damage assessment measurements considering (<b>a</b>) RMSD and (<b>b</b>) MAPD indices values of all PZTs of Specimen 3, and (<b>c</b>) cracking pattern of Specimen 3.</p>
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<p>Specimen 3: Typical voltage frequency response of the PZT sensor FTM.</p>
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<p>Damage assessment measurements considering (<b>a</b>) RMSD and (<b>b</b>) MAPD indices values of all PZTs of Specimen 4, and (<b>c</b>) cracking pattern of Specimen 4.</p>
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<p>Specimen 4: Typical voltage frequency response of the PZT sensor BL.</p>
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14 pages, 4480 KiB  
Article
Nacre-like Anisotropic Multifunctional Aramid Nanofiber Composites for Electromagnetic Interference Shielding, Thermal Management, and Strain Sensing
by Jin Dong, Jing Lin, Hebai Zhang, Jun Wang, Ye Li, Kelin Pan, Haichen Zhang and Dechao Hu
Molecules 2024, 29(17), 4000; https://doi.org/10.3390/molecules29174000 - 23 Aug 2024
Viewed by 885
Abstract
Developing multifunctional flexible composites with high-performance electromagnetic interference (EMI) shielding, thermal management, and sensing capacity is urgently required but challenging for next-generation smart electronic devices. Herein, novel nacre-like aramid nanofibers (ANFs)-based composite films with an anisotropic layered microstructure were prepared via vacuum-assisted filtration [...] Read more.
Developing multifunctional flexible composites with high-performance electromagnetic interference (EMI) shielding, thermal management, and sensing capacity is urgently required but challenging for next-generation smart electronic devices. Herein, novel nacre-like aramid nanofibers (ANFs)-based composite films with an anisotropic layered microstructure were prepared via vacuum-assisted filtration and hot-pressing. The formed 3D conductive skeleton enabled fast electron and phonon transport pathways in the composite films. As a result, the composite films showed a high electrical conductivity of 71.53 S/cm and an outstanding thermal conductivity of 6.4 W/m·K when the mass ratio of ANFs to MXene/AgNWs was 10:8. The excellent electrical properties and multi-layered structure endowed the composite films with superior EMI shielding performance and remarkable Joule heating performance, with a surface temperature of 78.3 °C at a voltage of 2.5 V. Additionally, it was found that the composite films also exhibited excellent mechanical properties and outstanding flame resistance. Moreover, the composite films could be further designed as strain sensors, which show great promise in monitoring real-time signals for human motion. These satisfactory results may open up a new opportunity for EMI shielding, thermal management, and sensing applications in wearable electronic devices. Full article
(This article belongs to the Special Issue Recent Advances in Functional Composite Materials)
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<p>(<b>a</b>) The fabrication process of ANFs/MXene/AgNWs composite films. (<b>b</b>) A schematic diagram of the application of ANFs/MXene/AgNWs composite films in a wearable electronic device with excellent EMI shielding, thermal management, human motion monitoring, flame retardancy, and Joule heating abilities.</p>
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<p>(<b>a</b>) Surface and (<b>b</b>,<b>c</b>) cross-section SEM images of ANFs-4 films; insert corresponds to optical photograph of ANFs-4 films with bending. (<b>d</b>–<b>g</b>) EDS mapping images of fractured surfaces of ANFs-4 films. (<b>h</b>) XRD patterns of pure ANFs and ANFs/MXene/AgNWs films.</p>
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<p>(<b>a</b>) Tensile stress–strain curves and (<b>b</b>) electrical conductivity of ANFs/MXene/AgNWs films. (<b>c</b>) Total EMI SE and (<b>d</b>) SE<sub>R</sub>, SE<sub>T</sub>, and SE<sub>A</sub> of ANFs/MXene/AgNWs films.</p>
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<p>(<b>a</b>) Thermal conductivity and (<b>b</b>) schematic diagram of heat transfer model for ANFs/MXene/AgNWs composite films. (<b>c</b>,<b>d</b>) Surface temperature response of ANFs-8 films with different supplied voltages. (<b>e</b>) Surface temperature response of ANFs-8 films during five cycles at 2 V. (<b>f</b>) Long-term durability test of ANFs-8 films at 2 V.</p>
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<p>(<b>a</b>) TGA and (<b>b</b>) DTG curves of pure ANFs and ANFs/MXene/AgNWs composite films. (<b>c</b>) Digital images of burning behaviors of ANFs/MXene/AgNWs composite films.</p>
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<p>(<b>a</b>) A diagram of the sensor attached to the finger and wrist. (<b>b</b>,<b>c</b>) The resistance response of the sensor while monitoring the bending of the finger and wrist. (<b>d</b>–<b>f</b>) The resistance response of the sensor when monitoring the pronunciation of the words can, nature, and believe. (<b>g</b>) The resistance response of the sensor over 1000 s cyclic tests under 10° bending.</p>
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22 pages, 2292 KiB  
Article
Integrated Low Electromagnetic Interference Design Method for Small, Fixed-Wing UAVs for Magnetic Anomaly Detection
by Jiahao Ge, Jinwu Xiang and Daochun Li
Drones 2024, 8(8), 347; https://doi.org/10.3390/drones8080347 - 25 Jul 2024
Viewed by 1282
Abstract
Unmanned aerial vehicles (UAVs) equipped with magnetic airborne detectors (MADs) represent a new combination for underground or undersea magnetic anomaly detection. The electromagnetic interference (EMI) generated by a UAV platform affects the acquisition of weak magnetic signals by the MADs, which brings unique [...] Read more.
Unmanned aerial vehicles (UAVs) equipped with magnetic airborne detectors (MADs) represent a new combination for underground or undersea magnetic anomaly detection. The electromagnetic interference (EMI) generated by a UAV platform affects the acquisition of weak magnetic signals by the MADs, which brings unique conceptual design difficulties. This paper proposes a systematic and integrated low-EMI design method for small, fixed-wing UAVs. First, the EMI at the MAD is analyzed. Second, sensor layout optimization for a single UAV is carried out, and the criteria for the sensor layout are given. To enhance UAV stability and resist atmospheric disturbances at sea, the configuration is optimized using an improved genetic algorithm. Then, three typical multi-UAV formations are analyzed. Finally, the trajectory is designed based on an analysis of its influence on EMI at the MAD. The simulation results show that the low-EMI design can keep MADs away from the EMI sources of UAVs and maintain flight stability. The thread-like formation is the best choice in terms of mutual interference and search width. The results also reveal the close relationship between the low-EMI design and flight trajectory. This research can provide a reference for the conceptual design and trajectory optimization of small, fixed-wing UAVs for magnetic anomaly detection. Full article
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<p>Basic geometry of EMI and a UAV. (<b>a</b>) Geometry of the azimuth angles. (<b>b</b>) Geometric coupling relationship.</p>
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<p>Flight profile of a small, fixed-wing magnetic anomaly detection UAV.</p>
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<p>Design framework of a small, fixed-wing magnetic anomaly detection UAV.</p>
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<p>The process of MAD deployment.</p>
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<p>Diagram of DM-GA.</p>
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<p>Classic multi-UAV formations.</p>
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<p>Geometry of the formations.</p>
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<p>Configuration of a small, fixed-wing magnetic anomaly detection UAV.</p>
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<p>Fitting curve of engine mass.</p>
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<p>Relationship between UAV mass estimation, cruise duration, and payload mass.</p>
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<p>Relationship between UAV fuel mass ratio, cruise duration, and payload mass.</p>
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<p>Relationship between UAV structural mass ratio, cruise duration, and payload mass.</p>
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<p>Optimization process and results.</p>
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<p>Main aerodynamic parameters. (<b>a</b>) AoA-related parameters. (<b>b</b>) Lift-to-drag ratio and efficiency. (<b>c</b>) Sideslip angle-related parameters.</p>
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<p>Mutual interference analysis of MAD formation.</p>
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<p>Distribution of ocean magnetic field with height.</p>
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<p>Low EMI search trajectory design. (<b>a</b>) Effect of heading on EMI. (<b>b</b>) Search trajectory in “lawnmower” mode.</p>
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<p>Effect of pitch angle on EMI.</p>
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23 pages, 15975 KiB  
Article
Integrating the Capsule-like Smart Aggregate-Based EMI Technique with Deep Learning for Stress Assessment in Concrete
by Quoc-Bao Ta, Quang-Quang Pham, Ngoc-Lan Pham and Jeong-Tae Kim
Sensors 2024, 24(14), 4738; https://doi.org/10.3390/s24144738 - 21 Jul 2024
Cited by 3 | Viewed by 1132
Abstract
This study presents a concrete stress monitoring method utilizing 1D CNN deep learning of raw electromechanical impedance (EMI) signals measured with a capsule-like smart aggregate (CSA) sensor. Firstly, the CSA-based EMI measurement technique is presented by depicting a prototype of the CSA sensor [...] Read more.
This study presents a concrete stress monitoring method utilizing 1D CNN deep learning of raw electromechanical impedance (EMI) signals measured with a capsule-like smart aggregate (CSA) sensor. Firstly, the CSA-based EMI measurement technique is presented by depicting a prototype of the CSA sensor and a 2 degrees of freedom (2 DOFs) EMI model for the CSA sensor embedded in a concrete cylinder. Secondly, the 1D CNN deep regression model is designed to adapt raw EMI responses from the CSA sensor for estimating concrete stresses. Thirdly, a CSA-embedded cylindrical concrete structure is experimented with to acquire EMI responses under various compressive loading levels. Finally, the feasibility and robustness of the 1D CNN model are evaluated for noise-contaminated EMI data and untrained stress EMI cases. Full article
(This article belongs to the Special Issue Feature Papers in Fault Diagnosis & Sensors 2024)
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<p>Prototype of CSA sensor (dimensions in mm).</p>
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<p>CSA-based EMI measurement 2 DOFs model for concrete structure: (<b>a</b>) CSA-embedded concrete structure; (<b>b</b>) 2 DOFs model.</p>
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<p>Behavior of CSA sensor in x-direction embedded in concrete cylinder under compression.</p>
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<p>Diagram of 1D CNN stress estimation model using CSA’s EMI signals.</p>
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<p>Architecture of 1D CNN stress estimation model using EMI signals [<a href="#B24-sensors-24-04738" class="html-bibr">24</a>].</p>
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<p>Data configuration for noise-contaminated EMI cases.</p>
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<p>Data configuration for untrained stress-EMI cases.</p>
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<p>CSA prototype (dimensions in mm): (<b>a</b>) CSA sensor’s components; (<b>b</b>) Fabricated CSA.</p>
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<p>Fabrication of CSA-embedded concrete cylinder (dimensions in mm).</p>
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<p>Testing setup for EMI measuring from x-CSA-embedded concrete cylinder under compression.</p>
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<p>Applied loading history on x-CSA-embedded cylinder.</p>
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<p>EMI responses (in average of ensembles) of CSA in cylinder under applied stresses S<sub>0–8</sub>: (<b>a</b>) S<sub>0</sub>; (<b>b</b>) S<sub>1</sub>; (<b>c</b>) S<sub>2</sub>; (<b>d</b>) S<sub>3</sub>; (<b>e</b>) S<sub>4</sub>; (<b>f</b>) S<sub>5</sub>; (<b>g</b>) S<sub>6</sub>; (<b>h</b>) S<sub>7</sub>; (<b>i</b>) S<sub>8</sub>.</p>
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<p>EMI responses (in average of ensembles) of CSA in cylinder under applied stresses S<sub>0</sub>–S<sub>8</sub>.</p>
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<p>Visual observation of cylinder during loading steps S<sub>0</sub>–S<sub>8</sub>.</p>
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<p>EMI features of x-CSA under applied stresses: (<b>a</b>) RMSE; (<b>b</b>) CCD.</p>
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<p>Visualization of labeled EMI data in training set.</p>
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<p>Example of noise-contaminated EMI signals under stress level S<sub>1</sub> in testing set: (<b>a</b>) 2%; (<b>b</b>) 4%; (<b>c</b>) 6%; (<b>d</b>) 8%; (<b>e</b>) 10%; (<b>f</b>) 12%; (<b>g</b>) 14%; (<b>h</b>) 16%.</p>
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<p>Loss values after 100 epochs.</p>
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<p>(<b>a</b>) 0%; (<b>b</b>) 2%; (<b>c</b>) 4%; (<b>d</b>) 6%; (<b>e</b>) 8%; (<b>f</b>) 10%; (<b>g</b>) 12%; (<b>h</b>) 14%; (<b>i</b>) 16%.</p>
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<p>(<b>a</b>) 0%; (<b>b</b>) 2%; (<b>c</b>) 4%; (<b>d</b>) 6%; (<b>e</b>) 8%; (<b>f</b>) 10%; (<b>g</b>) 12%; (<b>h</b>) 14%; (<b>i</b>) 16%.</p>
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<p>RMSE error under noise levels: (<b>a</b>) levels of noise 0–5% (trained levels); (<b>b</b>) levels of noise 6–16% (untrained levels).</p>
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<p>Training data in untrained cases: (<b>a</b>) untrained case 1 (excluded stress S<sub>2</sub>); (<b>b</b>) untrained case 2 (excluded stress S<sub>2</sub> and S<sub>4</sub>).</p>
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<p>Example of noise-added EMI signals under stress level S<sub>1</sub> in testing set: (<b>a</b>) 0%; (<b>b</b>) 1%; (<b>c</b>) 2%; (<b>d</b>) 3%; (<b>e</b>) 4%; (<b>f</b>) 5%.</p>
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<p>Loss values for untrained cases: (<b>a</b>) case 1 (excluded stress S<sub>2</sub>); (<b>b</b>) case 2 (excluded stress S<sub>2</sub> and S<sub>4</sub>); (<b>c</b>) case 3 (excluded stress S<sub>2</sub>, S<sub>4</sub>, and S<sub>6</sub>); (<b>d</b>) case 4 (excluded stress S<sub>2</sub>, S<sub>4</sub>, S<sub>6</sub>, and S<sub>8</sub>).</p>
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<p>Stress estimation for untrained case 1 (excluded stress S<sub>2</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 1% noise; (<b>c</b>) 2% noise; (<b>d</b>) 3% noise; (<b>e</b>) 4% noise; (<b>f</b>) 5% noise.</p>
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<p>Stress estimation for untrained case 2 (excluded stress S<sub>2</sub> and S<sub>4</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 1% noise; (<b>c</b>) 2% noise; (<b>d</b>) 3% noise; (<b>e</b>) 4% noise; (<b>f</b>) 5% noise.</p>
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<p>Stress estimation for untrained case 2 (excluded stress S<sub>2</sub> and S<sub>4</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 1% noise; (<b>c</b>) 2% noise; (<b>d</b>) 3% noise; (<b>e</b>) 4% noise; (<b>f</b>) 5% noise.</p>
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<p>Stress estimation for untrained case 3 (excluded stress S<sub>2</sub>, S<sub>4</sub>, and S<sub>6</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 1% noise; (<b>c</b>) 2% noise; (<b>d</b>) 3% noise; (<b>e</b>) 4% noise; (<b>f</b>) 5% noise.</p>
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<p>Stress estimation for untrained case 4 (excluded stress S<sub>2</sub>, S<sub>4</sub>, S<sub>6</sub>, and S<sub>8</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 1% noise; (<b>c</b>) 2% noise; (<b>d</b>) 3% noise; (<b>e</b>) 4% noise; (<b>f</b>) 5% noise.</p>
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<p>Stress estimation for untrained case 4 (excluded stress S<sub>2</sub>, S<sub>4</sub>, S<sub>6</sub>, and S<sub>8</sub>): (<b>a</b>) 0% noise; (<b>b</b>) 1% noise; (<b>c</b>) 2% noise; (<b>d</b>) 3% noise; (<b>e</b>) 4% noise; (<b>f</b>) 5% noise.</p>
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<p>RMSE error in untrained cases: (<b>a</b>) untrained case 1 (excluded stress S<sub>2</sub>); (<b>b</b>) untrained case 2 (excluded stress S<sub>2</sub> and S<sub>4</sub>); (<b>c</b>) untrained case 3 (excluded stress S<sub>2</sub>, S<sub>4</sub>, and S<sub>6</sub>); (<b>d</b>) untrained case 4 (excluded stress S<sub>2</sub>, S<sub>4</sub>, S<sub>6</sub>, and S<sub>8</sub>).</p>
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17 pages, 3530 KiB  
Review
Application of Long-Period Fiber Grating Sensors in Structural Health Monitoring: A Review
by Ying Zhuo, Pengfei Ma, Pu Jiao and Xinzhe Yuan
CivilEng 2024, 5(3), 559-575; https://doi.org/10.3390/civileng5030030 - 13 Jul 2024
Viewed by 1509
Abstract
Structural health monitoring (SHM) is crucial for preventing and detecting corrosion, leaks, and other risks in reinforced concrete (RC) structures, ensuring environmental safety and structural integrity. Optical fiber sensors (OFS), particularly long-period fiber gratings (LPFG), have emerged as a promising method for SHM. [...] Read more.
Structural health monitoring (SHM) is crucial for preventing and detecting corrosion, leaks, and other risks in reinforced concrete (RC) structures, ensuring environmental safety and structural integrity. Optical fiber sensors (OFS), particularly long-period fiber gratings (LPFG), have emerged as a promising method for SHM. Various LPFG sensors have been widely used in SHM due to their high sensitivity, durability, immunity to electromagnetic interference (EMI) and compact size. This review explores recent advancements in LPFG sensors and offers insights into their potential applications in SHM. Full article
(This article belongs to the Collection Recent Advances and Development in Civil Engineering)
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<p>Sensing principle of an LPFG sensor.</p>
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<p>Schematic setup for LPFG fabrication by a CO<sub>2</sub> laser.</p>
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<p>Schematic setup for LPFG fabrication by the EAD method.</p>
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<p>Schematic setup for the simultaneous measurement of strain and temperature.</p>
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<p>Schematic setup for the LPFG-based RH sensors [<a href="#B44-civileng-05-00030" class="html-bibr">44</a>].</p>
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<p>Structure of the PI-coated LPFG RH sensor with a silver mirror at the end.</p>
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<p>Schematic diagram of the SILPG Michelson Interferometer.</p>
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<p>Experimental setup of the corrosion sensors proposed by H. Liu [<a href="#B75-civileng-05-00030" class="html-bibr">75</a>].</p>
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<p>Schematic diagram of an LPFG corrosion sensor coated with nano iron/silica particles [<a href="#B76-civileng-05-00030" class="html-bibr">76</a>].</p>
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<p>A general design of Fe-C-coated LPFG sensors.</p>
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19 pages, 4925 KiB  
Article
Experimental Study on the Detection of the Existence and Location of Mimicked and Unexpected Interface Debonding Defects in an Existing Rectangular CFST Column with PZT Materials
by Qian Liu, Bin Xu, Genda Chen, Weilong Ni, Zhixun Liu, Chun Lin and Zhiyou Zhuang
Materials 2024, 17(13), 3154; https://doi.org/10.3390/ma17133154 - 27 Jun 2024
Cited by 1 | Viewed by 667
Abstract
Interface bonding conditions between concrete and steel materials play key roles in ensuring the composite effect and load-carrying capacity of concrete–steel composite structures such as concrete-filled steel tube (CFST) members in practice. A method using both surface wave and electromechanical impedance (EMI) measurement [...] Read more.
Interface bonding conditions between concrete and steel materials play key roles in ensuring the composite effect and load-carrying capacity of concrete–steel composite structures such as concrete-filled steel tube (CFST) members in practice. A method using both surface wave and electromechanical impedance (EMI) measurement for detecting the existence and the location of inaccessible interface debonding defects between the concrete core and steel tube in CFST members using piezoelectric lead zirconate titanate (PZT) patches as actuators and sensors is proposed. A rectangular CFST specimen with two artificially mimicked interface debonding defects was experimentally verified using PZT patches as the actuator and sensor. By comparing the surface wave measurement of PZT sensors at different surface wave travelling paths under both a continuous sinusoidal signal and a 10-period sinusoidal windowed signal, three potential interface debonding defects are quickly identified. Furthermore, the accurate locations of the three detected potential interface debonding defects are determined with the help of EMI measurements from a number of additional PZT sensors around the three potential interface debonding defects. Finally, the accuracy of the proposed interface debonding detection method is verified with a destructive observation by removing the local steel tube at the three detected interface debonding locations. The observation results show that the three detected interface debonding defects are two mimicked interface debonding defects, and an unexpected debonding defect occurred spontaneously due to concrete shrinkage in the past one and a half years before conducting the test. Results in this study indicate that the proposed method can be an efficient and accurate approach for the detection of unknown interface debonding defects in existing CFST members. Full article
(This article belongs to the Section Construction and Building Materials)
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<p>Propagation characteristics of stress waves in CFST based on stress wave detection method.</p>
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<p>EMI measuring system for 1D PZT-structure coupling model.</p>
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<p>Artificially mimicked interface debonding defects in CFST specimen (<b>a</b>) Acrylic plate with groove; (<b>b</b>) Mimicked interfacial debonding defects.</p>
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<p>The rectangular CFST column and arrangement of PZT sensors (unit: mm). (<b>a</b>) Rectangular CFST member; (<b>b</b>) Arrangement of PZT sensors.</p>
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<p>The rectangular CFST column and arrangement of PZT sensors (unit: mm). (<b>a</b>) Rectangular CFST member; (<b>b</b>) Arrangement of PZT sensors.</p>
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<p>Test system for surface wave measurement.</p>
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<p>The output voltage signals corresponding to different surface wave travelling paths under continuous sinusoidal signal: (<b>a</b>) Path 1–5; (<b>b</b>) Path 1–2; (<b>c</b>) Path 2–3; (<b>d</b>) Path 3–4; (<b>e</b>) Path 4–5.</p>
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<p>The output voltage signals corresponding to different surface wave travelling paths under a10-period sinusoidal windowed signal: (<b>a</b>) Path 1–5; (<b>b</b>) Path 1–2; (<b>c</b>) Path 2–3; (<b>d</b>) Path 3–4; (<b>e</b>) Path 4–5.</p>
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<p>Additional PZT sensors arrangement.</p>
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<p>Test setup based on EMI technology.</p>
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<p>Selection of impedance frequency band (B4–5).</p>
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<p>The impedance of PZT sensors at different measurement points: (<b>a</b>) Measurement points A1–2~D1–2; (<b>b</b>) Measurement points A2–3~D2–3; (<b>c</b>) Measurement points A4–5~D4–5.</p>
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<p>Destructive observation on the detected interface debonding defects by removing local steel tube treatment of detected defect locations: (<b>a</b>) Location of measurement point C1–2; (<b>b</b>) Location of measurement point D2–3; (<b>c</b>) Location of measurement point A4–5.</p>
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17 pages, 5044 KiB  
Article
Design, Development and Application of a Modular Electromagnetic Induction (EMI) Sensor for Near-Surface Geophysical Surveys
by Luzian Wolf and Adrian Flores Orozco
Sensors 2024, 24(13), 4159; https://doi.org/10.3390/s24134159 - 26 Jun 2024
Viewed by 1859
Abstract
Low-frequency electromagnetic induction (EMI) is a non-invasive geophysical method that is based on the induction of electromagnetic (EM) waves into the subsurface to quantify changes in electrical conductivity. In this study, we present an open (design details and software are accessible) and modular [...] Read more.
Low-frequency electromagnetic induction (EMI) is a non-invasive geophysical method that is based on the induction of electromagnetic (EM) waves into the subsurface to quantify changes in electrical conductivity. In this study, we present an open (design details and software are accessible) and modular system for the collection of EMI data. The instrument proposed allows for the separations between the transmitter to be adjusted and up to four receiving antennas as well as the acquisition frequency (in the range between 3 and 50 kHz) to permit measurements with variable depth of investigation. The sensor provides access to raw data and the software described in this study allows control of the signal processing chain. The design specifications permit apparent conductivity measurements in the range of between 1 mS/m and 1000 mS/m, with a resolution of 1.0 mS/m and with a sampling rate of up to 10 samples per second. The sensor allows for a synchronous acquisition of a time stamp and a location stamp for each data sample. The sensor has a mass of less than 5 kg, is portable and suitable for one-person operation, provides 4 h of operation time on one battery charge, and provides sufficient rigidity for practical field operations. Full article
(This article belongs to the Special Issue Sensors and Geophysical Electromagnetics)
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Graphical abstract

Graphical abstract
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<p>Hardware design of the Modular EMI System: The sensor comprises a variety of components that can be grouped in three sections: (1) the transmitter (<b>left-side</b>), (2) the receiver (<b>right-side</b>), and (3) software for processing and managing of the recorded data (<b>bottom left</b>). The label ‘V<sub>CC</sub>’ indicates the positive supply voltage input of sub-systems, ‘UART’ (Universal Asynchronous Receiver/Transmitter) indicates an asynchronous bi-directional serial communication port, ‘I2C’ (Inter-Integrated Circuit) indicates a standardized two-wire communication port between electronic components, ‘SPI’ (Serial Peripheral Interface) indicates a three-wire synchronous serial communication port between electronic components, and ‘WLAN’ (Wireless Local Area Network) is a network connection for system extensions.</p>
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<p>The proposed MEMIS: (<b>a</b>) schematic diagram explaining the main components and the dimensions; (<b>b</b>) picture of the device.</p>
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<p>Pictures of the electronic sub-system: (<b>a</b>) receiver coil antenna; (<b>b</b>) assembled signal generator, amplifier, recorder, GPS unit, IMU, and battery.</p>
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<p>Exemplary signal records, corresponding to 25 milliseconds of data in an eight-channel wav. file. Traces Rx-1 to Rx-4 show the analog signals originating from the receiver antennas, Tx-Mon the analog signal from the transmitter monitor, IMU the data stream from the inertial motion unit, and GPS and TP the digital NMEA data stream and the time pulse signal from the GPS unit. The amplitudes of the signals are determined during post-processing by combining recorded values with recorder gain and calibration parameters.</p>
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<p>Exemplary format of the NMEA message sent by the GPS unit: (<b>a</b>) standard NMEA message; (<b>b</b>) framing of 1 byte.</p>
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<p>Amplitude values of the Fast Fourier Transform (FFT) of a data segment containing 100 ms of data. The plot shows a distinct peak at 10 kHz, which corresponds to the frequency of the primary magnetic field.</p>
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<p>Apparent electrical conductivity (mS/m) measured along a 400 m long line in the shore of the lake Neusiedlersee. Measurements were performed with (<b>a</b>) the proposed MEMIS and (<b>b</b>) the CMD-Mini-Explorer from GF-instruments.</p>
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<p>Apparent electrical conductivity (mS/m) of a 25 m × 25 m mapping area located on the shoreline of the ‘Apetloner Meierhoflacke’. The measurement locations are presented to the left (<b>a</b>), with the <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>σ</mi> </mrow> <mrow> <mi>a</mi> </mrow> </msub> </mrow> </semantics></math> obtained with the (<b>b</b>) MEMIS (coil separation 170 cm) and (<b>c</b>), the CMD Explorer (coil separation 148 cm).</p>
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<p>Apparent electrical conductivity (mS/m) of the 25 m × 25 m mapping area shown in <a href="#sensors-24-04159-f008" class="html-fig">Figure 8</a> above, measured with the MEMIS at different transmitter-receiver coil separations: (<b>a</b>) coil separation 90 cm; (<b>b</b>) coil separation 170 cm; and (<b>c</b>) coil separation 370 cm.</p>
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10 pages, 2329 KiB  
Communication
Estimating Hardness of Cosmetic Cream Using Electro-Mechanical Impedance Sensing Technique
by Jun-Cheol Lee, Dan-Hee Yoo and In-Chul Lee
Appl. Sci. 2024, 14(3), 1110; https://doi.org/10.3390/app14031110 - 29 Jan 2024
Viewed by 1041
Abstract
This study investigates the application of electro-mechanical impedance (EMI) sensing technology to evaluate the hardness of cosmetic creams. Traditional methods, like penetration resistance testing, can be intrusive and disrupt continuous monitoring by impacting internal structures. To overcome this limitation, a piezoelectric sensor is [...] Read more.
This study investigates the application of electro-mechanical impedance (EMI) sensing technology to evaluate the hardness of cosmetic creams. Traditional methods, like penetration resistance testing, can be intrusive and disrupt continuous monitoring by impacting internal structures. To overcome this limitation, a piezoelectric sensor is embedded in cosmetic creams to capture EMI signals. This experiment explores varying wax content levels in the creams, establishing correlations between conventional hardness values and EMI signals. The results demonstrate a positive relationship between wax content, hardness values, and the magnitude of EMI resonance peaks. This study emphasizes a robust correlation between established hardness metrics and EMI signals, showcasing the potential of non-destructive testing to drive advancements in cosmetic industry practices. Full article
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<p>Piezoelectric sensor: structure model using dynamic approach method.</p>
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<p>Piezoelectric sensor used in this study.</p>
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<p>Test setup for measuring EMI of piezoelectric sensor.</p>
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<p>EMI signal of piezoelectric sensor in air.</p>
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<p>Hardness values according to wax content of cosmetic cream using texture analyzer.</p>
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<p>EMI signal change of piezoelectric sensor according to wax content of cosmetic cream: (<b>a</b>) Plain, (<b>b</b>) 2%, (<b>c</b>) 4%, (<b>d</b>) 6%, and (<b>e</b>) 8%.</p>
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<p>EMI resonance peak magnitude according to wax content of cosmetic cream.</p>
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<p>Correlation between the hardness value and EMI resonance peak magnitude of cosmetic cream.</p>
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