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Search Results (3,331)

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Keywords = noise control

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24 pages, 28615 KiB  
Article
Modal Parameter Identification of Jacket-Type Offshore Wind Turbines Under Operating Conditions
by Chen Zhang, Xu Han, Chunhao Li, Bernt Johan Leira, Svein Sævik, Dongzhe Lu, Wei Shi and Xin Li
J. Mar. Sci. Eng. 2024, 12(11), 2083; https://doi.org/10.3390/jmse12112083 - 18 Nov 2024
Abstract
Operational modal analysis (OMA) is essential for long-term health monitoring of offshore wind turbines (OWTs), helping identifying changes in structural dynamic characteristics. OMA has been applied under parked or idle states for OWTs, assuming a linear and time-invariant dynamic system subjected to white [...] Read more.
Operational modal analysis (OMA) is essential for long-term health monitoring of offshore wind turbines (OWTs), helping identifying changes in structural dynamic characteristics. OMA has been applied under parked or idle states for OWTs, assuming a linear and time-invariant dynamic system subjected to white noise excitations. The impact of complex operating environmental conditions on structural modal identification therefore requires systematic investigation. This paper studies the applicability of OMA based on covariance-driven stochastic subspace identification (SSI-COV) under various non-white noise excitations, using a DTU 10 MW jacket OWT model as a basis for a case study. Then, a scaled (1:75) 10 MW jacket OWT model test is used for the verification. For pure wave conditions, it is found that accurate identification for the first and second FA/SS modes can be achieved with significant wave energy. Under pure wind excitations, the unsteady servo control behavior leads to significant identification errors. The combined wind and wave actions further complicate the picture, leading to more scattered identification errors. The SSI-COV based modal identification method is suggested to be reliably applied for wind speeds larger than the rated speed and with sufficient wave energy. In addition, this method is found to perform better with larger misalignment of wind and wave directions. This study provides valuable insights in relation to the engineering applications of in situ modal identification techniques under operating conditions in real OWT projects. Full article
(This article belongs to the Topic Wind, Wave and Tidal Energy Technologies in China)
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<p>Illustration of the considered jacket OWT.</p>
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<p>The 3D turbulent wind map at a turbulence level of 18.75% simulated by Turbsim.</p>
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<p>Rotor speed time history at a wind speed of 9.5 m/s.</p>
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<p>Average rotor speed and variance of the rotor speed over different wind speeds.</p>
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<p>Acceleration response signals in FA and SS directions excited by a white noise spectrum.</p>
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<p>Stabilization diagram using 10 min acceleration response in the FA direction of the OWT when excited by white noise.</p>
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<p>Clustering results of the stable points under a white noise condition.</p>
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<p>The first two reference mode shapes in FA/SS directions.</p>
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<p>The identified first FA and SS modes for irregular wave conditions: (<b>a</b>) the natural frequency, and (<b>b</b>) the MAC. Note that the gradient color bars represent variations in Tp from 6.5 s to 17 s in the irregular wave excitation conditions, the blue color indicates FA, and the red color is SS.</p>
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<p>The second FA/SS modes for irregular wave conditions: (<b>a</b>) the second natural frequency, (<b>b</b>) the second MAC, and (<b>c</b>) the relative frequency error. Note that the gradient bars represent variations in Tp from 6.5 s to 17 s for the pure wave excitation conditions, the blue color indicates FA, and the red color is SS.</p>
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<p>Stabilization diagram using the 10 min of a condition where Hs is 0.5 m, Tp is 10.5 s.</p>
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<p>Clustering results of the stable points under a condition where Hs is 0.5 m, Tp is 10.5 s.</p>
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<p>The first FA/SS modes for turbulent wind conditions: (<b>a</b>) the first natural frequency, (<b>b</b>) the first MAC.</p>
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<p>The identified harmonic frequencies for turbulent wind conditions.</p>
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<p>The identified second modes for different turbulent wind conditions: (<b>a</b>) second frequency, (<b>b</b>) second MAC.</p>
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<p>The first frequency at different Hs for combined wave and wind conditions. Note that the gradient bars represent variations in Tp from 6.5 s to 17 s, the blue color indicates FA, and the red color is SS.</p>
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<p>The first MAC at different Hs for combined wave and wind conditions. Note that the gradient bars represent variations in Tp from 6.5 s to 17 s, the blue color indicates FA, and the red color is SS.</p>
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<p>The second frequency at different Hs for combined wave and wind conditions. Note that the gradient bars represent variations in Tp from 6.5 s to 17 s, the blue color indicates FA, and the red color is SS.</p>
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<p>The second MAC at different Hs for combined wave and wind conditions. Note that the gradient bars represent variations in Tp from 6.5 s to 17 s, the blue color indicates FA, and the red color is SS.</p>
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<p>The first two modes of OWT by combined wave and wind conditions under different noise levels.</p>
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<p>The first frequency for variation in wave directions, while at a wind direction of 0°.</p>
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<p>The second frequency for variation in wave directions, for a constant wind direction of 0°.</p>
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<p>The test configurations.</p>
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<p>Modal parameter identification results for the scale test.</p>
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25 pages, 10177 KiB  
Article
Forecasting Gate-Front Water Levels Using a Coupled GRU–TCN–Transformer Model and Permutation Entropy Algorithm
by Jiwei Zhao, Taotao He, Luyao Wang and Yaowen Wang
Water 2024, 16(22), 3310; https://doi.org/10.3390/w16223310 - 18 Nov 2024
Abstract
Water level forecasting has significant impacts on transportation, agriculture, and flood control measures. Accurate water level values can enhance the safety and efficiency of water conservancy hub operation scheduling, reduce flood risks, and are essential for ensuring sustainable regional development. Addressing the nonlinearity [...] Read more.
Water level forecasting has significant impacts on transportation, agriculture, and flood control measures. Accurate water level values can enhance the safety and efficiency of water conservancy hub operation scheduling, reduce flood risks, and are essential for ensuring sustainable regional development. Addressing the nonlinearity and non-stationarity characteristics of gate-front water level sequences, this paper introduces a gate-front water level forecasting method based on a GRU–TCN–Transformer coupled model and permutation entropy (PE) algorithm. Firstly, an analysis method combining Singular Spectrum Analysis (SSA) and Complete Ensemble Empirical Mode Decomposition with Adaptive Noise (CEEMDAN) is used to separate the original water level data into different frequency modal components. The PE algorithm subsequently divides each modal component into sequences of high and low frequencies. The GRU model is applied to predict the high-frequency sequence part, while the TCN–Transformer combination model is used for the low-frequency sequence part. The forecasting from both models are combined to obtain the final water level forecasting value. Multiple evaluation metrics are used to assess the forecasting performance. The findings indicate that the combined GRU–TCN–Transformer model achieves a Mean Absolute Error (MAE) of 0.0154, a Root Mean Square Error (RMSE) of 0.0205, and a Coefficient of Determination (R2) of 0.8076. These metrics indicate that the model outperforms machine learning Support Vector Machine (SVM) models, GRU models, Transformer models, and TCN–Transformer combination models in forecasting performance. The forecasting results have high credibility. This model provides a new reference for improving the accuracy of gate-front water level forecasting and offers significant insights for water resource management and flood prevention, demonstrating promising application prospects. Full article
(This article belongs to the Topic Water and Energy Monitoring and Their Nexus)
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<p>Structure of the basic GRU unit.</p>
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<p>TCN network modules: (<b>left</b>) cell structure details; (<b>center</b>) residual block 1; (<b>right</b>) residual block 2.</p>
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<p>Transformer model structure.</p>
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<p>TCN–Transformer coupled model structure.</p>
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<p>Architecture of the coupled GRU–TCN–Transformer framework.</p>
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<p>Geographic location map of Mengcheng.</p>
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<p>Schematic diagram of the Mengcheng hub layout.</p>
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<p>Pre-gate level data.</p>
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<p>Mann–Kendall test result chart for upstream water level data.</p>
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<p>SSA decomposition of upstream water level data. (<b>a</b>) fluctuation diagram of IMF2-5 after SSA decomposition of upstream water level data. (<b>b</b>) overall SSA decomposition diagram of upstream water level data.</p>
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<p>SSA decomposition of upstream water level data. (<b>a</b>) fluctuation diagram of IMF2-5 after SSA decomposition of upstream water level data. (<b>b</b>) overall SSA decomposition diagram of upstream water level data.</p>
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<p>CEEMDAN decomposition of upstream water level reconstruction data.</p>
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<p>ACF and PACF plots of upstream water levels.</p>
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<p>Results of entropy calculations for upstream water level alignments.</p>
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<p>Upstream water level GRU–TCN–Transformer coupled model forecasting vs. validation set data.</p>
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<p>Upstream water level forecasting model fits scatter plots.</p>
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<p>Comparison of different model evaluation indicators.</p>
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18 pages, 903 KiB  
Article
Robustness of Deep-Learning-Based RF UAV Detectors
by Hilal Elyousseph and Majid Altamimi
Sensors 2024, 24(22), 7339; https://doi.org/10.3390/s24227339 (registering DOI) - 17 Nov 2024
Viewed by 417
Abstract
The proliferation of low-cost, small radar cross-section UAVs (unmanned aerial vehicles) necessitates innovative solutions for countering them. Since these UAVs typically operate with a radio control link, a promising defense technique involves passive scanning of the radio frequency (RF) spectrum to detect UAV [...] Read more.
The proliferation of low-cost, small radar cross-section UAVs (unmanned aerial vehicles) necessitates innovative solutions for countering them. Since these UAVs typically operate with a radio control link, a promising defense technique involves passive scanning of the radio frequency (RF) spectrum to detect UAV control signals. This approach is enhanced when integrated with machine-learning (ML) and deep-learning (DL) methods. Currently, this field is actively researched, with various studies proposing different ML/DL architectures competing for optimal accuracy. However, there is a notable gap regarding robustness, which refers to a UAV detector’s ability to maintain high accuracy across diverse scenarios, rather than excelling in just one specific test scenario and failing in others. This aspect is critical, as inaccuracies in UAV detection could lead to severe consequences. In this work, we introduce a new dataset specifically designed to test for robustness. Instead of the existing approach of extracting the test data from the same pool as the training data, we allowed for multiple categories of test data based on channel conditions. Utilizing existing UAV detectors, we found that although coefficient classifiers have outperformed CNNs in previous works, our findings indicate that image classifiers exhibit approximately 40% greater robustness than coefficient classifiers under low signal-to-noise ratio (SNR) conditions. Specifically, the CNN classifier demonstrated sustained accuracy in various RF channel conditions not included in the training set, whereas the coefficient classifier exhibited partial or complete failure depending on channel characteristics. Full article
(This article belongs to the Section Sensors and Robotics)
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<p>Market study breakdown of counter-UAV techniques [<a href="#B1-sensors-24-07339" class="html-bibr">1</a>].</p>
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<p>Block diagram of UAV detection via passive RF scanning and ML/DL techniques.</p>
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<p>Example training data, showing the UAV control signal isolated between dotted black lines.</p>
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<p>Hardware and software setup along with UAV controller.</p>
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<p>Examples from the test dataset. The UAV signal is present at the right edge of the bottom two images, showing three peaks which decay with distance.</p>
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<p>Robustness scores for low SNR performance.</p>
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<p>Accuracy Plots for different UAV test categories.</p>
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13 pages, 3354 KiB  
Article
On-Line Parameter Identification and SOC Estimation for Lithium-Ion Batteries Based on Improved Sage–Husa Adaptive EKF
by Xuan Tang, Hai Huang, Xiongwu Zhong, Kunjun Wang, Fang Li, Youhang Zhou and Haifeng Dai
Energies 2024, 17(22), 5722; https://doi.org/10.3390/en17225722 - 15 Nov 2024
Viewed by 248
Abstract
For the Battery Management System (BMS) to manage and control the battery, State of Charge (SOC) is an important battery performance indicator. In order to identify the parameters of the LiFePO4 battery, this paper employs the forgetting factor recursive least squares (FFRLS) [...] Read more.
For the Battery Management System (BMS) to manage and control the battery, State of Charge (SOC) is an important battery performance indicator. In order to identify the parameters of the LiFePO4 battery, this paper employs the forgetting factor recursive least squares (FFRLS) method, which considers the computational volume and model correctness, to determine the parameters of the LiFePO4 battery. On this basis, the two resistor-capacitor equivalent circuit model is selected for estimating the SOC of the Li-ion battery by combining the extended Kalman filter (EKF) with the Sage–Husa adaptive algorithm. The positivity is improved by modifying the system noise estimation matrix. The paper concludes with a MATLAB 2016B simulation, which serves to validate the SOC estimation algorithm. The results demonstrate that, in comparison to the conventional EKF, the enhanced EKF exhibits superior estimation precision and resilience to interference, along with enhanced convergence during the estimation process. Full article
(This article belongs to the Special Issue Electric Vehicles for Sustainable Transport and Energy: 2nd Edition)
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<p>Global electric car stock trends from 2010 to 2023 [<a href="#B1-energies-17-05722" class="html-bibr">1</a>].</p>
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<p>2RC equivalent circuit model.</p>
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<p>HPPC test. (<b>A</b>) Voltage. (<b>B</b>) Current.</p>
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<p>OCV-SOC fitting curve.</p>
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<p>In pulse discharge mode, the voltage comparison and its error curve are as follows: (<b>A</b>) voltage comparison, (<b>B</b>) error curve.</p>
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<p>Schematic of SOC online estimation.</p>
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<p>Curves of each algorithm versus real SOC.</p>
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<p>Error curves of each algorithm with respect to real SOC.</p>
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18 pages, 6433 KiB  
Article
High-Performance Telescope System Design for Space-Based Gravitational Waves Detection
by Huiru Ji, Lujia Zhao, Zichao Fan, Rundong Fan, Jiamin Cao, Yan Mo, Hao Tan, Zhiyu Jiang and Donglin Ma
Sensors 2024, 24(22), 7309; https://doi.org/10.3390/s24227309 - 15 Nov 2024
Viewed by 260
Abstract
Space-based gravitational wave (GW) detection employs the Michelson interferometry principle to construct ultra-long baseline laser interferometers in space for detecting GW signals with a frequency band of 10−4–1 Hz. The spaceborne telescope, as a core component directly integrated into the laser [...] Read more.
Space-based gravitational wave (GW) detection employs the Michelson interferometry principle to construct ultra-long baseline laser interferometers in space for detecting GW signals with a frequency band of 10−4–1 Hz. The spaceborne telescope, as a core component directly integrated into the laser link, comes in various configurations, with the off-axis four-mirror design being the most prevalent. In this paper, we present a high-performance design based on this configuration, which exhibits a stable structure, ultra-low wavefront aberration, and high-level stray light suppression capabilities, effectively eliminating background noise. Also, a scientifically justified positioning of the entrance and exit pupils has been implemented, thereby paving adequate spatial provision for the integration of subsequent optical systems. The final design realizes a wavefront error of less than λ/500 in the science field of view, and after tolerance allocation and Monte Carlo analysis, a wavefront error of less than λ/30 can be achieved with a probability of 92%. The chief ray spot diagram dimensions are significantly small, indicating excellent control of pupil aberrations. Additionally, the tilt-to-length (TTL) noise and stray light meet the stringent requirements for space-based gravitational wave detection. The refined design presented in this paper proves to be a more fitting candidate for GW detection projects, offering more accurate and rational guidance. Full article
(This article belongs to the Special Issue Advanced Optics and Sensing Technologies for Telescopes)
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<p>Raytracing of the initial coaxial PM and SM.</p>
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<p>Raytracing of the initial coaxial TM and QM.</p>
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<p>Multi-configuration field of view settings (units: μrad).</p>
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<p>Pupil distortion caused by pupil aberration.</p>
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<p>The initial layout of PM and SM: (<b>a</b>) coaxial layout after calculation; (<b>b</b>) off-axis layout.</p>
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<p>PM-SM initial structure spot diagram.</p>
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<p>Initial off-axis system layout of TM and QM: (<b>a</b>) co-axial layout after calculation; (<b>b</b>) off-axis layout.</p>
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<p>Initial off-axis four-mirror system layout.</p>
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<p>Chief ray spot diagram of Initial off-axis four-mirror system at the theoretical exit pupil position.</p>
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<p>Final system layout of GW detection telescope.</p>
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<p>The spot diagram of the improved GW detection telescope system.</p>
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<p>The wavefront error across the science FOV of the improved telescope system.</p>
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<p>Chief ray spot diagrams at the exit pupil.</p>
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<p>Analysis of TTL coupling noise. (<b>a</b>) The curve of LPS with beam angle; (<b>b</b>) TTL noise caused by wavefront error.</p>
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<p>RMS WFE distribution of Monte Carlo 1000 trials.</p>
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<p>Displacement nephogram of mirrors: (<b>a</b>) PM; (<b>b</b>) SM; (<b>c</b>) TM; (<b>d</b>) QM.</p>
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20 pages, 1759 KiB  
Article
Knock Detection with Ion Current and Vibration Sensor: A Comparative Study of Logistic Regression and Neural Networks
by Ola Björnsson and Per Tunestål
Energies 2024, 17(22), 5693; https://doi.org/10.3390/en17225693 - 14 Nov 2024
Viewed by 289
Abstract
Knock detection is critical for maintaining engine performance and preventing damage in spark-ignition engines. This study explores the use of ion current and knock indicators derived from a vibration sensor (KIv) and ion current (KIi) [...] Read more.
Knock detection is critical for maintaining engine performance and preventing damage in spark-ignition engines. This study explores the use of ion current and knock indicators derived from a vibration sensor (KIv) and ion current (KIi) to improve knock detection accuracy. Traditional threshold-based methods rely on KIv, but they are susceptible to mechanical noise and cylinder variations. In this work, we applied both logistic regression and neural networks, including fully connected (FCNN) and convolutional neural networks (CNN), to classify knock events based on these indicators. The CNN models used ion current as the primary input, with an extended version incorporating both KIv and KIi into the fully connected layers. The models were evaluated using area under the curve (AUC) as the primary performance metric. The results show that the CNN model with additional inputs outperformed the other models, achieving a better and more consistent performance across cylinders. The dual-input logistic regression and CNN models demonstrated reduced cylinder-to-cylinder variation in classification performance, providing a more consistent knock detection accuracy across all cylinders. These findings suggest that combining ion current and knock indicators enhances knock detection reliability, offering a robust solution for real-time applications in engine control systems. Full article
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<p>Schematic of experimental setup.</p>
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<p>Schematic representation of an FCNN architecture, showing an input layer with <span class="html-italic">n</span> inputs, two hidden layers (with <span class="html-italic">m</span> nodes in the first layer and <span class="html-italic">j</span> nodes in the second), and an output layer producing a single output, <math display="inline"><semantics> <msub> <mi>O</mi> <mrow> <mi>p</mi> <mi>r</mi> <mi>e</mi> <mi>d</mi> </mrow> </msub> </semantics></math>, representing the prediction. The diagram illustrates the ion current as the input data.</p>
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<p>Flowchart of the dual-input CNN architecture. The model receives an ion current signal as input, which passes through the convolutional part of the network to extract features. The resulting flattened output is concatenated with knock indicators (<math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>v</mi> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>i</mi> </msub> </mrow> </semantics></math>), before passing through the fully connected part. The final output from the network is a prediction of the probability of knock occurrence.</p>
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<p>Characteristics of sensor signals for knock and no-knock cases. (<b>a</b>) In-cylinder pressure, (<b>b</b>) ion current, and (<b>c</b>) vibration sensor signals, illustrating differences in signal behavior between knock and no-knock events.</p>
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<p>Depicts the ROC curves and the corresponding AUCs for the best and worst performing cylinders for the single-variable logistic regression classifiers based on either <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>v</mi> </msub> </mrow> </semantics></math> or <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>i</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Depicts the ROC curves and the corresponding AUCs for the best and worst performing cylinders for the logistic regression classifiers based on both <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>v</mi> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>i</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Depicts the ROC curves and the corresponding AUCs for the best and worst performing cylinders for the CNN model trained on the ion current measurements.</p>
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<p>Depicts the ROC curves and the corresponding AUCs for the best and worst performing cylinders for the CNN model trained on the ion current measurements and knock indicators.</p>
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<p>Confusion matrices for the logistic regression model (<b>a</b>) and the CNN model (<b>b</b>). The logistic regression model was based on both knock indicators (<math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>v</mi> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>i</mi> </msub> </mrow> </semantics></math>), while the CNN model used the ion current signal in the convolutional layers and incorporated both knock indicators in the fully connected layers. The confusion matrix compares actual and predicted classifications, with each cell indicating the number of instances and their percentage of the total instances for each class (no-knock, knock). The diagonal elements represent the instances that were correctly classified, while the off-diagonal elements show the instances that were misclassified.</p>
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<p>Swarm plot for the logistic regression model (<b>a</b>) and the CNN model (<b>b</b>). The logistic regression model was based on both knock indicators (<math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>v</mi> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>K</mi> <msub> <mi>I</mi> <mi>i</mi> </msub> </mrow> </semantics></math>), while the CNN model used the ion current signal in the convolutional layers and incorporated both knock indicators in the fully connected layers. The swarm plot depicts the distribution of MAPO values for each predicted class. Blue points signify correctly classified instances, and red points indicate misclassified ones. The horizontal dashed line represents the MAPO threshold that separates the true classes of no-knock and knock. Note that some points have been omitted to fit the plot’s scale. The plot includes all misclassified examples but excludes examples with MAPO values greater than 2, as they were always correctly classified. Very low MAPO values of correctly classified instances have also been omitted.</p>
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19 pages, 14549 KiB  
Article
Improvement of Noise Reduction Structure of Direct-Acting Pressure Reducing Valve
by Rongsheng Liu, Baosheng Wang, Rongren Wang, Liu Yang, Lihui Wang and Chao Ai
Machines 2024, 12(11), 807; https://doi.org/10.3390/machines12110807 - 14 Nov 2024
Viewed by 230
Abstract
As a key pressure control component of a hydraulic system, the noise of the direct-acting pressure reducing valve affects the working state of the system directly. However, the existing pressure reducing valves generally have the problem of excessive pure noise. In order to [...] Read more.
As a key pressure control component of a hydraulic system, the noise of the direct-acting pressure reducing valve affects the working state of the system directly. However, the existing pressure reducing valves generally have the problem of excessive pure noise. In order to solve this problem, this study explored various structural combinations with the aim of improving the noise level of a direct-acting pressure reducing valve. Firstly, the flow field model of the direct-acting pressure reducing valve was established by using FEA (Finite Element Analysis), and the relationship between the flow field state and noise state was demonstrated through CFD (Computational Fluid Dynamics) simulation. Secondly, the position, number, and diameter of the oil holes on the valve spool were comprehensively analyzed, and the sound field analysis using LMS Virtual Lab was carried out. Finally, a prototype of the pressure reducing valve was manufactured, and the noise level before and after improvement was compared. The results showed that the effective sound pressure after improvement was reduced by 6.1% compared with that before at 50% of the opening, which verified the precision of the simulation model. The research results could provide a guideline for the design and improvement of direct-acting pressure reducing valves. Full article
(This article belongs to the Section Machine Design and Theory)
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<p>Research methods of this paper.</p>
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<p>Working principal diagram of direct-acting pressure reducing valve.</p>
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<p>Computational domain of pressure reducing valve. (<b>a</b>) Fluid domain under decompression working condition. (<b>b</b>) The fluid domain after adding the valve seat.</p>
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<p>Two selected flow field planes.</p>
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<p>Simplified model and meshing of the fluid domain of the pressure reducing valve.</p>
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<p>Pressure reducing valve boundary element grid model.</p>
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<p>Distribution diagram of pressure reducing valve spherical monitoring points.</p>
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<p>Pressure reducing valve experimental platform.</p>
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<p>Improved valve spool.</p>
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<p>Plane flow velocity cloud at the center of the pressure reducing valve. (<b>a</b>) Inlet pressure 100 bar, outlet pressure 25 bar. (<b>b</b>) Inlet pressure 150 bar, outlet pressure 25 bar. (<b>c</b>) Inlet pressure 200 bar, outlet pressure 25 bar. (<b>d</b>) Inlet pressure 250 bar, outlet pressure 25 bar.</p>
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<p>The velocity of the three points of the pressure reducing valve changes under different boundary conditions.</p>
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<p>Pressure cloud at the center plane of the pressure reducing valve. (<b>a</b>) Inlet pressure 100 bar, outlet pressure 25 bar. (<b>b</b>) Inlet pressure 150 bar, outlet pressure 25 bar. (<b>c</b>) Inlet pressure 200 bar, outlet pressure 25 bar. (<b>d</b>) Inlet pressure 250 bar, outlet pressure 25 bar.</p>
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<p>The pressure of the three points of the pressure reducing valve changes under different boundary conditions.</p>
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<p>Flow line cloud atlas at the center plane of pressure reducing valve. (<b>a</b>) Inlet pressure 100 bar, outlet pressure 25 bar. (<b>b</b>) Inlet pressure 150 bar, outlet pressure 25 bar. (<b>c</b>) Inlet pressure 200 bar, outlet pressure 25 bar. (<b>d</b>) Inlet pressure 250 bar, outlet pressure 25 bar.</p>
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<p>Sound power level distribution cloud atlas at the center plane of pressure reducing valve. (<b>a</b>) Inlet pressure 100 bar, outlet pressure 25 bar. (<b>b</b>) Inlet pressure 150 bar, outlet pressure 25 bar. (<b>c</b>) Inlet pressure 200 bar, outlet pressure 25 bar. (<b>d</b>) Inlet pressure 250 bar, outlet pressure 25 bar.</p>
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<p>Sound power level curve of the pressure reducing valve.</p>
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<p>Sound pressure spectrum.</p>
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<p>Spool structure schematic.</p>
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<p>Noise level of different groups.</p>
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<p>Inlet pressure 100 bar, outlet pressure 25 bar. Modified flow velocity cloud atlas of direct-acting pressure reducing valve.</p>
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<p>Inlet pressure 100 bar, outlet pressure 25 bar. Modified flow line cloud atlas of direct-acting pressure reducing valve.</p>
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<p>Inlet pressure 100 bar, outlet pressure 25 bar. Sound power level distribution cloud atlas of direct-acting pressure reducing valve.</p>
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<p>Comparison of the measured noise of the pressure reducing valve before and after improvement.</p>
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12 pages, 5273 KiB  
Article
Development of a New Sound Quality Parameter for Road Noise Perception Inside Vehicle Cabinet
by Aytekin Ozkan, Mehdi Yildiz and Ahmet Yildiz
Appl. Sci. 2024, 14(22), 10473; https://doi.org/10.3390/app142210473 - 14 Nov 2024
Viewed by 280
Abstract
Road noise significantly impacts how customers perceive vehicle noise, especially in electric vehicles, where it becomes more noticeable with the lack of the masking effect of the internal combustion engine. In this study, a novel sound quality (SQ) metric to capture the perception [...] Read more.
Road noise significantly impacts how customers perceive vehicle noise, especially in electric vehicles, where it becomes more noticeable with the lack of the masking effect of the internal combustion engine. In this study, a novel sound quality (SQ) metric to capture the perception of road noise was established with the help of both objective measurements and subjective evaluations on six different vehicles under smooth and rough road conditions. A jury of 50 individuals participated in subjective evaluations in controlled settings, experiencing road noise on six vehicles under both smooth and rough conditions. The same vehicles were also objectively measured in these conditions. Using subjective responses and objective measurements, this study identified key sound quality parameters influencing perception. These parameters were used to develop a new regression model predicting customer perception of road noise, considering both aspects of comfort and satisfaction to follow as a key indicator for road noise, particularly in electric vehicles. While an R2 of 0.312 was obtained with SPL, R2 of 0.972 and 0.999 were obtained with the new comfort and satisfaction metrics, respectively. The effectiveness of the newly created SQ metrics was further validated across various vehicles. Full article
(This article belongs to the Section Acoustics and Vibrations)
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<p>Position of microphones in drivers’ seat.</p>
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<p>Age distribution of the jury members.</p>
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<p>Gender distribution of the jury members.</p>
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<p>Profession distribution of the jury members.</p>
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<p>Automotive-experience distribution of the jury members.</p>
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<p>Overall level and articulation index of the vehicles in basket.</p>
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<p>SPL and various SQ metrics during coast-down tests.</p>
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<p>SQ metrics for road noise perception.</p>
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23 pages, 2805 KiB  
Article
Autonomous Underwater Vehicle Docking Under Realistic Assumptions Using Deep Reinforcement Learning
by Narcís Palomeras and Pere Ridao
Drones 2024, 8(11), 673; https://doi.org/10.3390/drones8110673 - 13 Nov 2024
Viewed by 598
Abstract
This paper addresses the challenge of docking an Autonomous Underwater Vehicle (AUV) under realistic conditions. Traditional model-based controllers are often constrained by the complexity and variability of the ocean environment. To overcome these limitations, we propose a Deep Reinforcement Learning (DRL) approach to [...] Read more.
This paper addresses the challenge of docking an Autonomous Underwater Vehicle (AUV) under realistic conditions. Traditional model-based controllers are often constrained by the complexity and variability of the ocean environment. To overcome these limitations, we propose a Deep Reinforcement Learning (DRL) approach to manage the homing and docking maneuver. First, we define the proposed docking task in terms of its observations, actions, and reward function, aiming to bridge the gap between theoretical DRL research and docking algorithms tested on real vehicles. Additionally, we introduce a novel observation space that combines raw noisy observations with filtered data obtained using an Extended Kalman Filter (EKF). We demonstrate the effectiveness of this approach through simulations with various DRL algorithms, showing that the proposed observations can produce stable policies in fewer learning steps, outperforming not only traditional control methods but also policies obtained by the same DRL algorithms in noise-free environments. Full article
(This article belongs to the Special Issue Advances in Autonomous Underwater Drones)
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<p>AUV entrance pose in DS coordinates and contact reward.</p>
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<p>Main elements featured in the control algorithm presented in [<a href="#B5-drones-08-00673" class="html-bibr">5</a>].</p>
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<p>Proposed learning approach. The figure shows the observations obtained from the environment and illustrates how the compound observation is created by combining both filtered and unfiltered observations. Additionally, it displays the actions sent by the DRL agent to the environment, along with the reward generated by the environment and processed by the agent.</p>
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<p>Elements involved in proposed EKF state and observation.</p>
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<p>Effect of the noise in the observations and the EKF implemented.</p>
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<p>SAC agent training results: evolution of (<b>a</b>) total reward and (<b>b</b>) time to complete the task per episode.</p>
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<p>TD3 agent training results: evolution of (<b>a</b>) total reward and (<b>b</b>) time to complete the task per episode.</p>
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<p>PPO agent training results: evolution of (<b>a</b>) total reward and (<b>b</b>) time to complete the task per episode.</p>
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<p>Success rate map according to ocean current for: (<b>a</b>) managed surge controller and (<b>b</b>) SAC agent trained with the proposed compund observations.</p>
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<p>Obtained trajectories (small green arrows) with the SAC policy for different levels of ocean current. Results in (<b>a</b>,<b>b</b>) are obtained with <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>≈</mo> <mo>[</mo> <mn>0.05</mn> <mo>,</mo> <mo>−</mo> <mn>0.1</mn> <mo>]</mo> </mrow> </semantics></math>, in (<b>c</b>,<b>d</b>) with <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>≈</mo> <mo>[</mo> <mo>−</mo> <mn>0.15</mn> <mo>,</mo> <mo>−</mo> <mn>0.3</mn> <mo>]</mo> </mrow> </semantics></math>, and (<b>e</b>–<b>h</b>) with <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>≈</mo> <mo>[</mo> <mn>0.3</mn> <mo>,</mo> <mo>−</mo> <mn>0.3</mn> <mo>]</mo> </mrow> </semantics></math>. The ocean current direction and magnitude are shown as a red arrow in the bottom right corner of each trajectory. Negative <math display="inline"><semantics> <msub> <mi>r</mi> <mi>g</mi> </msub> </semantics></math> values denote failed maneuvers.</p>
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<p>Obtained trajectories (small green arrows) with the SAC policy for different levels of ocean current. Results in (<b>a</b>,<b>b</b>) are obtained with <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>≈</mo> <mo>[</mo> <mn>0.05</mn> <mo>,</mo> <mo>−</mo> <mn>0.1</mn> <mo>]</mo> </mrow> </semantics></math>, in (<b>c</b>,<b>d</b>) with <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>≈</mo> <mo>[</mo> <mo>−</mo> <mn>0.15</mn> <mo>,</mo> <mo>−</mo> <mn>0.3</mn> <mo>]</mo> </mrow> </semantics></math>, and (<b>e</b>–<b>h</b>) with <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>≈</mo> <mo>[</mo> <mn>0.3</mn> <mo>,</mo> <mo>−</mo> <mn>0.3</mn> <mo>]</mo> </mrow> </semantics></math>. The ocean current direction and magnitude are shown as a red arrow in the bottom right corner of each trajectory. Negative <math display="inline"><semantics> <msub> <mi>r</mi> <mi>g</mi> </msub> </semantics></math> values denote failed maneuvers.</p>
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<p>(<b>a</b>) Stonefish simulator graphical user interface, (<b>b</b>) Docking maneuver execution in the Stonefish simulator, and (<b>c</b>, <b>d</b>) Trajectories (small green arrows) obtained with the SAC policy trained in the Gymnasium environment but executed in the Stonefish simulator. Reward values achieved were <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>g</mi> </msub> <mo>=</mo> <mn>174</mn> </mrow> </semantics></math> for (<b>c</b>) and <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>g</mi> </msub> <mo>=</mo> <mn>23</mn> </mrow> </semantics></math> for (<b>d</b>). Both results are obtained with low ocean current values <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>=</mo> <mo>[</mo> <mn>0.1</mn> <mo>,</mo> <mo>−</mo> <mn>0.05</mn> <mo>]</mo> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>=</mo> <mo>[</mo> <mn>0.1</mn> <mo>,</mo> <mn>0.1</mn> <mo>]</mo> </mrow> </semantics></math> represented as red arrows.</p>
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<p>(<b>a</b>) Stonefish simulator graphical user interface, (<b>b</b>) Docking maneuver execution in the Stonefish simulator, and (<b>c</b>, <b>d</b>) Trajectories (small green arrows) obtained with the SAC policy trained in the Gymnasium environment but executed in the Stonefish simulator. Reward values achieved were <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>g</mi> </msub> <mo>=</mo> <mn>174</mn> </mrow> </semantics></math> for (<b>c</b>) and <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>g</mi> </msub> <mo>=</mo> <mn>23</mn> </mrow> </semantics></math> for (<b>d</b>). Both results are obtained with low ocean current values <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>=</mo> <mo>[</mo> <mn>0.1</mn> <mo>,</mo> <mo>−</mo> <mn>0.05</mn> <mo>]</mo> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>o</mi> <mi>c</mi> <mo>=</mo> <mo>[</mo> <mn>0.1</mn> <mo>,</mo> <mn>0.1</mn> <mo>]</mo> </mrow> </semantics></math> represented as red arrows.</p>
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19 pages, 7262 KiB  
Article
Comfortable Sound Design Based on Auditory Masking with Chord Progression and Melody Generation Corresponding to the Peak Frequencies of Dental Treatment Noises
by Masato Nakayama, Takuya Hayashi, Toru Takahashi and Takanobu Nishiura
Appl. Sci. 2024, 14(22), 10467; https://doi.org/10.3390/app142210467 - 13 Nov 2024
Viewed by 365
Abstract
Noise reduction methods have been proposed for various loud noises. However, in a quiet indoor environment, even small noises often cause discomfort. One of the small noises that causes discomfort is noise with resonant frequencies. Since resonant frequencies are often high frequencies, it [...] Read more.
Noise reduction methods have been proposed for various loud noises. However, in a quiet indoor environment, even small noises often cause discomfort. One of the small noises that causes discomfort is noise with resonant frequencies. Since resonant frequencies are often high frequencies, it is difficult to apply conventional active noise control methods to them. To solve this problem, we focused on auditory masking, a phenomenon in which synthesized sounds increase the audible threshold. We have performed several studies on reducing discomfort based on auditory masking. However, it was difficult for comfortable sound design to be achieved using the previously proposed methods, even though they were able to reduce feelings of discomfort. Here, we focus on a pleasant sound: music. Comfortable sound design is made possible by introducing music theory into the design of masker signals. In this paper, we therefore propose comfortable sound design based on auditory masking with chord progression and melody generation to match the peak frequencies of dental treatment noises. Full article
(This article belongs to the Special Issue Noise Measurement, Acoustic Signal Processing and Noise Control)
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<p>Scene of dental treatment noise recording.</p>
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<p>Waveforms of dental treatment noise for four types of dental instruments.</p>
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<p>Spectrograms of dental treatment noise for four types of dental instruments.</p>
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<p>Flowchart of the proposed method.</p>
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<p>Image diagram of scale degree progression for the C key.</p>
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<p>Frequency characteristics of sawtooth wave.</p>
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<p>Image of the chord sound database construction.</p>
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<p>Image of concatenation of the chord sounds.</p>
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<p>Overview of style palette main UI in Flow Machines.</p>
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<p>Image of the melody sound database construction.</p>
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<p>Image of selection of the melody sounds.</p>
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<p>Comfort scores for the evaluation style palettes of melodies.</p>
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<p>Spectrograms of signals observed from an air turbine (rotational speed fluctuation: large) with the conventional and proposed methods.</p>
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<p>Spectrograms of signals observed from an air turbine (rotational speed fluctuation: small) with the conventional and proposed methods.</p>
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<p>Spectrograms of signals observed from a scaler with the conventional and proposed methods.</p>
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<p>Spectrograms of signals observed from a contra-angle with the conventional and proposed methods.</p>
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<p>Match rates of peak frequency and nearest neighbor harmonics.</p>
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<p>Scores of comfort.</p>
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<p>Scores for discomfort reduction.</p>
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21 pages, 7067 KiB  
Article
Research on Key Technologies of Image Steganography Based on Simultaneous Deception of Vision and Deep Learning Models
by Fan Zhang, Yanhua Dong and Hongyu Sun
Appl. Sci. 2024, 14(22), 10458; https://doi.org/10.3390/app142210458 - 13 Nov 2024
Viewed by 378
Abstract
As machine learning continues to evolve, traditional image steganography techniques find themselves increasingly unable to meet the dual challenge of deceiving both the human visual system and machine learning models. In response, this paper introduces the Visually Robust Image Steganography (VRIS) model, specifically [...] Read more.
As machine learning continues to evolve, traditional image steganography techniques find themselves increasingly unable to meet the dual challenge of deceiving both the human visual system and machine learning models. In response, this paper introduces the Visually Robust Image Steganography (VRIS) model, specifically tailored for this dual deception task. The VRIS model elevates visual security through the use of specialized feature extraction and processing methodologies. It meticulously conducts feature-level fusion between secret images and cover images, ensuring a high level of visual similarity between them. To effectively mislead machine learning models, the VRIS model incorporates a sophisticated strategy utilizing random noise factors and discriminators. This involves adding controlled amounts of random Gaussian noise to the encrypted image, thereby enhancing the difficulty for machine learning frameworks to recognize it. Furthermore, the discriminator is trained to discern between the noise-infused encrypted image and the original cover image. Through adversarial training, the discriminator and VRIS model refine each other, successfully deceiving the machine learning systems. Additionally, the VRIS model presents an innovative method for extracting and reconstructing secret images. This approach safeguards secret information from unauthorized access while enabling legitimate users to non-destructively extract and reconstruct images by leveraging multi-scale features from the encrypted image, combined with advanced feature fusion and reconstruction techniques. Experimental results validate the effectiveness of the VRIS model, achieving high PSNR and SSIM scores on the LFW dataset and demonstrating significant deception capabilities against the ResNet50 model on the Mini-ImageNet dataset, with an impressive misclassification rate of 99.24%. Full article
(This article belongs to the Special Issue Security and Privacy in Complicated Computing Environments)
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<p>The fundamental architecture of the VRIS Steganography Network.</p>
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<p>The curve of the loss function over time.</p>
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<p>Comparison of runtime performance after applying random subsampling.</p>
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<p>Visual-Masker module structure.</p>
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<p>Hidden-Insight module structure.</p>
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<p>Histogram comparison of cover image and steganographic image.</p>
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<p>Contrast diagram of residual differences between reconstructed secret image and cover image with varying intensities. (<b>a</b>) Cover image; (<b>b</b>) encrypted image; (<b>c</b>) secret image; (<b>d</b>) reconstruction image; (<b>e</b>) residual ×1; (<b>f</b>) residual ×5; (<b>g</b>) residual ×10; (<b>h</b>) residual ×15; (<b>i</b>) residual ×20.</p>
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<p>Residual image comparison: the first row is generated by the ISGAN model, the second row is generated by the model proposed in the literature [<a href="#B38-applsci-14-10458" class="html-bibr">38</a>], and the third row is generated by the VRIS model.</p>
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<p>Histogram comparison between secret image and reconstructed secret image.</p>
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36 pages, 5740 KiB  
Review
PEMFC Gas-Feeding Control: Critical Insights and Review
by Shiyi Fang, Jianan Feng, Xinyu Fan, Daifen Chen and Cao Tan
Actuators 2024, 13(11), 455; https://doi.org/10.3390/act13110455 - 13 Nov 2024
Viewed by 209
Abstract
Proton exchange membrane fuel cells (PEMFCs) are currently a relatively mature type of hydrogen energy device due to their high efficiency and low noise compared to traditional power devices. However, there are still challenges that hinder the large-scale application of PEMFCs. One key [...] Read more.
Proton exchange membrane fuel cells (PEMFCs) are currently a relatively mature type of hydrogen energy device due to their high efficiency and low noise compared to traditional power devices. However, there are still challenges that hinder the large-scale application of PEMFCs. One key challenge lies in the gas supply system, which is a complex, coupled nonlinear system. Therefore, an effective control strategy is essential for the efficient and stable operation of the gas control system. This paper aims to provide a comprehensive and systematic overview of the control strategies for PEMFC anode and cathode supply systems based on an analysis of 182 papers. The review covers modern control theories and optimization algorithms, including their design, objectives, performance, applications, and so on. Additionally, the advantages and disadvantages of these control methods are thoroughly evaluated and summarized. Full article
(This article belongs to the Section Control Systems)
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<p>Structure of PEMFC.</p>
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<p>Principles and control structure for PEMFC supply system.</p>
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<p>Optimized PID controls.</p>
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<p>Overall assessments for PID series control.</p>
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<p>Optimized sliding mode controls.</p>
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<p>Overall assessments for SMC series control.</p>
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<p>The linearization process for PEMFC supply system.</p>
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<p>Optimized optimal control and MPC.</p>
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<p>Overall assessments for optimal control and MPC.</p>
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<p>Structures of selected Type-2 fuzzy control approaches.</p>
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<p>Structures for selected DNC approaches.</p>
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<p>Structures for DRL controllers.</p>
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<p>Overall evaluation for intelligent controllers.</p>
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<p>Selected Fault-tolerance mechanism.</p>
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<p>Structures for anode control method.</p>
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<p>Recommended controllers’ performance comparison.</p>
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19 pages, 6597 KiB  
Article
Advanced, Real-Time Programmable FPGA-Based Digital Filtering Unit for IR Detection Modules
by Krzysztof Achtenberg, Ryszard Szplet and Zbigniew Bielecki
Electronics 2024, 13(22), 4449; https://doi.org/10.3390/electronics13224449 - 13 Nov 2024
Viewed by 291
Abstract
This paper presents a programmable digital filtering unit dedicated to operating with signals from infrared (IR) detection modules. The designed device is quite useful for increasing the signal-to-noise ratio due to the reduction in noise and interference from detector–amplifier circuits or external radiation [...] Read more.
This paper presents a programmable digital filtering unit dedicated to operating with signals from infrared (IR) detection modules. The designed device is quite useful for increasing the signal-to-noise ratio due to the reduction in noise and interference from detector–amplifier circuits or external radiation sources. Moreover, the developed device is flexible due to the possibility of programming the desired filter types and their responses. In the circuit, an advanced field-programmable gate array FPGA chip was used to ensure an adequate number of resources that are necessary to implement an effective filtration process. The proposed circuity was assisted by a 32-bit microcontroller to perform controlling functions and could operate at frequency sampling of up to 40 MSa/s with 16-bit resolution. In addition, in our application, the sampling frequency decimation enabled obtaining relatively narrow passband characteristics also in the low frequency range. The filtered signal was available in real time at the digital-to-analog converter output. In the paper, we showed results of simulations and real measurements of filters implementation in the FPGA device. Moreover, we also presented a practical application of the proposed circuit in cooperation with an InAsSb mid-IR detector module, where its self-noise was effectively reduced. The presented device can be regarded as an attractive alternative to the lock-in technique, artificial intelligence algorithms, or wavelet transform in applications where their use is impossible or problematic. Comparing the presented device with the previous proposal, a higher signal-to-noise ratio improvement and wider bandwidth of operation were obtained. Full article
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<p>Generalized hardware block diagram of typical DSP system with ADC and DAC that can be used to implement digital filter.</p>
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<p>The block diagram of the hardware platform for the digital filtering unit.</p>
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<p>The photo of the hardware platform developed for the digital filtering unit.</p>
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<p>Block diagram of the internal functional module implemented in the FPGA device.</p>
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<p>Example schematic block diagrams of direct form FIR (<b>a</b>) and direct form I-biquad IIR (<b>b</b>) filter implementations. Square blocks are delayers, and triangular blocks are multipliers by constants.</p>
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<p>Frequency (<b>a</b>), phase (<b>b</b>), impulse (<b>c</b>), and step (<b>d</b>) responses for normalized 840-order windowed-sinc filter. The passband was set from 0.01 to 0.02 of normalized frequency.</p>
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<p>Simulated FIR BPF frequency responses designed using the equiripple algorithm for different orders (<b>a</b>). Dependence between the filter order and minimum attenuation in stopband (<b>b</b>). The low-pass stopband was set to 0.01, the passband from 0.02 to 0.03, and the high-pass stopband to 0.04 of normalized frequency.</p>
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<p>Frequency (<b>a</b>), phase (<b>b</b>), impulse (<b>c</b>), and step (<b>d</b>) responses simulated for the normalized 50-order (20-order for elliptic) IIR filter. The passband was set from 0.01 to 0.02 of normalized frequency.</p>
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<p>Simulated Butterworth IIR BPF frequency responses. The passband was set from 0.01 to 0.02 of normalized frequency.</p>
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<p>Detector–amplifier circuit with noise sources (IR detection module).</p>
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<p>The InAsSb IR detection module output noise signal (<b>a</b>) and its PSD (<b>b</b>). The measurements were provided with a gain set to 40 dB and bandwidth set to 1.6 MHz.</p>
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<p>Frequency (<b>a</b>) and phase (<b>b</b>) responses were simulated and measured for the 800-order FIR BPF (FIR#1). The passband was set from 2 kHz to 3 kHz, stopbands at 1 kHz and 4 kHz, and sampling frequency to 250 kS/s. The measured phase was rolled up (from −π to π rad).</p>
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<p>Frequency (<b>a</b>) and phase (<b>b</b>) responses were simulated and measured for 800-order FIR BPF (FIR#2). The passband was set from 200 kHz to 300 kHz, stopbands at 100 kHz and 400 kHz, and a sampling frequency of 40 MS/s. The measured phase was rolled up (from −π to π rad). The log scale was used for the frequency axis.</p>
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<p>FIR#2 measures filter response to the chirp signal with a sweep from 10 kHz to 1 MHz.</p>
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<p>FIR#2 graphical schematic of implementation in FPGA chip (<b>a</b>); utilization of resources (<b>b</b>).</p>
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<p>Frequency (<b>a</b>) and phase (<b>b</b>) responses were simulated and measured for the 38-order IIR BPF (IIR#1). The passband was set from 3 kHz to 8 kHz, stopbands at 1 kHz and 10 kHz, and sampling frequency at 250 kS/s. The measured phase was rolled up (from −π to π rad). The log scale was used for the frequency axis.</p>
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<p>A measurement setup is used to verify the digital filtering unit’s operation with a noisy signal.</p>
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<p>Results of filtering noisy signal from the InAsSb IR detection module using the proposed unit and FIR#2 in the time domain (<b>a</b>) and frequency domain (<b>b</b>).</p>
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11 pages, 5675 KiB  
Communication
780 nm Narrow Linewidth External Cavity Diode Laser for Quantum Sensing
by Junzhu Ye, Chenggang Guan, Puchu Lv, Weiqi Wang, Xuan Chen, Ziyi Wang, Yifan Xiao, Linfeng Zhan, Jiaoli Gong and Yucheng Yao
Sensors 2024, 24(22), 7237; https://doi.org/10.3390/s24227237 - 13 Nov 2024
Viewed by 341
Abstract
To meet the demands of laser communication, quantum precision measurement, cold atom technology, and other fields for narrow linewidth and low-noise light sources, an external cavity diode laser (ECDL) operating in the wavelength range around 780 nm was set up with a Fabry–Pérot [...] Read more.
To meet the demands of laser communication, quantum precision measurement, cold atom technology, and other fields for narrow linewidth and low-noise light sources, an external cavity diode laser (ECDL) operating in the wavelength range around 780 nm was set up with a Fabry–Pérot etalon (F–P) and an interference filter (IF) in the experiment. The interference filter type ECDL (IF–ECDL) with butterfly-style packaging configuration has continuous wavelength tuning within a specified range through precise temperature and current control and has excellent single-mode characteristics. Experimental results indicate that the output power of the IF–ECDL is 14 mW, with a side-mode suppression ratio (SMSR) of 54 dB, a temperature-controlled mode-hop-free tuning range of 527 GHz (1.068 nm), and an output linewidth of 570 Hz. Compared to traditional lasers operating at 780 nm, the IF–ECDL exhibits narrower linewidth, lower noise, and higher spectral purity, and its dimensions are merely 25 × 15 × 8.5 mm3 weighing only 19.8 g, showcasing remarkable miniaturization and lightweight advantages over similar products in current research fields. Full article
(This article belongs to the Section Optical Sensors)
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<p>Basic model of the ECDL.</p>
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<p>Structure diagram of butterfly IF–ECDL.</p>
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<p>Manufacturing of the IF–ECDL with the automatic coupling device. (<b>a</b>) Installing the collimating lens with the automatic coupling device; (<b>b</b>) Partial enlargement of the coupling device; (<b>c</b>) Internal structure of the IF–ECDL; (<b>d</b>) Butterfly-shaped IF–ECDL.</p>
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<p>PIV Curve of IF–ECDL.</p>
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<p>Spectra of IF–ECDL at a driving current of 60 mA and TEC temperature of 22.5 °C.</p>
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<p>Energy distribution of IF–ECDL. (<b>a</b>) Two-dimensional energy distribution; (<b>b</b>) Three-dimensional energy distribution.</p>
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<p>Curves of the bidirectional temperature scanning of the IF–ECDL.</p>
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<p>Temperature rising scanning curves at different ambient temperatures.</p>
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<p>Test results of frequency noise and phase noise of IF–ECDL. (<b>a</b>) Test results of frequency noise; (<b>b</b>) Test results of phase noise.</p>
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29 pages, 2822 KiB  
Article
Quantitative Analysis of Predictors of Acoustic Materials for Noise Reduction as Sustainable Strategies for Materials in the Automotive Industry
by Bianca-Mihaela Cășeriu, Manuela-Rozalia Gabor, Petruța Blaga and Cristina Veres
Appl. Sci. 2024, 14(22), 10400; https://doi.org/10.3390/app142210400 - 12 Nov 2024
Viewed by 474
Abstract
This study proposes a qualitative analysis for identifying the best predictors for ensuring passive noise control, aiming to achieve superior acoustic comfort in transportation systems. The study is based on real experimental data, collected through acoustic measurements performed by the authors on materials [...] Read more.
This study proposes a qualitative analysis for identifying the best predictors for ensuring passive noise control, aiming to achieve superior acoustic comfort in transportation systems. The study is based on real experimental data, collected through acoustic measurements performed by the authors on materials from six different classes and employs a multidisciplinary approach, including Mann–Whitney U tests, Kruskal–Wallis analysis with Dunn’s post hoc multiple comparisons and multilinear regression. This research presents an analysis and evaluation of how the physical properties of various materials influence acoustic comfort, acoustic absorption class and absorption class performance and proposes quantitative models for material selection to address sustainable strategies in the automotive industry. The results highlight significant differences between material categories in terms of acoustic absorption properties and demonstrate the importance of rigorous material selection in vehicle design to enhance acoustic comfort. Additionally, the research contributes to the development of predictive models that estimate acoustic performance based on the physical properties of materials, providing a basis for optimizing material selection in the design phase. Full article
(This article belongs to the Section Acoustics and Vibrations)
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<p>SPSS codification.</p>
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<p>Box plots and pairwise comparisons of class material, acoustic comfort and material type. The Kruskal–Wallis test with Dunn’s post hoc multiple comparisons was applied to test the differences in the (<b>a</b>) thickness, (<b>c</b>) sound absorption coefficient and (<b>e</b>) frequency among different class materials. The pairwise comparisons (<b>b</b>,<b>d</b>,<b>f</b>) illustrate the statistical significance of differences between each pair of class materials, with lines connecting pairs where the adjusted significance level is less than 0.05.</p>
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<p>Box plots and pairwise comparisons of class material, acoustic comfort and material type. The Kruskal–Wallis test with Dunn’s post hoc multiple comparisons was applied to test the differences in the (<b>a</b>) thickness, (<b>c</b>) sound absorption coefficient and (<b>e</b>) frequency among different class materials. The pairwise comparisons (<b>b</b>,<b>d</b>,<b>f</b>) illustrate the statistical significance of differences between each pair of class materials, with lines connecting pairs where the adjusted significance level is less than 0.05.</p>
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<p>Box plots and pairwise comparisons of the absorption acoustic class and absorption class performance. (<b>a</b>) thickness, (<b>c</b>) sound absorption coefficient and (<b>e</b>) frequency among different class materials, (<b>b</b>,<b>d</b>,<b>f</b>) the pairwise comparisons. (<b>g</b>) Thickness across ACP. (<b>h</b>) Sound absorption across ACP. (<b>i</b>) Frequencies.</p>
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<p>Box plots and pairwise comparisons of the absorption acoustic class and absorption class performance. (<b>a</b>) thickness, (<b>c</b>) sound absorption coefficient and (<b>e</b>) frequency among different class materials, (<b>b</b>,<b>d</b>,<b>f</b>) the pairwise comparisons. (<b>g</b>) Thickness across ACP. (<b>h</b>) Sound absorption across ACP. (<b>i</b>) Frequencies.</p>
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<p>Box plots and pairwise comparisons of the absorption acoustic class and absorption class performance. (<b>a</b>) thickness, (<b>c</b>) sound absorption coefficient and (<b>e</b>) frequency among different class materials, (<b>b</b>,<b>d</b>,<b>f</b>) the pairwise comparisons. (<b>g</b>) Thickness across ACP. (<b>h</b>) Sound absorption across ACP. (<b>i</b>) Frequencies.</p>
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<p>Box plots and pairwise comparisons of the absorption acoustic class and absorption class performance. (<b>a</b>) thickness, (<b>c</b>) sound absorption coefficient and (<b>e</b>) frequency among different class materials, (<b>b</b>,<b>d</b>,<b>f</b>) the pairwise comparisons. (<b>g</b>) Thickness across ACP. (<b>h</b>) Sound absorption across ACP. (<b>i</b>) Frequencies.</p>
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<p>Decision tree for acoustic comfort.</p>
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<p>Decision tree for the absorption acoustic class.</p>
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<p>Decision tree for absorption class performance.</p>
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