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16 pages, 2594 KiB  
Article
Mitigating Mode Switching Oscillation in a One-Motor-One-Pump Motor-Controlled Hydraulic Cylinder via System Pressure Control: Simulation Study
by Wei Zhao, Morten Kjeld Ebbesen, Michael Rygaard Hansen and Torben Ole Andersen
Energies 2024, 17(24), 6334; https://doi.org/10.3390/en17246334 (registering DOI) - 16 Dec 2024
Abstract
This study focuses on a hydraulic cylinder that is directly connected to a fixed-displacement hydraulic pump driven by an electric servo motor. This particular setup is referred to as a one-motor-one-pump motor-controlled hydraulic cylinder (MCC). This paper presents a new approach to address [...] Read more.
This study focuses on a hydraulic cylinder that is directly connected to a fixed-displacement hydraulic pump driven by an electric servo motor. This particular setup is referred to as a one-motor-one-pump motor-controlled hydraulic cylinder (MCC). This paper presents a new approach to address mode switching oscillation (MSO) in MCCs by incorporating system pressure control capabilities. It conducts a detailed investigation into the factors that contribute to MSO in standard MCCs and thoroughly evaluates the effectiveness of the proposed system in mitigating MSO. The simulation results demonstrate the successful suppression of MSO. In conclusion, the proposed MCC with system pressure control capabilities is validated and, furthermore, it shows great potential for practical applications involving small loads and rapid retraction. Full article
(This article belongs to the Section F: Electrical Engineering)
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<p>Structure of a one-motor-one-pump motor-controlled cylinder (MCC) [<a href="#B1-energies-17-06334" class="html-bibr">1</a>].</p>
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<p>A standard MCC with two POCVs.</p>
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<p>Four-quadrant operations of the cylinder and the MCC drive unit.</p>
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<p>The proposed MCC [<a href="#B1-energies-17-06334" class="html-bibr">1</a>].</p>
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<p>Demonstration of four-quadrant operation in operation mode [<a href="#B1-energies-17-06334" class="html-bibr">1</a>].</p>
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<p>Sketch of the laboratory single-boom crane [<a href="#B1-energies-17-06334" class="html-bibr">1</a>].</p>
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<p>Block diagram of the control algorithm [<a href="#B1-energies-17-06334" class="html-bibr">1</a>].</p>
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<p>Simulation results for the standard MCC in MSO.</p>
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<p>Simulation results for the proposed MCC mitigating MSO.</p>
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16 pages, 677 KiB  
Article
Localization Optimization Algorithm Based on Phase Noise Compensation
by Yanming Liu, Yingkai Cao, Charilaos C. Zarakovitis, Disheng Xiao, Kai Ying and Xianfu Chen
Electronics 2024, 13(24), 4947; https://doi.org/10.3390/electronics13244947 (registering DOI) - 16 Dec 2024
Viewed by 77
Abstract
Phase noise is a consequence of the instability inherent in the operation of oscillators, making it impossible to entirely eliminate. For low-cost internet of things (IoT) devices, this type of noise can be particularly pronounced, posing a challenge in providing high-quality localization services. [...] Read more.
Phase noise is a consequence of the instability inherent in the operation of oscillators, making it impossible to entirely eliminate. For low-cost internet of things (IoT) devices, this type of noise can be particularly pronounced, posing a challenge in providing high-quality localization services. To tackle this issue, this paper introduces an improved localization algorithm that includes phase noise compensation. The proposed algorithm enhances the direction of arrival (DoA) estimation for each base station by employing the EM–MUSIC method, subsequently forming a non-convex optimization problem based on the mean square error (MSE) of the estimated DoA results. Finally, a closed-form solution is derived through rational assumptions and approximations. Results show that this algorithm effectively minimizes localization errors and achieves accuracy levels within the sub-meter range. Full article
(This article belongs to the Special Issue Energy-Efficient Wireless Solutions for 6G/B6G)
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<p>SIMO localization system.</p>
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<p>Phase noise diagram.</p>
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<p>Multiple base stations localization scenario based on triangulation.</p>
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<p>EM–MUSIC algorithm flowchart.</p>
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<p>Multiple base stations optimization algorithm flowchart.</p>
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<p>Effect of phase noise on the performance of MUSIC algorithm.</p>
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<p>The RMSE of different DoA estimation algorithms.</p>
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<p>Layout diagram of eight base stations.</p>
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<p>The variation of mean estimation error with the number of iterations.</p>
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<p>CDF of location error when some base stations receive signals with high noise.</p>
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<p>The relationship between average error and the number of uninterfered base stations.</p>
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<p>Variation of average estimation error with the number of participated base stations.</p>
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<p>Results of 20 single localizations.</p>
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2 pages, 1143 KiB  
Correction
Correction: Mallphanov et al. Novel Approach to Increasing the Amplitude of the Mechanical Oscillations of Self-Oscillating Gels: Introduction of Catalysts Both as Pendant Groups and as Crosslinkers. Gels 2024, 10, 727
by Ilya L. Mallphanov, Michail Y. Eroshik, Dmitry A. Safonov, Alexander V. Sychev, Vyacheslav E. Bulakov and Anastasia I. Lavrova
Gels 2024, 10(12), 830; https://doi.org/10.3390/gels10120830 (registering DOI) - 16 Dec 2024
Viewed by 24
Abstract
In the original publication [...] Full article
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Figure 1
<p>(<b>a</b>) Synthesis of ligand (<b>1</b>) and catalysts (<b>2</b>) and (<b>3</b>). (<b>b</b>) Synthesis of ligand (<b>4</b>) and catalysts (<b>5</b>) and (<b>6</b>). TEA—triethylamine, TMEDA—tetramethylethylenediamine, Ru(bpy)<sub>2</sub>Cl<sub>2</sub>—bis(2,2′-bipyridine)ruthenium(II) chloride, THF—tetrahydrofuran, MeOH—methanol, EtOH—ethanol.</p>
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12 pages, 2645 KiB  
Article
Dynamic Survivability Centrality in Nonlinear Oscillator Systems
by Yuexin Wang, Zhongkui Sun, Sijun Ye, Tao Zhao, Xinshuai Zhang and Wei Xu
Symmetry 2024, 16(12), 1661; https://doi.org/10.3390/sym16121661 (registering DOI) - 16 Dec 2024
Viewed by 112
Abstract
In light of the fact that existing centrality indexes disregard the influence of dynamic characteristics and lack generalizability due to standard diversification, this study investigates dynamic survivability centrality, which enables quantification of oscillators’ capacity to impact the dynamic survivability of nonlinear oscillator systems. [...] Read more.
In light of the fact that existing centrality indexes disregard the influence of dynamic characteristics and lack generalizability due to standard diversification, this study investigates dynamic survivability centrality, which enables quantification of oscillators’ capacity to impact the dynamic survivability of nonlinear oscillator systems. Taking an Erdős–Rényi random graph system consisting of Stuart–Landau oscillators as an illustrative example, the typical symmetry synchronization is considered as the key mission to be accomplished in light of the study and the dynamic survivability centrality value is found to be dependent on both the system size and connection density. Starting with a small scale system, the correctness of the theoretical results and the superiority in comparison to traditional indexes are verified. Further, we present the quantitative results by means of error analysis, distribution comparison of various indexes and relationship with system structure exploration, and give the position of the key oscillator. The results demonstrate a negligible error between the theoretical and numerical outcomes, and highlighting that the distribution of dynamic survivability centrality closely resembles the distribution of system state changes. The conclusions serve as evidence for the accuracy and validity of the proposed index. The findings provide an effective approach to protect systems to improve dynamic survivability. Full article
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Figure 1
<p>The diagram block for methodology.</p>
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<p>Dynamic survivability centrality of nonlinear oscillator system with ER structures (<math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>10</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.4</mn> </mrow> </semantics></math>), which display the excellent agreement of theoretical and numerical results. (<b>a</b>) The normalized dynamic survivability centrality index <math display="inline"><semantics> <mrow> <mi>S</mi> <msup> <mi>C</mi> <mo>′</mo> </msup> <mrow> <mo>(</mo> <mi>i</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> and the corresponding mission completion probability S when each oscillator is removed. (<b>b</b>) Schematic of the system.</p>
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<p>Comparison of dynamic survivability centrality with other centrality indexes (<math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>10</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.4</mn> </mrow> </semantics></math>), which prove the superiority of dynamic survivability centrality. (<b>a</b>) Dynamic survivability centrality. (<b>b</b>) Degree centrality. (<b>c</b>) Closeness centrality. (<b>d</b>) Betweennesss centrality.</p>
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<p>The dynamic survivability centrality of the coupled nonlinear oscillator system with ER structures under different connection densities (<math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>100</mn> </mrow> </semantics></math>), which reflects the influence of connection density. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.08</mn> </mrow> </semantics></math>. (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.1</mn> </mrow> </semantics></math>. (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.4</mn> </mrow> </semantics></math>.</p>
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<p>Visualizing the importance ranking of oscillators in the ER system with <math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>100</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.08</mn> </mrow> </semantics></math> according to the dynamic survivability centrality. (<b>a</b>) Order of importance of each oscillator. (<b>b</b>) Schematic of the system.</p>
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<p>Error analysis of dynamic survivability centrality (<math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>100</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.08</mn> </mrow> </semantics></math>), embodying the correctness of theoretical derivation. (<b>a</b>) Relative error value corresponding to each oscillator. (<b>b</b>) Distribution of errors.</p>
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<p>The distribution diagrams of state of system and centrality indexes (<math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>100</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>d</mi> <mo>=</mo> <mn>0.1</mn> </mrow> </semantics></math>), which prove the superiority of dynamic survivability centrality. (<b>a</b>) Normalized distribution of <math display="inline"><semantics> <mrow> <mo>Δ</mo> <mi>Z</mi> </mrow> </semantics></math>. (<b>b</b>) Normalized distribution of dynamic survivability centrality. (<b>c</b>) Normalized distribution of degree centrality. (<b>d</b>) Normalized distribution of closeness centrality. (<b>e</b>) Normalized distribution of betweenness centrality.</p>
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<p>The influence of system topology parameters on the dynamic survivability centrality. (<b>a</b>) <math display="inline"><semantics> <mfenced separators="" open="(" close=")"> <mrow> <msup> <mi>d</mi> <mi>i</mi> </msup> <mo>,</mo> <mi>N</mi> </mrow> </mfenced> </semantics></math> parameter plane contour plot (<math display="inline"><semantics> <mrow> <msup> <mi>d</mi> <mn>0</mn> </msup> <mo>=</mo> <mn>0.8</mn> </mrow> </semantics></math>). (<b>b</b>) <math display="inline"><semantics> <mfenced separators="" open="(" close=")"> <mrow> <msup> <mi>d</mi> <mi>i</mi> </msup> <mo>,</mo> <msup> <mi>d</mi> <mn>0</mn> </msup> </mrow> </mfenced> </semantics></math> parameter plane contour plot (<math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>100</mn> </mrow> </semantics></math>).</p>
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16 pages, 4856 KiB  
Article
Multistep Prediction Analysis of Pure Pursuit Method for Automated Guided Vehicles in Aircraft Industry
by Biling Wang, Gaojian Fan, Xinming Zhang, Liangjie Gao, Xiaobo Wang and Weijie Fu
Actuators 2024, 13(12), 518; https://doi.org/10.3390/act13120518 (registering DOI) - 15 Dec 2024
Viewed by 359
Abstract
The pure pursuit (PP) method has been widely employed in automated guided vehicles (AGVs) to address path tracking challenges. However, the traditional pure pursuit method exhibits certain limitations in tracking performance. For instance, selecting a look-ahead point that is too close can lead [...] Read more.
The pure pursuit (PP) method has been widely employed in automated guided vehicles (AGVs) to address path tracking challenges. However, the traditional pure pursuit method exhibits certain limitations in tracking performance. For instance, selecting a look-ahead point that is too close can lead to oscillations during tracking, while selecting one that is too far away can result in slow tracking and corner-cutting issues. To address these challenges, this paper proposes a multistep prediction pure pursuit method. First, the look-ahead distance calculation equation is adjusted by incorporating path curvature, allowing it to adaptively adjust according to road conditions. Next, to avoid oscillations caused by constant changes in the look-ahead distance, this paper adopts the prediction concept of model predictive control (MPC) to make multistep predictions for the pure pursuit method. The final input is derived from a linear weighted combination of the multistep prediction results. Simulation analyses and experiments demonstrate that the multistep predictive pure pursuit method significantly enhances the tracking performance of the traditional pure pursuit method. Full article
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<p>Bicycle model.</p>
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<p>Schematic diagram of the pure pursuit method.</p>
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<p>Problems associated with the pure pursuit method: (<b>a</b>) long look-ahead distance, (<b>b</b>) short look-ahead distance.</p>
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<p>The relationship between the look-ahead distances of tracking errors.</p>
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<p>The influence of look-ahead distance on tracking performance.</p>
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<p>The relationship between <span class="html-italic">ld</span> and maximum error when curvature is fixed.</p>
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<p>The change rule of function <span class="html-italic">f</span>(<span class="html-italic">x</span>) with respect to <span class="html-italic">a</span>.</p>
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<p>Linear two degrees of freedom model.</p>
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<p>Multistep prediction principle.</p>
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<p>Experimental facility.</p>
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<p>The simulation results of sin-path: (<b>a</b>) tracking effect when <span class="html-italic">k</span> = 1; (<b>b</b>) tracking effect when <span class="html-italic">k</span> = 5; (<b>c</b>) lateral tracking error when <span class="html-italic">k</span> = 1; (<b>d</b>) lateral tracking error when <span class="html-italic">k</span> = 5; (<b>e</b>) heading tracking error when <span class="html-italic">k</span> = 1; (<b>f</b>) heading tracking error when <span class="html-italic">k</span> = 5.</p>
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<p>The simulation results of <span class="html-italic">k</span>1: (<b>a</b>) tracking effect when <span class="html-italic">Ld</span> = 0.2; (<b>b</b>) tracking effect when <span class="html-italic">Ld</span> = 5; (<b>c</b>) lateral tracking error when <span class="html-italic">Ld</span> = 0.2; (<b>d</b>) lateral tracking error when <span class="html-italic">Ld</span> = 5; (<b>e</b>) heading tracking error when <span class="html-italic">Ld</span> = 0.2; (<b>f</b>) heading tracking error when <span class="html-italic">Ld</span> = 5.</p>
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<p>The simulation results of <span class="html-italic">Nc</span>: (<b>a</b>) tracking effect when <span class="html-italic">Ld</span> = 0.2; (<b>b</b>) tracking effect when <span class="html-italic">Ld</span> = 5; (<b>c</b>) lateral tracking error when <span class="html-italic">Ld</span> = 0.2; (<b>d</b>) lateral tracking error when <span class="html-italic">Ld</span> = 5; (<b>e</b>) heading tracking error when <span class="html-italic">Ld</span> = 0.2; (<b>f</b>) heading tracking error when <span class="html-italic">Ld</span> = 5.</p>
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<p>The experiment results of U-path: (<b>a</b>) tracking effect; (<b>b</b>) lateral tracking error; (<b>c</b>) heading tracking error.</p>
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18 pages, 8713 KiB  
Article
Smoke Precipitation by Exposure to Dual-Frequency Ultrasonic Oscillations
by Vladimir Khmelev, Andrey Shalunov, Sergey Tsyganok and Pavel Danilov
Fire 2024, 7(12), 476; https://doi.org/10.3390/fire7120476 (registering DOI) - 15 Dec 2024
Viewed by 210
Abstract
The analysis conducted herein has shown that the efficiency of smoke precipitation can be improved by additionally making smoke particles interact with ultrasonic (US) oscillations. Because the efficiency of US coagulation lowers when small particles assemble into agglomerates, the authors of this work [...] Read more.
The analysis conducted herein has shown that the efficiency of smoke precipitation can be improved by additionally making smoke particles interact with ultrasonic (US) oscillations. Because the efficiency of US coagulation lowers when small particles assemble into agglomerates, the authors of this work have suggested studying how smoke particles interact with complex sound fields. The fields are formed by at least two US transducers which work at a similar frequency or on frequencies with small deviations. To form these fields, high-efficiency bending wave ultrasonic transducers have been developed and suggested. It has been shown that a complex ultrasonic field significantly enhances smoke precipitation. The field in question was constructed by simultaneously emitting 22 kHz US oscillations with a sound pressure level no lower than 140 dB at a distance of 1 m. The difference in US oscillations’ frequencies was no more than 300 Hz. Due to the effect of multi-frequency ultrasonic oscillations induced in the experimental smoke chamber, it was possible to provide a transmissivity value of 0.8 at a distance of 1 m from the transducers and 0.9 at a distance of 2 m. Thus, the uniform visibility improvement and complete suppression of incoming smoke was achieved. At the same time, the dual-frequency effect does not require an increase in ultrasonic energy for smoke due to the agglomeration of small particles under the influence of high-frequency ultrasonic vibrations and the further aggregation of the formed agglomerates by creating conditions for the additional rotational movement of the agglomerates due to low-frequency vibrations. Full article
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<p>Design and simulation results fora disk emitter. (<b>a</b>) Distribution of amplitude; (<b>b</b>) distribution of stress. 1—emitter; 2—emitting pad of the piezoelectric transducer; 3—piezoceramic rings; 4—reflecting pad; 5—tightening bolt; 6—copper electrode; 7—tightening screw.</p>
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<p>The manufactured emitter with an electronic generator for supplying its power.</p>
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<p>Dual emitter for equal frequency action on smoke.</p>
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<p>Emitters for multi-frequency action on smoke.</p>
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<p>Stand for measuring the directional pattern of ultrasonic emitters. 1—Ultrasonic disk emitter, 2—electronic generator; 3—emitter stand, 4—microphone; 5—noise meter measuring unit; 6—microphone stand; 7—microphone direction point.</p>
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<p>Experimental setup; (<b>a</b>) with one emitter; (<b>b</b>) with two emitters. 1—Ultrasonic disk emitter; 2—electronic generator; 3—smoke chamber; 4—smoke generator; 5—infrared radiation source; 6—photodetector.</p>
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<p>Directivity pattern for a single emitter.</p>
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<p>Attenuation in relation to distance from the source in a smoke chamber (one emitter).</p>
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<p>Directivity pattern of dual disk emitters.Red color—two simultaneously operating disks at the same frequency; blue color—two simultaneously operating disks of different frequencies.</p>
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<p>Attenuation over distance in a smoke chamber (two emitters). Blue color—two simultaneously operating disks of different frequencies; red color—two simultaneously operating disks of equal frequencies.</p>
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<p>Difference frequency directivity pattern.</p>
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<p>Beat frequency attenuation over distance in smoke chamber.</p>
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<p>Results of visual observation of ultrasonic smoke agglomeration.</p>
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<p>Measurement of relative visibility from the time of ultrasonic exposure for different distances (in m) from the emitter.</p>
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<p>Measurement of relative visibility from the time of ultrasonic exposure for different distances (in m) from the emitters.</p>
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<p>Histogram of agglomerate size distribution.</p>
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<p>Images of smoke particle agglomerates (100×). (<b>a</b>) Single-frequency action; (<b>b</b>) dual-frequency action.</p>
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13 pages, 253 KiB  
Article
Adaptive Compensatory Neurophysiological Biomarkers of Motor Recovery Post-Stroke: Electroencephalography and Transcranial Magnetic Stimulation Insights from the DEFINE Cohort Study
by Guilherme J. M. Lacerda, Fernanda M. Q. Silva, Kevin Pacheco-Barrios, Linamara Rizzo Battistella and Felipe Fregni
Brain Sci. 2024, 14(12), 1257; https://doi.org/10.3390/brainsci14121257 - 15 Dec 2024
Viewed by 272
Abstract
Objective: This study aimed to explore longitudinal relationships between neurophysiological biomarkers and upper limb motor function recovery in stroke patients, focusing on electroencephalography (EEG) and transcranial magnetic stimulation (TMS) metrics. Methods: This longitudinal cohort study analyzed neurophysiological, clinical, and demographic data from 102 [...] Read more.
Objective: This study aimed to explore longitudinal relationships between neurophysiological biomarkers and upper limb motor function recovery in stroke patients, focusing on electroencephalography (EEG) and transcranial magnetic stimulation (TMS) metrics. Methods: This longitudinal cohort study analyzed neurophysiological, clinical, and demographic data from 102 stroke patients enrolled in the DEFINE cohort. We investigated the associations between baseline and post-intervention changes in the EEG theta/alpha ratio (TAR) and TMS metrics with upper limb motor functionality, assessed using the outcomes of five tests: the Fugl-Meyer Assessment (FMA), Handgrip Strength Test (HST), Pinch Strength Test (PST), Finger Tapping Test (FTT), and Nine-Hole Peg Test (9HPT). Results: Our multivariate models identified that a higher baseline TAR in the lesioned hemisphere was consistently associated with poorer motor outcomes across all five assessments. Conversely, a higher improvement in the TAR was positively associated with improvements in FMA and 9HPT. Additionally, an increased TMS motor-evoked potential (MEP) amplitude in the non-lesioned hemisphere correlated with greater FMA-diff, while a lower TMS Short Intracortical Inhibition (SICI) in the non-lesioned hemisphere was linked to better PST improvements. These findings suggest the potential of the TAR and TMS metrics as biomarkers for predicting motor recovery in stroke patients. Conclusion: Our findings highlight the significance of the TAR in the lesioned hemisphere as a predictor of motor function recovery post-stroke and also a potential signature for compensatory oscillations. The observed relationships between the TAR and motor improvements, as well as the associations with TMS metrics, underscore the potential of these neurophysiological measures in guiding personalized rehabilitation strategies for stroke patients. Full article
(This article belongs to the Special Issue The Application of EEG in Neurorehabilitation)
20 pages, 7305 KiB  
Article
The Use of Air Pressure Measurements Within a Sealed Moonpool for Sea-State Estimation
by Brendan Walsh, Robert Carolan, Mark Boland, Thomas Dooley and Thomas Kelly
J. Mar. Sci. Eng. 2024, 12(12), 2306; https://doi.org/10.3390/jmse12122306 (registering DOI) - 15 Dec 2024
Viewed by 236
Abstract
To assess the viability of locations for wave energy farms and design effective coastal protection measures, knowledge of local wave regimes is required. The work described herein aims to develop a low-cost, self-powering wave-measuring device that comprises a floating buoy with a central [...] Read more.
To assess the viability of locations for wave energy farms and design effective coastal protection measures, knowledge of local wave regimes is required. The work described herein aims to develop a low-cost, self-powering wave-measuring device that comprises a floating buoy with a central moonpool. The relative motion of the water level in the moonpool to the buoy will pressurise and depressurise the air above the water column. The variation in air pressure may then be used to estimate the sea-state incident upon the buoy. Small-scale proof of concept tank testing was conducted at a 1:20 scale and at a larger 1:2.4 scale before a full-scale prototype was deployed at the Smartbay test site facility in Galway Bay, Ireland. A number of techniques by which full-scale sea states may be estimated from the pressure spectrum are explored. A successful technique, based on the average of multiple linear squared magnitude of the transfer functions obtained under different wave regimes is developed. The applicability of this technique is then confirmed using validation data obtained during the full-scale sea trials. While the technique has proven useful, investigation into potential seasonal bias has been conducted, and suggestions for further improvements to the technique, based on further calibration testing in real sea states, are proposed. Full article
(This article belongs to the Special Issue The Interaction of Ocean Waves and Offshore Structures)
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<p>A schematic showing the general arrangement of the JFC Seagull 5G3000 buoy as the full-scale tests [<a href="#B14-jmse-12-02306" class="html-bibr">14</a>]. (Dimensions in millimetres).</p>
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<p>The WASP deployed at the Marine Institute Galway Bay observatory, Ireland, in 2019.</p>
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<p>A single input/output system in the time domain and the frequency domain.</p>
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<p>Variation in battery voltage over the complete 24 h period of 21 April 2019.</p>
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<p>The air temperature in the day mark over the complete 24 h period of 21 April 2019.</p>
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<p>Variation in the air pressure above the water column in the sealed chamber of the WASP with respect to time for the complete 24 h period for 21 April 2019.</p>
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<p>Waverider spectrum for 21 April 04:00–04:30 (Note: for this spectrum, <span class="html-italic">Hs</span> was 0.48 m and <span class="html-italic">Tz</span> was 2.79 s).</p>
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<p>WASP pressure Spectrum for 21 April 04:00–04:30.</p>
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<p>All squared magnitude of transfer functions for each day in the month of March 2019. Each line represents results for a different day.</p>
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<p>Average squared magnitude of the transfer function for the entire month of March 2019.</p>
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<p>WASP vs. Waverider spectra for 21 April 2019, 12:00–12:30.</p>
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<p>WASP vs. Waverider spectra for 5 May 2019, 14:00–14:30.</p>
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<p>Comparison between estimated WASP vs. measured Rider <span class="html-italic">Hs</span> values for June 2019 using the March average of the squared magnitude of the transfer function.</p>
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<p>Comparison between estimated WASP vs. measured Rider <span class="html-italic">Tz</span> values for June 2019 using the March average of the squared magnitude of the transfer function.</p>
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<p>WASP vs. Rider <span class="html-italic">Hs</span> values for June 2019 using data for the squared magnitude of the average transfer function for June.</p>
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<p>WASP vs. Rider <span class="html-italic">Hs</span> values for June 2019 using the squared magnitude of the average squared magnitude of the transfer function from the March, April, and May data.</p>
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<p>Five average pressure RMS of the squared magnitude of the transfer functions for March in a range of bands.</p>
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<p>Comparison between the Waverider and the WASP <span class="html-italic">Hs</span> values for June using the single squared magnitude of the transfer function approach and the pressure RMS average of the squared magnitude of the transfer function piecewise approach.</p>
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15 pages, 463 KiB  
Review
Lepton Asymmetries in Cosmology
by Massimiliano Lattanzi and Mauro Moretti
Symmetry 2024, 16(12), 1657; https://doi.org/10.3390/sym16121657 (registering DOI) - 15 Dec 2024
Viewed by 328
Abstract
The cosmological lepton asymmetry, i.e., an excess of leptons over antileptons, is still only loosely constrained, and might be much larger than its tiny baryonic counterpart. If this is the case, charge neutrality requires the lepton asymmetries to be confined in the neutrino [...] Read more.
The cosmological lepton asymmetry, i.e., an excess of leptons over antileptons, is still only loosely constrained, and might be much larger than its tiny baryonic counterpart. If this is the case, charge neutrality requires the lepton asymmetries to be confined in the neutrino sector. We recall the observational effects of neutrino asymmetries on the abundance of light elements produced during Big Bang Nucleosynthesis and on the pattern of cosmic microwave background anisotropies. We point to the necessity of solving the neutrino transport equations, taking into account the effect of flavour oscillation, to derive general and robust constraints on lepton asymmetries. We review the current bounds and briefly discuss prospects for next-generation CMB experiments. Full article
(This article belongs to the Special Issue Symmetry in Cosmological Theories and Observations)
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Figure 1
<p>Constraints on <math display="inline"><semantics> <msub> <mi>N</mi> <mi>eff</mi> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>Y</mi> <mi>p</mi> </msub> </semantics></math> from Planck 2018 temperature, polarization and lensing data. The shaded yellow ellipses show the 68% and 95% regions when both <math display="inline"><semantics> <msub> <mi>N</mi> <mi>eff</mi> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>Y</mi> <mi>p</mi> </msub> </semantics></math> are left free to vary. The blue bands show constraints on each individual parameter when either <math display="inline"><semantics> <msub> <mi>N</mi> <mi>eff</mi> </msub> </semantics></math> is fixed to the standard value <math display="inline"><semantics> <msub> <mi>N</mi> <mi>eff</mi> </msub> </semantics></math> = 3.044 (for <math display="inline"><semantics> <msub> <mi>Y</mi> <mi>p</mi> </msub> </semantics></math>) or <math display="inline"><semantics> <msub> <mi>Y</mi> <mi>p</mi> </msub> </semantics></math> is computed according to the standard BBN picture (for <math display="inline"><semantics> <msub> <mi>N</mi> <mi>eff</mi> </msub> </semantics></math>). The dashed lines are the curves of constant <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>d</mi> </msub> <mo>/</mo> <msub> <mi>r</mi> <mi>s</mi> </msub> </mrow> </semantics></math>, according to Equation (<a href="#FD20-symmetry-16-01657" class="html-disp-formula">20</a>).</p>
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<p><math display="inline"><semantics> <mrow> <mo>Δ</mo> <msup> <mi>χ</mi> <mn>2</mn> </msup> </mrow> </semantics></math> (relative to the case of vanishing chemical potentials), as a function of <math display="inline"><semantics> <mi>ξ</mi> </semantics></math>. In both panels we assume a determination of the ratio <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>d</mi> </msub> <mo>/</mo> <msub> <mi>r</mi> <mi>s</mi> </msub> </mrow> </semantics></math> from CMB observations, with relative accuracy ranging from <math display="inline"><semantics> <msup> <mn>10</mn> <mrow> <mo>−</mo> <mn>3</mn> </mrow> </msup> </semantics></math> (leftmost curve) to <math display="inline"><semantics> <mrow> <mn>3</mn> <mo>×</mo> <msup> <mn>10</mn> <mrow> <mo>−</mo> <mn>3</mn> </mrow> </msup> </mrow> </semantics></math> (rightmost curve). The horizontal lines correspond to 95% and 99% frequentist CLs. (<b>Left</b>): case <math display="inline"><semantics> <mrow> <msub> <mi>ξ</mi> <mi>e</mi> </msub> <mo>≳</mo> <msub> <mi>ξ</mi> <mrow> <mi>μ</mi> <mo>,</mo> <mi>τ</mi> </mrow> </msub> </mrow> </semantics></math> (see text for details). (<b>Right</b>): case <math display="inline"><semantics> <mrow> <msub> <mi>ξ</mi> <mi>e</mi> </msub> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math>. Note the different scale in the horizontal axes of the two panels.</p>
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<p>(<b>Left</b>): common value of the dimensionless chemical potential after equalization <math display="inline"><semantics> <msub> <mi>ξ</mi> <mi>fin</mi> </msub> </semantics></math> as a function of the electron neutrino chemical potential <math display="inline"><semantics> <msub> <mi>ξ</mi> <mrow> <mi>e</mi> <mo>,</mo> <mi>i</mi> <mi>n</mi> </mrow> </msub> </semantics></math> before equalization (solid blue line). We assume that perfect equalization occurs, i.e., <math display="inline"><semantics> <mrow> <msub> <mi>ξ</mi> <mrow> <mi>e</mi> <mo>,</mo> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <msub> <mi>ξ</mi> <mrow> <mi>μ</mi> <mo>,</mo> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <msub> <mi>ξ</mi> <mrow> <mi>τ</mi> <mo>,</mo> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <msub> <mi>ξ</mi> <mrow> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math>, and that it takes place well before neutrino decoupling. We use conservation of the total lepton asymmetry and of comoving energy to relate the initial temperature and chemical potentials to their final value, as in Section IIA of [<a href="#B50-symmetry-16-01657" class="html-bibr">50</a>]. We further assume that <math display="inline"><semantics> <mrow> <msub> <mi>ξ</mi> <mrow> <mi>μ</mi> <mo>,</mo> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <msub> <mi>ξ</mi> <mrow> <mi>τ</mi> <mo>,</mo> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math>. The dashed black line corresponds to <math display="inline"><semantics> <mrow> <msub> <mi>ξ</mi> <mi>fin</mi> </msub> <mo>=</mo> <msub> <mi>ξ</mi> <mi>e</mi> </msub> <mo>/</mo> <mn>3</mn> </mrow> </semantics></math>. The plot shows how the final chemical potential is very close to the average of the initial values. (<b>Right</b>): Initial (blue) and final (yellow) values of <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>N</mi> <mi>eff</mi> </msub> </mrow> </semantics></math> computed from Equation (<a href="#FD8-symmetry-16-01657" class="html-disp-formula">8</a>) with the corresponding chemical potentials. Comparison between the curves shows that the final <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>N</mi> <mi>eff</mi> </msub> </mrow> </semantics></math> can be sensibly smaller than its initial value. We also show, as the red curve, the value of <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>N</mi> <mi>eff</mi> </msub> </mrow> </semantics></math> derived from the full solution of the neutrino QKE with the same initial conditions [<a href="#B50-symmetry-16-01657" class="html-bibr">50</a>] (the data used to reconstruct this curve are publicly available at <a href="https://doi.org/10.5281/zenodo.11123226" target="_blank">https://doi.org/10.5281/zenodo.11123226</a> (accessed date: 15 November 2024)). This further shows that the assumptions of perfect equilibration of the asymmetries and thermalization with the plasma, used to derive the yellow curve, can still lead to a significant misestimation of <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>N</mi> <mi>eff</mi> </msub> </mrow> </semantics></math> as compared to the one obtained from the solution of the QKEs.</p>
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19 pages, 496 KiB  
Review
Pulsar Kick: Status and Perspective
by Gaetano Lambiase and Tanmay Kumar Poddar
Symmetry 2024, 16(12), 1649; https://doi.org/10.3390/sym16121649 - 13 Dec 2024
Viewed by 216
Abstract
The high speeds seen in rapidly rotating pulsars after supernova explosions present a longstanding puzzle in astrophysics. Numerous theories have been suggested over the years to explain this sudden "kick" imparted to the neutron star, yet each comes with its own set of [...] Read more.
The high speeds seen in rapidly rotating pulsars after supernova explosions present a longstanding puzzle in astrophysics. Numerous theories have been suggested over the years to explain this sudden "kick" imparted to the neutron star, yet each comes with its own set of challenges and limitations. Key explanations for pulsar kicks include hydrodynamic instabilities in supernovae, anisotropic neutrino emission, asymmetries in the magnetic field, binary system disruption, and physics beyond the Standard Model. Unraveling the origins of pulsar kicks not only enhances our understanding of supernova mechanisms but also opens up possibilities for exploring new physics. In this brief review, we will introduce pulsar kicks, examine the leading hypotheses, and explore future directions for this intriguing phenomenon. Full article
(This article belongs to the Section Physics)
21 pages, 5317 KiB  
Article
A 6.7 μW Low-Noise, Compact PLL with an Input MEMS-Based Reference Oscillator Featuring a High-Resolution Dead/Blind Zone-Free PFD
by Ahmed Kira, Mohannad Y. Elsayed, Karim Allidina, Vamsy P. Chodavarapu and Mourad N. El-Gamal
Sensors 2024, 24(24), 7963; https://doi.org/10.3390/s24247963 - 13 Dec 2024
Viewed by 271
Abstract
This article reports a 110.2 MHz ultra-low-power phase-locked loop (PLL) for MEMS timing/frequency reference oscillator applications. It utilizes a 6.89 MHz MEMS-based oscillator as an input reference. An ultra-low-power, high-resolution phase-frequency detector (PFD) is utilized to achieve low-noise performance. Eliminating the reset feedback [...] Read more.
This article reports a 110.2 MHz ultra-low-power phase-locked loop (PLL) for MEMS timing/frequency reference oscillator applications. It utilizes a 6.89 MHz MEMS-based oscillator as an input reference. An ultra-low-power, high-resolution phase-frequency detector (PFD) is utilized to achieve low-noise performance. Eliminating the reset feedback path used in conventional PFDs leads to dead/blind zone-free phase characteristics, which are crucial for low-noise applications within a wide operating frequency range. The PFD operates up to 2.5 GHz and achieves a linear resolution of 100 ps input time difference (Δtin), without the need for any additional calibration circuits. The linearity of the proposed PFD is tested over a phase difference corresponding to aa Δtin ranging from 100 ps to 50 ns. At a 1 V supply voltage, it shows an error of <±1.6% with a resolution of 100 ps and a frequency-normalized power consumption (Pn) of 0.106 pW/Hz. The PLL is designed and fabricated using a TSMC 65 nm CMOS process instrument and interfaced with the MEMS-based oscillator. The system reports phase noises of −106.21 dBc/Hz and −135.36 dBc/Hz at 1 kHz and 1 MHz offsets, respectively. It consumes 6.709 μW at a 1 V supply and occupies an active CMOS area of 0.1095 mm2. Full article
(This article belongs to the Special Issue Innovative Devices and MEMS for Sensing Applications)
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<p>The PLL system with its MEMS-based input reference oscillator.</p>
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<p>MEMS -based oscillator: (<b>a</b>) system block diagram; (<b>b</b>) measured MEMS electrical transmission (S21); (<b>c</b>) extracted RLC electrical equivalent linear model; (<b>d</b>) TIA circuit design.</p>
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<p>A simplified diagram of the PLL (<b>a</b>) ring-based VCO and (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>N</mi> <mo>=</mo> <mn>16</mn> </mrow> </semantics></math> divider.</p>
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<p>(<b>a</b>) Standard current-based and (<b>b</b>) charge transfer-based CPs.</p>
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<p>(<b>a</b>) A PFD state machine. (<b>b</b>) Traditional tri-state PFD block and (<b>c</b>) timing diagrams.</p>
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<p>Circuit diagram of the proposed PFD.</p>
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<p>Proposed PFD: (<b>a</b>) transfer curve; (<b>b</b>) Monte Carlo histograms (N = 500) of the <math display="inline"><semantics> <mrow> <mi>U</mi> <mi>P</mi> </mrow> </semantics></math> output at <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>t</mi> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math> = 1 ns.</p>
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<p>Error under PVT variations.</p>
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<p>(<b>a</b>) Fabricated die micrograph; (<b>b</b>) photograph of the testing board used to test the PFD.</p>
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<p><math display="inline"><semantics> <mrow> <mi>R</mi> <mi>E</mi> <mi>F</mi> </mrow> </semantics></math> leads <math display="inline"><semantics> <mrow> <mi>F</mi> <mi>B</mi> </mrow> </semantics></math>: (<b>a</b>) <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>t</mi> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math> = 125 ns; (<b>b</b>) <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>t</mi> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math> = 470 ns.</p>
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<p><math display="inline"><semantics> <mrow> <mi>R</mi> <mi>E</mi> <mi>F</mi> </mrow> </semantics></math> lags <math display="inline"><semantics> <mrow> <mi>F</mi> <mi>B</mi> </mrow> </semantics></math>: (<b>a</b>) <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>t</mi> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math> = −125 ns; and (<b>b</b>) <math display="inline"><semantics> <mrow> <mo>Δ</mo> <msub> <mi>t</mi> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math> = −470 ns.</p>
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<p>Stand-alone PFD validation: (<b>a</b>) picture of the actual setup; (<b>b</b>) setup block diagram.</p>
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<p>Measured PFD error compared to simulation.</p>
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<p>Measured phase noise at a 110.2 MHz output frequency.</p>
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<p>Breakdown of the power consumption of the system at a 110.2 MHz output frequency.</p>
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<p>(<b>a</b>) Picture of the wire-bonded dies in the package. (<b>b</b>) Zoomed-in view of the MEMS device wire-bonded to the CMOS die, forming the system. (<b>c</b>) Photograph of the testing board used to test the system.</p>
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18 pages, 2145 KiB  
Article
Modified Ji-Huan He’s Frequency Formulation for Large-Amplitude Electron Plasma Oscillations
by Stylianos Vasileios Kontomaris, Anna Malamou, Ioannis Psychogios and Gamal M. Ismail
Atoms 2024, 12(12), 68; https://doi.org/10.3390/atoms12120068 - 12 Dec 2024
Viewed by 310
Abstract
This paper examines oscillations governed by the generic nonlinear differential equation u=ωp021u2β2uγ, where ωp0, β and γ are positive constants. The aforementioned differential [...] Read more.
This paper examines oscillations governed by the generic nonlinear differential equation u=ωp021u2β2uγ, where ωp0, β and γ are positive constants. The aforementioned differential equation is of particular importance, as it describes electron plasma oscillations influenced by temperature effects and large oscillation amplitudes. Since no analytical solution exists for the oscillation period in terms of ωp0, β,γ and the oscillation amplitude, accurate approximations are derived. A modified He’s approach is used to account for the non-symmetrical oscillation around the equilibrium position. The motion is divided into two parts: uminu<ueq and ueq<uumax, where umin and umax are the minimum and maximum values of u, and ueq is its equilibrium value. The time intervals for each part are calculated and summed to find the oscillation period. The proposed method shows remarkable accuracy compared to numerical results. The most significant result of this paper is that He’s approach can be readily extended to strongly non-symmetrical nonlinear oscillations. It is also demonstrated that the same approach can be extended to any case where each segment of the function f(u) in the differential equation u+fu=0 (for uminu<ueq and for ueq<uumax) can be approximated by a fifth-degree polynomial containing only odd powers. Full article
(This article belongs to the Special Issue Electronic, Photonic and Ionic Interactions with Atoms and Molecules)
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Figure 1
<p>Phase diagrams for the positive sign in Equations (7)–(10) are shown in (<b>a</b>) (i–iii) and phase diagrams for the negative sign in Equations (7)–(10) are shown in (<b>b</b>) (i–iii) for <math display="inline"><semantics> <mrow> <mi>β</mi> <mo>=</mo> <mn>0.25</mn> <mo>,</mo> <mn>0.26</mn> <mo>,</mo> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">n</mi> <mi mathvariant="normal">d</mi> <mn>0.27</mn> </mrow> </semantics></math>.</p>
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<p>The case of γ = 1 (<math display="inline"><semantics> <mrow> <mn>0</mn> <mo>≤</mo> <mi>β</mi> <mo>≤</mo> <mn>0.26</mn> </mrow> </semantics></math>). The oscillation’s period with respect to parameter β for the case of the upper negative sign in Equation (6). The accurate numerical results are presented comparatively to the results obtained using Equation (17).</p>
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<p>The case of γ = 1 (<math display="inline"><semantics> <mrow> <mn>0</mn> <mo>≤</mo> <mi>β</mi> <mo>≤</mo> <mn>0.26</mn> </mrow> </semantics></math>). The oscillation’s period with respect to parameter β for the case of the positive sign in Equation (6). The accurate numerical results are presented comparatively to the results obtained using Equation (17).</p>
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<p>The case of γ = 3 (<math display="inline"><semantics> <mrow> <mn>0</mn> <mo>≤</mo> <mi>β</mi> <mo>≤</mo> <mn>0.14</mn> </mrow> </semantics></math>). The oscillation period with respect to the parameter <span class="html-italic">β</span> for the upper negative sign in Equation (6). The accurate numerical results are presented in comparison to the first and second approximations.</p>
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<p>The case of γ = 3 (<math display="inline"><semantics> <mrow> <mn>0</mn> <mo>≤</mo> <mi>β</mi> <mo>≤</mo> <mn>0.26</mn> </mrow> </semantics></math>). The oscillation period with respect to the parameter <span class="html-italic">β</span> for the positive sign in Equation (6). The accurate numerical results are compared with those obtained using Equation (17).</p>
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<p>The case of γ = 1 and β = 0.26. The data of the two parts of the curve (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> <mo>&lt;</mo> <mi>u</mi> <mo>≤</mo> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>m</mi> <mi>a</mi> <mi>x</mi> </mrow> </msub> </mrow> </semantics></math>) and (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>m</mi> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>≤</mo> <mi>u</mi> <mo>&lt;</mo> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </semantics></math>) were accurately fitted to an equation of the form <math display="inline"><semantics> <mrow> <mi>g</mi> <mfenced separators="|"> <mrow> <mi>u</mi> </mrow> </mfenced> <mo>=</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mn>1</mn> </mrow> </msub> <mfenced separators="|"> <mrow> <mi>u</mi> <mo>−</mo> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </mfenced> <mo>+</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mn>2</mn> </mrow> </msub> <msup> <mrow> <mfenced separators="|"> <mrow> <mi>u</mi> <mo>−</mo> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </mfenced> </mrow> <mrow> <mn>3</mn> </mrow> </msup> <mo>+</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mn>3</mn> </mrow> </msub> <msup> <mrow> <mfenced separators="|"> <mrow> <mi>u</mi> <mo>−</mo> <msub> <mrow> <mi>u</mi> </mrow> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </mfenced> </mrow> <mrow> <mn>5</mn> </mrow> </msup> </mrow> </semantics></math>.</p>
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15 pages, 1457 KiB  
Article
Artificial Intelligence in the New Era of Decision-Making: A Case Study of the Euro Stoxx 50
by Javier Parra-Domínguez and Laura Sanz-Martín
Mathematics 2024, 12(24), 3918; https://doi.org/10.3390/math12243918 - 12 Dec 2024
Viewed by 354
Abstract
This study evaluates machine learning models for stock market prediction in the European stock market EU50, with emphasis on the integration of key technical indicators. Advanced techniques, such as ANNs, CNNs and LSTMs, are applied to analyze a large EU50 dataset. Key indicators, [...] Read more.
This study evaluates machine learning models for stock market prediction in the European stock market EU50, with emphasis on the integration of key technical indicators. Advanced techniques, such as ANNs, CNNs and LSTMs, are applied to analyze a large EU50 dataset. Key indicators, such as the simple moving average (SMA), exponential moving average (EMA), moving average convergence/divergence (MACD), stochastic oscillator, relative strength index (RSI) and accumulation/distribution (A/D), were employed to improve the model’s responsiveness to market trends and momentum shifts. The results show that CNN models can effectively capture localized price patterns, while LSTM models excel in identifying long-term dependencies, which is beneficial for understanding market volatility. ANN models provide reliable benchmark predictions. Among the models, CNN with RSI obtained the best results, with an RMSE of 0.0263, an MAE of 0.0186 and an R2 of 0.9825, demonstrating high accuracy in price prediction. The integration of indicators such as SMA and EMA improves trend detection, while MACD and RSI increase the sensitivity to momentum, which is essential for identifying buy and sell signals. This research demonstrates the potential of machine learning models for refined stock prediction and informs data-driven investment strategies, with CNN and LSTM models being particularly well suited for dynamic price prediction. Full article
(This article belongs to the Special Issue Artificial Intelligence and Data Science)
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<p>Evolution of closing price of EURO STOXX 50.</p>
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<p>Evolution of volatility of EURO STOXX 50.</p>
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<p>Candlestick chart for the last 100 days with the 20-day and 100-day SMA, green candles indicate an increase in the price of the asset and red candles indicate a decrease.</p>
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<p>Comparison of predictions with actual model values with CNN+RSI characteristics.</p>
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27 pages, 10660 KiB  
Article
Numerical Simulation of Hydrodynamic Performance of an Offshore Oscillating Water Column Wave Energy Converter Device
by Peng Tang, Xinyi Lin, Wei Wang and Hongsheng Zhang
J. Mar. Sci. Eng. 2024, 12(12), 2289; https://doi.org/10.3390/jmse12122289 - 12 Dec 2024
Viewed by 319
Abstract
Wave energy, as a renewable energy source, plays a significant role in sustainable energy development. This study focuses on a dual-chamber offshore oscillating water column (OWC) wave energy device and performs numerical simulations to analyze the influence of chamber geometry on hydrodynamic characteristics [...] Read more.
Wave energy, as a renewable energy source, plays a significant role in sustainable energy development. This study focuses on a dual-chamber offshore oscillating water column (OWC) wave energy device and performs numerical simulations to analyze the influence of chamber geometry on hydrodynamic characteristics and wave energy conversion efficiency. Unlike existing studies primarily focused on single-chamber configurations, the hydrodynamic characteristics of dual-chamber OWCs are relatively underexplored, especially regarding the impact of critical design parameters on performance. In this study, STAR-CCM+ V2302 software (Version 2410, Siemens Digital Industrial Software, Plano, TX, USA) is utilized to systematically evaluate the effects of key design parameters (including turbine configuration, mid-wall draught depth, and wall angles) on the hydrodynamic performance, wave energy capture efficiency, and wave reflection and loading characteristics of the device. The findings aim to provide a reference framework for the optimal design of dual-chamber OWC systems. The results show that the dual-chamber, dual-turbine (2C2T) configuration offers a 31.32% improvement in efficiency compared to the single-chamber, single-turbine (1C1T) configuration at low wave frequencies. In terms of reducing wave reflection and transmission, the 2C2T configuration outperforms the dual-chamber, single-turbine configuration. When the wall angle increases from 0° to 40°, the total efficiency increases by 166.37%, and the horizontal load decreases by 20.05%. Additionally, optimizing the mid-wall draught depth results in a 9.6% improvement in efficiency and a reduction of vertical load by 11.69%. Full article
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Figure 1
<p>Schematic diagram of a two-dimensional OWC device.</p>
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<p>Diagram of the offshore-stationary OWC devices. (<b>a</b>) Dual chambers dual turbines OWC with sloping wall(2C2T); (<b>b</b>) Dual chambers single turbine OWC (2C1T).</p>
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<p>Mesh of single chamber.</p>
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<p>Comparison of numerical simulation results with physical experimental data from Elhanafi et al. [<a href="#B37-jmse-12-02289" class="html-bibr">37</a>] for H = 0.05 m and T = 1.2 s. (<b>a</b>) Wave height at the center of the chamber; (<b>b</b>) Pressure in the chamber.</p>
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<p>Verification results with physical experimental data from Elhanafi et al. [<a href="#B37-jmse-12-02289" class="html-bibr">37</a>] of energy conversion efficiency of single chamber OWC device.</p>
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<p>Comparison of numerical simulation of wave loads with physical experiment results of Elhanafi et al. [<a href="#B38-jmse-12-02289" class="html-bibr">38</a>]. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of numerical simulation of wave loads with physical experiment results of Elhanafi et al. [<a href="#B38-jmse-12-02289" class="html-bibr">38</a>]. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of wave energy conversion efficiency of different chamber types.</p>
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<p>Comparison of Pressure of different chamber types.</p>
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<p>Comparison of orifice flow rates of different chamber types.</p>
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<p>Vortex distribution of different structures. (<b>a</b>) Vortex distribution on 2C1T at T = 1.3 s. (<b>b</b>) Vortex distribution on 2C2T at T = 1.3 s. (<b>c</b>) Vortex distribution on 2C1T at T = 1.6 s. (<b>d</b>) Vortex distribution on 2C2T at T = 1.6 s.</p>
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<p>Comparison of loads of different chamber types. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of reflection coefficients of different chamber types.</p>
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<p>Comparison of transmission coefficients of different chamber types.</p>
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<p>Comparison of the efficiency of different intermediate wall drafts. (<b>a</b>) The front chamber efficiency; (<b>b</b>) The rear chamber efficiency; (<b>c</b>) Total efficiency.</p>
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<p>Comparison of the efficiency of different intermediate wall drafts. (<b>a</b>) The front chamber efficiency; (<b>b</b>) The rear chamber efficiency; (<b>c</b>) Total efficiency.</p>
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<p>Comparison of loads of different intermediate wall draughts. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of loads of different intermediate wall draughts. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of reflection coefficients of different intermediate wall draughts.</p>
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<p>Comparison of transmission coefficients of different intermediate wall draughts.</p>
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<p>Comparison of the efficiency of different intermediate wall drafts. (<b>a</b>) The front chamber efficiency; (<b>b</b>) The rear chamber efficiency; (<b>c</b>) Total efficiency.</p>
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<p>Comparison of loads of different intermediate wall draughts. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of loads of different intermediate wall draughts. (<b>a</b>) Horizontal wave loads; (<b>b</b>) Vertical wave loads.</p>
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<p>Comparison of reflection coefficients of different wall angles.</p>
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<p>Comparison of transmission coefficients of different wall angles.</p>
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19 pages, 12447 KiB  
Article
Characteristics of Strong Cooling Events in Winter of Northeast China and Their Association with 10–20 d Atmosphere Low-Frequency Oscillation
by Qianhao Wang and Liping Li
Atmosphere 2024, 15(12), 1486; https://doi.org/10.3390/atmos15121486 (registering DOI) - 12 Dec 2024
Viewed by 314
Abstract
In the past 42 years from 1980 to 2021, 103 regional strong cooling events (RSCEs) occurred in winter in Northeast China, and the frequency has increased significantly in the past 10 years, averaging 2.45 per year. The longest (shortest) duration is 10 (2) [...] Read more.
In the past 42 years from 1980 to 2021, 103 regional strong cooling events (RSCEs) occurred in winter in Northeast China, and the frequency has increased significantly in the past 10 years, averaging 2.45 per year. The longest (shortest) duration is 10 (2) days. The minimum temperature series in 60 events exists in 10–20 d of significant low-frequency (LF) periods. The key LF circulation systems affecting RSCEs include the Lake Balkhash–Baikal ridge, the East Asian trough (EAT), the robust Siberian high (SH) and the weaker (stronger) East Asian temperate (subtropical) jet, with the related anomaly centers moving from northwest to southeast and developing into a nearly north–south orientation. The LF wave energy of the northern branch from the Atlantic Ocean disperses to Northeast China, which excites the downstream disturbance wave train. The corresponding LF positive vorticity enhances and moves eastward, leading to the formation of deep EAT. The enhanced subsidence motion behind the EAT leads to SH strengthening. The cold advection related to the northeast cold vortex is the main thermal factor causing the local temperature to decrease. The Scandinavian Peninsula is the primary cold air source, and the Laptev Sea is the secondary one, with cold air from the former along northwest path via the West Siberian Plain and Lake Baikal, and from the latter along the northern path via the Central Siberian Plateau, both converging towards Northeast China. Full article
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<p>The regional average frequency of the winter RSCEs in Northeast China from 1980 to 2021. Unit: number of occurrences.</p>
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<p>(<b>a</b>) Morlet wavelet energy spectrum of the regional average daily minimum temperature in the winter of 2020 in Northeast China (contours). The shaded area is significant at the 0.1 level. The area between the red vertical lines is winter, while the red horizontal lines correspond to 10 d, 20 d, 30 d, 60 d, and 90 d, respectively. (<b>b</b>) The above minimum temperature series (bar, °C) and its 10–20 d components (solid line, °C). The interval between the two vertical lines denotes the strong cooling process, with the 3–7 phase.</p>
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<p>The 10–20 d (<b>a1</b>–<b>a3</b>) 300 hPa zonal wind fields (shaded, m/s), (<b>b1</b>–<b>b3</b>) 500 hPa geopotential height fields (shaded, gpm; contours: unfiltered), (<b>c1</b>–<b>c3</b>) 850 hPa wind (vectors, m/s) and temperature fields (shaded, <span class="html-italic">K</span>), and (<b>d1</b>–<b>d3</b>) SLP fields (shaded, hPa; contours: unfiltered) composited by 60 RSCEs at phases 3, 5, and 7, respectively. The dotted areas are significant at the 0.01 level. “+” (“−”) indicates a positive (negative) anomaly.</p>
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<p>(<b>a</b>–<b>c</b>) The 850 hPa 10–20 d isobaric PV (shaded, <math display="inline"><semantics> <mrow> <mi>P</mi> <mi>V</mi> <mi>U</mi> </mrow> </semantics></math>) fields composited by 60 RSCEs at phases 3, 5, and 7, respectively. The dotted areas are significant at the 0.01 level. “+” (“−”) indicates a positive (negative) anomaly.</p>
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<p>Height–longitude profiles of meridional average 10–20 d (<b>a</b>–<b>c</b>) vorticity (shaded, <math display="inline"><semantics> <msup> <mn>10</mn> <mrow> <mo>−</mo> <mn>6</mn> </mrow> </msup> </semantics></math> s<sup>−1</sup>) and (<b>d</b>–<b>f</b>) divergence (shaded, 10<sup>−7</sup> s<sup>−1</sup>) along the latitudes 50–70° N, 50–60° N and 40–55° N at phases 3, 5, and 7, respectively. The vector is 10–20 d vertical zonal circulation (m/s). The dotted areas are significant at the 0.01 level.</p>
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<p>(<b>a</b>–<b>c</b>) 300 hPa 10–20 d horizontal WAF (vector, m<sup>2</sup>/s<sup>2</sup>) and its divergence (shaded, <math display="inline"><semantics> <msup> <mn>10</mn> <mrow> <mo>−</mo> <mn>8</mn> </mrow> </msup> </semantics></math> m/s<sup>2</sup>) and 10–20 d geostrophic stream function (contours, <math display="inline"><semantics> <msup> <mn>10</mn> <mn>5</mn> </msup> </semantics></math> m<sup>2</sup>s) composited by 60 RSCEs at phases 3, 5, and 7, respectively. The dotted areas are significant at the 0.01 level.</p>
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<p>The 850 hPa 10–20 d (<b>a</b>–<b>c</b>) local temperature change, (<b>d</b>–<b>f</b>) temperature advection, (<b>g</b>–<b>i</b>) vertical motion adiabatic change, and (<b>j</b>–<b>l</b>) diabatic heating composited by 60 RSCEs at phases 3, 5, and 7, respectively. Unit: K/day, the dotted areas are significant at the 0.01 level.</p>
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<p>The 850 hPa 10–20 d thermodynamic energy equation evolution of each term’s regional mean in Northeast China at phases 3–7.</p>
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<p>(<b>a</b>) Weighted K-means clustering of stations in Northeast China; the “▼” are for four representative stations (S1, S2, S3, and S4) and the “★” are for the cluster centers. (<b>b</b>) The cold air HYSPLIT backward trajectory simulation for 60 RSCEs at four representative stations in Northeast China. The percentage represents the contribution ratio.</p>
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