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30 pages, 17191 KiB  
Review
Review of the Near-Water Effect of Rotors in Cross-Media Vehicles
by Xingzhi Bai, Mingqing Lu, Qi Zhan, Yu Wang, Daixian Zhang, Xiao Wang and Wenhua Wu
Drones 2025, 9(3), 195; https://doi.org/10.3390/drones9030195 - 7 Mar 2025
Abstract
Cross-media vehicles, which combine the advantages of airplanes and submarines, are capable of performing complex tasks in different media and have attracted significant interest in recent years. In practice, however, cross-media rotorcrafts face numerous challenges during the cross-media transition, one of which is [...] Read more.
Cross-media vehicles, which combine the advantages of airplanes and submarines, are capable of performing complex tasks in different media and have attracted significant interest in recent years. In practice, however, cross-media rotorcrafts face numerous challenges during the cross-media transition, one of which is the complex mixed air–water flows induced by their rotors operating in close proximity to the water surface. These flows can result in aerodynamic penalties and structural damage to the rotors. The interactions between a water surface and a rotor wake bring about potential risks of cross-media locomotion, which is known as the near-water effect of rotors. Given that the distinctions between the near-water effect and the ground effect of rotors are not yet widely understood, this study details the discovery of the near-water effect and provides a comprehensive review of the evolutionary development of the near-water effect, tracing its understanding from the ground effect to the influence of droplets through aerodynamic modeling, numerical simulations, and near-water experimental studies. Furthermore, open problems and challenges associated with the near-water effect are discussed, including flow field measurements and numerical simulation approaches. Additionally, potential applications of the near-water effect for the development of cross-media rotorcraft are also described, which are valuable for aerodynamic design and cross-media control. Full article
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Figure 1

Figure 1
<p>Representative cross-media vehicles (CMVs): (<b>a</b>) multi-rotored [<a href="#B12-drones-09-00195" class="html-bibr">12</a>]; (<b>b</b>) fixed-winged [<a href="#B7-drones-09-00195" class="html-bibr">7</a>]; (<b>c</b>) hybrid-winged [<a href="#B9-drones-09-00195" class="html-bibr">9</a>]; (<b>d</b>) bioinspired [<a href="#B11-drones-09-00195" class="html-bibr">11</a>]; and (<b>e</b>) hydrofoil [<a href="#B13-drones-09-00195" class="html-bibr">13</a>] vehicles.</p>
Full article ">Figure 2
<p>Typical water exit modes for multi-rotor and fixed-wing CMVs [<a href="#B16-drones-09-00195" class="html-bibr">16</a>].</p>
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<p>(<b>a</b>) Schematic of near–water effect; (<b>b</b>) mixed air–water flows induced by rotor [<a href="#B17-drones-09-00195" class="html-bibr">17</a>].</p>
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<p>Image sequence showing the mini-CMV breaching the water surface [<a href="#B27-drones-09-00195" class="html-bibr">27</a>].</p>
Full article ">Figure 5
<p>(<b>a</b>) Tested <span class="html-italic">D</span> = 0.56 m and <span class="html-italic">D</span> = 0.25 m commercial rotor blades; (<b>b</b>) mixed air–water flows induced by rotor at <span class="html-italic">z</span>/<span class="html-italic">R</span> = 0.4 [<a href="#B17-drones-09-00195" class="html-bibr">17</a>].</p>
Full article ">Figure 6
<p>Aerodynamic performance affected by near-water effect [<a href="#B17-drones-09-00195" class="html-bibr">17</a>]: (<b>a</b>) thrust coefficient of <span class="html-italic">D</span> = 0.56 m blade; (<b>b</b>) torque coefficient of <span class="html-italic">D</span> = 0.56 m blade; (<b>c</b>) thrust coefficient of <span class="html-italic">D</span> = 0.25 m blade; (<b>d</b>) thrust versus power of <span class="html-italic">D</span> = 0.56 m blade under NEW, IGE, and OGE states at <span class="html-italic">z</span>/<span class="html-italic">R</span> = 0.1; (<b>e</b>) thrust fluctuation caused by droplets of <span class="html-italic">D</span> = 0.56 m blade at <span class="html-italic">z</span>/<span class="html-italic">R</span> = 0.3; (<b>f</b>) structural damage caused by droplets on lower wing of <span class="html-italic">D</span> = 0.56 m blade.</p>
Full article ">Figure 7
<p>(<b>a</b>) Test platform; (<b>b</b>) rotor speed characteristic with height under the NWE at different throttle settings; (<b>c</b>) thrust characteristic with height under the NWE at different throttle settings; (<b>d</b>) comparison of rotor thrust under IGE vs. NWE [<a href="#B29-drones-09-00195" class="html-bibr">29</a>].</p>
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<p>(<b>a</b>) Image of rotor in transition (top: at low throttle, bottom: at high throttle); (<b>b</b>) the variance of the Transition Index as the rotor enters or exits the water at various throttle settings; (<b>c</b>) RPM versus throttle at various heights between fully-in-air and fully-in-water results [<a href="#B30-drones-09-00195" class="html-bibr">30</a>].</p>
Full article ">Figure 9
<p>Sequence diagram of cross-media locomotion [<a href="#B31-drones-09-00195" class="html-bibr">31</a>]. (<b>a</b>) t<sub>1</sub>=1.82 s; (<b>b</b>) t<sub>2</sub>=3.47 s; (<b>c</b>) t<sub>c</sub>=4.84 s; (<b>d</b>) t<sub>4</sub>=5.82 s; (<b>e</b>) t<sub>6</sub>=7.00 s.</p>
Full article ">Figure 10
<p>(<b>a</b>) Tilting ducted fan CMV; (<b>b</b>) rotor thrust characteristics under NWE and OGE conditions [<a href="#B32-drones-09-00195" class="html-bibr">32</a>].</p>
Full article ">Figure 11
<p>Comparison of experimental results (OGE vs. NWE) [<a href="#B34-drones-09-00195" class="html-bibr">34</a>]: (<b>a</b>) thrust; (<b>b</b>) power.</p>
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<p>Schematic of typical depression modes [<a href="#B35-drones-09-00195" class="html-bibr">35</a>] (the green arrows show the approximate trajectory of air, the red curve shows the approximate trajectory of the droplets entering the rotor disk): (<b>a</b>) dimpling; (<b>b</b>) splashing; (<b>c</b>) penetrating.</p>
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<p>Comparison of experimental results (OGE vs. NWE): (<b>a</b>) thrust characteristic of <span class="html-italic">D</span> = 1.3 m ducted fan under OGE, IGE, and NWE states [<a href="#B44-drones-09-00195" class="html-bibr">44</a>]; (<b>b</b>) spatial streamlines under NWE state [<a href="#B44-drones-09-00195" class="html-bibr">44</a>]; (<b>c</b>) thrust characteristic of <span class="html-italic">D</span> = 0.15 m ducted fan [<a href="#B45-drones-09-00195" class="html-bibr">45</a>]; (<b>d</b>) diagram of velocity vector [<a href="#B45-drones-09-00195" class="html-bibr">45</a>].</p>
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<p>Water surface shape: (<b>a</b>) simulation result for <span class="html-italic">D</span> = 1.3 m ducted fan [<a href="#B44-drones-09-00195" class="html-bibr">44</a>]; (<b>b</b>) simulation result for 0.15 m diameter ducted fan [<a href="#B45-drones-09-00195" class="html-bibr">45</a>]; (<b>c</b>) experimental result for <span class="html-italic">D</span> = 0.07 m ducted fan [<a href="#B35-drones-09-00195" class="html-bibr">35</a>].</p>
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<p>Velocity contour map and aerodynamic characteristics [<a href="#B47-drones-09-00195" class="html-bibr">47</a>]: (<b>a</b>) thrust coefficient at different rotor heights; (<b>b</b>) torque coefficient at different rotor heights; (<b>c</b>) the velocity magnitude field under the IGE state; (<b>d</b>) the velocity magnitude field under the NWE state.</p>
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<p>Time-averaged velocity field measured via PIV at different rotor heights off the water surface [<a href="#B35-drones-09-00195" class="html-bibr">35</a>] (arrows represent streamlines): (<b>a</b>) <span class="html-italic">z</span>/<span class="html-italic">R</span> = 0.5; (<b>b</b>) <span class="html-italic">z</span>/<span class="html-italic">R</span> = 0.2; (<b>c</b>) <span class="html-italic">z</span>/<span class="html-italic">R</span> = 0.1.</p>
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<p>Droplets generated by interface instability at low rotor speeds [<a href="#B35-drones-09-00195" class="html-bibr">35</a>]: (<b>a</b>) crown formation; (<b>b</b>) finger structure.</p>
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<p>Flow field through a hovering rotor under IGE (the left column in each subgraph) or FSE (the right column in each subgraph) conditions. Plots show sectional contours of dimensionless vorticity. The dark blue solid line represents the free surface at the end, while the black dashed line represents the free surface at the initial state [<a href="#B49-drones-09-00195" class="html-bibr">49</a>].</p>
Full article ">Figure 19
<p>Comparison of the normalized rotor thrust vs. dimensionless rotor-plane distance between the two proximity conditions. The black solid line represents the fitted curve under the IGE, while the red one represents the fitted curve under the FSE. <span class="html-italic">γ</span> represents dimensionless rotor height [<a href="#B49-drones-09-00195" class="html-bibr">49</a>].</p>
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<p>Experimental results [<a href="#B50-drones-09-00195" class="html-bibr">50</a>]: (<b>a</b>) thrust curve; (<b>b</b>) change in water surface.</p>
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<p>Simulation results [<a href="#B51-drones-09-00195" class="html-bibr">51</a>]: (<b>a</b>) trajectory tracking in the second simulation; (<b>b</b>) forces involved in the vehicle displacement.</p>
Full article ">Figure 22
<p>Optical interference caused by droplets and splashing.</p>
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<p>The effect of splash-reflected light outside the laser sheet on the cross-correlation calculations: (<b>a</b>) raw image; (<b>b</b>) cross-correlation results.</p>
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<p>Schematic of potential fountain effect as part of near-water effect for multi-rotor CMVs.</p>
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<p>Mixed air–water flows induced by multi-rotor system and thrust characteristics at <span class="html-italic">n</span> = 6600 r/min and <span class="html-italic">z/R</span> = 0.5.</p>
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<p>The water film remaining on the blade.</p>
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22 pages, 24215 KiB  
Article
Evaluation of Light Electric Flying-Wing Unmanned Aerial System Energy Consumption During Holding Maneuver
by Artur Kierzkowski, Bartłomiej Dziewoński, Krzysztof Kaliszuk and Mateusz Kucharski
Energies 2025, 18(5), 1300; https://doi.org/10.3390/en18051300 - 6 Mar 2025
Viewed by 154
Abstract
This study evaluates the energy consumption of a light electric flying-wing unmanned aerial system (UAS) during low-altitude holding maneuvers. Two flight patterns were investigated: circular holding at a specified altitude and a figure-eight trajectory. Test flights were conducted under varying meteorological and wind [...] Read more.
This study evaluates the energy consumption of a light electric flying-wing unmanned aerial system (UAS) during low-altitude holding maneuvers. Two flight patterns were investigated: circular holding at a specified altitude and a figure-eight trajectory. Test flights were conducted under varying meteorological and wind conditions, including scenarios where wind aligned and crossed the flight path. Key flight parameters such as pitch, yaw, heading deviation, flight altitude, ground speed, and airspeed were monitored. Concurrently, current and battery voltage were measured to compute the instantaneous power consumption of the propulsion system. This approach allowed for the determination and comparison of energy consumption across the two holding patterns. The outcomes contribute to a better understanding of power efficiency during prolonged flight maneuvers, supporting advancements in autonomous low-altitude UAS operations. Full article
(This article belongs to the Special Issue Challenges and Opportunities for Energy Economics and Policy)
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Figure 1

Figure 1
<p>PADA holding path with green holding enter zones and flight paths [<a href="#B3-energies-18-01300" class="html-bibr">3</a>].</p>
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<p>(<b>a</b>,<b>b</b>) USAF 10-2045 Northrop Grumman RQ4 Global Hawk UAV during high-altitude reconnaissance holding over Polish airspace [<a href="#B10-energies-18-01300" class="html-bibr">10</a>].</p>
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<p>Research flow chart.</p>
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<p>A design of an experiment path for assessing battery health [<a href="#B18-energies-18-01300" class="html-bibr">18</a>].</p>
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<p>Relation of battery capacity and flight endurance [<a href="#B20-energies-18-01300" class="html-bibr">20</a>].</p>
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<p>A two-dimensional free-body of the airplane in level flight. Reprinted with permission from ref. [<a href="#B26-energies-18-01300" class="html-bibr">26</a>]. Copyright 2022 Elsevier.</p>
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<p>Wing lift, drag, and moment acting at the wing’s aerodynamic center. Reprinted with permission from ref. [<a href="#B27-energies-18-01300" class="html-bibr">27</a>]. Copyright 2022 Elsevier.</p>
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<p>A turn performance map with compliance to 14 CFR Part 23. Reprinted with permission from refs. [<a href="#B26-energies-18-01300" class="html-bibr">26</a>,<a href="#B29-energies-18-01300" class="html-bibr">29</a>]. Copyright 2022 Elsevier.</p>
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<p>Forces on an aircraft in a level constant velocity turn. Reprinted with permission from ref. [<a href="#B26-energies-18-01300" class="html-bibr">26</a>]. Copyright 2022 Elsevier.</p>
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<p>Top view of a PADA airframe.</p>
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<p>The airfoils: MH45 (<b>a</b>) used in the wing section and S1046 (<b>b</b>) used in the central section [<a href="#B30-energies-18-01300" class="html-bibr">30</a>].</p>
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<p>Lift (<b>a</b>) and drag (<b>b</b>) coefficients characteristics for airfoils, with MH45 used in the wing section and S1045 used in the central section [<a href="#B30-energies-18-01300" class="html-bibr">30</a>].</p>
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<p>Aerodynamic polar of the PADA airframe.</p>
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<p>Theoretical holding patterns considered for energy consumption evaluation: circular (<b>a</b>) and figure-eight (<b>b</b>) patterns.</p>
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<p>PADA single motor thrust to power dependency in the effective range of over 4 g/W.</p>
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<p>Powered Autonomous Delivery Aircraft composite airframe.</p>
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<p>Diagram of measurement of voltage and current drawn within a circuit.</p>
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<p>Parts of measurement system: (<b>a</b>) measurement unit with INA139 amplifier and (<b>b</b>) LiPo battery.</p>
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<p>Example flight paths for the circle trajectory.</p>
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<p>Example flight paths for a trajectory in the shape of an 8 and straight sections. (<b>a</b>) straight segment; (<b>b</b>) figure-eight trajectories; (<b>c</b>) figure-eight with straight segment; (<b>d</b>) single figure-eight trajcetory.</p>
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<p>Three-dimensional view of the flight path with height profile. (<b>a</b>) trajectory; (<b>b</b>) barometer altitude and airspeed.</p>
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28 pages, 60546 KiB  
Article
Adapting Cross-Sensor High-Resolution Remote Sensing Imagery for Land Use Classification
by Wangbin Li, Kaimin Sun and Jinjiang Wei
Remote Sens. 2025, 17(5), 927; https://doi.org/10.3390/rs17050927 - 5 Mar 2025
Viewed by 182
Abstract
High-resolution visible remote sensing imagery, as a fundamental contributor to Earth observation, has found extensive application in land use classification. However, the heterogeneous array of optical sensors, distinguished by their unique design architectures, exhibit disparate spectral responses and spatial distributions when observing ground [...] Read more.
High-resolution visible remote sensing imagery, as a fundamental contributor to Earth observation, has found extensive application in land use classification. However, the heterogeneous array of optical sensors, distinguished by their unique design architectures, exhibit disparate spectral responses and spatial distributions when observing ground objects. These discrepancies between multi-sensor data present a significant obstacle to the widespread application of intelligent methods. In this paper, we propose a method tailored to accommodate these disparities, with the aim of achieving a smooth transfer for the model across diverse sets of images captured by different sensors. Specifically, to address the discrepancies in spatial resolution, a novel positional encoding has been incorporated to capture the correlation between the spatial resolution details and the characteristics of ground objects. To tackle spectral disparities, random amplitude mixup augmentation is introduced to mitigate the impact of feature anisotropy resulting from discrepancies in low-level features between multi-sensor images. Additionally, we integrate convolutional neural networks and Transformers to enhance the model’s feature extraction capabilities, and employ a fine-tuning strategy with dynamic pseudo-labels to reduce the reliance on annotated data from the target domain. In the experimental section, the Gaofen-2 images (4 m) and the Sentinel-2 images (10 m) were selected as training and test datasets to simulate cross-sensor model transfer scenarios. Also, Google Earth images of Suzhou City, Jiangsu Province, were utilized for further validation. The results indicate that our approach effectively mitigates the degradation in model performance attributed to image source inconsistencies. Full article
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Graphical abstract

Graphical abstract
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<p>Differences in spatial resolution scale and spectral characteristics of high-resolution visible images from different sources.</p>
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<p>The framework of this paper.</p>
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<p>Illustration of conventional MSA module and efficient MSA module.</p>
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<p>Decoder block architecture, including DeConv (transposed convolution) and DWConv (depthwise convolution) layers.</p>
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<p>Comparison of various color correction methods. (<b>a</b>) displays the input, (<b>b</b>) presents the reference, (<b>c</b>) shows the results of histogram matching, and (<b>d</b>) features the results of our method.</p>
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<p>The process of random amplitude mixup augmentation.</p>
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<p>Illustration of pseudo-label generation and dynamic update.</p>
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<p>Illustration of the experimental area and sample points.</p>
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<p>Visualizations of detailed results on Five-Billion-Pixels dataset.</p>
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<p>Visualizations of detailed results on Five-Billion-Pixels dataset.</p>
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<p>Visualizations of detailed results on MultiSenGE dataset.</p>
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<p>Visualizations of the results using mixup augmentation and model fine-tuning techniques for the “GF-2 images→Sentinel-2 images” scenario.</p>
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<p>Visualizations of the results using mixup augmentation and model fine-tuning techniques for the “Sentinel-2 images→ GF-2 images” scenario.</p>
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<p>Visualizations of the results using mixup augmentation and model fine-tuning techniques for the “Sentinel-2 images→ GF-2 images” scenario.</p>
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<p>Visual comparison of results using models pre-trained on Sentinel-2 images in Suzhou.</p>
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<p>Visual comparison of results using models pre-trained on GF-2 images in Suzhou.</p>
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<p>Visualization of feature maps with different positional encoding methods.</p>
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34 pages, 13658 KiB  
Project Report
Clean Propulsion Technologies: Securing Technological Dominance for the Finnish Marine and Off-Road Powertrain Sectors
by Maciej Mikulski, Teemu Ovaska, Rodrigo Rabetino, Merja Kangasjärvi and Aino Myllykangas
Energies 2025, 18(5), 1240; https://doi.org/10.3390/en18051240 - 3 Mar 2025
Viewed by 202
Abstract
The Clean Propulsion Technologies (CPT) project, established in 2021, brought together 15 research partners and original equipment manufacturers. The goal was to create a common vision and sustainable business solutions so that the worldwide technological leadership of the Finnish powertrain industry is secured. [...] Read more.
The Clean Propulsion Technologies (CPT) project, established in 2021, brought together 15 research partners and original equipment manufacturers. The goal was to create a common vision and sustainable business solutions so that the worldwide technological leadership of the Finnish powertrain industry is secured. With a EUR 15.5 M budget, CPT brought early-stage innovative concepts towards technology readiness level (TRL) 6. The project’s particular significance was its unique cross-coupling of marine and off-road sectors, which have similar emission reduction targets but which do not compete for similar customers. The project yielded 21 innovative solutions, from accelerated model-based design methodologies and progress in combustion and aftertreatment control to hybrid energy management solutions. These were encapsulated in four ground-breaking demonstrations, including a next-generation marine engine working in low-temperature, reactivity-controlled compression ignition (RCCI) mode and a hydrogen off-road engine. An advanced close-coupled selective catalyst reduction (SCR) system and a hybrid wheel-platform with digital hydraulics were also demonstrated. The University of Vaasa led the consortium and was responsible for coordinated model-based rapid prototyping. This report examines University of Vaasa’s achievements during the CPT in terms of 26 milestones, 13 deliverables, and 32 research papers. It focuses also on other aspects, including lessons learned from managing large-scale academic–industry research. Full article
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Figure 1

Figure 1
<p>CPT consortium structure above and WPs of the public project below [<a href="#B14-energies-18-01240" class="html-bibr">14</a>,<a href="#B15-energies-18-01240" class="html-bibr">15</a>].</p>
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<p>The CPT technological roadmap produced in WP1. The roadmap provides guidelines for strategically aligned research actions to be undertaken jointly by the Finnish marine and off-road OEMs until 2035 [<a href="#B19-energies-18-01240" class="html-bibr">19</a>].</p>
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<p>Interlinking the activities of the University of Vaasa in WP2 (task T2.5) with the model-based development framework for the innovative RCCI concept in WP3. Adapted from CPT presentation by Mikulski, M. [<a href="#B22-energies-18-01240" class="html-bibr">22</a>].</p>
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<p>Sample results of the MIL framework component validation—UVATZ-RTM (<b>a</b>) and UVATZ-COM (<b>b</b>)—against detail parent model UVATZ-MZ. The results are adapted from CPT publications by Storm et al. [<a href="#B23-energies-18-01240" class="html-bibr">23</a>] and Modabberian et al. [<a href="#B25-energies-18-01240" class="html-bibr">25</a>].</p>
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<p>Transient RCCI control simulation results. Adaptive MPC handles disturbances well that otherwise render conventional PID control infeasible for RCCI. The results are adapted from CPT publications by Storm et al. [<a href="#B23-energies-18-01240" class="html-bibr">23</a>].</p>
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<p>Structure of the MPC-RCCI closed-loop controller in the MIL test [<a href="#B23-energies-18-01240" class="html-bibr">23</a>].</p>
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<p>This shows the main tasks of WP3, including responsible project partners. The University of Vaasa has an enabling role in all WP3 tasks and subobjectives presented in the figure [<a href="#B29-energies-18-01240" class="html-bibr">29</a>].</p>
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<p>UVATZ-CFD modeling framework (<b>on the left below</b>) and its validation results against Wartsila-6L20DF engine running RCCI combustion at 50% load point (<b>on the right</b>). Adapted from CPT publication of Kakoee et al. [<a href="#B34-energies-18-01240" class="html-bibr">34</a>] and CPT results archive.</p>
Full article ">Figure 9
<p>(<b>Upper plot</b>)—in-cylinder diesel fuel distribution at CA = −15 for different RCCI injection timings; direct CFD results; the color-maps denote mass fractions of n-dodecane (diesel surrogate) from 0.001 (dark blue) to 0.01 (deep read). (<b>Lower plot</b>)—corresponding total fuel mass alongside the cylinder axis at 10 equal zone intervals. Adapted from CPT publication of Kakoee et al. [<a href="#B34-energies-18-01240" class="html-bibr">34</a>].</p>
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<p>Conceptualization of the UVATZ-MZ framework on the left against detailed CFD in fully-stratified fuel case on the right (only thermal stratification effects shown in color map). Red and blue arrows, on the left-hand side of the figure, indicate the modeling assumptions for interzonal heat and mass transfer, respectively. Adapted from CPT publications Vasudev et al. [<a href="#B32-energies-18-01240" class="html-bibr">32</a>,<a href="#B35-energies-18-01240" class="html-bibr">35</a>].</p>
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<p>Medium-speed W20 RCCI-cycle engine at VEBIC laboratories (public RCCI engine demonstration developed in task T3.3). Figure shows major modifications to the engine including new cylinder head with electro-hydraulic valve actuation system (EHVA) and Speedgoat Controller. CPT project archive.</p>
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<p>Benchmark of RCCI technology: Wärtsilä 6L20DF–RCCI (Wärtsilä Finland Oy, Vaasa, Finland) experiments compared with UVATZ-MZ 3.0 model predictions. Plot (<b>a</b>) is in-cylinder pressure; plot (<b>b</b>) is emissions. Plot (<b>c</b>) compares emissions from Wärtsilä 8V31DF (Wärtsilä Finland Oy, Vaasa, Finland) on board M/V Aurora Botnia, piloting RCCI technology (main engine 3, ME3) with a conventional dual-fuel combustion (main engine 2, ME2). Plots adapted from CPT publications [<a href="#B33-energies-18-01240" class="html-bibr">33</a>,<a href="#B42-energies-18-01240" class="html-bibr">42</a>].</p>
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<p>(<b>a</b>) AGCO CORE 50 engine used as a baseline for the VVA study; (<b>b</b>) exemplary realization of VVA considered in the simulations; (<b>c</b>) results of different VVA strategies in terms of the EGT increment and BSFC tradeoff; (<b>d</b>) CDA simulation predictions experimentally verified on the AGCO CORE 50 platform in different modes of operation. Figures adapted from CPT publication by Kim et al. [<a href="#B11-energies-18-01240" class="html-bibr">11</a>].</p>
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<p>The vanadium-based SCR and ammonia slip catalyst performance in terms of NOx conversion, NH<sub>3</sub> slip, and N<sub>2</sub>O formation at exhaust gas temperatures of (<b>a</b>) 320, (<b>b</b>) 350, and (<b>c</b>) 400 °C in an off-road diesel engine before and after LDI and after 40 min operation at 450 °C at an engine speed of 2100 rpm. Figure adapted from CPT publication by Ovaska et al. [<a href="#B43-energies-18-01240" class="html-bibr">43</a>].</p>
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<p>The main tasks of WP5, including responsible project partners: The University of Vaasa has the main direct contribution in task T5.1 and coordinates the project partners’ activities in all other tasks [<a href="#B56-energies-18-01240" class="html-bibr">56</a>].</p>
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<p>The structure of the main electrical components of the hybrid system model designed in task T5.1. Upper: the squirrel cage induction generator (SCIG) model, together with the frequency converter and its control on the generator side and grid side; lower: BESS, divided into the battery model and battery management system (BMS) model [<a href="#B57-energies-18-01240" class="html-bibr">57</a>].</p>
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<p>(<b>Left</b>): the physical structure of the VEBIC system setup for emulating hybrid diesel-electric drive in CPT task T5.1, including relevant measurement equipment and communication interfaces. (<b>Right</b>): the sample validation results of the hybrid system digital twin build to replicate the physical system (simulations with inactive BESS). Figures adapted from CPT publication by Söderäng et al. [<a href="#B57-energies-18-01240" class="html-bibr">57</a>].</p>
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<p>Basic technical data of the BESS system designed for the VEBIC lab, with sample results of co-simulation with the hybrid system depicted in <a href="#energies-18-01240-f010" class="html-fig">Figure 10</a> and <a href="#energies-18-01240-f011" class="html-fig">Figure 11</a>. The results show the battery’s state of charge and active power demand from the engine during a fast load transient in typical ship operation. Figures adapted from the CPT publication by Söderäng et al. [<a href="#B57-energies-18-01240" class="html-bibr">57</a>] and from internal material from the planning phase of the University of Vaasa in task T5.1.</p>
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<p>The management structure of Clean Propulsion Technologies, including the key responsible persons.</p>
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20 pages, 6348 KiB  
Article
Application Research on High-Precision Tiltmeter with Rapid Deployment Capability
by Fuxi Yang, Dongxiao Guan, Xiaodong Li and Chen Dou
Sensors 2025, 25(5), 1559; https://doi.org/10.3390/s25051559 - 3 Mar 2025
Viewed by 172
Abstract
This article introduces a high-precision vertical pendulum tiltmeter with rapid deployment capability to improve the observation efficiency, practicality, and reliability of geophysical site tilt observation instruments. The system consists of a pendulum body, a triangular platform, a locking pendulum motor, a sealed cover, [...] Read more.
This article introduces a high-precision vertical pendulum tiltmeter with rapid deployment capability to improve the observation efficiency, practicality, and reliability of geophysical site tilt observation instruments. The system consists of a pendulum body, a triangular platform, a locking pendulum motor, a sealed cover, a ratio measurement bridge, a high-precision ADC, and an embedded data acquisition unit. The sensing unit adopts a vertical pendulum system suspended by a cross spring and a differential capacitance bridge measurement circuit, which can simultaneously measure two orthogonal directions of ground tilt. The pendulum is installed on a short baseline triangular platform, sealed as a whole with the platform, and equipped with a locking pendulum motor. When the pendulum is locked and packaged, it can withstand a 2 m free fall impact, with high reliability and easy use. It can be quickly deployed without the need for professional technicians. This article analyzes its various performance and technical indicators based on its application in the rapid deployment of the Zeketai seismic station in Xinjiang. It is of great significance for emergency response, mobile observation, base detection, anomaly verification, and other applications of ground tilt. Full article
(This article belongs to the Special Issue Sensors Technologies for Measurements and Signal Processing)
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<p>Schematic diagram of high-precision integrated chamber inclinometer.</p>
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<p>Installation diagram of ICT-1 integrated inclinometer, VP Single-component vertical pendulum inclinometer, SQ-70D quartz horizontal pendulum inclinometer, and DSQ-type water pipe inclinometer ((<b>a</b>) shows ICT-1 integrated inclinometer; (<b>b</b>) shows VP single-component vertical pendulum inclinometer; (<b>c</b>) shows a comparison of ICT-1 integrated inclinometer and SQ-70D quartz horizontal pendulum inclinometer, in which the two black instruments are the quartz horizontal pendulum; (<b>d</b>) shows DSQ-type water pipe inclinometer).</p>
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<p>Schematic diagram of inclined pendulum system. (<b>a</b>) is the dual-leaf spring suspension structure. (<b>b</b>) is when the dual-leaf spring suspension structure receives an impact in a non-moving direction, the spring blade will be damaged, and the red arrow is the direction of the impact force. (<b>c</b>) is the cross-spring pendulum structure. (<b>d</b>,<b>e</b>) represent a unidirectional pendulum and its motion process.).</p>
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<p>The phenomenon of skipping frames that occurred with the CBT-1 inclinometer using a unidirectional spring blade at the Xinyuan seismic station in Xinjiang on 30 December 2024. The red circle in the figure shows the phenomenon of skipping frames in the experiment.</p>
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<p>Physical image of the CBT-1 inclinometer’s spring blade after being impacted (the red circle indicates the location of the crease).</p>
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<p>Electrical schematic diagram of integrated chamber inclinometer. Subfigure (<b>a</b>) shows the unbalanced signals of two groups of differential Bridges. Subfigure (<b>b</b>) shows the superposition of two sets of differential bridge unbalanced signals on the pendulum. Subfigure (<b>c</b>) shows that the excitation signals of the two groups of Bridges are transformed into square waves after shaping, which is the waveform of the reference signal. Subfigures (<b>d</b>,<b>e</b>) show the waveforms of the two groups of differential Bridges after being detected by the phase-sensitive detection circuit using different reference signals.</p>
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<p>Structural diagram of the pendulum-locking motor (<b>left</b> figure) and schematic diagram of the ICT-1 tiltmeter triangular platform (<b>right</b> figure).</p>
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<p>Diagram of the tilting measurement platform structure and physical appearance.</p>
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<p>North–South Direction Tilt Platform Changes and Inclinometer Voltage Output Variation Chart.</p>
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<p>East–West Direction Tilt Platform Changes and Inclinometer Voltage Output Variation Chart.</p>
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<p>Observation curve of inclinometer at Zeketai Seismic Station in Xinjiang. The protrusion of CH1 on August 8 was used to collect data from the cave.</p>
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<p>Observation curve of inclinometer at Zeketai Seismic Station in Xinjiang. The protrusion of CH1 on August 8 was used to collect data from the cave.</p>
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<p>North–South Direction Theoretical and Observational Value Curve on 16 October 2023.</p>
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<p>East–West Direction Theoretical and Observational Value Curve on 16 October 2023.</p>
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18 pages, 28482 KiB  
Article
Forward Modeling Analysis in Advanced Exploration of Cross-Hole Grounded-Wire-Source Transient Electromagnetic Method
by Jiao Zhu, Zhihai Jiang, Maofei Li, Zhonghao Dou and Zhaofeng Gao
Appl. Sci. 2025, 15(5), 2672; https://doi.org/10.3390/app15052672 - 2 Mar 2025
Viewed by 319
Abstract
To address the challenge of accurately detecting hidden water inrush hazards ahead of working faces, a cross-hole transient electromagnetic (TEM) method utilizing a grounded-wire source is proposed. The technique positions a step-current-driven grounded-wire source within a working-face borehole, while electrode arrays in adjacent [...] Read more.
To address the challenge of accurately detecting hidden water inrush hazards ahead of working faces, a cross-hole transient electromagnetic (TEM) method utilizing a grounded-wire source is proposed. The technique positions a step-current-driven grounded-wire source within a working-face borehole, while electrode arrays in adjacent boreholes measure secondary electric field responses. This configuration minimizes interference from metal supports or machines, thereby enhancing the signal-to-noise ratio of the TEM signals. A theoretical analysis based on the unstructured finite-element (FE) method is used to investigate the configuration. The collected data are processed using differential techniques, and the results confirm the method’s effectiveness in detecting anomalies. This paper investigates the response of our cross-hole method to anomalies in terms of size, resistivity contrasts, and spatial location, with anomaly boundaries quantitatively delineated via first-order differential analysis. This significantly enhances the capability of TEM detection in identifying anomalies. A comparison between our cross-hole method and the traditional roadway–borehole TEM method, using the trapped column model, demonstrates that the proposed cross-hole device more effectively locates anomalies and improves accuracy. Furthermore, this technique enables the formation of a 3D observation framework by utilizing existing boreholes, presenting promising prospects for future applications. Full article
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<p>Schematic diagram of cross-hole grounded-wire-source transient electromagnetic method.</p>
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<p>Grid subdivision for full-space EM model.</p>
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<p>The forward modeling responses of the full-space model along with the relative errors compared to the 1D semi-analytical solution, where (<b>a</b>,<b>b</b>) are the results for the induced electromotive force (EMF), while (<b>c</b>,<b>d</b>) are those of the electric field.</p>
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<p>A comparison between the results obtained using our FE and FD methods for a half-space model. Specifically, (<b>a</b>) shows the EMF parameters, while (<b>b</b>) displays the relative errors compared to the 1D semi-analytical solution.</p>
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<p>Diffusion of electric field response of grounded-wire-source EM method for full space model for time channel of (<b>a</b>) 0.020108 ms; (<b>b</b>) 0.069614 ms; (<b>c</b>) 0.241 ms; (<b>d</b>) 0.83435 ms; (<b>e</b>) 2.8885 ms; and (<b>f</b>) 10 ms.</p>
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<p>The forward modeling grid for a single cube with side lengths of (<b>a</b>) 5 m; (<b>b</b>) 7.5 m; (<b>c</b>) 10 m; and (<b>d</b>) 12.5 m.</p>
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<p>Multi-channel electric field and differential curves for cubes with (<b>a</b>,<b>e</b>) 5 m side length; (<b>b</b>,<b>f</b>) 7.5 m side length; (<b>c</b>,<b>g</b>) 10 m side length; and (<b>d</b>,<b>h</b>) 12.5 m side length.</p>
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<p>Cubic anomalies located at (<b>a</b>) 25 m (resistivity of 10 Ω·m or 1000 Ω·m), (<b>b</b>) 50 m, and (<b>c</b>) 75 m in the midline of the transmitters and receivers.</p>
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<p>Multi-channel electric field curves and differential curves for cube located at (<b>a</b>,<b>e</b>) 25 m (resistivity of 10 Ω·m), (<b>b</b>,<b>f</b>) 25 m (resistivity of 1000 Ω·m), (<b>c</b>,<b>g</b>) 50 m, and (<b>d</b>,<b>h</b>) 75 m in the midline of the transmitters and receivers.</p>
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<p>The cubes (<b>a</b>) close to the transmitters; (<b>b</b>) on the inner side and close to the survey line; and (<b>c</b>) on the outer side and close to the survey line.</p>
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<p>Multi-channel and difference curves for cubic anomalies (<b>a</b>,<b>d</b>) close to the transmitters; (<b>b</b>,<b>e</b>) on the inner side and close to the survey line; and (<b>c</b>,<b>f</b>) on outer side and close to the survey line.</p>
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<p>The positioning of the two anomalies (<b>a</b>) along the centerline between the grounded-wire source and the survey line and (<b>b</b>) near the survey line.</p>
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<p>Multi-channel electric field and differential curves for two cubic anomalies: (<b>a</b>,<b>d</b>) aligned along the centerline between the grounded-wire source and survey line; (<b>b</b>,<b>e</b>) located near the survey line with both anomalies of low resistance; (<b>c</b>,<b>f</b>) located near the survey line with one anomaly of low resistance and the other of high resistance.</p>
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<p>Model of water-bearing trap column and three-view drawing.</p>
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<p>Contour plots of electric field obtained by (<b>a</b>–<b>f</b>) full-space model and (<b>g</b>–<b>l</b>) water-bearing trap column model.</p>
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<p>Contour plots of first-order difference in electric field obtained by (<b>a</b>–<b>f</b>) full-space model and (<b>g</b>–<b>l</b>) water-bearing trap column model.</p>
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<p>Contour plots of EMF obtained by (<b>a</b>–<b>f</b>) full-space model and (<b>g</b>–<b>l</b>) water-bearing trap column model.</p>
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10 pages, 2974 KiB  
Article
A New Observation in Decoupling and Sequential Rotation Array Configurations Using Loop Radiation Elements
by Kazuhide Hirose, Koki Nishino and Hisamatsu Nakano
J 2025, 8(1), 9; https://doi.org/10.3390/j8010009 - 1 Mar 2025
Viewed by 253
Abstract
Using the method of moments, we analyze three array antennas for low cross-polarized radiation. Each antenna comprises two dual-loop elements connected to a feedline horizontal to the ground plane. First, a feedline end is excited with an unbalanced source as a reference antenna. [...] Read more.
Using the method of moments, we analyze three array antennas for low cross-polarized radiation. Each antenna comprises two dual-loop elements connected to a feedline horizontal to the ground plane. First, a feedline end is excited with an unbalanced source as a reference antenna. Next, the feedline center is excited with a balanced source, after the transformation of a decoupling array configuration. It is found that the antenna exhibits a cross-polarized radiation lower by 12 dB than the reference antenna. Last, the decoupling antenna is modified to have an unbalanced source without a complicated balun circuit design. It is pointed out that the modified antenna is an array of four loop elements, sequentially rotated by 90º. Full article
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<p>Reference antenna with a horizontal feedline <span class="html-italic">F</span>–<span class="html-italic">T</span>, excited at one end <span class="html-italic">F</span> via a vertical wire <span class="html-italic">F</span>–<span class="html-italic">F</span>′. (<b>a</b>) Perspective view. (<b>b</b>) Top view. (<b>c</b>) Side view.</p>
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<p>Present antenna with a horizontal feedline <span class="html-italic">F</span>–<span class="html-italic">T</span> excited at the center <span class="html-italic">C</span>. (<b>a</b>) Perspective view. (<b>b</b>) Top view. (<b>c</b>) Side view.</p>
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<p>Modified antenna with a horizontal feedline <span class="html-italic">F</span>–<span class="html-italic">T</span> excited at one end <span class="html-italic">F</span> via a vertical wire <span class="html-italic">F</span>–<span class="html-italic">F</span>′. (<b>a</b>) Perspective view. (<b>b</b>) Top view. (<b>c</b>) Side view.</p>
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<p>Simulated radiation patterns of a reference antenna at <span class="html-italic">f</span><sub>0</sub>.</p>
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<p>Simulated radiation patterns of the present antenna at <span class="html-italic">f</span><sub>0</sub>.</p>
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<p>Simulated frequency responses of axial ratio and gain of present and reference antennas.</p>
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<p>Simulated radiation patterns of the modified antenna at <span class="html-italic">f</span><sub>0</sub>.</p>
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<p>Simulated frequency responses of the axial ratio, gain, and VSWR of the modified antenna.</p>
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<p>Photographs of a prototype for a modified antenna. (<b>a</b>) Perspective view. (<b>b</b>) Side view.</p>
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<p>Radiation patterns of a modified antenna at <span class="html-italic">f</span><sub>0</sub>. (<b>a</b>) simulated results. (<b>b</b>) experimental results.</p>
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<p>Frequency responses of axial ratio, gain, and VSWR of a modified antenna.</p>
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22 pages, 1932 KiB  
Article
The Synergy of Entrepreneurial Leadership and Team Diversity: Pathways to Entrepreneurial Success in Pakistan’s SMEs
by Khalid Rehman, Kah Boon Lim, Sook Fern Yeo, Muhammad Ameeq and Muhammad Asad Ullah
Sustainability 2025, 17(5), 2063; https://doi.org/10.3390/su17052063 - 27 Feb 2025
Viewed by 228
Abstract
Small and medium-sized enterprises (SMEs) play a crucial role in fostering economic growth and sustainability, requiring a deliberate emphasis on innovation and applying knowledge to navigate ever-changing markets. This study, grounded in resource-based view (RBV) theory, explores the synergy of entrepreneurial leadership and [...] Read more.
Small and medium-sized enterprises (SMEs) play a crucial role in fostering economic growth and sustainability, requiring a deliberate emphasis on innovation and applying knowledge to navigate ever-changing markets. This study, grounded in resource-based view (RBV) theory, explores the synergy of entrepreneurial leadership and team diversity, exploring pathways to entrepreneurial success in Pakistan’s SMEs. This study employed a cross-sectional design, utilizing a non-probability convenience sampling approach to survey 350 owners, supervisors, managers, and employees of SMEs in Khyber Pakhtunkhwa, Pakistan. Data were gathered through a survey questionnaire and subsequently analyzed using SPSS and SMART-PLS to validate the measurement model and examine the hypotheses for moderated analysis. The results indicated a significant moderating influence. Entrepreneurial leadership accounted for 15.8% of the variation in entrepreneurial success, while team diversity contributed 8.5%. Moreover, the moderating influence of team diversity substantially affected ES (59.7%), underscoring the pivotal role of team diversity in the interplay between EL and ES. Drawing from RBV theory, this study advances the framework by acknowledging that team diversity is a crucial element that strengthens the connections between EL and ES. This study enhances the existing literature by clarifying the mechanisms by which leadership and diversity collaboratively promote entrepreneurial outcomes. This highlights the necessity for SME leaders and policymakers to utilize team diversity as a strategic asset to improve competitive advantage and ensure sustainable success. Full article
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<p>Moderating the role of team diversity between EL and ES.</p>
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<p>Factor Loadings.</p>
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<p>Moderation path.</p>
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<p>Simple slope analysis.</p>
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26 pages, 13054 KiB  
Article
Retrieval of Atmospheric XCH4 via XGBoost Method Based on TROPOMI Satellite Data
by Wenhao Zhang, Yao Li, Bo Li, Tong Li, Zhengyong Wang, Xiufeng Yang, Yongtao Jin and Lili Zhang
Atmosphere 2025, 16(3), 279; https://doi.org/10.3390/atmos16030279 - 26 Feb 2025
Viewed by 110
Abstract
Accurate retrieval of column-averaged dry-air mole fraction of methane (XCH4) in the atmosphere is important for greenhouse gas emission management. Traditional XCH4 retrieval methods are complex, while machine learning can be used to model nonlinear relationships by analyzing large datasets, [...] Read more.
Accurate retrieval of column-averaged dry-air mole fraction of methane (XCH4) in the atmosphere is important for greenhouse gas emission management. Traditional XCH4 retrieval methods are complex, while machine learning can be used to model nonlinear relationships by analyzing large datasets, providing an efficient alternative. This study proposes an XGBoost algorithm-based retrieval method to improve the efficiency of atmospheric XCH4 retrieval. First, the key wavelengths affecting XCH4 retrieval were determined using a radiative transfer model. The TROPOspheric Monitoring Instrument (TROPOMI) L1B satellite data, L2 XCH4 products, and auxiliary data were matched to construct the dataset. The dataset constructed was used to train the XGBoost model and obtain the TRO_XGB_XCH4 model. Finally, the accuracy of the proposed model was evaluated using various parameter values and validated against XCH4 products and Total Carbon Column Observing Network (TCCON) ground-based observations. The results showed that the proposed TRO_XGB_XCH4 model had a tenfold cross-validation accuracy R of 0.978, a ground-based validation R of 0.749, and a temporal extension accuracy R of 0.863. Therefore, the accuracy of the TRO_XGB_XCH4 retrieval model is comparable to that of the official TROPOMI L2 product. Full article
(This article belongs to the Special Issue Feature Papers in Atmospheric Techniques, Instruments, and Modeling)
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<p>Overall flowchart.</p>
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<p>Selection of high-sensitivity wavelengths.</p>
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<p>Selection of candidate low-sensitivity wavelengths.</p>
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<p>Research area.</p>
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<p>(<b>a</b>) Scatter plot of ten-fold cross-validation results using nine training datasets; (<b>b</b>) scatter plot comparing the model estimation results with TROPOMI L2 XCH<sub>4</sub> data for one independent validation dataset (the solid line indicates the fitted line, while the dashed line represents the line of equality y = x).</p>
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<p>Comparison of the spatial distributions of model inversion results and TROPOMI L2 XCH<sub>4</sub> data.</p>
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<p>Accuracy line chart comparing the model inversion results for the entire year of 2020 with L2 XCH<sub>4</sub>.</p>
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<p>Line chart of the differences between the model inversion results for the entire year of 2020 and L2 XCH<sub>4</sub>.</p>
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<p>Model validation based on station data. (<b>a</b>) Scatter plot comparing the TRO_XGB_XCH<sub>4</sub> model retrieval results with the Xianghe station XCH<sub>4</sub>; (<b>b</b>) scatter plot comparing TROPOMI L2 XCH<sub>4</sub> with the Xianghe station XCH<sub>4</sub>.(the solid line indicates the fitted line, while the dashed line represents the line of equality y = x).</p>
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<p>Scatter plot comparing the temporal extension data inversion results with TROPOMI L2 XCH<sub>4</sub>.</p>
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<p>Scatter plots of the ten-fold cross-validation results, independent validation dataset results, and temporal extension validation results for four different parameter models.</p>
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<p>Beeswarm plot of SHAP values and feature importance bar chart.</p>
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<p>Dependence plots for each parameter feature.</p>
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<p>(<b>a</b>) Annual average spatial distribution map of XCH<sub>4</sub> derived from the TRO_XGB_XCH<sub>4</sub> model; (<b>b</b>) annual average spatial distribution map of XCH<sub>4</sub> from the TROPOMI L2 product; (<b>c</b>) the XCH<sub>4</sub> difference between the TRO_XGB_XCH<sub>4</sub> model and the TROPOMI L2 product; (<b>d</b>) the comparison scatter plot.</p>
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<p>Seasonal average distribution of XCH<sub>4</sub> in the study area for 2020.</p>
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<p>The scatter plots of comparison between XCH<sub>4</sub> from inversion results of TRO_XGB_XCH<sub>4</sub> model and TROPOMI L2 XCH<sub>4</sub> for one day each month in 2020 (the solid line indicates the fitted line, while the dashed line represents the line of equality y = x).</p>
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<p>The difference histograms between XCH<sub>4</sub> from inversion results of TRO_XGB_XCH<sub>4</sub> model and TROPOMI L2 XCH<sub>4</sub> for one day each month in 2020.</p>
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19 pages, 8944 KiB  
Article
Fault Detection and Protection Strategy for Multi-Terminal HVDC Grids Using Wavelet Analysis
by Jashandeep Kaur, Manilka Jayasooriya, Muhammad Naveed Iqbal, Kamran Daniel, Noman Shabbir and Kristjan Peterson
Energies 2025, 18(5), 1147; https://doi.org/10.3390/en18051147 - 26 Feb 2025
Viewed by 240
Abstract
The growing demand for electricity, integration of renewable energy sources, and recent advances in power electronics have driven the development of HVDC systems. Multi-terminal HVDC (MTDC) grids, enabled by Voltage Source Converters (VSCs), provide increased operational flexibility, including the ability to reverse power [...] Read more.
The growing demand for electricity, integration of renewable energy sources, and recent advances in power electronics have driven the development of HVDC systems. Multi-terminal HVDC (MTDC) grids, enabled by Voltage Source Converters (VSCs), provide increased operational flexibility, including the ability to reverse power flow and independently control both active and reactive power. However, fault propagation in DC grids occurs more rapidly, potentially leading to significant damage within milliseconds. Unlike AC systems, HVDC systems lack natural zero-crossing points, making fault isolation more complex. This paper presents the implementation of a wavelet-based protection algorithm to detect faults in a four-terminal VSC-HVDC grid, modelled in MATLAB and SIMULINK. The study considers several fault scenarios, including two internal DC pole-to-ground faults, an external DC fault in the load branch, and an external AC fault outside the protected area. The discrete wavelet transform, using Symlet decomposition, is applied to classify faults based on the wavelet entropy and sharp voltage and current signal variations. The algorithm processes the decomposition coefficients to differentiate between internal and external faults, triggering appropriate relay actions. Key factors influencing the algorithm’s performance include system complexity, fault location, and threshold settings. The suggested algorithm’s reliability and suitability are demonstrated by the real-time implementation. The results confirmed the precise fault detection, with fault currents aligning with the values in offline models. The internal faults exhibit more entropy than external faults. Results demonstrate the algorithm’s effectiveness in detecting faults rapidly and accurately. These outcomes confirm the algorithm’s suitability for a real-time environment. Full article
(This article belongs to the Special Issue Renewable Energy System Technologies: 2nd Edition)
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<p>Single line diagram of the LCC HVDC system.</p>
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<p>Structure of VSC-HVDC system.</p>
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<p>Two-level wavelet decomposition trees.</p>
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<p>Fault detection and protection flow.</p>
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<p>Simulation of four terminal VSC-HVDC systems.</p>
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<p>DC current for fault F1.</p>
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<p>Voltage for internal fault F1.</p>
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<p>Detailed coefficients for F1.</p>
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<p>DC current for fault F2.</p>
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<p>Voltage for internal fault F2.</p>
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<p>Detailed coefficients for fault F2.</p>
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<p>Detailed coefficients for fault F3.</p>
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<p>Detailed coefficients for fault F4.</p>
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<p>Current for DC fault F3.</p>
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<p>DC current for fault F4.</p>
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<p>Voltage for external fault F3.</p>
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<p>Voltage for internal fault F4.</p>
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<p>OpComm blocks for output.</p>
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<p>Real-time model for four terminal grid.</p>
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<p>Current for DC fault F1.</p>
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<p>Current for DC fault F2.</p>
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<p>Current for AC fault F3.</p>
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<p>Current for DC fault F4.</p>
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15 pages, 716 KiB  
Article
Presence of Pain Shows Greater Effect than Tendon Structural Alignment During Landing Dynamics
by Silvia Ortega-Cebrián, Diogo C. F. Silva, Daniela F. Carneiro, Victor Zárate, Leonel A. T. Alves, Diana C. Guedes, Carlos A. Zárate-Tejero, Aïda Cadellans-Arróniz and António Mesquita Montes
J. Funct. Morphol. Kinesiol. 2025, 10(1), 74; https://doi.org/10.3390/jfmk10010074 - 24 Feb 2025
Viewed by 136
Abstract
Background/Objectives: Eccentric loading during landing is considered a key factor in the development of patellar tendinopathy and is associated with stiff landings and patellar tendinopathy. This study aims to investigate the relationship between tendon structure, presence of pain, and sex differences in [...] Read more.
Background/Objectives: Eccentric loading during landing is considered a key factor in the development of patellar tendinopathy and is associated with stiff landings and patellar tendinopathy. This study aims to investigate the relationship between tendon structure, presence of pain, and sex differences in landing kinematics and kinetics during countermovement jumps (CMJ) and tuck jump tests (TJT) in professional volleyball players. Methods: Professional volleyball players aged 18 to 30 years old (14 females and 25 males) participated in a cross-sectional study. Data included the Victorian Institute of Sport Assessment Patellar Tendon (VISA-P) questionnaire; patellar tendon ultrasound characterization tissue (UTC) scans, in order to identify groups with misaligned tendon fibers (MTF) or aligned tendon fibers (ATF); and biomechanical assessments for CMJ and TJT. The joint angle (JA) at the lower limb was measured at peak ground reaction force (peak_vGRF) and maximal knee flexion (max_KF). A general linear model was used to evaluate joint JA differences between tendon alignment, pain, and sex variables. Sample t-tests compared peak_vGRF, load time, load rate, and area based on tendon alignment, pain presence, sex, and jump. The statistical significance of p-value is >0.05, and the effect size (ES) was also calculated. Results: The MTF group revealed decreased knee JA during TJT at peak_vGRF (p = 0.01; ES = −0.66) and max_KF (p = 0.02; ES = −0.23). The presence of pain was associated with increased JA during the CMJ, particularly at peak_vGRF and max_KF for trunk, hip, and ankle joints. Females showed decreased peak_vGRF than males. Landing with misaligned tendon fibers showed longer load times compared to aligned tendon fibers (p = 0.021; ES = −0.80). The TJT exhibited a greater load rate than the CMJ (p = 0.00; ES = −0.62). Conclusions: Pain is a critical factor influencing greater JA during landing, particularly at the trunk, hip, and ankle joints in CMJ. Misaligned tendon fibers compromise landing dynamics by increasing trunk JA during TJT. Kinetics varied significantly by sex and jump type, while pain and tendon structure revealed limited differences. Full article
(This article belongs to the Special Issue Physical Activity for Optimal Health)
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<p>Group definition flowchart. UTC = ultrasound tissue characterization; MFT = misaligned fibrillar tendon.</p>
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<p>Significant differences of JA at the trunk, hip, knee, and ankle between tendon structure, pain, and sex. <span class="html-italic">p</span>-value &lt; 0.005; AFT = aligned fibrillar tendon; MFT = misaligned fibrillar tendon; CMJ = counter movement jump; Peak vGRF = peak vertical ground reaction force; Max_KF = maximal knee flexion.</p>
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21 pages, 45648 KiB  
Article
A Big Data Approach for the Regional-Scale Spatial Pattern Analysis of Amazonian Palm Locations
by Matthew J. Drouillard and Anthony R. Cummings
Remote Sens. 2025, 17(5), 784; https://doi.org/10.3390/rs17050784 - 24 Feb 2025
Viewed by 179
Abstract
Arecaceae (palms) are an important resource for indigenous communities as well as fauna populations across Amazonia. Understanding the spatial patterns and the environmental factors that determine the habitats of palms is of considerable interest to rainforest ecologists. Here, we utilize remotely sensed imagery [...] Read more.
Arecaceae (palms) are an important resource for indigenous communities as well as fauna populations across Amazonia. Understanding the spatial patterns and the environmental factors that determine the habitats of palms is of considerable interest to rainforest ecologists. Here, we utilize remotely sensed imagery in conjunction with topography and soil attribute data and employ a generalized cluster identification algorithm, Hierarchical Density-Based Spatial Clustering of Applications with Noise (HDBSCAN), to study the underlying patterns of palms in two areas of Guyana, South America. The results of the HDBSCAN assessment were cross-validated with several point pattern analysis methods commonly used by ecologists (the quadrat test for complete spatial randomness, Morista Index, Ripley’s L-function, and the pair correlation function). A spatial logistic regression model was generated to understand the multivariate environmental influences driving the placement of cluster and outlier palms. Our results showed that palms are strongly clustered in the areas of interest and that the HDBSCAN’s clustering output correlates well with traditional analytical methods. The environmental factors influencing palm clusters or outliers, as determined by logistic regression, exhibit qualitative similarities to those identified in conventional ground-based palm surveys. These findings are promising for prospective research aiming to integrate remote flora identification techniques with traditional data collection studies. Full article
(This article belongs to the Special Issue Advancements in Environmental Remote Sensing and GIS)
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<p>Example of a subcanopy waterway in the Guyanese rainforest. Photo taken by M. Drouillard, December 2022.</p>
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<p>Graphical demonstration of comparison between traditional SPPA of scales of interaction and cluster geometry.</p>
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<p>Topography and heat map of locations of palm clusters in AOI-1. The number of clustered palms is 121,837. Outlier palm locations are not accounted for in the heat map, but are often commingled in the vicinity of the clustered palms. Zones of interest for detailed analysis are shown using blue boxes and are 1 by 1 km square. The basemap image is a 30 m digital elevation model. Drainage features were derived utilizing a conventional geospatial hydrology workflow and were inferred using the elevation model.</p>
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<p>Topography and heat map of the locations of clustered palms in AOI-2. The number of clustered palms is 172,489. Outlier palm locations are not accounted for in the heat map, but are often commingled in the vicinity of the clustered palms. Zones of interest for detailed analysis are shown using blue boxes and are 1 by 1 km square. The basemap image is a 30 m digital elevation model. Drainage features were derived utilizing a conventional geospatial hydrology workflow and were inferred using the elevation model, with the exception of the Parabara River, which is discernible in satellite imagery.</p>
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<p>HDBSCAN-generated cluster-diagnostic metrics for AOI-1 (<b>a</b>) and AOI-2 (<b>b</b>). An exemplar feature is the most representative feature of a cluster based upon the underlying statistics; across all cluster size ranges, the proportion of exemplars is linear and approximately 20% of the total number of palms in the cluster. The density of the clusters is computed as the number of palms in a given cluster divided by the area of the cluster’s minimum bounding geometry polygon, in hectares.</p>
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<p>Example Morista Index plots from AOI-1 (<b>a</b>) and AOI-2 (<b>b</b>) with the summary and distribution of HDBSCAN clusters for comparison. The Freedman–Diaconis algorithm was used for histogram breaks due to differing cluster counts per ZOI. Where the Morista Index demonstrates variability in the locus of its aggregation scales, the HDBSCAN’s cluster size distribution correspondingly conforms, extending into the broader spatial scale in its tail-end. See <a href="#app1-remotesensing-17-00784" class="html-app">Supplementary Figures S3 and S4</a> for Morista Index plots of all ZOI.</p>
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<p>Significantaggregation distances derived from the envelope of 99 simulations of the inhomogeneous L-function, compared against the <math display="inline"><semantics> <mstyle scriptlevel="0" displaystyle="true"> <mfrac> <mrow> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <mi>h</mi> </mrow> <mn>2</mn> </mfrac> </mstyle> </semantics></math> obtained from the largest cluster geometry within each ZOI. See <a href="#app1-remotesensing-17-00784" class="html-app">Supplementary Figures S5 and S6</a> for L-function plots of all ZOI.</p>
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<p>Peak probability distribution distances from inhomogeneous pair correlation function vs. distribution and mean of HDBSCAN clusters’ nearest neighbor distances. See <a href="#app1-remotesensing-17-00784" class="html-app">Supplementary Tables S7 and S8</a> for pair correlation function plots of all ZOI.</p>
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<p>AOI-1: The impacts of environmental predictors on point process intensity (interpreted as aggregation) at an individual level. The x-axis is in units of the independent variable, and the y-axis is the estimated intensity of the point pattern process as a function of the variable. The greatest peaks indicate the variable values where environmental predictors are inferred to have the greatest influence. Notably, the pH of soil water demonstrates very narrow peaks of variably influenced pattern intensity.</p>
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<p>AOI-2: The impacts of environmental predictors on point process intensity (interpreted as aggregation) at an individual level. The x-axis is in units of the independent variable, and the y-axis is the estimated intensity of the point pattern process as a function of the variable. The greatest peaks indicate the variable values where environmental predictors are inferred to have the greatest influence. Within AOI-2, the pH of soil water demonstrates similar narrow peaks of intensity to those in AOI-1, and the distance to drainage channels appears to have limited influence on point pattern intensity.</p>
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<p>ROC plots with AUC values for AOI-1 (<b>top</b>) and AOI2- (<b>bottom</b>). The observed AUC is the value of the actual model, while the theoretical AUC is the expected value of the model.</p>
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<p>Comparison of coefficient magnitudes. Top row: AOI-1 cluster (<b>left</b>) and outlier (<b>right</b>) models. Bottom row: AOI-2 cluster (<b>left</b>) and outlier (<b>right</b>) models.</p>
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<p>Comparison of the linear distance between individual palms in both the cluster and outlier sets versus the linear distance to the nearest drainage feature. (<b>a</b>): AOI-1 cluster and outlier palms; (<b>b</b>): AOI-2 cluster and outlier palms. Box plots are grouped by their Hack magnitude value (1 is the drainage feature with the highest magnitude, 5 is the lowest). Color shading and box widths are indicative of the overall number of palm features in each group. The overall number of features in each subdivision is annotated in red.</p>
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<p>AOI-2, with an example of the Parabara River flood zone. From north to south, the distance devoid of palms is approximately 600 m. The DEM shows this to be a shallow basin surrounding the river; in the satellite image, it is heavily vegetated, yet no palms are detected in this location.</p>
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19 pages, 3546 KiB  
Article
Proxy-Based Semi-Supervised Cross-Modal Hashing
by Hao Chen, Zhuoyang Zou and Xinghui Zhu
Appl. Sci. 2025, 15(5), 2390; https://doi.org/10.3390/app15052390 - 23 Feb 2025
Viewed by 176
Abstract
Due to the difficulty in obtaining label information in practical applications, semi-supervised cross-modal retrieval has emerged. However, the existing semi-supervised cross-modal hashing retrieval methods mainly focus on exploring the structural relationships between data and generating high-quality discrete pseudo-labels while neglecting the relationships between [...] Read more.
Due to the difficulty in obtaining label information in practical applications, semi-supervised cross-modal retrieval has emerged. However, the existing semi-supervised cross-modal hashing retrieval methods mainly focus on exploring the structural relationships between data and generating high-quality discrete pseudo-labels while neglecting the relationships between data and categories, as well as the structural relationships between data and categories inherent in continuous pseudo-labels. Based on this, Proxy-based Semi-Supervised Cross-Modal Hashing (PSSCH) is proposed. Specifically, we propose a category proxy network to generate category center points in both feature and hash spaces. Additionally, we design an Adaptive Dual-Label Loss function, which applies different learning strategies to discrete ground truth labels and continuous pseudo-labels and adaptively increases the training weights of unlabeled data with more epochs. Experiments on the MIRFLICKR-25K, NUS-WIDE, and MS COCO datasets show that PSSCH achieves the highest mAP improvements of 3%, 1%, and 4%, respectively, demonstrating better results than the latest baseline methods. Full article
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<p>The proposed PSSCH framework is shown in the figure. PSSCH consists of three networks: ImgNet, TxtNet, and CPNet, where the CPNet takes the one-hot encoding of categories as input and, through forward propagation, generates feature proxies and hash proxies. The feature proxies are updated using loss <math display="inline"><semantics> <msubsup> <mi mathvariant="script">L</mi> <mrow> <mi>f</mi> </mrow> <mi>I</mi> </msubsup> </semantics></math> and loss <math display="inline"><semantics> <msubsup> <mi mathvariant="script">L</mi> <mrow> <mi>f</mi> </mrow> <mi>T</mi> </msubsup> </semantics></math>. The cosine similarity between the unlabeled data features and feature proxies is calculated through the pseudo-label generation module to generate continuous pseudo-labels. Finally, the hash codes of the data, hash proxies, and continuous pseudo-labels are used to compute the loss through Adaptive Dual-Label Loss, and the network parameters of the TxtNet, ImgNet, and CPNet are updated via backpropagation.</p>
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<p>Precision–recall curve results on MIRFLICKR-25K, NUS-WIDE, and MS COCO datasets. The code length is 64.</p>
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<p>The mAP of the semi-supervised cross-modal hashing methods under different percentages of labeled samples on the MIRFLICKR-25K, NUS-WIDE, and MS COCO datasets.</p>
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<p>Sensitivity of parameters <math display="inline"><semantics> <mi>α</mi> </semantics></math> and <math display="inline"><semantics> <mi>β</mi> </semantics></math> on MIRFLICKR-25K, NUS-WIDE, and MS COCO datasets. The code length is 64.</p>
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<p>Comparing the training time and encoding time with baseline methods on the MIRFLICKR-25K dataset.</p>
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<p>T-SNE visualization results of TS3H, GCSCH, and PSSCH on the NUS-WIDE dataset with respect to 32-bit codes.</p>
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17 pages, 2164 KiB  
Article
Development of Clinical-Radiomics Nomogram for Predicting Post-Surgery Functional Improvement in High-Grade Glioma Patients
by Tamara Ius, Maurizio Polano, Michele Dal Bo, Daniele Bagatto, Valeria Bertani, Davide Gentilini, Giuseppe Lombardi, Serena D’agostini, Miran Skrap and Giuseppe Toffoli
Cancers 2025, 17(5), 758; https://doi.org/10.3390/cancers17050758 - 23 Feb 2025
Viewed by 310
Abstract
Introduction: Glioma Grade 4 (GG4) tumors, which include both IDH-mutated and IDH wild-type astrocytomas, are the most prevalent and aggressive form of primary brain tumor. Radiomics is gaining ground in neuro-oncology. The integration of this data into machine learning models has the potential [...] Read more.
Introduction: Glioma Grade 4 (GG4) tumors, which include both IDH-mutated and IDH wild-type astrocytomas, are the most prevalent and aggressive form of primary brain tumor. Radiomics is gaining ground in neuro-oncology. The integration of this data into machine learning models has the potential to improve the accuracy of prognostic models for GG4 patients. Karnofsky Performance Status (KPS), an established preoperative prognostic factor for survival, is commonly used in these patients. In this study, we developed a nomogram to identify patients with improved functional performance as indicated by an increase in KPS after surgery by analyzing radiomic features from preoperative 3D MRI scans. Methods: Quantitative imaging features were extracted from the -3D T1 GRE sequence of 157 patients from a single center and were used to develop the machine learning (ML) model. To improve applicability and create a nomogram, multivariable logistic regression analysis was performed to build a model incorporating clinical characteristics and radiomics features. Results: We labeled 55 cases in which KPS was improved after surgery (35%, KPS-flag = 1). The resulting model was evaluated according to test series results. The best model was obtained by XGBoost using the features extracted by pyradiomics, with a Matthew coefficient score (MCC) of 0.339 (95% CI: 0.330–0.3483) in cross-validation. The out-of-sample evaluation on the test set yielded an MCC of 0.302. A nomogram evaluating the improvement of KPS post-surgery was built based on statistically significant variables from multivariate logistic regression including clinical and radiomics data (c-index = 0.760, test set). Conclusions: MRI radiomic analysis represents a powerful tool to predict postoperative functional outcomes, as evaluated by KPS. Full article
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<p>A Sankey diagram to visualize the flow and relationships between categorical variables created based on the relationship among localization, EOR, and flag to predict KPS improvement. The width of the flow represents the proportion of patients moving from one category to another. Of note, GG4 cases labeled with a KPS-flag = 1 showed an improvement of performance status by a heterogeneity of localization, side, and different rates of EOR. For these reasons, we evaluate the informative effect of radiomics data to classify that condition (<a href="#cancers-17-00758-f001" class="html-fig">Figure 1</a>).</p>
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<p>A unsupervised clustering heatmap of the radiomic features extracted from 157 GG4 cases using PyRadiomics. Each row represents a radiomic feature, while each column corresponds to a patient case. The features are standardized using z-score normalization, and hierarchical clustering was performed using Euclidean distance and Ward’s linkage method. The top annotation bar includes key clinical and molecular features such as FLAG status, IDH mutation status, MGMT methylation status, tumor laterality, location, and additional clinical data. This visualization highlights potential patterns and subgroup structures within the radiological landscape of the GG4 cases.</p>
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<p>The top 20 feature variables and their importance in the FLAG-KPS model. The figure illustrates the top 20 most influential features identified by the FLAG-KPS model, ranked by their importance scores. The importance was determined using the average SHAP (Shapley Additive Explanations) values over 1000 bootstrap model iterations. Higher SHAP values indicate greater influence on model predictions and provide insight into the key factors driving the model’s decision-making process.</p>
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<p>A comparison of the top 20 radiomic features selected by the XGBoost model with the Wilcoxon signed-rank test between the GG4 patient cohort and the IDH wild-type (IDHwt) patient subgroup classified according to the 2021 WHO guidelines. The Wilcoxon signed-rank test is used to detect statistically significant differences in the distribution of radiomic features between these groups identified by the xgboost model. The results are presented in a log10-transformed <span class="html-italic">p</span>-value plot highlighting the most important features based on their statistical significance. This analysis sheds light on the radiomic features that differentiate the GG4 cases from the IDHwt subgroup and can thus contribute to classification and prognostic assessment.</p>
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<p>Receiver Operating Characteristic (ROC) curve of the clinical-radiomics nomogram model. The ROC curve illustrates the model’s ability to distinguish between outcome classes by plotting the true positive rate (sensitivity) against the false positive rate (1—specificity) across different probability thresholds. The area under the curve (AUC) was 0.823 (95% CI: 66.1–96.41%), computed using 100 stratified bootstrap iterations. A higher AUC indicates stronger discriminative performance, highlighting the model’s effectiveness in clinical decision-making and predictive accuracy.</p>
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<p>A clinical-radiomics nomogram. The clinical-radiomics nomogram developed for the GG4 cohort by integrating a multivariate logistic regression model constructed using the rms package. This nomogram combines both clinical and radiomic features to provide a quantitative tool for individual risk assessment and outcome prediction. By assigning a weighted contribution to each predictor, the model facilitates the intuitive interpretation of complex relationships among the variables. The use of the rms package ensures robust model calibration, validation, and visualization and increases the reliability and clinical applicability of the nomogram.</p>
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12 pages, 1394 KiB  
Article
Biomechanical Determinants of Anterior Cruciate Ligament Stress in Individuals Post–ACL Reconstruction During Side-Cutting Movements
by Huijuan Shi, Yuanyuan Yu, Hongshi Huang, Hanjun Li, Shuang Ren and Yingfang Ao
Bioengineering 2025, 12(3), 222; https://doi.org/10.3390/bioengineering12030222 - 22 Feb 2025
Viewed by 273
Abstract
This cross-sectional laboratory-based study investigates the stress characteristics of the anterior cruciate ligament (ACL) during side-cutting using a knee finite element (FE) model and identifies biomechanical factors influencing ACL stress. Kinematics and ground reaction forces (GRF) were collected from eight participants (age: 30.3 [...] Read more.
This cross-sectional laboratory-based study investigates the stress characteristics of the anterior cruciate ligament (ACL) during side-cutting using a knee finite element (FE) model and identifies biomechanical factors influencing ACL stress. Kinematics and ground reaction forces (GRF) were collected from eight participants (age: 30.3 ± 5.3 years; BMI: 25.6 ± 2.4 kg/m2; time since surgery: 12.8 ± 1.2 months) one year post–ACL reconstruction during side-cutting tasks. A knee FE model incorporating time-varying knee angles, knee forces, and femoral translation was developed to simulate the knee biomechanics. The relationships between ACL stress and lower limb biomechanics were analyzed. The results indicated the highest stress concentrations at the femoral attachment during the early landing phase. Posterior femoral displacement relative to the tibia was significantly correlated with peak ACL equivalent stress (r = 0.89, p = 0.003) and peak ACL shear stress (r = 0.82, p = 0.023). Peak ACL equivalent stress also showed positive correlations with posterior GRF (r = 0.77, p = 0.025) and knee extension moments (r = 0.71, p = 0.049). In contrast, peak ACL shear stress exhibited a significant negative correlation with hip extension moment (r = −0.80, p = 0.032). This study identified key biomechanical factors affecting ACL stress, highlighting the roles of femoral displacement, knee extension moments, and ground reaction forces, while demonstrating a negative relationship with hip extension moments. Full article
(This article belongs to the Section Biomechanics and Sports Medicine)
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<p>Data collection and analysis process. In the ACL stress distribution map, the color gradient indicates relative stress magnitude, with red representing the highest stress, followed by yellow, green, and blue (lowest stress).</p>
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<p>Equivalent stress of the ACL during side-cutting. 0 to 100% indicates the corresponding time phase of the side-cutting. The color scale indicates the magnitude of stress, with blue representing low stress and red representing high stress. Low-stress condition: stress concentrations are observed primarily at the tibial attachment. High-stress condition: significant stress concentrations at the femoral attachment during the early landing phase.</p>
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<p>The shear stress of the ACL in the sagittal plane during side-cutting. 0 to 100% indicates the corresponding time phase of the side-cutting. The color scale indicates the magnitude of stress, with blue representing low stress and red representing high stress. Low-stress condition: stress concentrations are observed primarily at the tibial attachment. High-stress condition: significant stress concentrations at the femoral attachment during the early landing phase.</p>
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