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26 pages, 46995 KiB  
Article
New Evidence of Holocene Faulting Activity and Strike-Slip Rate of the Eastern Segment of the Sunan–Qilian Fault from UAV-Based Photogrammetry and Radiocarbon Dating, NE Tibetan Plateau
by Pengfei Niu, Zhujun Han, Peng Guo, Siyuan Ma and Haowen Ma
Remote Sens. 2024, 16(24), 4704; https://doi.org/10.3390/rs16244704 - 17 Dec 2024
Viewed by 353
Abstract
The eastern segment of the Sunan-Qilian Fault (ES-SQF) is located within the seismic gap between the 1927 M8.0 Gulang earthquake and the 1932 M7.6 Changma earthquake in China. It also aligns with the extension direction of the largest surface rupture zone associated with [...] Read more.
The eastern segment of the Sunan-Qilian Fault (ES-SQF) is located within the seismic gap between the 1927 M8.0 Gulang earthquake and the 1932 M7.6 Changma earthquake in China. It also aligns with the extension direction of the largest surface rupture zone associated with the 2022 Mw6.7 Menyuan earthquake. Understanding the activity parameters of this fault is essential for interpreting strain distribution patterns in the central–western segment of the Qilian–Haiyuan fault zone, located along the northeastern margin of the Tibetan Plateau, and for evaluating the seismic hazards in the region. High-resolution Google Earth satellite imagery and UAV (Unmanned Aerial Vehicle)-based photogrammetry provide favorable conditions for detailed mapping and the study of typical landforms along the ES-SQF. Combined with field geological surveys, the ES-SQF is identified as a continuous, singular-fault structure extending approximately 68 km in length. The fault trends in the WNW direction and along its trace, distinctive features, such as ridges, gullies, and terraces, show clear evidence of synchronous left lateral displacement. This study investigates the Qingsha River and the Dongzhong River. High-resolution digital elevation models (DEMs) derived from UAV imagery were used to conduct a detailed mapping of faulted landforms. An analysis of stripping trench profiles and radiocarbon dating of collected samples indicates that the most recent surface-rupturing seismic event in the area occurred between 3500 and 2328 y BP, pointing to the existence of an active fault from the Holocene epoch. Using the LaDiCaoz program to restore and measure displaced terraces at the study site, combined with geomorphological sample collection and testing, we estimated the fault’s slip rate since the Holocene to be approximately 2.0 ± 0.3 mm/y. Therefore, the ES-SQF plays a critical role in strain distribution across the central–western segment of the Qilian–Haiyuan fault zone. Together with the Tuolaishan fault, it accommodates and dissipates the left lateral shear deformation in this region. Based on the slip rate and the elapsed time since the last event, it is estimated that a seismic moment equivalent to Mw 7.5 has been accumulated on the ES-SQF. Additionally, with the significant Coulomb stress loading on the ES-SQF caused by the 2016 Mw 5.9 and 2022 Mw 6.7 Menyuan earthquakes, there is a potential for large earthquakes to occur in the future. Our results also indicate that high-resolution remote sensing imagery can facilitate detailed studies of active tectonics. Full article
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<p>The distribution of the major active faults and earthquake epicenters (M ≥ 6.0) along the northeastern margin of the Tibetan Plateau. (<b>a</b>) The red box indicates the area shown in panel (<b>b</b>), while the black arrows indicate the direction of block movement. Abbreviations: ATF, Altyn Tagh fault; KF, Kunlun fault; QHF, Qilian-Haiyuan fault; XF, Xianshuihe fault. (<b>b</b>) The locations and characteristics of the faults are based on [<a href="#B9-remotesensing-16-04704" class="html-bibr">9</a>]. The seismic data are sourced from the China Earthquake Information Network (<a href="https://news.ceic.ac.cn/index.html?time=1698442872" target="_blank">https://news.ceic.ac.cn/index.html?time=1698442872</a>, accessed on 3 October 2024), while the GPS velocity field relative to the stable Eurasian continent is derived from [<a href="#B21-remotesensing-16-04704" class="html-bibr">21</a>]. Abbreviations: ATF, Altyn Tagh fault; CMF, Changma fault; TLSF, Tuolaishan fault; HLHF, Halahu fault; SN-QLF, Sunan-Qilian fault; ES-SQF, Eastern segment of the Sunan–Qilian Fault; LLLF, Lenglongling fault; JQHF, Jinqianghe fault; MMSF, Maomaoshan fault; LHSF, Laohushan fault; HYF, Haiyuan fault; GLF, Gulang fault; XS-TJSF, Xiangshan-Tianjingshan fault.</p>
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<p>The distribution map of the eastern segment of the Sunan–Qilian Fault. (<b>a</b>) A fault distribution map, with the fault trace based on [<a href="#B9-remotesensing-16-04704" class="html-bibr">9</a>], primarily interpreted using high-resolution remote sensing images (Google Earth, 0.4 m resolution). (<b>b</b>) Geomorphic features along and on both sides of the fault.</p>
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<p>The faulted geomorphic features north of Ebao town (base map: Google Earth 2024 image). (<b>a</b>) Google Earth imagery; (<b>b</b>) fault trace with Google Earth imagery as the base map.</p>
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<p>A shaded relief map of the mountainous area north of Ebao town, captured using UAVs.</p>
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<p>Fault and displaced geomorphic features in the Qingsha River section. (<b>a</b>) Shaded relief map generated from the Unmanned Aerial Vehicle (UAV)-derived digital elevation model (DEM), with a resolution of 0.24 m. The contour interval is 2 m. (<b>b</b>) Interpreted map of displaced geomorphic features; (<b>c</b>–<b>f</b>) are close-up views.</p>
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<p>The measurement and restoration of T2/T1 riser displacement in the Qingsha River section using LaDiCaozsoftware (V2.1). (<b>a</b>) Shaded relief map of the T2/T1 riser on the left bank of the Qingsha River; the cyan line indicates the fault location, the light yellow lines show the trend of the risers on both sides of the fault, and the red and blue lines mark the locations of topographic profiles of the risers; (<b>b</b>) the optimal displacement restoration map of the T2/T1 riser; (<b>c</b>) the original riser and gully topographic profile (top left), the restored riser and gully topographic profile (bottom left), and the misfit distribution map for displacement measurements (right).</p>
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<p>Trench profile mosaic (<b>a</b>) and interpretation map (<b>b</b>) at the bend of the Qingsha River section.</p>
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<p>Close-up photo and interpretation map of the Qingsha River trench profile. (<b>a</b>) Close-up photo. (<b>b</b>) Fault interpretation map.</p>
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<p>The stratigraphic profile of the top of the T2 terrace in the Qingsha River section and sampling locations.</p>
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<p>Fault and displacement geomorphology features in the Dangzhong River section: (<b>a</b>) Shaded relief map generated from the Unmanned Aerial Vehicle (UAV)-derived digital elevation model (DEM), with a resolution of 0.24 m. The contour interval is 2 m. (<b>b</b>) Interpreted map of displaced geomorphic features.</p>
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<p>The displacement measurement and restoration of the T2/T1 riser in the Dangzhong River section based on LaDiCaoz software (V2.1). (<b>a</b>) Shaded relief map of the T2/T1 riser on the left bank of the Dangzhong River; the cyan line indicates the fault location, the light yellow lines show the trend of the risers on both sides of the fault, and the red and blue lines mark the locations of topographic profiles of the risers; (<b>b</b>) the optimal displacement restoration map of the T2/T1 riser; (<b>c</b>) the original riser and gully topographic profile (top left), the restored riser and gully topographic profile (bottom left), and the misfit distribution map for displacement measurements (right).</p>
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<p>Trench profile mosaic (<b>a</b>) and interpretation map (<b>b</b>) at the bend of the Dangzhong River.</p>
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<p>The stratigraphic profile of the top of the T2 terrace in the Dangzhong River section and sampling locations.</p>
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<p>The geological slip rate distribution map of the QHF [<a href="#B5-remotesensing-16-04704" class="html-bibr">5</a>,<a href="#B7-remotesensing-16-04704" class="html-bibr">7</a>,<a href="#B8-remotesensing-16-04704" class="html-bibr">8</a>,<a href="#B24-remotesensing-16-04704" class="html-bibr">24</a>,<a href="#B27-remotesensing-16-04704" class="html-bibr">27</a>,<a href="#B28-remotesensing-16-04704" class="html-bibr">28</a>,<a href="#B30-remotesensing-16-04704" class="html-bibr">30</a>,<a href="#B31-remotesensing-16-04704" class="html-bibr">31</a>,<a href="#B32-remotesensing-16-04704" class="html-bibr">32</a>,<a href="#B33-remotesensing-16-04704" class="html-bibr">33</a>,<a href="#B34-remotesensing-16-04704" class="html-bibr">34</a>,<a href="#B35-remotesensing-16-04704" class="html-bibr">35</a>,<a href="#B36-remotesensing-16-04704" class="html-bibr">36</a>,<a href="#B37-remotesensing-16-04704" class="html-bibr">37</a>,<a href="#B38-remotesensing-16-04704" class="html-bibr">38</a>,<a href="#B62-remotesensing-16-04704" class="html-bibr">62</a>,<a href="#B63-remotesensing-16-04704" class="html-bibr">63</a>,<a href="#B64-remotesensing-16-04704" class="html-bibr">64</a>,<a href="#B65-remotesensing-16-04704" class="html-bibr">65</a>,<a href="#B66-remotesensing-16-04704" class="html-bibr">66</a>,<a href="#B67-remotesensing-16-04704" class="html-bibr">67</a>]. Abbreviations: CMF, Changma fault; TLSF, Tuolaishan fault; HLHF, Halahu fault; SN-QLF, Sunan-Qilian fault; ES-SQF, Eastern segment of the Sunan–Qilian Fault; LLLF, Lenglongling fault; JQHF, Jinqianghe fault; MMSF, Maomaoshan fault; LHSF, Laohushan fault; HYF, Haiyuan fault; GLF, Gulang fault; XS-TJSF, Xiangshan-Tianjingshan fault.</p>
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<p>The influence of the 2022 Menyuan earthquake on the Coulomb stress of ES-SQF. Abbreviations: ES-SQF, Eastern segment of the Sunan–Qilian Fault. (<b>a</b>) A depth of 5 km; (<b>b</b>) A depth of 10 km.</p>
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16 pages, 6401 KiB  
Article
Estimation of Water Interception of Winter Wheat Canopy Under Sprinkler Irrigation Using UAV Image Data
by Xueqing Zhou, Haijun Liu and Lun Li
Water 2024, 16(24), 3609; https://doi.org/10.3390/w16243609 - 15 Dec 2024
Viewed by 408
Abstract
Canopy water interception is a key parameter to study the hydrological cycle, water utilization efficiency, and energy balance in terrestrial ecosystems. Especially in sprinkler-irrigated farmlands, the canopy interception further influences field energy distribution and microclimate, then plant transpiration and photosynthesis, and finally crop [...] Read more.
Canopy water interception is a key parameter to study the hydrological cycle, water utilization efficiency, and energy balance in terrestrial ecosystems. Especially in sprinkler-irrigated farmlands, the canopy interception further influences field energy distribution and microclimate, then plant transpiration and photosynthesis, and finally crop yield and water productivity. To reduce the field damage and increase measurement accuracy under traditional canopy water interception measurement, UAVs equipped with multispectral cameras were used to extract in situ crop canopy information. Based on the correlation coefficient (r), vegetative indices that are sensitive to canopy interception were screened out and then used to develop canopy interception models using linear regression (LR), random forest (RF), and back propagation neural network (BPNN) methods, and lastly these models were evaluated by root mean square error (RMSE) and mean relative error (MRE). Results show the canopy water interception is first closely related to relative normalized difference vegetation index (R△NDVI) with r of 0.76. The first seven indices with r from high to low are R△NDVI, reflectance values of the blue band (Blue), reflectance values of the near-infrared band (Nir), three-band gradient difference vegetation index (TGDVI), difference vegetation index (DVI), normalized difference red edge index (NDRE), and soil-adjusted vegetation index (SAVI) were chosen to develop canopy interception models. All the developed linear regression models based on three indices (R△NDVI, Blue, and NDRE), the RF model, and the BPNN model performed well in canopy water interception estimation (r: 0.53–0.76, RMSE: 0.18–0.27 mm, MRE: 21–27%) when the interception is less than 1.4 mm. The three methods underestimate the canopy interception by 18–32% when interception is higher than 1.4 mm, which could be due to the saturation of NDVI when leaf area index is higher than 4.0. Because linear regression is easy to perform, then the linear regression method with NDVI is recommended for canopy interception estimation of sprinkler-irrigated winter wheat. The proposed linear regression method and the R△NDVI index can further be used to estimate the canopy water interception of other plants as well as forest canopy. Full article
(This article belongs to the Special Issue Agricultural Water-Land-Plant System Engineering)
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<p>Map of experimental location and experimental field in this study.</p>
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<p>Heat map of correlation analysis between vegetation indices and canopy water interception. Note: * indicates the correlation coefficient between the two indices is significant at 0.05 level; ** indicates the relationship is significant at 0.01 level.</p>
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<p>Performance of linear regression models using unary and multiple vegetative indices. Panel (<b>a</b>) represents the linear model based on R<sub>△NDVI</sub> (model 7 in <a href="#water-16-03609-t003" class="html-table">Table 3</a>); (<b>b</b>) represents the model based on R<sub>△NDVI</sub> and Blue (model 8 in <a href="#water-16-03609-t003" class="html-table">Table 3</a>); (<b>c</b>) represents model based on R<sub>△NDVI</sub>, Blue, and NDRE (model 11 in <a href="#water-16-03609-t003" class="html-table">Table 3</a>).</p>
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<p>The estimated and measured canopy interceptions by RF model in the model developing and calibrating processes.</p>
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<p>The estimated and measured canopy interceptions by BP neural network model in the model developing and calibrating processes.</p>
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<p>The relationship between normalized difference vegetation index (NDVI) and leaf area index (LAI) in winter wheat.</p>
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21 pages, 7608 KiB  
Article
A Multi-Objective Optimization Design Method for High-Aspect-Ratio Wing Structures Based on Mind Evolution Algorithm Backpropagation Surrogate Model
by Jin Nan, Junhua Zheng, Bochuan Jiang, Yuhang Li, Jiayun Chen and Xuanqing Fan
Machines 2024, 12(12), 907; https://doi.org/10.3390/machines12120907 - 10 Dec 2024
Viewed by 258
Abstract
The design of high-aspect-ratio wings enhances the flight efficiency of UAVs but also introduces significant aeroelasticity challenges. The efficient optimization of wing structures in complex environments has become critical. To address the current challenges in balancing wing strength with lightweight structural designs, this [...] Read more.
The design of high-aspect-ratio wings enhances the flight efficiency of UAVs but also introduces significant aeroelasticity challenges. The efficient optimization of wing structures in complex environments has become critical. To address the current challenges in balancing wing strength with lightweight structural designs, this study proposed an intelligent solution method for optimizing wing dimensions and structural layout. Driven by mechanical simulation data, the method established a mapping relationship between the structural layout and dimensions of the wing and its bending stiffness. This approach was further enhanced by the mind evolution algorithm (MEA) to optimize the solution performance of the surrogate model. The wing structure optimization model was established using the multi-objective grey wolf optimizer (MOGWO) based on the surrogate model for search and optimization. This study focused on the composite material wing of a long-endurance unmanned aerial vehicle (UAV). The established MEA-BP surrogate model demonstrated high computational efficiency, with the prediction error standard deviation (STD) of wing deflection not exceeding 0.495 mm. The optimization model required 175 s to calculate the Pareto front solutions. The optimized structure resulted in a 28.32% increase in wing equivalent stiffness, and weight only increased by 6.67% compared to the original structure. These results showcased the effectiveness of the proposed method and validated the feasibility of integrating intelligent optimization algorithms and machine learning in the field of aircraft design. Full article
(This article belongs to the Section Machine Design and Theory)
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<p>General structure of UAV and wing.</p>
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<p>Diagram of the load on the wing.</p>
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<p>Schematic diagram of MEA and BP neural network. (<b>a</b>) Topologic diagram of BP neural network; (<b>b</b>) diagram of MEA structure.</p>
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<p>Flow chart of the MEA-BP neural network model training.</p>
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<p>Wolf pack classification and location update process in MOGWO.</p>
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<p>Flow chart of the MOGWO algorithm.</p>
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<p>Research approaches and procedure.</p>
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<p>Details of the wing structure.</p>
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<p>Spatial distribution of LHS parameters.</p>
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<p>Analysis of prediction results for different hidden layer structures. The pentagon markers represent the two BP network structures with the best prediction performance for each data set: (<b>a</b>) training set; (<b>b</b>) validation set; (<b>c</b>) test set; (<b>d</b>) entire data set; (<b>e</b>) X-axis labels correspond to hidden layer structures.</p>
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<p>Analysis of optimization effects of different population parameter settings of MEA.</p>
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<p>Processes of population convergence before and after alienation. (<b>a</b>) Processes of convergence in superior populations; (<b>b</b>) processes of convergence of temporary subpopulations; (<b>c</b>) processes of convergence in superior populations after alienation; (<b>d</b>) processes of convergence in temporary subpopulations after alienation.</p>
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<p>Regression of the surrogate model in the source domain.</p>
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<p>Error distribution of the model output in different datasets. (<b>a</b>) Error distribution of the total mass (<span class="html-italic">M</span><sub>all</sub>); (<b>b</b>) error distribution of the total mass (<span class="html-italic">W</span><sub>max</sub>).</p>
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<p>Distribution of Pareto front solution set. The red triangle represents the solution with the minimum <span class="html-italic">W</span><sub>max</sub> in the Pareto frontier solution set, the red rectangle represents the solution with the minimum <span class="html-italic">M</span><sub>all</sub>, and the red star represents the optimal solution in the Pareto frontier.</p>
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<p>Distribution of Pareto frontier solution sets obtained by solving with different parameters. (<b>a</b>) #1 Pareto frontier solution set; (<b>b</b>) #2 Pareto frontier solution set; (<b>c</b>) #3 Pareto frontier solution set; (<b>d</b>) #4 Pareto frontier solution set.</p>
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<p>Wing displacement cloud diagram based on simulation results. (<b>a</b>) Displacement cloud diagram of the selected optimal structure; (<b>b</b>) displacement cloud diagram of the minimal <span class="html-italic">W</span><sub>max</sub> model; (<b>c</b>) displacement cloud diagram of the minimal <span class="html-italic">M</span><sub>all</sub> model; (<b>d</b>) displacement cloud diagram of the original model.</p>
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20 pages, 16248 KiB  
Article
Design and Prototype Testing of a Smart SMA Actuator for UAV Foldable Tail Wings
by Yan Cheng, Jun Wang, Rui Li, Xiaojun Gu, Yahui Zhang, Jihong Zhu and Weihong Zhang
Actuators 2024, 13(12), 499; https://doi.org/10.3390/act13120499 - 6 Dec 2024
Viewed by 394
Abstract
The foldable tail wing system of UAVs offers advantages such as reducing the envelope size and improving storage space utilization. However, due to the compact tail wing space, achieving multi-modal locking and unlocking functionality presents significant challenges. This paper designs a new smart [...] Read more.
The foldable tail wing system of UAVs offers advantages such as reducing the envelope size and improving storage space utilization. However, due to the compact tail wing space, achieving multi-modal locking and unlocking functionality presents significant challenges. This paper designs a new smart SMA actuator for the use of UAV foldable tail wings. The prototype testing demonstrated the advantages and engineering practicality of the actuator. The core content includes three main parts: thermomechanical testing of the SMA actuation performance, structural design of the actuator, and the fabrication and actuation testing of the prototype. The key parameters related to actuation performance, such as phase transformation temperature and actuation force, were determined through DSC and tensile testing. The geometric parameters of the tail wing were determined through kinetics and kinematic analyses. Through the linkage design of two kinematic pairs, the SMA actuator enables both the deployment and locking of the tail wing. The prototype testing results of the folding tail wing show that, after vibration and temperature variation tests, the SMA actuator is still able to output an actuation stroke of 2.15 mm within 20 ms. The SMA actuator integrates locking for both modes of the tail wing and unlocking during mode transitions, offering advantages such as fast response and minimal space requirements. It provides an effective solution tailored to the needs of the foldable tail wing system. Full article
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<p>Actuator design schematic.</p>
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<p>Variable load actuator.</p>
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<p>The detailed design flowchart of the linear variable load actuator.</p>
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<p>Results of DSC experiments.</p>
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<p>NiTi tensile curve.</p>
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<p>Curves of Maximum Recoverable Force and Energization Time for NiTi Wires. (<b>a</b>) Maximum Recoverable Force Variation of 0.3 mm NiTi Wires. (<b>b</b>) Time Required for 0.3 mm NiTi Wires to Reach Maximum Recoverable Force.</p>
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<p>Experimental Platform for NiTi SMA Actuation Testing under Constant Load.</p>
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<p>Relationship between Load and Actuation Displacement.</p>
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<p>Relationship between NiTi wire displacement and load weight.</p>
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<p>Envelope Circle Size.</p>
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<p>Kinematics-Related Parameters. (<b>a</b>) Front View of the Tail Wing in Folded State. (<b>b</b>) Left View of the Tail Wing in Folded State. (<b>c</b>) Variables Related to Envelope Circle D. (<b>d</b>) Variables Related to Fold Angle <math display="inline"><semantics> <mi>α</mi> </semantics></math>.</p>
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<p>Schematic of related parameters at the rotational axis position.</p>
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<p>Torque Analysis.</p>
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<p>Tail wing rectangular coordinate system diagram.</p>
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<p>Kinetic Analysis of the Deployment Process.</p>
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<p>Foldable tail wing structure.</p>
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<p>Schematic Diagram of the Actuation Module.</p>
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<p>Schematic Diagram of Torsion Spring Actuation.</p>
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<p>Schematic Diagram of the Unlocking Mechanism.</p>
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<p>Schematic Diagram of the Mechanism in Different States.</p>
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<p>Complete Physical View of the Tail Wing. (<b>a</b>) Module Coordination in the Folded State. (<b>b</b>) Module Coordination in the Deployed State. (<b>c</b>) Complete Assembly of the System in the Folded State. (<b>d</b>) Complete Assembly of the System in the Deployed State.</p>
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<p>Physical Diagram of the Unlocking Mechanism.</p>
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<p>Response and Actuation Time Testing Platform.</p>
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<p>Actuation process diagram.</p>
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19 pages, 5696 KiB  
Article
Optimization Design and Atomization Performance of a Multi-Disc Centrifugal Nozzle for Unmanned Aerial Vehicle Sprayer
by Zhaoyan Zhu, Mengran Yang, Yangfan Li, Supakorn Wongsuk, Cheng Zhao, Lin Xu, Yongping Zhang, Xiongkui He and Changling Wang
Agronomy 2024, 14(12), 2914; https://doi.org/10.3390/agronomy14122914 - 6 Dec 2024
Viewed by 432
Abstract
The nozzle is a crucial component in unmanned aerial vehicle (UAV) sprayers. The centrifugal nozzle offers unique advantages; however, there is a scarcity of published research regarding the structural parameters, spraying parameters, and practical applications specifically for UAV spraying. Furthermore, there is a [...] Read more.
The nozzle is a crucial component in unmanned aerial vehicle (UAV) sprayers. The centrifugal nozzle offers unique advantages; however, there is a scarcity of published research regarding the structural parameters, spraying parameters, and practical applications specifically for UAV spraying. Furthermore, there is a need for UAV-specific nozzles that demonstrate high efficiency and excellent atomization performance. In this present study, a multi-disc centrifugal nozzle (MCN) capable of controlling droplet size was designed and optimized. The droplet size spectra with different atomizing discs were tested, and indoor and field tests were conducted to investigate the atomization and spray deposition characteristics of the MCN. It was found that the MCN with six atomizing discs with a curved groove, a disc angle of 120°, and a disc diameter of 77 mm demonstrated better atomizing performance. The volume median diameter was 96–153 μm, and the relative span was 1.0–1.3. Compared with the conventional hydraulic nozzle, this nozzle increased the effective spray swath width from 2.5–3.0 m to 4.0–5.0 m and promoted the average deposition rate by 132.4% at a flying height of 1.0 m and a flying speed of 3.0 m/s, which tends to raise the operation efficiency by four to five times. This study can provide a reference for the design and optimization of centrifugal nozzles for a UAV sprayer and the selection of operating parameters in aerial spraying operations. Full article
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<p>(<b>a</b>) Centrifugal Nozzle with different number of atomizing discs; (<b>b</b>) Structure diagram of multi-disc centrifugal nozzle (1. Brushless motor, 2. Copper backing ring, 3. Set screw, 4. Detachable infusion tube, 5. Top atomizing disc, 6. Middle atomizing disc, 7. Bottom atomizing disc).</p>
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<p>Component parts of multi-disc centrifugal nozzle: (<b>a</b>) outer rotor brushless motor with hollow axle; (<b>b</b>) detachable infusion tube; (<b>c</b>) outside and inside of atomizing disc.</p>
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<p>(<b>a</b>) Schematic diagram of droplet size testing system for multi-disc centrifugal nozzle (MCN); (<b>b</b>) droplet size test process (1. Tank, 2. Brushless diaphragm pump, 3. Flowmeter, 4. MCN, 5. Laser tachometer, 6. Laser droplet size analyzer, 7. Computer).</p>
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<p>Multi-disc centrifugal nozzle droplet deposition distribution test.</p>
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<p>Tests of deposition distribution: (<b>a</b>) equipment layout diagram in test; (<b>b</b>) test process. 1–15: The position where the droplet collector is placed.</p>
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<p>Effect of grooves on relative span (RS) of droplets in multi-disc centrifugal nozzles. Note: different lowercase letters in the graphs indicate significant differences in the data of each group at the <span class="html-italic">p</span> &lt; 0.05 level by Dunn’s multiple comparison test. Dispersion points indicate RS values of droplets at different flow rates and atomizing disc speeds.</p>
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<p>Effect of disc angle on relative span (RS) of droplets from multi-disc centrifugal nozzles. Note: different lowercase letters in the graphs indicate significant differences in the data of each group at the <span class="html-italic">p</span> &lt; 0.05 level by Dunn’s multiple comparison test. Dispersion points indicate RS values of droplets at different flow rates and atomizing disc speeds.</p>
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<p>Effect of disc diameter on the atomization characteristics (Dv<sub>50</sub> and RS) of multi-disc centrifugal nozzles. (<b>a</b>) Effect of disc diameter on Dv<sub>50</sub>; (<b>b</b>) effect of disc diameter on relative span (RS). Note: different lowercase letters in the graphs indicate significant differences in the data of each group at the <span class="html-italic">p</span> &lt; 0.05 level by Dunn’s multiple comparison test.</p>
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<p>Influence of the number of atomizing discs on relative span (RS) of droplets in the centrifugal nozzle. Note: different lowercase letters in the graphs indicate significant differences in the data of each group at the <span class="html-italic">p</span> &lt; 0.05 level by Dunn’s multiple comparison test.</p>
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<p>Effect of rotational speed and flow rate on atomization characteristics (Dv<sub>50</sub> and RS) of multi-disc centrifugal nozzle. (<b>a</b>) Influence of rotational speed on Dv<sub>50</sub>; (<b>b</b>) impact of flow rate on relative span (RS). Note: different lowercase letters in the graphs indicate significant differences in the data of each group at the <span class="html-italic">p</span> &lt; 0.05 level by Dunn’s multiple comparison test. The dispersion points indicate the Dv<sub>50</sub> of the droplets at different flow rates.</p>
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<p>Droplet deposition distribution of multi-disc centrifugal nozzles at various spray heights in indoor tests. (<b>a</b>) Nozzle height 0.5 m; (<b>b</b>) nozzle height 1.0 m; (<b>c</b>) nozzle height 1.5 m; (<b>d</b>) nozzle height 2.0 m.</p>
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<p>Droplet deposition distribution of multi-disc centrifugal nozzles at various spray heights in indoor tests. (<b>a</b>) Nozzle height 0.5 m; (<b>b</b>) nozzle height 1.0 m; (<b>c</b>) nozzle height 1.5 m; (<b>d</b>) nozzle height 2.0 m.</p>
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<p>Droplet deposition distribution of multi-rotor unmanned aerial vehicle (UAV) sprayer equipped with 2 models of nozzles.</p>
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<p>Effective spray swath width of multi-rotor unmanned aerial vehicle (UAV) sprayer with hydraulic nozzle and multi-disc centrifugal nozzle in field test.</p>
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16 pages, 7838 KiB  
Article
Quaternary Activity and Paleoearthquakes of the Fushan Fault, Shanxi, China
by Xiaobing Yan, Yongsheng Zhou, Xuejing Hao, Ruiguo Ren and Xiaoying Sun
Appl. Sci. 2024, 14(23), 11250; https://doi.org/10.3390/app142311250 - 2 Dec 2024
Viewed by 525
Abstract
The AD 1209 M6.5 Fushan earthquake caused significant casualties and damage. The Fushan Fault, forming the boundary between the Linfen Faulted Basin and uplifted Taihang Mountains, may have been the seismogenic fault, but research is lacking. Based on UAV and field surveys, we [...] Read more.
The AD 1209 M6.5 Fushan earthquake caused significant casualties and damage. The Fushan Fault, forming the boundary between the Linfen Faulted Basin and uplifted Taihang Mountains, may have been the seismogenic fault, but research is lacking. Based on UAV and field surveys, we found that the Fushan Fault has a surface exposure length of 24 km and displaces Holocene strata. Samples from offset layers within a trench showed that the most recent event occurred within the last 7 ka (i.e., Holocene activity) and that the fault has the potential to generate earthquakes exceeding magnitude 7. Since 17 ka (late Quaternary), two significant paleoearthquakes have been identified: (1) between 17 and 7 ka (displacement: 2.04 m, average slip: 0.2 mm/yr) and (2) within the last 7 ka (displacement: 3.93 m, average slip: 0.56 mm/yr). Since the Late Pleistocene, the displacement rate has increased, indicating an increasing potential seismic hazard. These results were confirmed by terrestrial LiDAR; the bedrock fault surface fractal dimensions are consistent with two paleoearthquake events since the late Quaternary (coseismic displacements of 2.51 and 3.18 m). This article uses an empirical formula to evaluate the potential maximum magnitude of the Fushan Fault based on the relationship between the distribution range of the fault surface and the magnitude. Therefore, the maximum assessed earthquake magnitudes of the Fushan Fault are Ms = 7.07, 6.94, and 7.31. This assessment result basically matches the strength of the 6.5 magnitude Fushan earthquake in 1209 AD. By comparing with historical records, our results confirm that the Fushan Fault was the seismogenic structure responsible for the AD 1209 M6.5 Fushan earthquake. Full article
(This article belongs to the Special Issue Paleoseismology and Disaster Prevention)
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<p>Earthquake distribution and geological background of the research area. (<b>a</b>) Simplified tectonic map of China. The red frame marks the extent of (<b>b</b>). (<b>b</b>) Tectonic setting of the Linfen Basin and Shanxi graben system. The black dashed rectangle represents the main study area (see <a href="#applsci-14-11250-f002" class="html-fig">Figure 2</a> for details). F1: Jiaocheng Fault; F2: Qixian–Dongyang Fault; F3: Taigu Fault; F4: Huoshan Piedmont Fault; F5: Hongdong Fault; F6: Lishi Fault; F7: Luoyunshan Fault; F8: Dayang Fault; F9: Fushan Fault; F10: Hancheng Fault; F11: Northern Fault of Emei table; F12: Southern Fault of Emei table; F13: Northern Zhongtiaoshan Fault; F14: Southern Zhongtiaoshan Fault; F15: Jinhuo Fault.</p>
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<p>The research framework diagram.</p>
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<p>(<b>a</b>) Structural characteristics of the Fushan Fault area and locations of unmanned aerial vehicle (UAV) survey control points, exploration trenches, and bedrock surfaces. The black border in the figure (<b>a</b>) represents the range of (<b>b</b>).</p>
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<p>Map of the Fushan Fault from the combination of unmanned aerial vehicle (UAV) and satellite remote sensing data.</p>
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<p>Qianjiao village trench fault profile. QJC-01 and QJC-02 denote sample numbers.</p>
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<p>Workflow for calculating two-dimensional fractal dimension values of the fault surface morphology. (<b>a</b>) Subdivision of units on the bedrock fault surface. N × N represents the sliding window size, where N is the product of the number of DEM cells within the sliding window and the length of each DEM cell. (<b>b</b>) Fractal dimension values for each calculation unit. (<b>c</b>) Mean values of the normal distribution fit for the fractal dimension values of each row calculation unit on the fault surface. The length of the error bars on one side represents the standard deviation of the normal distribution fit for each row calculation unit’s fractal dimension values.</p>
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<p>Two-dimensional fractal dimensions of fault surface morphology. The color-rendered images illustrate planar distributions of two-dimensional fractal dimension values (D values) of the fault surface; scatter plots represent the normal fitting mean of D values along the fault strike, with bidirectional error bars indicating the 95% confidence interval of the estimated values. The red solid line represents the optimal normal fit of the D values within a single band of the fault surface.</p>
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<p>Simplified regional geological map of the Ordos Block and nearby areas (cited from Deng, 2008 [<a href="#B15-applsci-14-11250" class="html-bibr">15</a>]). A: Sertengshan range-front Fault. B: Xinzhou Fault. C: Luoyunshan Fault. D: Fushan Fault.</p>
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19 pages, 5764 KiB  
Article
Optimization Design and Experimental Study of Solid Particle Spreader for Unmanned Aerial Vehicle
by Linhuan Zhang, Ruirui Zhang, Tongchuan Yi, Danzhu Zhang, Chenchen Ding, Mingqi Wu and Ryozo Noguchi
Drones 2024, 8(12), 726; https://doi.org/10.3390/drones8120726 - 1 Dec 2024
Viewed by 492
Abstract
This study designed and investigated a solid particle spreader, as well as parameter optimization and experimental for a groove wheel, to mitigate the problems of low uniformity and poor control accuracy of solid particulate material UAV spreading. The discrete element method was used [...] Read more.
This study designed and investigated a solid particle spreader, as well as parameter optimization and experimental for a groove wheel, to mitigate the problems of low uniformity and poor control accuracy of solid particulate material UAV spreading. The discrete element method was used to simulate and analyze the displacement range and stability of each grooved wheel at low speeds. Furthermore, orthogonal regression and response surface analyses were used to analyze the influence of each factor on the stability of the discharge rate and pulsation amplitude. The results showed that the helix angle, sharpness, and length of the groove significantly influenced the application performance, whereas the number of grooves had no significant influence. The groove shape was eccentric, the helix angle was 50°, the length was 35 mm, and the number of grooves was 7. Additionally, the bench test results showed that in the range of 10–60 rpm, the relative deviation of the discharging rate between the simulation and bench test is from 0.47% to 10.39%, and the average relative deviation is 3.93%. Between the groove wheel rotation speed and discharge rate, R2 was 0.991, and the adjustable range of the discharge amount was between 3.68 and 23.43 g/s. The minimum and maximum variation coefficients of the average discharge rate among individual applicators were 1.01% and 2.79%, respectively, whereas the standard deviations were 0.09 and 0.46 g/s, respectively. In conclusion, the discharge stability and adjustable range of the spreader using the optimized groove wheel satisfied the requirements for solid particulate material discharge. Full article
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<p>UAV-based particulate material spreading system.</p>
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<p>Structure of the particulate unit spreader.</p>
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<p>Structure of the discharging apparatus.</p>
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<p>Section view of three typical groove wheels: (<b>a</b>) circular-arc type, (<b>b</b>) eccentric-arc type, and (<b>c</b>) circumscribed-arc type.</p>
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<p>Force analyzing particulates in the helix groove: (<b>a</b>) particle force analysis, (<b>b</b>) particles and pane force analysis.</p>
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<p>Circumferential and axial force of particulates under different helix angles.</p>
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<p>Simulation model of the discharge apparatus.</p>
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<p>Two-factor response surface of discharge apparatus performance: (<b>a</b>) groove shape and helix angle interaction, (<b>b</b>) groove helix angle and number interaction, (<b>c</b>) groove helix angle and length interaction, (<b>d</b>) groove shape and number interaction, (<b>e</b>) groove shape and length interaction, and (<b>f</b>) groove length and number interaction.</p>
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<p>Two-factor response surface of discharge apparatus performance: (<b>a</b>) groove shape and helix angle interaction, (<b>b</b>) groove helix angle and number interaction, (<b>c</b>) groove helix angle and length interaction, (<b>d</b>) groove shape and number interaction, (<b>e</b>) groove shape and length interaction, and (<b>f</b>) groove length and number interaction.</p>
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<p>Simulated discharging amount at different groove wheel rotation speeds.</p>
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<p>Discharge apparatus performance evaluation experiments.</p>
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<p>Relationship between the discharge rate and groove wheel rotation speed.</p>
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<p>Coefficient of variation and standard deviation of spreader units.</p>
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24 pages, 6941 KiB  
Article
Discriminating Seagrasses from Green Macroalgae in European Intertidal Areas Using High-Resolution Multispectral Drone Imagery
by Simon Oiry, Bede Ffinian Rowe Davies, Ana I. Sousa, Philippe Rosa, Maria Laura Zoffoli, Guillaume Brunier, Pierre Gernez and Laurent Barillé
Remote Sens. 2024, 16(23), 4383; https://doi.org/10.3390/rs16234383 - 23 Nov 2024
Viewed by 758
Abstract
Coastal areas support seagrass meadows, which offer crucial ecosystem services, including erosion control and carbon sequestration. However, these areas are increasingly impacted by human activities, leading to habitat fragmentation and seagrass decline. In situ surveys, traditionally performed to monitor these ecosystems, face limitations [...] Read more.
Coastal areas support seagrass meadows, which offer crucial ecosystem services, including erosion control and carbon sequestration. However, these areas are increasingly impacted by human activities, leading to habitat fragmentation and seagrass decline. In situ surveys, traditionally performed to monitor these ecosystems, face limitations on temporal and spatial coverage, particularly in intertidal zones, prompting the addition of satellite data within monitoring programs. Yet, satellite remote sensing can be limited by too coarse spatial and/or spectral resolutions, making it difficult to discriminate seagrass from other macrophytes in highly heterogeneous meadows. Drone (unmanned aerial vehicle—UAV) images at a very high spatial resolution offer a promising solution to address challenges related to spatial heterogeneity and the intrapixel mixture. This study focuses on using drone acquisitions with a ten spectral band sensor similar to that onboard Sentinel-2 for mapping intertidal macrophytes at low tide (i.e., during a period of emersion) and effectively discriminating between seagrass and green macroalgae. Nine drone flights were conducted at two different altitudes (12 m and 120 m) across heterogeneous intertidal European habitats in France and Portugal, providing multispectral reflectance observation at very high spatial resolution (8 mm and 80 mm, respectively). Taking advantage of their extremely high spatial resolution, the low altitude flights were used to train a Neural Network classifier to discriminate five taxonomic classes of intertidal vegetation: Magnoliopsida (Seagrass), Chlorophyceae (Green macroalgae), Phaeophyceae (Brown algae), Rhodophyceae (Red macroalgae), and benthic Bacillariophyceae (Benthic diatoms), and validated using concomitant field measurements. Classification of drone imagery resulted in an overall accuracy of 94% across all sites and images, covering a total area of 467,000 m2. The model exhibited an accuracy of 96.4% in identifying seagrass. In particular, seagrass and green algae can be discriminated. The very high spatial resolution of the drone data made it possible to assess the influence of spatial resolution on the classification outputs, showing a limited loss in seagrass detection up to about 10 m. Altogether, our findings suggest that the MultiSpectral Instrument (MSI) onboard Sentinel-2 offers a relevant trade-off between its spatial and spectral resolution, thus offering promising perspectives for satellite remote sensing of intertidal biodiversity over larger scales. Full article
(This article belongs to the Section Ecological Remote Sensing)
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<p>Location of drone flights in France and Portugal. (<b>A</b>) Gulf of Morbihan (Two sites), (<b>B</b>) Bourgneuf Bay (Two sites), and (<b>C</b>) Ria de Aveiro Coastal Lagoon (Three sites). The golden areas represent the intertidal zone.</p>
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<p>The five taxonomic classes of vegetation used to train the Neural Network model and an example of their raw spectral signatures at the spectral resolution of the Micasense RedEdge Dual MX. (<b>A</b>): Magnoliopsida (<span class="html-italic">Zostera noltei</span>); (<b>B</b>): Phaeophyceae (<span class="html-italic">Fucus</span> sp.); (<b>C</b>): Rhodophyceae (<span class="html-italic">Gracilaria vermiculophylla</span>); (<b>D</b>): Chlorophyceae (<span class="html-italic">Ulva</span> sp.); (<b>E</b>): Bacillariophyceae (Benthic diatoms). (<b>F</b>): Spectral signature of each vegetation class. Classes and species taxonomy following the WORMS—World Register of Marine Species classification.</p>
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<p>Schematic representation of the workflow. Parallelograms represent input or output data, and rectangles represent Python processing algorithms. The overall workflow of this study is divided into two distinct parts based on the spatial resolution of the drone flights: high-resolution flights (pixel size: 8 mm) were utilized for training and prediction of the Neural Network model, whereas lower-resolution flights (pixel size: 80 mm) were solely employed for prediction and validation purposes. Validation has been performed on both high- and low-resolution flights.</p>
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<p>Comparison of reflectance retrieved from both low-altitude and high-altitude flights over a common area. The black dashed line represents a 1 to 1 relationship. The left (<b>A</b>) plots raw data, and the right (<b>B</b>) plots standardized data (Equation (1)).</p>
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<p>RGB ortho-mosaic (<b>Left</b>) and Prediction (<b>Right</b>) of the low altitude flight of Gafanha, Portugal. The total extent of this flight was 3000 m<sup>2</sup> with a resolution of 8 mm per pixel. The zoom covers an area equivalent to a 10 m Sentinel-2 pixel size.</p>
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<p>RGB ortho-mosaic (<b>Left</b>) and Prediction (<b>Right</b>) of the high-altitude flight of Gafanha, Portugal. The total extent of this flight was about 1 km<sup>2</sup> with a resolution of 80 mm per pixel. The yellow outline shows the extent of Gafanha’s low-altitude flight, as presented in <a href="#remotesensing-16-04383-f005" class="html-fig">Figure 5</a>. The zoom covers an area equivalent to a 10 m Sentinel-2 pixel size.</p>
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<p>RGB ortho-mosaic (<b>Top</b>) and Prediction (<b>Bottom</b>) of the flight made in the inner part of Ria de Aveiro coastal lagoon, Portugal. The total extent of this flight was about 1.5 km<sup>2</sup> with a resolution of 80 mm per pixel. The zoom inserts cover an area equivalent to the size of a 10 m Sentinel-2 pixel.</p>
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<p>RGB ortho-mosaic (<b>Top</b>) and Prediction (<b>Bottom</b>) of L’Epine, France. The total extent of this flight was about 28,000 m<sup>2</sup> with a resolution of 80 mm per pixel. The zoom covers an area equivalent to a 10 m Sentinel-2 pixel size.</p>
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<p>A global confusion matrix on the left is derived from validation data across each flight, while a mosaic of confusion matrices from individual flights is presented on the right. The labels inside the matrices indicate the balanced accuracy for each class. The labels at the bottom of the global matrix indicate the User’s accuracy for each class, and those on the right indicate the Producer’s Accuracy. The values adjacent to the names of each site represent the proportion of total pixels from that site contributing to the overall matrix. Grey lines within the mosaic indicate the absence of validation data for the class at that site. The table at the bottom summarizes the Sensitivity, Specificity, and Accuracy for each class and for the overall model.</p>
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<p>Variable Importance of the Neural Network Classifier for each taxonomic class. The longer the slice, the more important the variable for prediction of each class. The right plot shows the drone raw and standardized reflectance spectra of each class. Each slice represents the Variable Importance (VI) of both raw and standardized reflectance combined.</p>
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<p>Predicted area loss for different vegetation types (green algae, seagrass, brown algae, and red algae) as a function of spatial resolution. The lines represent Generalized Linear Model (GLM) predictions, and shaded areas indicate standard errors. As the resolution decreases, predicted area loss increases for all vegetation types, with green algae showing the highest loss and seagrass the smallest at coarser resolutions.</p>
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<p>Kernel density plot showing the proportion of pixels well classified based on the percent cover of the class in high-altitude flight pixels of Gafanha, Portugal. Each subplot shows all the pixels of the same classes on the high-altitude flight. The cover (%) of classes was retrieved using the result of the classification of the low-altitude flight in Gafanha, Portugal.</p>
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<p>Photosynthetic and carotenoid pigments present (Green) or absent (Red) in each taxonomic class present in the Neural Network Classifier, along with their absorption wavelength measured with spectroradiometer, Chl-b—chlorophyll-b, Chl-c—chlorophyll-c, Fuco—fucoxanthin, Zea—zeaxanthin, Diad—diadinoxanthin, Lut—lutein, Neo—neoxanthin, PE—phycoerythrin, PC—phycocyanin; [<a href="#B25-remotesensing-16-04383" class="html-bibr">25</a>,<a href="#B26-remotesensing-16-04383" class="html-bibr">26</a>,<a href="#B54-remotesensing-16-04383" class="html-bibr">54</a>,<a href="#B55-remotesensing-16-04383" class="html-bibr">55</a>,<a href="#B56-remotesensing-16-04383" class="html-bibr">56</a>].</p>
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<p>Sample of <a href="#remotesensing-16-04383-f009" class="html-fig">Figure 9</a> focusing on green macrophytes. The labels inside the matrix indicate the number of pixels.</p>
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43 pages, 4383 KiB  
Review
Integrating UAVs and RISs in Future Wireless Networks: A Review and Tutorial on IoTs and Vehicular Communications
by Mohsen Eskandari and Andrey V. Savkin
Future Internet 2024, 16(12), 433; https://doi.org/10.3390/fi16120433 - 21 Nov 2024
Viewed by 850
Abstract
The rapid evolution of smart cities relies heavily on advancements in wireless communication systems and extensive IoT networks. This paper offers a comprehensive review of the critical role and future potential of integrating unmanned aerial vehicles (UAVs) and reconfigurable intelligent surfaces (RISs) to [...] Read more.
The rapid evolution of smart cities relies heavily on advancements in wireless communication systems and extensive IoT networks. This paper offers a comprehensive review of the critical role and future potential of integrating unmanned aerial vehicles (UAVs) and reconfigurable intelligent surfaces (RISs) to enhance Internet of Vehicles (IoV) systems within beyond-fifth-generation (B5G) and sixth-generation (6G) networks. We explore the combination of quasi-optical millimeter-wave (mmWave) signals with UAV-enabled, RIS-assisted networks and their applications in urban environments. This review covers essential areas such as channel modeling and position-aware beamforming in dynamic networks, including UAVs and IoVs. Moreover, we investigate UAV navigation and control, emphasizing the development of obstacle-free trajectory designs in dense urban areas while meeting kinodynamic and motion constraints. The emerging potential of RIS-equipped UAVs (RISeUAVs) is highlighted, along with their role in supporting IoVs and in mobile edge computing. Optimization techniques, including convex programming methods and machine learning, are explored to tackle complex challenges, with an emphasis on studying computational complexity and feasibility for real-time operations. Additionally, this review highlights the integrated localization and communication strategies to enhance UAV and autonomous ground vehicle operations. This tutorial-style overview offers insights into the technical challenges and innovative solutions of the next-generation wireless networks in smart cities, with a focus on vehicular communications. Finally, future research directions are outlined. Full article
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<p>Organization of the paper based on the taxonomy of the UAV-enabled, RIS-assisted communication into quintuple studied and topics.</p>
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<p>Illustration of direct LoS path and multi-path.</p>
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<p>UAV-enabled, RIS-assisted communication: (<b>a</b>) RISeUAV with a UPA of the RIS aligned in the XY plane facing the ground; (<b>b</b>) UAV-BS as an active aerial (airborne) BS.</p>
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<p>Schematic of RISeUAV-assisted communication for channel modeling: (<b>a</b>) geometry of system in 3D coordinates; (<b>b</b>) UPA of the RIS in XY plane; <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>v</mi> </mrow> <mrow> <mi>R</mi> <mi>U</mi> </mrow> </msup> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>u</mi> </mrow> <mrow> <mi>R</mi> <mi>U</mi> </mrow> </msup> </mrow> </semantics></math> denote UAV’s horizontal and vertical linear velocities, respectively; <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>ω</mi> </mrow> <mrow> <mi>R</mi> <mi>U</mi> </mrow> </msup> </mrow> </semantics></math> denotes the UAV’s horizontal rotational velocity and <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>θ</mi> </mrow> <mrow> <mi>R</mi> <mi>U</mi> </mrow> </msup> </mrow> </semantics></math> denotes the UAV heading (angle) with respect to the X-axis. The UAV motion is studied in <a href="#sec4-futureinternet-16-00433" class="html-sec">Section 4</a>.</p>
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<p>Schematic of UAV-enabled, RIS-assisted wireless communication for intelligent vehicles (IVs) in IoVs with mMIMO BSs. Notice that, for the sake of illustration, the sizes of the mMIMO BS and RISeUAV are exaggerated compared with the distances.</p>
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<p>Aerial backhauling through the RISeUAV to UAV-BSs.</p>
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<p>The schematic of the actor-critic deep deterministic policy gradient DRL agent.</p>
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<p>The geometry of the SLAPS for RISeUAV.</p>
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34 pages, 15986 KiB  
Article
A Comprehensive Framework for Transportation Infrastructure Digitalization: TJYRoad-Net for Enhanced Point Cloud Segmentation
by Zhen Yang, Mingxuan Wang and Shikun Xie
Sensors 2024, 24(22), 7222; https://doi.org/10.3390/s24227222 - 12 Nov 2024
Viewed by 729
Abstract
This research introduces a cutting-edge approach to traffic infrastructure digitization, integrating UAV oblique photography with LiDAR point clouds for high-precision, lightweight 3D road modeling. The proposed method addresses the challenge of accurately capturing the current state of infrastructure while minimizing redundancy and optimizing [...] Read more.
This research introduces a cutting-edge approach to traffic infrastructure digitization, integrating UAV oblique photography with LiDAR point clouds for high-precision, lightweight 3D road modeling. The proposed method addresses the challenge of accurately capturing the current state of infrastructure while minimizing redundancy and optimizing computational efficiency. A key innovation is the development of the TJYRoad-Net model, which achieves over 85% mIoU segmentation accuracy by including a traffic feature computing (TFC) module composed of three critical components: the Regional Coordinate Encoder (RCE), the Context-Aware Aggregation Unit (CAU), and the Hierarchical Expansion Block. Comparative analysis segments the point clouds into road and non-road categories, achieving centimeter-level registration accuracy with RANSAC and ICP. Two lightweight surface reconstruction techniques are implemented: (1) algorithmic reconstruction, which delivers a 6.3 mm elevation error at 95% confidence in complex intersections, and (2) template matching, which replaces road markings, poles, and vegetation using bounding boxes. These methods ensure accurate results with minimal memory overhead. The optimized 3D models have been successfully applied in driving simulation and traffic flow analysis, providing a practical and scalable solution for real-world infrastructure modeling and analysis. These applications demonstrate the versatility and efficiency of the proposed methods in modern traffic system simulations. Full article
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<p>The technical roadmap of the entire paper.</p>
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<p>DJI M300RTK UAV with Zenith P1 gimbal camera.</p>
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<p>Dense UAV point cloud of road infrastructure.</p>
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<p>Laser point cloud of road infrastructure.</p>
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<p>TJYRoad-Net network.</p>
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<p>TJYRoad-Net network.</p>
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<p>Traditional machine learning versus transfer learning.</p>
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<p>Fine-tuning ideas of enhanced TJYRoad-Net.</p>
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<p>Image point cloud and laser point cloud.</p>
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<p>Semantic segmentation result of laser point cloud.</p>
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<p>Semantic segmentation results of image point cloud.</p>
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<p>Semantic segmentation results of image point clouds from a road intersection scene, showing Input (original point cloud), Ground Truth (manually annotated labels), and Predicted Value (model output with misclassifications circled).</p>
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<p>Comparison of segmentation results across different state-of-the-art methods, with red circles highlighting the segmentation outputs at identical locations for each method.</p>
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<p>ICP fine alignment error of pavement point cloud.</p>
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<p>Registered results of road surface point clouds.</p>
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<p>Process of building façade precision.</p>
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<p>ICP fine alignment error of building façade point clouds.</p>
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<p>Alignment result of point clouds.</p>
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<p>Variation in model error with downsampling voxel size.</p>
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<p>Downsampling results of road surface point clouds.</p>
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<p>Result of road reconstruction.</p>
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<p>Marker triangle network structure based on Poisson reconstruction.</p>
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<p>A section of the grid center of mass.</p>
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<p>Design of road marking template library.</p>
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<p>Marking reconstruction results.</p>
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<p>Vegetation reconstruction results.</p>
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<p>Real scene of road infrastructure.</p>
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<p>Driving simulation data visualization platform.</p>
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18 pages, 6544 KiB  
Article
Remote Inspection of Bridges with the Integration of Scanning Total Station and Unmanned Aerial Vehicle Data
by Piotr Olaszek, Edgar Maciejewski, Anna Rakoczy, Rafael Cabral, Ricardo Santos and Diogo Ribeiro
Remote Sens. 2024, 16(22), 4176; https://doi.org/10.3390/rs16224176 - 8 Nov 2024
Viewed by 805
Abstract
Remote visual inspections are valuable tools for maintaining bridges in safe operation. In the case of old structures with incomplete documentation, the verification of dimensions is also an essential aspect. This paper presents an attempt to use a Scanning Total Station (STS) and [...] Read more.
Remote visual inspections are valuable tools for maintaining bridges in safe operation. In the case of old structures with incomplete documentation, the verification of dimensions is also an essential aspect. This paper presents an attempt to use a Scanning Total Station (STS) and Unmanned Aerial Vehicle (UAV) for the inspection and inventory of bridge dimensions. The STS’s measurements are conducted by applying two methods: the direct method using a total station (TS) and advanced geometric analyses of the collected point cloud. The UAV’s measurements use a Structure from Motion (SfM) method. Verification tests were conducted on a steel truss railway bridge over the largest river in Poland. The measurements concerned both the basic dimensions of the bridge and the details of a selected truss connection. The STS identified a significant deviation in the actual geometry of the measured connection and the design documentation. The UAV’s inspection confirmed these findings. The integration of STS and UAV technologies has demonstrated significant advantages, including STS’s high accuracy in direct measurements, with deviations within acceptable engineering tolerances (below a few mm), and the UAV’s efficiency in covering large areas, achieving over 90% compliance with reference dimensions. This combined approach not only reduces operating costs and enhances safety by minimizing the need for heavy machinery or scaffolding but also provides a more comprehensive understanding of the structural condition. Full article
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Graphical abstract
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<p>Applied algorithms for determining dimensions from the point cloud calculations.</p>
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<p>The applied algorithms for determining dimensions from the photogrammetry calculations.</p>
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<p>The possibilities of integrating data from STS and UAV methods.</p>
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<p>Bridge selected for verification tests: (<b>a</b>) satellite image with selected bridge highlighted—Google Maps; (<b>b</b>) view of the truss spans over the river; (<b>c</b>) view from the side of the truss spans over the road.</p>
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<p>Views from the riverbank of the span selected for the experiment with the analyzed connection marked: (<b>a</b>) side view; (<b>b</b>) view from below.</p>
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<p>Part of the documentation drawings of the span showing the selected basic dimensions: (<b>a</b>) the longitudinal section and enlargements; (<b>b</b>) cross-section with the span width marked—SW; (<b>c</b>) the start and end points of the span length measurement—(SL); (<b>d</b>) the span height marked—SH; (<b>e</b>) the diagonal length—DL—and the post length—PL—marked.</p>
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<p>The main truss connection: (<b>a</b>) a close-up view and (<b>b</b>) part of the documentation drawing of the connection showing the selected dimensions.</p>
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<p>Photographs of the analyzed connection: (<b>a</b>) taken from a UAV; (<b>b</b>) taken from the STS.</p>
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<p>Measuring the diagonal and post length with the STS; points defining the dimensions were marked automatically with a red cross: (<b>a</b>) the top of the diagonal; (<b>b</b>) the top of the post; (<b>c</b>) the bottom of the diagonal; (<b>d</b>) the bottom of the post.</p>
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<p>Photogrammetry of the inspected bridge span.</p>
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<p>A point cloud of the analyzed connection projected onto the 2D plane: (<b>a</b>) the STS system calculation; (<b>b</b>) the UAV system calculation.</p>
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<p>Geometry verification: STS point cloud contour (black solid line), UAV point cloud contour (green solid line), and documentation drawing (red dotted line).</p>
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<p>The occurrence of an analyzed discrepancy between the documentation and the observed structure in other connections of the span (based on photos taken by the UAV).</p>
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13 pages, 1510 KiB  
Article
A Three-Dimensional Time-Varying Channel Model for THz UAV-Based Dual-Mobility Channels
by Kai Zhang, Fenglei Zhang, Yongjun Li, Xiang Wang, Zhaohui Yang, Yuanhao Liu, Changming Zhang and Xin Li
Entropy 2024, 26(11), 924; https://doi.org/10.3390/e26110924 - 30 Oct 2024
Viewed by 567
Abstract
Unmanned aerial vehicle (UAV) as an aerial base station or relay device is a promising technology to rapidly provide wireless connectivity to ground device. Given UAV’s agility and mobility, ground user’s mobility, a key question is how to analyze and value the performance [...] Read more.
Unmanned aerial vehicle (UAV) as an aerial base station or relay device is a promising technology to rapidly provide wireless connectivity to ground device. Given UAV’s agility and mobility, ground user’s mobility, a key question is how to analyze and value the performance of UAV-based wireless channel in the terahertz (THz) band. In this paper, a three-dimensional (3D) time-varying channel model is proposed for UAV-based dual-mobility wireless channels based on geometric channel model theory in THz band. In this proposed channel model, the small-scale fading (e.g., scattering fading and reflection fading) on rough surfaces of communication environment and the atmospheric molecule absorption attenuations are considered in THz band. Moreover, the statistical properties of the proposed channel model, including path loss, time autocorrelation function (T-ACF) and Doppler power spectrum density (DPSD), have been derived and the impact of several important UAV-related and vehicle-related parameters have been investigated and compared to millimeter wave (mm-wave) band. Furthermore, the correctness of the proposed channel model has been verified via simulation, and some useful observations are provided for the system design of THz UAV-based dual-mobility wireless communication systems. Full article
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<p>Real UAV-based dual-mobility wireless communications scenario in the THz band.</p>
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<p>Different propagation paths between UAV and vehicle in time-varying UAV-based wireless communication system in the THz band: (<b>a</b>) LoS propagation path survival; (<b>b</b>) LoS propagation path death and NLoS propagation path birth.</p>
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<p>The T-ACF with different moving speeds of Tx and Rx for the NLoS path (including reflection and scattering paths).</p>
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<p>The T-ACF with different vertical distance of Tx and Rx for the NLoS path (including reflection and scattering paths).</p>
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<p>The T-ACF with different power ratio of reflection and scattering propagations for the NLoS path (including reflection and scattering paths).</p>
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<p>The T-ACF with different Ricican <span class="html-italic">K</span>-factor.</p>
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<p>Path loss of the MPCs (including LoS, reflection, and scattering paths) with different carrier frequencies.</p>
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<p>The DPSD with different moving times and different paths.</p>
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21 pages, 19359 KiB  
Article
Landslide Hazard Prediction Based on UAV Remote Sensing and Discrete Element Model Simulation—Case from the Zhuangguoyu Landslide in Northern China
by Guangming Li, Yu Zhang, Yuhua Zhang, Zizheng Guo, Yuanbo Liu, Xinyong Zhou, Zhanxu Guo, Wei Guo, Lihang Wan, Liang Duan, Hao Luo and Jun He
Remote Sens. 2024, 16(20), 3887; https://doi.org/10.3390/rs16203887 - 19 Oct 2024
Viewed by 838
Abstract
Rainfall-triggered landslides generally pose a high risk due to their sudden initiation, massive impact force, and energy. It is, therefore, necessary to perform accurate and timely hazard prediction for these landslides. Most studies have focused on the hazard assessment and verification of landslides [...] Read more.
Rainfall-triggered landslides generally pose a high risk due to their sudden initiation, massive impact force, and energy. It is, therefore, necessary to perform accurate and timely hazard prediction for these landslides. Most studies have focused on the hazard assessment and verification of landslides that have occurred, which were essentially back-analyses rather than predictions. To overcome this drawback, a framework aimed at forecasting landslide hazards by combining UAV remote sensing and numerical simulation was proposed in this study. A slow-moving landslide identified by SBAS-InSAR in Tianjin city of northern China was taken as a case study to clarify its application. A UAV with laser scanning techniques was utilized to obtain high-resolution topography data. Then, extreme rainfall with a given return period was determined based on the Gumbel distribution. The Particle Flow Code (PFC), a discrete element model, was also applied to simulate the runout process after slope failure under rainfall and earthquake scenarios. The results showed that the extreme rainfall for three continuous days in the study area was 151.5 mm (P = 5%), 184.6 mm (P = 2%), and 209.3 mm (P = 1%), respectively. Both extreme rainfall and earthquake scenarios could induce slope failure, and the failure probabilities revealed by a seepage–mechanic interaction simulation in Geostudio reached 82.9% (earthquake scenario) and 92.5% (extreme rainfall). The landslide hazard under a given scenario was assessed by kinetic indicators during the PFC simulation. The landslide runout analysis indicated that the landslide had a velocity of max 23.4 m/s under rainfall scenarios, whereas this reached 19.8 m/s under earthquake scenarios. In addition, a comparison regarding particle displacement also showed that the landslide hazard under rainfall scenarios was worse than that under earthquake scenarios. The modeling strategy incorporated spatial and temporal probabilities and runout hazard analyses, even though landslide hazard mapping was not actually achieved. The present framework can predict the areas threatened by landslides under specific scenarios, and holds substantial scientific reference value for effective landslide prevention and control strategies. Full article
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<p>(<b>a</b>) Location of the study area in China, (<b>b</b>) the topographic information of the area, where 30 m resolution DEM is the base map, and (<b>c</b>) the lithology map.</p>
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<p>The cross-section of the ZhuangGuoYu landslide.</p>
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<p>The macro deformation of the ZGYL: (<b>a</b>) an overview of the landslide from Google Earth images and (<b>b</b>) the small-scale landsliding and the protective net at the toe of the slope.</p>
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<p>The deformation results from SBAS-InSAR analysis: (<b>a</b>) spatial deformation of the pixels on the landslide and (<b>b</b>) the displacement of points between 2014 and 2023, where the locations of P1, P2, and P3 are shown in (<b>a</b>).</p>
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<p>The proposed methodological framework of this study for landslide hazard assessment.</p>
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<p>The route setting of the UAV and obtained results: (<b>a</b>,<b>b</b>) are the two overlapping UAV routes, (<b>c</b>) the obtained DSM data from the remote sensing images, and (<b>d</b>) the digital orthophoto map (DOM) of the landslide.</p>
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<p>The dataset for the extreme rainfall analysis: (<b>a</b>) annual rainfall of the study area from 1980 to 2017 and (<b>b</b>) the largest continuous 3-day rainfall for each month.</p>
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<p>The settings for the stability evaluation in Geostudio: (<b>a</b>) the established geological model and (<b>b</b>) the hydrological parameter settings.</p>
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<p>The geological models of the ZGYL in PFC: (<b>a</b>) 2D and (<b>b</b>) 3D.</p>
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<p>The extreme rainfall under various return periods of the study area.</p>
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<p>The stability analysis results from Geostudio v2024. The left column is the factor of safety under (<b>a</b>) the rainfall with 50-year return period, (<b>b</b>) rainfall with 100-year return period, (<b>c</b>) earthquake scenario; The right column is the displacement under (<b>d</b>) the rainfall with 50-year return period, (<b>e</b>) rainfall with 100-year return period, (<b>f</b>) earthquake scenario.</p>
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<p>The 2D landslide kinetics at different moments under the rainfall scenario with 100-year return period.</p>
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<p>The landslide kinetics at different moments under the earthquake scenario.</p>
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<p>The 3D landslide kinetics at different moments: (<b>a</b>) rainfall scenario with 50-year return period, (<b>b</b>) rainfall scenario with 100-year return period, and (<b>c</b>) earthquake scenario.</p>
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<p>The velocity versus time of four monitoring particles: (<b>a</b>) #1, (<b>b</b>) #2, (<b>c</b>) #3, and (<b>d</b>) #4.</p>
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<p>The velocity versus time of four monitoring particles: (<b>a</b>) #1, (<b>b</b>) #2, (<b>c</b>) #3, and (<b>d</b>) #4.</p>
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<p>The displacement versus time of four monitoring particles: (<b>a</b>) #1, (<b>b</b>) #2, (<b>c</b>) #3, and (<b>d</b>) #4.</p>
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29 pages, 6771 KiB  
Article
Water Use Efficiency in Rice Under Alternative Wetting and Drying Technique Using Energy Balance Model with UAV Information and AquaCrop in Lambayeque, Peru
by Lia Ramos-Fernández, Roxana Peña-Amaro, José Huanuqueño-Murillo, David Quispe-Tito, Mayra Maldonado-Huarhuachi, Elizabeth Heros-Aguilar, Lisveth Flores del Pino, Edwin Pino-Vargas, Javier Quille-Mamani and Alfonso Torres-Rua
Remote Sens. 2024, 16(20), 3882; https://doi.org/10.3390/rs16203882 - 18 Oct 2024
Viewed by 766
Abstract
In the context of global warming, rising air temperatures are increasing evapotranspiration (ETc) in all agricultural crops, including rice, a staple food worldwide. Simultaneously, the occurrence of droughts is reducing water availability, affecting traditional irrigation methods for rice cultivation (flood [...] Read more.
In the context of global warming, rising air temperatures are increasing evapotranspiration (ETc) in all agricultural crops, including rice, a staple food worldwide. Simultaneously, the occurrence of droughts is reducing water availability, affecting traditional irrigation methods for rice cultivation (flood irrigation). The objective of this study was to determine ETc (water use) and yield performance in rice crop under different irrigation regimes: treatments with continuous flood irrigation (CF) and irrigations with alternating wetting and drying (AWD5, AWD10, and AWD20) in an experimental area in INIA–Vista Florida. Water balance, rice physiological data, and yield were measured in the field, and local weather data and thermal and multispectral images were collected with a meteorological station and a UAV (a total of 13 flights). ETc values obtained by applying the METRICTM (Mapping Evapotranspiration at High Resolution using Internalized Calibration) energy balance model ranged from 2.4 to 8.9 mm d−1 for the AWD and CF irrigation regimes. In addition, ETc was estimated by a water balance using the AquaCrop model, previously parameterized with RGB image data and field weather data, soil, irrigation water, and crops, obtaining values between 4.3 and 7.1 mm d−1 for the AWD and CF irrigation regimes. The results indicated that AWD irrigation allows for water savings of 27 to 28%, although it entails a yield reduction of from 2 to 15%, which translates into an increase in water use efficiency (WUE) of from 18 to 36%, allowing for optimizing water use and improving irrigation management. Full article
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<p>Flow diagram of the methodology followed in this study.</p>
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<p>Study area: (<b>a</b>) geographical location; (<b>b</b>) Lambayeque region; (<b>c</b>) Experimental Agricultural Station (EEA) “Vista Florida” with four plots of <math display="inline"><semantics> <mrow> <mrow> <mn>24</mn> <mo> </mo> <mo>×</mo> <mo> </mo> <mn>11</mn> <mo> </mo> <mi mathvariant="normal">m</mi> </mrow> </mrow> </semantics></math> each, divided into three subplots of <math display="inline"><semantics> <mrow> <mrow> <mn>8</mn> <mo> </mo> <mo>×</mo> <mo> </mo> <mn>11</mn> </mrow> </mrow> </semantics></math> m, with two irrigation regimes of continuous flooding (CF) and alternating wetting and drying (AWD), the latter having water levels at 5 cm, 10 cm, and 20 cm below the soil surface level (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> <mo>,</mo> <mo> </mo> <msub> <mrow> <mrow> <mo> </mo> <mi>AWD</mi> </mrow> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>).</p>
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<p>Flow chart for the calculation of evapotranspiration.</p>
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<p>Tukey’s HSD test: comparisons of treatments with CF.</p>
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<p>Graphical summary with the irrigation techniques used: CF and AWD, the latter with water levels at a depth of 5 cm, 10 cm, and 20 cm below the soil surface level (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> <mo>,</mo> <msub> <mrow> <mrow> <mo> </mo> <mi>AWD</mi> </mrow> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>), and equipment used in the field data collection.</p>
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<p>Relationship between the NDVI measured with the GreenSeeker and the LAI estimated by the extractive method, both carried out in the field. Days post sowing (DPS) are indicated.</p>
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<p>Hourly variation in reference evapotranspiration (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi mathvariant="normal">E</mi> <mi mathvariant="normal">T</mi> </mrow> <mrow> <mn>0</mn> </mrow> </msub> </mrow> </semantics></math>) according to vegetative stage (<b>a</b>), reproductive stage, and crop maturity (<b>b</b>) according to the 13 flight dates.</p>
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<p>Meteorological conditions according to UAV flights: (<b>a</b>) temperature (T, °C), (<b>b</b>) relative humidity (RH, %), (<b>c</b>) wind speed (WS, <math display="inline"><semantics> <mrow> <mrow> <mi mathvariant="normal">m</mi> <mo> </mo> </mrow> <msup> <mrow> <mi mathvariant="normal">s</mi> </mrow> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </mrow> </semantics></math>), and (<b>d</b>) solar radiation (SR, <math display="inline"><semantics> <mrow> <mrow> <mi mathvariant="normal">W</mi> <mo> </mo> </mrow> <msup> <mrow> <mi mathvariant="normal">m</mi> </mrow> <mrow> <mo>−</mo> <mn>2</mn> </mrow> </msup> </mrow> </semantics></math>).</p>
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<p>Energy balance components and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi mathvariant="normal">E</mi> <mi mathvariant="normal">T</mi> </mrow> <mrow> <mi mathvariant="normal">C</mi> </mrow> </msub> <mo>:</mo> </mrow> </semantics></math> with CF (<b>a</b>,<b>e</b>,<b>i</b>,<b>m</b>,<b>q</b>), <math display="inline"><semantics> <mrow> <msub> <mrow> <mi mathvariant="normal">A</mi> <mi mathvariant="normal">W</mi> <mi mathvariant="normal">D</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> </mrow> </semantics></math> (<b>b</b>,<b>f</b>,<b>j</b>,<b>n</b>,<b>r</b>), <math display="inline"><semantics> <mrow> <msub> <mrow> <mi mathvariant="normal">A</mi> <mi mathvariant="normal">W</mi> <mi mathvariant="normal">D</mi> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math> (<b>c</b>,<b>g</b>,<b>k</b>,<b>o</b>,<b>s</b>), and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math> (<b>d</b>,<b>h</b>,<b>l</b>,<b>p</b>,<b>t</b>), with water level depths at 5 cm, 10 cm, and 20 cm below the soil surface.</p>
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<p>Spatial variation in <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>ET</mi> </mrow> <mrow> <mi mathvariant="normal">c</mi> </mrow> </msub> </mrow> </semantics></math> in vegetative (38 to 92 DPS), reproductive (103 to 127 DPS), and ripening (147 and 149 DPS) phases of the rice crop.</p>
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<p>Relationship between simulated vs. measured canopy cover (CC%) under irrigation management conditions and AWD, the latter with water levels below the soil surface of 5 cm, 10 cm, and 20 cm (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> <mo>,</mo> <msub> <mrow> <mrow> <mo> </mo> <mi>AWD</mi> </mrow> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>).</p>
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<p>Water balance components according to previously calibrated AquaCrop model: (<b>a</b>) total values during crop development according to CF and AWD irrigation management. Monthly values according to irrigation management for (<b>b</b>) CF, (<b>c</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and (<b>e</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Water balance components according to previously calibrated AquaCrop model: (<b>a</b>) total values during crop development according to CF and AWD irrigation management. Monthly values according to irrigation management for (<b>b</b>) CF, (<b>c</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and (<b>e</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Evapotranspiration from AquaCrop water balance model according to CF and AWD irrigation management.</p>
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<p>Relationship between energy balance (METRIC model) and water balance (AquaCrop model) under CF and AWD irrigation management.</p>
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<p>(<b>a</b>) Cumulative irrigation applied days post-sowing (DPS) (<math display="inline"><semantics> <mrow> <msup> <mrow> <mi mathvariant="normal">m</mi> </mrow> <mrow> <mn>3</mn> </mrow> </msup> <mo> </mo> <msup> <mrow> <mi>ha</mi> </mrow> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </mrow> </semantics></math>) throughout the growing season, and (<b>b</b>) Irrigation amounts (<math display="inline"><semantics> <mrow> <msup> <mrow> <mi mathvariant="normal">m</mi> </mrow> <mrow> <mn>3</mn> </mrow> </msup> <mo> </mo> <msup> <mrow> <mi>ha</mi> </mrow> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </mrow> </semantics></math>) measured under different irrigation treatments: CF, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> <mrow> <mo>,</mo> <mo> </mo> </mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>).</p>
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<p>Temporal variation in evapotranspiration obtained with the previously calibrated AquaCrop model under CF and AWD irrigation management.</p>
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<p>Yield comparison between field measurements and AquaCrop simulations for CF, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math> treatments.</p>
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<p>Comparison of field yield and cumulative irrigation under different irrigation treatments (CF, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>5</mn> </mrow> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>10</mn> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>AWD</mi> </mrow> <mrow> <mn>20</mn> </mrow> </msub> </mrow> </semantics></math>).</p>
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21 pages, 6250 KiB  
Article
Recognition of Urbanized Areas in UAV-Derived Very-High-Resolution Visible-Light Imagery
by Edyta Puniach, Wojciech Gruszczyński, Paweł Ćwiąkała, Katarzyna Strząbała and Elżbieta Pastucha
Remote Sens. 2024, 16(18), 3444; https://doi.org/10.3390/rs16183444 - 17 Sep 2024
Viewed by 677
Abstract
This study compared classifiers that differentiate between urbanized and non-urbanized areas based on unmanned aerial vehicle (UAV)-acquired RGB imagery. The tested solutions included numerous vegetation indices (VIs) thresholding and neural networks (NNs). The analysis was conducted for two study areas for which surveys [...] Read more.
This study compared classifiers that differentiate between urbanized and non-urbanized areas based on unmanned aerial vehicle (UAV)-acquired RGB imagery. The tested solutions included numerous vegetation indices (VIs) thresholding and neural networks (NNs). The analysis was conducted for two study areas for which surveys were carried out using different UAVs and cameras. The ground sampling distances for the study areas were 10 mm and 15 mm, respectively. Reference classification was performed manually, obtaining approximately 24 million classified pixels for the first area and approximately 3.8 million for the second. This research study included an analysis of the impact of the season on the threshold values for the tested VIs and the impact of image patch size provided as inputs for the NNs on classification accuracy. The results of the conducted research study indicate a higher classification accuracy using NNs (about 96%) compared with the best of the tested VIs, i.e., Excess Blue (about 87%). Due to the highly imbalanced nature of the used datasets (non-urbanized areas constitute approximately 87% of the total datasets), the Matthews correlation coefficient was also used to assess the correctness of the classification. The analysis based on statistical measures was supplemented with a qualitative assessment of the classification results, which allowed the identification of the most important sources of differences in classification between VIs thresholding and NNs. Full article
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Figure 1
<p>Jerzmanowice dataset: (<b>a</b>) the area covered by UAV photogrammetry missions with the locations of ground control points (GCPs) and check points (CPs) and the boundary of the study area; (<b>b</b>) the study area with the sample area locations.</p>
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<p>Wieliczka dataset: (<b>a</b>) the area covered by UAV photogrammetry missions with the locations of GCPs and CPs and the boundary of the study area; (<b>b</b>) the study area with the sample area locations.</p>
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<p>Workflow for VI threshold (<b>a</b>) calibration, and (<b>b</b>) validation and testing. The optimal threshold value was determined using the JERZ dataset (<b>a</b>), which employed orthomosaics and manually performed reference classification. Subsequently (<b>b</b>), the assessment of classification accuracy was tested for both the calibration (JERZ) and the WIEL datasets, utilizing the optimal threshold value determined in step (<b>a</b>). This ensured that the accuracies determined for the WIEL dataset were independent and unbiased.</p>
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<p>Workflow for NN (<b>a</b>) training, and (<b>b</b>) validation and testing. The training was conducted using the JERZ dataset (<b>a</b>), which employed orthomosaics and manually performed reference classification. Subsequently (<b>b</b>), classification accuracy assessment was tested for both the validation part of the JERZ dataset and the WIEL dataset. This ensured that the accuracies determined for the WIEL dataset were independent and unbiased.</p>
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<p>Dendrogram of associations between VIs obtained for 1 − |<span class="html-italic">r</span>| metric and UPGMA method using the JERZ dataset. Taking into account the 0.1 distance criterium, six clusters were identified, i.e., (1) ExG, CIVE, GLI, ExGR, AL (in red); (2) GBdiff, ExB, ExGB, RGBVI (in green); (3) ExR, NGRDI, MGRVI (in blue); (4) MExG; (5) TGI, AI (in violet); and (6) AB.</p>
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<p>Histograms of VIs with optimal thresholds for the JERZ dataset. This figure also shows the percentage of pixels classified as urbanized and non-urbanized areas.</p>
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<p>The variability in the optimal threshold depending on the survey date, with the horizontal axes displaying dates in the year.month format.</p>
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<p>The influence of the adopted threshold value on MCC and <span class="html-italic">accuracy</span>.</p>
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<p>Examples of classification results for dark orthomosaic fragments: (<b>a</b>) for roof, and (<b>b</b>) for trees. The figure shows a fragment of an orthomosaic, reference classification, classification predicted by ExB and NNs (linear, MLP, and CNN), and classification errors. In the classification images, pixels classified as urbanized areas are red, and pixels classified as non-urbanized areas are green. In the error images, blue indicates correctly classified pixels, and yellow indicates misclassified pixels.</p>
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