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Drones, Volume 7, Issue 1 (January 2023) – 64 articles

Cover Story (view full-size image): The use of autonomous drones and particularly beyond visual line-of-sight (BVLOS) flying has increased in recent years. This is offering new possibilities to develop efficient drone-based applications. Due to possible disruptions in GNSS positioning, redundant positioning systems are required to ensure reliable operation. In this study, a new visual–inertial sensor suite was developed to enable visual–inertial odometry (VIO)-based positioning at high flying altitudes. Empirical testing of the system was carried out at flying altitudes of 40–100 m. Results showed that the proposed VIO-based positioning system could be used as a redundant system for high flying altitude operations. The data collected for the study are openly shared to enable further research and development. View this paper
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21 pages, 1888 KiB  
Article
Proposals of Processes and Organizational Preventive Measures against Malfunctioning of Drones and User Negligence
by Mircea Constantin Șcheau, Monica Violeta Achim, Larisa Găbudeanu, Viorela Ligia Văidean, Alexandru Lucian Vîlcea and Liliana Apetri
Drones 2023, 7(1), 64; https://doi.org/10.3390/drones7010064 - 16 Jan 2023
Cited by 10 | Viewed by 2944
Abstract
Drones have been included in more and more activities in various domains, such as military, commercial and personal use. The existing legislative framework insufficiently addresses the responsibility and preventive measures angles in case of vulnerability exploitation and negligence in drone usage. Such aspects [...] Read more.
Drones have been included in more and more activities in various domains, such as military, commercial and personal use. The existing legislative framework insufficiently addresses the responsibility and preventive measures angles in case of vulnerability exploitation and negligence in drone usage. Such aspects can be addressed by the industry in technological processes and standardization. These are especially important aspects given the high impact that misuse of drones can have on individuals, property and buildings within the flight zone when the drone is misused. The aim of this research paper is to investigate how these elements are viewed in existing legislation and by individuals, while taking into account the technical specifics and the stakeholder ecosystem of drone usage. In this respect, we use a complex questionnaire which was sent to a final number of 233 respondents pertaining to firms specialized in IT, legal and cybersecurity. The responses have been analyzed from a qualitative and quantitative perspective. Our results highlight the areas of improvement in the existing standardization and find the followings: (1) stakeholders across the drone ecosystem are viewed as having a shared liability in certain use cases, (2) preventive measure implementation should be dispersed across the stakeholders of drone usage and (3) automation of prevention measures is considered more useful in case of malfunctioning or misuse of drones rather than user manual intervention. In addition, we make proposals to accommodate new policy requirements for the above use cases. The results of this research paper assist policy makers in improving existing standardization framework and technological processes concerning drone usage, but also stakeholders of the drone ecosystem in generating increased trust of the drone users. Further, this research paper can also assist drone software and hardware producers in calibrating their products to ensure trust of the users. In addition, trust in the use of drones for commercial and personal purposes is increased through standardization and proper approaches for situations that may cause damages to drones and to third parties. Full article
(This article belongs to the Special Issue Drones: Opportunities and Challenges)
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<p>Map of articles relevant for the keywords using the Web of Science database.</p>
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<p>Distribution of respondents from a geographical perspective (blue represents the countries of the responders). Source: QuestionPro; analytics derived from the questionnaire and provided by the authors.</p>
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<p>Question responses—responsible for damages. Source: Author’s processing.</p>
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<p>Question responses—malfunctioning of hardware components. Source: Author’s processing.</p>
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<p>Question—liability in case of outset vulnerabilities. Source: Author’s processing.</p>
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20 pages, 294 KiB  
Article
Reconciling Registration Policies for Unmanned Aircraft with Unmanned Aircraft Ownership Characteristics
by Isaac Levi Henderson
Drones 2023, 7(1), 63; https://doi.org/10.3390/drones7010063 - 16 Jan 2023
Cited by 2 | Viewed by 2127
Abstract
Registration of unmanned aircraft is a common policy around the world and forms part of the International Civil Aviation Organisation’s model regulations for unmanned aircraft. This study conducts a review of the various registration policies that have been implemented amongst advanced economies to [...] Read more.
Registration of unmanned aircraft is a common policy around the world and forms part of the International Civil Aviation Organisation’s model regulations for unmanned aircraft. This study conducts a review of the various registration policies that have been implemented amongst advanced economies to find commonalities and differences. New Zealand is then used as a case study. The country does not currently have registration of unmanned aircraft; however, their Ministry of Transport has put forward the idea of implementing a registration scheme. As part of this case study, the ownership characteristics of 919 New Zealand unmanned aircraft users were collected using an online survey. The results highlight that personally owned aircraft tend to only be used by their owner, with the number of users being lower than the number of aircraft. For organisationally owned aircraft, there are multiple users per aircraft; however, these users tend to only be employees of the organisation. These findings suggest that for New Zealand, the best way to implement a registration scheme would be to register users and organisations rather than individual aircraft. While specific to New Zealand, these findings also prompt the need for future research worldwide to see whether registration schemes reconcile with ownership data. Full article
45 pages, 6835 KiB  
Review
UAV Formation Trajectory Planning Algorithms: A Review
by Yunhong Yang, Xingzhong Xiong and Yuehao Yan
Drones 2023, 7(1), 62; https://doi.org/10.3390/drones7010062 - 16 Jan 2023
Cited by 62 | Viewed by 23365
Abstract
With the continuous development of UAV technology and swarm intelligence technology, the UAV formation cooperative mission has attracted wide attention because of its remarkable function and flexibility to complete complex and changeable tasks, such as search and rescue, resource exploration, reconnaissance and surveillance. [...] Read more.
With the continuous development of UAV technology and swarm intelligence technology, the UAV formation cooperative mission has attracted wide attention because of its remarkable function and flexibility to complete complex and changeable tasks, such as search and rescue, resource exploration, reconnaissance and surveillance. The collaborative trajectory planning of UAV formation is a key part of the task execution. This paper attempts to provide a comprehensive review of UAV formation trajectory planning algorithms. Firstly, from the perspective of global planning and local planning, a simple framework of the UAV formation trajectory planning algorithm is proposed, which is the basis of comprehensive classification of different types of algorithms. According to the proposed framework, a classification method of existing UAV formation trajectory planning algorithms is proposed, and then, different types of algorithms are described and analyzed statistically. Finally, the challenges and future research directions of the UAV formation trajectory planning algorithm are summarized and prospected according to the actual requirements. It provides reference information for researchers and workers engaged in the formation flight of UAVs. Full article
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<p>Statistics and forecast of global UAV market size from 2015 to 2024 (data source: Drone II): (<b>a</b>) Global UAV market 2015–2024 (blue column: global UAV investment; yellow line: upward trend); (<b>b</b>) Global UAV segment market share (blue column: proportion of consumer drones; yellow column: proportion of industrial drones).</p>
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<p>Unmanned aerial vehicles fly in formation to perform tasks. (<b>a</b>) UAV formation flight; (<b>b</b>) UAV formation electronic warfare; (<b>c</b>) Unmanned aerial vehicle (UAV) formation performs mission; (<b>d</b>) UAV formation communication relay; (<b>e</b>) UAV formation strikes target; (<b>f</b>) UAV formation reconnaissance.</p>
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<p>Framework diagram of global trajectory planning algorithm.</p>
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<p>Frame diagram of local trajectory planning algorithm.</p>
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<p>A cost diagram of a Dijkstra algorithm (A–G: nodes; lines: trajectories; numbers: the distance between vertices).</p>
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<p>An LRL trajectory diagram of Dubins curve (black circle: circle curvature; yellow lines: the connecting line between the centers of trajectories; blue line: initial flight direction; green line: final flight direction; pt1–pt2: intersection point between curvatures; C1–C3: curvature name).</p>
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<p>Optical path function solution model diagram (Δ<span class="html-italic">x</span> and Δ<span class="html-italic">y</span>: spacing in <span class="html-italic">x</span> and <span class="html-italic">y</span> directions on discrete space).</p>
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<p>A Voronoi diagram method of trajectory diagram (blue area: obstacles; yellow lines: feasible trajectories).</p>
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<p>A PRM trajectory map (color areas: obstacles; black lines: feasible trajectories; red line: optimal trajectory).</p>
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<p>A RRT trajectory diagram (black areas: obstacles; pink lines: feasible trajectories; blue line: optimal trajectory; green: starting point; red: end point).</p>
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<p>Trajectory diagram of a simulated annealing algorithm (dots: nodes; lines: trajectories; numbers: the distance between vertices).</p>
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<p>Trajectory diagram of A* algorithm (dots: nodes; lines: trajectories; black areas: obstacles; green dotted line: optimized trajectory).</p>
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<p>A cross-variation operation diagram and EA trajectory diagram. (<b>a</b>) A cross-mutation operation diagram; (<b>b</b>) An Evolutionary Algorithm (EA) trajectory diagram (red circles: obstacles; blue line: optimal trajectory).</p>
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<p>A particle motion diagram.</p>
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<p>A PIO map and compass operator model and PIO trajectory map. (<b>a</b>) A PIO map compass operator model (arrows: the direction of attraction); (<b>b</b>) A Pigeon-Inspired Optimization (PIO) trajectory diagram (diamonds: starting points; Pentagrams: the end points; black areas: obstacles).</p>
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<p>An iterative evolution search diagram and FOA trajectory diagram. (<b>a</b>) An iterative evolution search diagram; (<b>b</b>) An FOA trajectory diagram (circles: nodes; lines: trajectory; numbers: the distance between vertices).</p>
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<p>A kind of ABC trajectory diagram (Black areas: obstacles; blue line: optimal trajectory).</p>
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<p>A SSA trajectory diagram (circles: obstacles).</p>
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<p>An ACO trajectory diagram (“cell” is the map block after rasterizing the map, “number” is the number of the map block, and the black part represents obstacles.).</p>
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<p>A position update model and GWO trajectory map. (<b>a</b>) A location updating model of the Gray Wolf Optimization algorithm; (<b>b</b>) Trajectory diagram of a Gray Wolf Optimization algorithm (black areas: obstacles; blue line: optimal trajectory).</p>
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<p>A kind of HS trajectory diagram (colored areas: obstacles).</p>
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<p>A neural network model (connection: different combinations).</p>
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<p>A reinforcement learning model.</p>
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<p>A Deep Reinforcement Learning Model.</p>
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<p>Schematic diagram of artificial potential field.</p>
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<p>DWA velocity vector space diagram.</p>
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<p>A mathematical optimization algorithm model.</p>
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<p>Schematic diagram of Model Predictive Control.</p>
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25 pages, 17884 KiB  
Article
The Effects of Spatial Resolution and Resampling on the Classification Accuracy of Wetland Vegetation Species and Ground Objects: A Study Based on High Spatial Resolution UAV Images
by Jianjun Chen, Zizhen Chen, Renjie Huang, Haotian You, Xiaowen Han, Tao Yue and Guoqing Zhou
Drones 2023, 7(1), 61; https://doi.org/10.3390/drones7010061 - 15 Jan 2023
Cited by 30 | Viewed by 4570
Abstract
When employing remote sensing images, it is challenging to classify vegetation species and ground objects due to the abundance of wetland vegetation species and the high fragmentation of ground objects. Remote sensing images are classified primarily according to their spatial resolution, which significantly [...] Read more.
When employing remote sensing images, it is challenging to classify vegetation species and ground objects due to the abundance of wetland vegetation species and the high fragmentation of ground objects. Remote sensing images are classified primarily according to their spatial resolution, which significantly impacts the classification accuracy of vegetation species and ground objects. However, there are still some areas for improvement in the study of the effects of spatial resolution and resampling on the classification results. The study area in this paper was the core zone of the Huixian Karst National Wetland Park in Guilin, Guangxi, China. The aerial images (Am) with different spatial resolutions were obtained by utilizing the UAV platform, and resampled images (An) with different spatial resolutions were obtained by utilizing the pixel aggregation method. In order to evaluate the impact of spatial resolutions and resampling on the classification accuracy, the Am and the An were utilized for the classification of vegetation species and ground objects based on the geographic object-based image analysis (GEOBIA) method in addition to various machine learning classifiers. The results showed that: (1) In multi-scale images, both the optimal scale parameter (SP) and the processing time decreased as the spatial resolution diminished in the multi-resolution segmentation process. At the same spatial resolution, the SP of the An was greater than that of the Am. (2) In the case of the Am and the An, the appropriate feature variables were different, and the spectral and texture features in the An were more significant than those in the Am. (3) The classification results of various classifiers in the case of the Am and the An exhibited similar trends for spatial resolutions ranging from 1.2 to 5.9 cm, where the overall classification accuracy increased and then decreased in accordance with the decrease in spatial resolution. Moreover, the classification accuracy of the Am was higher than that of the An. (4) When vegetation species and ground objects were classified at different spatial scales, the classification accuracy differed between the Am and the An. Full article
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<p>Overview of the study area.</p>
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<p>Ground truth reference image.</p>
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<p>Technical route of this study.</p>
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<p>Spatial distribution of training samples.</p>
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<p>The change in separability between the number of features and classes (1.2 cm spatial resolution image), and the blue diamond (indicating value 2.949) was the maximum separation distance.</p>
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<p>Results of ESP2 scale analysis (1.2 cm spatial resolution image).</p>
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<p>Segmentation results of vegetation species and ground objects (1.2 cm spatial resolution image).</p>
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<p>The variation trend of the optimal SP and segmentation time in the Am and the An.</p>
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<p>Evaluation results of the importance of each feature in the Am.</p>
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<p>Evaluation results of the importance of each feature in the An.</p>
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<p>The Am classification results under RF classifier; the UAV-RGB image and ground truth reference image of the study area are shown in <a href="#drones-07-00061-f001" class="html-fig">Figure 1</a> and <a href="#drones-07-00061-f002" class="html-fig">Figure 2</a>, respectively.</p>
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<p>Identification accuracy of vegetation species and ground objects in the Am.</p>
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<p>The An classification results under RF classifier; the UAV-RGB image and ground truth reference image in the study area are shown in <a href="#drones-07-00061-f001" class="html-fig">Figure 1</a> and <a href="#drones-07-00061-f002" class="html-fig">Figure 2</a>, respectively.</p>
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<p>Identification accuracy of vegetation species and ground objects in the An results.</p>
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14 pages, 3911 KiB  
Article
A Novel Gripper Prototype for Helical Bird Diverter Manipulation
by Jonathan Cacace, Lorenzo Giampetraglia, Fabio Ruggiero and Vincenzo Lippiello
Drones 2023, 7(1), 60; https://doi.org/10.3390/drones7010060 - 15 Jan 2023
Cited by 5 | Viewed by 2858
Abstract
Energy grids represent a fundamental infrastructure of any country. These structures consist of many kilometres of power lines that must be periodically inspected and maintained. Among the necessary operations are installing and removing bird diverters to reduce bird strikes on power lines. These [...] Read more.
Energy grids represent a fundamental infrastructure of any country. These structures consist of many kilometres of power lines that must be periodically inspected and maintained. Among the necessary operations are installing and removing bird diverters to reduce bird strikes on power lines. These devices are intended to improve birds’ detection of power lines and reduce the risk of collision. Often, the installation and removal of bird diverters from power lines is accomplished by humans operating from helicopters or directly on the power lines. Apart from the considerable cost of these operations, working in elevated environments creates human safety risks. To reduce these risks, this paper proposes a novel solution to automatize these tasks. The proposed solution is a prototype gripper that can be mounted on unmanned aerial vehicles (UAVs) and remotely operated to install or remove bird diverters. This work presents a mechatronic device and software architecture system that is experimentally evaluated in a laboratory mock-up, which consists of a manipulator equipped with the proposed tool for removing a bird diverter. Future work is needed to deploy the proposed tool on a UAV. Full article
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<p>Different bird diverters installed on power lines.</p>
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<p>Installation process bird flight diverter. From (<b>a</b>) to (<b>c</b>), the insertion of the divert and its rotation around the power cable to lock it.</p>
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<p>Bird diverter removal device.</p>
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<p><b>Left</b>: external chassis of the device; <b>right</b>: system shafts.</p>
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<p>(<b>Left</b>): internal mechanism; (<b>right</b>): wheeled tooth with internal guillotine system.</p>
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<p>Protrusion.</p>
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<p>The guillotine mechanism acts like pincers to lock the diverter in the final phase of the diverter removal.</p>
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<p>Left: rear cover of the device; right: the internal components of the device.</p>
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<p>System architecture.</p>
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<p>YOLO libraries in the detection of the helical diverter. Top: the raw output of the YOLO algorithm for a red helical diverter. Bottom: the image elaboration algorithm running as the output of the YOLO algorithm. In blue and yellow, possible grasping points.</p>
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<p>Mock-up.</p>
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<p>The different phases from grasping to releasing of the diverter removal process. The full experiment can be seen at the following link <a href="https://youtu.be/-VVHq-wBBWA" target="_blank">https://youtu.be/-VVHq-wBBWA</a>, accessed on 1 January 2023.</p>
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<p>Time series of the position of the end effector during the task. Red: x; green: y; blue: z.</p>
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<p>Time series of the orientation of the end effector during the task. Red: roll; green: pitch; blue: yaw.</p>
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<p>Time series of the estimated force on the end effector during the task. Red: x; green: y; blue: z.</p>
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20 pages, 1312 KiB  
Article
Cooperative Truck–Drone Delivery Path Optimization under Urban Traffic Restriction
by Ying-Ying Weng, Rong-Yu Wu and Yu-Jun Zheng
Drones 2023, 7(1), 59; https://doi.org/10.3390/drones7010059 - 14 Jan 2023
Cited by 12 | Viewed by 4418
Abstract
In the traditional express delivery sector, trucks are the most available and efficient transportation mode in urban areas. However, due to the pressures of traffic congestion and air pollution problems, many cities have implemented strict measures to restrict trucks’ access to many zones [...] Read more.
In the traditional express delivery sector, trucks are the most available and efficient transportation mode in urban areas. However, due to the pressures of traffic congestion and air pollution problems, many cities have implemented strict measures to restrict trucks’ access to many zones during specified time periods, which has caused significant effects on the business of the industry. Due to their advantages, which include high speed, flexibility, and environmental friendliness, drones have great potential for being combined with trucks for efficient delivery in restricted traffic zones. In this paper, we propose a cooperative truck and drone delivery path optimization problem, in which a truck carrying cargo travels along the outer boundary of the restricted traffic zone to send and receive a drone, and the drone is responsible for delivering the cargo to customers. The objective of the problem is to minimize the completion time of all delivery tasks. To efficiently solve this problem, we propose a hybrid metaheuristic optimization algorithm to cooperatively optimize the outer path of the truck and the inner path of the drone. We conduct experiments on a set of test instances; the results demonstrate that the proposed algorithm exhibits a competitive performance compared to other selected popular optimization algorithms. Full article
(This article belongs to the Special Issue Cooperation of Drones and Other Manned/Unmanned Systems)
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<p>Illustration of the cooperative truck–drone delivery.</p>
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<p>An illustration of the intersection of the truck and the drone. Six possible intersection points are drawn; however, the rightmost intersection is not considered, as it exceeds the orthogonal projection of the current customer onto the boundary.</p>
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<p>Flowchart of the hybrid metaheuristic optimization method.</p>
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<p>Box plots of the results of the comparative algorithms on the nine test instances. (<b>a</b>) Ins. 1. (<b>b</b>) Ins. 2. (<b>c</b>) Ins. 3. (<b>d</b>) Ins. 4. (<b>e</b>) Ins. 5. (<b>f</b>) Ins. 6. (<b>g</b>) Ins. 7. (<b>h</b>) Ins. 8. (<b>i</b>) Ins. 9.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 1. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 2. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 3. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 4. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 5. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 6. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 7. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 8. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Resulting drone routes (in dash lines) and truck routes (in solid lines) obtained by the nine algorithms on instance 9. (<b>a</b>) GA. (<b>b</b>) PSO. (<b>c</b>) DE. (<b>d</b>) BBO. (<b>e</b>) EBO. (<b>f</b>) WWO. (<b>g</b>) SimWWO.</p>
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<p>Convergence curves of the comparative algorithms for the test instances. (<b>a</b>) Ins. 1. (<b>b</b>) Ins. 2. (<b>c</b>) Ins. 3. (<b>d</b>) Ins. 4. (<b>e</b>) Ins. 5. (<b>f</b>) Ins. 6. (<b>g</b>) Ins. 7. (<b>h</b>) Ins. 8. (<b>i</b>) Ins. 9.</p>
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16 pages, 2699 KiB  
Article
Distributed Motion Planning for Multiple Quadrotors in Presence of Wind Gusts
by Pramod Abichandani, Deepan Lobo, Meghna Muralidharan, Nathan Runk, William McIntyre, Donald Bucci and Hande Benson
Drones 2023, 7(1), 58; https://doi.org/10.3390/drones7010058 - 13 Jan 2023
Cited by 6 | Viewed by 2847
Abstract
This work demonstrates distributed motion planning for multi-rotor unmanned aerial vehicle in a windy outdoor environment. The motion planning is modeled as a receding horizon mixed integer nonlinear programming (RH-MINLP) problem. Each quadrotor solves an RH-MINLP to generate its time-optimal speed profile along [...] Read more.
This work demonstrates distributed motion planning for multi-rotor unmanned aerial vehicle in a windy outdoor environment. The motion planning is modeled as a receding horizon mixed integer nonlinear programming (RH-MINLP) problem. Each quadrotor solves an RH-MINLP to generate its time-optimal speed profile along a minimum snap spline path while satisfying constraints on kinematics, dynamics, communication connectivity, and collision avoidance. The presence of wind disturbances causes the motion planner to continuously regenerate new motion plans, thereby significantly increasing the computational time and possibly leading to safety violations. Control Barrier Functions (CBFs) are used for assist in collision avoidance in the face of wind disturbances while alleviating the need to recalculate the motion plans continually. The RH-MINLPs are solved using a novel combination of heuristic and optimal methods, namely Simulated Annealing and interior-point methods, respectively, to handle discrete variables and nonlinearities in real-time feasibly. The framework is validated in simulations featuring up to 50 quadrotors and Hardware-in-the-loop (HWIL) experiments, followed by outdoor field tests featuring up to 6 DJI M100 quadrotors. Results demonstrate (1) fast online motion planning for outdoor communication-centric multi-quadrotor operations and (2) the utility of CBFs in providing effective motion plans. Full article
(This article belongs to the Special Issue Multi-UAVs Control)
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<p>Snapshots of quadrotors flying in different flight formations namely straight line (2 quadrotors—top left), rectangle (6 quadrotors—top right), and triangle (3 quadrotors—bottom left). The bottom right image shows an FT-205 wind sensor mounted on the DJI Matrice 100 quadrotor to collect real-time wind data during flight test.</p>
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<p>A multi-quadrotor mission with six quadrotors moving along their spline paths (represented by solid, colored lines) in the presence of wind. Control Barrier Functions (CBFs) and associated safety certificates visualized as super-ellipsoids assisted in collision avoidance in the face of wind disturbances during transit. The vector field (blue arrows) indicates spatially varying wind gusts generated using the Dryden wind model at an altitude of 15 m. Red triangular and square markers indicate the start and endpoints of the spline paths arranged in a geometric formation. Black round markers indicate spline-path waypoints. The inertial reference frame and the body frame (b<math display="inline"><semantics> <msub> <mrow/> <mi>x</mi> </msub> </semantics></math>, b<math display="inline"><semantics> <msub> <mrow/> <mi>y</mi> </msub> </semantics></math>, and b<math display="inline"><semantics> <msub> <mrow/> <mi>z</mi> </msub> </semantics></math>) are shown. The quadrotors are depicted here operating in a 40 m × 40 m × 40 m airspace.</p>
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<p>(<b>Top</b>) In HWIL tests without CBF, the number of actual safety violations is shown in the red bars. As CBFs were not used, none of these actual safey violations could be avoided. (<b>Bottom</b>) In HWIL tests with CBF, the number of CBF-activations <math display="inline"><semantics> <msub> <mi>n</mi> <mi>CBF</mi> </msub> </semantics></math> are shown in the green bars. Each of these CBF activations helped the quadrotors to avoid potential future safety violations. As such, the use of CBFs resulted in zero actual safety violations. Data averaged over nine runs.</p>
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<p>For <math display="inline"><semantics> <msub> <mi>d</mi> <mi>safe</mi> </msub> </semantics></math> = 3 m, the above charts depict <math display="inline"><semantics> <msub> <mi>T</mi> <mi>mission</mi> </msub> </semantics></math> in seconds for different HWIL scenarios. The presence of wind increases the computational times and results in severe safety violations. Adding CBFs to the overall motion planning strategy reduces the overall computational times while resulting in zero safety violations. Data averaged over nine runs.</p>
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24 pages, 6960 KiB  
Article
Effect of Operational Parameters of Unmanned Aerial Vehicle (UAV) on Droplet Deposition in Trellised Pear Orchard
by Peng Qi, Lanting Zhang, Zhichong Wang, Hu Han, Joachim Müller, Tian Li, Changling Wang, Zhan Huang, Miao He, Yajia Liu and Xiongkui He
Drones 2023, 7(1), 57; https://doi.org/10.3390/drones7010057 - 13 Jan 2023
Cited by 15 | Viewed by 3533
Abstract
Background: Unmanned Aerial Vehicles (UAVs) are increasingly being used commercially for crop protection in East Asia as a new type of equipment for pesticide applications, which is receiving more and more attention worldwide. A new model of pear cultivation called the ‘Double Primary [...] Read more.
Background: Unmanned Aerial Vehicles (UAVs) are increasingly being used commercially for crop protection in East Asia as a new type of equipment for pesticide applications, which is receiving more and more attention worldwide. A new model of pear cultivation called the ‘Double Primary Branches Along the Row Flat Type’ standard trellised pear orchards (FT orchard) is widely used in China, Japan, Korea, and other Asian countries because it saves manpower and is suitable for mechanization compared to traditional spindle and open-center cultivation. The disease and pest efficacy of the flat-type trellised canopy structure of this cultivation is a great challenge. Therefore, a UAV spraying trial was conducted in an FT orchard, and a four-factor (SV: Spray application volume rate, FS: Flight speed, FH: Flight height, FD: Flight direction) and 3-level orthogonal test were designed. Results: These data were used to analyze the effect, including spray coverage, deposit density, coefficient of variation, and penetration coefficient on the canopy, to determine the optimal operating parameters of the UAV for pest efficacy in FT orchards. The analysis of extremes of variance showed that factor FD had a significant effect on both spray coverage and deposition density. Followed by factor FS, which had a greater effect on spray coverage (p < 0.05), and factor SV, FH, which had a greater effect on deposition density (p < 0.05). The effects of different factors on spray coverage and deposit density were FD > FS > FH > SV, FD > FH > SV > FS, in that order. The SV3-FS1-FH1-FD3, which flight along the row with an application rate of 90 L/ha, a flight speed of 1.5 m/s, and a flight height of 4.5 m, was the optimal combination, which produced the highest deposit density and spray coverage. It was determined through univariate analysis of all experimental groups, using droplet density of 25/cm2 and spray coverage of 1%, and uniformity of 40% as the measurement index, that T4 and T8 performed the best and could meet the control requirements in different horizontal and vertical directions of the pear canopy. The parameters were as follows: flight along the tree rows, application rate not less than 75 L/ha, flight speed no more than 2 m/s, and flight height not higher than 5 m. Conclusion: This article provides ample data to promote innovation in the use of UAVs for crop protection programs in pergola/vertical trellis system orchards such as FT orchards. At the same time, this project provided a comprehensive analysis of canopy deposition methods and associated recommendations for UAV development and applications. Full article
(This article belongs to the Section Drones in Agriculture and Forestry)
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<p>Experimental location in Hubei and Shanxi Province. (<b>A</b>) represents the test site at Shanxi Province Agricultural Academy Fruit Tree Institute, and (<b>B</b>) represents the test site at Hubei Province Agricultural Academy Fruit Tree Institute.</p>
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<p>FT orchard tree shape results from the distribution of branch groups. (<b>A</b>) represents the front view and the distribution of the main branch structures. (<b>B</b>) represents the top view, which mainly shows various branch growth structures, where 0 represents the main stem, 1 represents the main branch, 2 represents the main branch extension, 3 represents the group of branches growing fruit, 4 represents the group of F branches growing fruits, 5 represents the fixed connection point with the bracket, 6 represents funnel-shaped space.</p>
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<p>DJI T20 series plant protection UAV. (1) represents the propeller, which provides lift, (2) represents the nozzle, the droplet atomization device, (3) represents omnidirectional radar, which senses obstacles, (4) represents D-RTK, which is used for localization, (5) represents tank, which is used to hold the pesticide solution.</p>
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<p>Sampling locations for assessing spray deposition. (<b>A</b>) represents the structural characteristics of the <b>FT orchard</b> cultivation, (<b>B</b>) represents sampling locations in the target pear tree canopy and ground, and (<b>C</b>) represents <b>a</b> schematic diagram of site layout and flight patterns in <b>FT orchard</b> tests.</p>
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<p>Deposition characteristics of droplet density (DD) in the canopy. Numbers in the chart are mean values, and different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05.</p>
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<p>Deposition characteristics of spray coverage (SC) in the canopy. Numbers in the chart are mean values, and different lowercase letters indicate significant differences at <span class="html-italic">p ≤</span> 0.05.</p>
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<p>Deposition characteristics of DV50 in the canopy. Numbers in the chart are mean values, and different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05.</p>
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<p>DD characteristics on both sides of the leaves. T1 to T9 represent different test groups. Numbers in the chart are mean values, and different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05.</p>
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<p>SC characteristics on both sides of the leaves. T1 to T9 represent different test groups. Numbers in the chart are mean values, and different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05.</p>
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<p>Deposition characteristics of DD in the horizontal of the canopy. F represents the front of the pear tree canopy, B represents the back, L represents the left, R represents the right, and C represents the middle of the canopy. Different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05. The box plot represents DD, and the dashed line represents CV.</p>
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<p>Deposition characteristics of SC in the horizontal direction of the canopy. F represents the front of the pear tree canopy, B represents the back, L represents the left, R represents the right, and C represents the middle of the canopy. Different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05. The box plot represents DD, and the dashed line represents CV.</p>
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<p>Deposition characteristics of DD in the vertical direction of the canopy. L1 and L2 represent the upper and lower layers of the nutrient layer (NL), and L3 and L4 represent the upper and lower layers of the fruit layer (FL). Different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05. The box plot represents DD, and the dashed line represents CV, the dotted line represents PC.</p>
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<p>Deposition characteristics of SC in the vertical direction of the canopy. L1 and L2 represent the upper and lower layers of the nutrient layer (NL), and L3 and L4 represent the upper and lower layers of the fruit layer (FL). Different lowercase letters indicate significant differences at <span class="html-italic">p</span> ≤ 0.05. The box plot represents DD, and the dashed line represents CV, the dotted line represents PC.</p>
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<p>Response surface analysis of DD.</p>
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<p>Response surface analysis of SC.</p>
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<p>Comprehensive evaluation of the quality of droplet deposition. T1 to T9 represent different test groups.</p>
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13 pages, 747 KiB  
Article
Compressed Sensing-Based Genetic Markov Localization for Mobile Transmitters
by Sai Huang, Yuqing Chai, Shanchuan Ying, Shuo Chang and Nan Xia
Drones 2023, 7(1), 56; https://doi.org/10.3390/drones7010056 - 13 Jan 2023
Viewed by 1749
Abstract
With the strengths of quickness, low cost, and adaptability, unmanned aerial vehicle (UAV) communication is widely utilized in the next-generation wireless network. However, some risks and hidden dangers such as UAV “black flight” disturbances, attacks, and spying incidents lead to the necessity of [...] Read more.
With the strengths of quickness, low cost, and adaptability, unmanned aerial vehicle (UAV) communication is widely utilized in the next-generation wireless network. However, some risks and hidden dangers such as UAV “black flight” disturbances, attacks, and spying incidents lead to the necessity of the real-time supervision of UAVs. A compressed sensing-based genetic Markov localization method is proposed in this paper for two-dimensional trajectory tracking of the mobile transmitter in a finite domain, which consists of three modules: the multi-station sampling module, the reconstruction module, and the localization module. In the multi-station sampling module, multiple stations are deployed to receive the signal transmitted by the UAV using compressed sensing, and the motion model of the mobile transmitter is the constant turn rate and acceleration (CTRA) model. In the reconstruction module, we propose a direct reconstruction method to extract the joint cross-spatial spectrum. In the genetic Markov localization module, we propose a two-step localization method to genetically correct the inaccurate points in the preliminary results and generate the tracking result. Extensive simulations are conducted to verify the effectiveness of the proposed method. The results show that the proposed method is superior to the particle filter method and the Markov Monte Carlo method at all sampling moments. Specifically, when SNR = 15dB, the root-mean-square error (RMSE) of the proposed method is 39% and 60% lower than that of the other two methods, respectively. Moreover, under the premise that the RMSE of the localization result is less than 30 m, the reconstruction module can reduce the running time of the proposed method by 33.3%. Full article
(This article belongs to the Special Issue UAVs Communications for 6G)
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<p>The proposed method framework.</p>
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<p>The trajectory tracking results of the mobile signal: (<b>a</b>) tracking results of the fast Markov method; (<b>b</b>) tracking results after genetic correction.</p>
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<p>Performance comparison of the proposed method versus the compressed gain G. (<b>a</b>) RMSE of the method versus the compressed gain G; (<b>b</b>) running time of the method versus the compressed gain G.</p>
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<p>Performance comparison of the proposed method versus the number of particles N. (<b>a</b>) RMSE of the method versus number of particles; (<b>b</b>) running time of the method versus the number of particles.</p>
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<p>Performance comparison of different localization methods at different sampling moments, with SNR = 20 dB.</p>
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<p>Performance comparison of different localization methods versus SNRs.</p>
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<p>The estimation time of different localization methods versus RMSEs.</p>
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26 pages, 22508 KiB  
Article
Multi-UAV Cooperative Trajectory Planning Based on FDS-ADEA in Complex Environments
by Gang Huang, Min Hu, Xueying Yang and Peng Lin
Drones 2023, 7(1), 55; https://doi.org/10.3390/drones7010055 - 12 Jan 2023
Cited by 11 | Viewed by 2637
Abstract
Multi-UAV cooperative trajectory planning (MUCTP) refers to the planning of multiple flyable trajectories based on the location of each UAV and mission point in a complex environment. In the planning process, the complex 3D space structure increases the difficulty of solving the trajectory [...] Read more.
Multi-UAV cooperative trajectory planning (MUCTP) refers to the planning of multiple flyable trajectories based on the location of each UAV and mission point in a complex environment. In the planning process, the complex 3D space structure increases the difficulty of solving the trajectory points, and the mutual constraints of the UAV cooperative constraints can degrade the performance of the planning system. Therefore, to improve the efficiency of MUCTP, this study proposes MUCTP based on feasible domain space and adaptive differential evolution algorithm (FDS-ADEA). The method first constructs a three-dimensional feasible domain space to reduce the complexity of the search space structure; then, the constraints of heterogeneous UAVs are linearly weighted and transformed into a new objective function, and the information of the fitness value is shared in accordance with the adaptive method and the code correction method to improve the search efficiency of the algorithm; finally, the trajectories are smoothed to ensure the flyability of the UAVs performing the mission by combining the cubic B-spline curves. Experiments 1, 2, 3, and 4 validate the proposed algorithm. Simulation results verify that FDS-ADEA has fast convergence, high cooperative capability, and more reasonable planned trajectory sets when processing MUCTP. Full article
(This article belongs to the Special Issue A UAV Platform for Flight Dynamics and Control System)
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<p>Schematic of classical DEA.</p>
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<p>Terrain obstacles and threatening obstructions in the environment.</p>
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<p>Construction of fitness value of objective function.</p>
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<p>Setting the feasible region between the starting point and the mission point.</p>
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<p>Setting the feasible region between the starting point and the target point.</p>
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<p>Classical mutation strategy. (<b>a</b>) DE/rand/1, (<b>b</b>) DE/best/1.</p>
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<p>Adaptive DEA.</p>
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<p>Code correction rule.</p>
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<p>Flowchart based on FDS-ADEA algorithm.</p>
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<p>Verification of the feasibility of the feasible domain space construction. (<b>a</b>) indicates that a single UAV, a single mission point, was selected to verify the feasibility of the feasible domain space with a defined execution relationship; (<b>b</b>,<b>c</b>) indicate that the feasible domain flight space was observed from different angles, respectively; (<b>d</b>) indicates that obstacles were hidden for better observation.</p>
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<p>Verification of the stability of feasible domain space construction.</p>
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<p>Verification of the stability of feasible domain space construction.</p>
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<p>Multi-UAV coordinated trajectory execution relationship. (<b>a</b>) shows the multi-UAV cooperative trajectory execution relationship; (<b>b</b>) hides the mountainous terrain type and shows the effect of each obstacle on the UAVs; (<b>c</b>) can visually represent the planning of each UAVs; and (<b>d</b>) shows the convergence curve of the total adaptation value of each UAV.</p>
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<p>Multi-UAV coordinated trajectory execution relationship. (<b>a</b>) shows the multi-UAV cooperative trajectory execution relationship; (<b>b</b>) hides the mountainous terrain type and shows the effect of each obstacle on the UAVs; (<b>c</b>) can visually represent the planning of each UAVs; and (<b>d</b>) shows the convergence curve of the total adaptation value of each UAV.</p>
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<p>Effect of feasible domain parameters on fitness values. (<b>a</b>) effect of feasible domain parameters on total fitness values; (<b>b</b>) effect of feasible domain parameters on optimal generation value; (<b>c</b>) effect of feasible domain parameters on mean algebra value; and (<b>d</b>) effect of feasible domain parameters on highest generation value.</p>
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<p>Multi-UAV cooperative path planning based on FDS-ADEA.</p>
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<p>Simulation diagram of multi-UAV cooperative trajectory planning; (<b>a</b>–<b>c</b>) show the multi-UAV cooperative trajectory viewed from different angles.</p>
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<p>Average generation value comparison between FDS-ADEA and similar algorithms.</p>
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22 pages, 13708 KiB  
Article
Preliminary Concept of Urban Air Mobility Traffic Rules
by Wenqiu Qu, Chenchen Xu, Xiang Tan, Anqi Tang, Hongbo He and Xiaohan Liao
Drones 2023, 7(1), 54; https://doi.org/10.3390/drones7010054 - 12 Jan 2023
Cited by 14 | Viewed by 5329
Abstract
Driven by recent technological breakthroughs, the electric vertical take-off and landing (eVTOL) aircraft has gained considerable attention. The widespread demand for eVTOL aircraft can be attributed to their potential use in the commercialisation of urban air mobility (UAM) in low-altitude urban airspaces. However, [...] Read more.
Driven by recent technological breakthroughs, the electric vertical take-off and landing (eVTOL) aircraft has gained considerable attention. The widespread demand for eVTOL aircraft can be attributed to their potential use in the commercialisation of urban air mobility (UAM) in low-altitude urban airspaces. However, the urban low-altitude airspace environment is complex. UAM has a high traffic density and the eVTOL aircraft specifications are not uniform. Particularly in commercial scenarios, controlling eVTOL aircraft and ensuring safety in UAMs are the two major problems that should be addressed in future studies. The design of reasonable traffic rules is a potential solution; hence, we organised a UAM traffic rule system and proposed several alternative UAM traffic rules from three perspectives: a single eVTOL aircraft, a certain route, and key control areas. In addition, we validated these traffic rules using multi-rotor and fixed-wing eVTOL aircraft. The results show that designing reasonable traffic rules can facilitate attaining the primary objectives of commercialisation of UAM. Full article
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<p>Analytical framework.</p>
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<p>Space-time capsule. (<b>a</b>) Multi-rotor eVTOL aircraft, (<b>b</b>) fixed-wing eVTOL aircraft.</p>
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<p>Multi-rotor eVTOL aircraft turning schematic.</p>
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<p>Space-time capsule. (<b>a</b>) Multi-rotor eVTOL aircraft, (<b>b</b>) fixed-wing eVTOL aircraft.</p>
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<p>eVTOL aircraft entering or leaving routes at different stages. (<b>a</b>) Early stage, (<b>b</b>) middle stage.</p>
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<p>Collision avoidance diagram. (<b>a</b>) Emergency missions, (<b>b</b>) Same mission level.</p>
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<p>Turning diagram. (<b>a</b>) Circular intersection, (<b>b</b>) cross intersection.</p>
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<p>Turning diagram. (<b>a</b>) Circular intersection, (<b>b</b>) cross intersection.</p>
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<p>Altitude transition corridor.</p>
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<p>Entering height transition corridor.</p>
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<p>Leaving height transition corridor.</p>
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<p>Vertipod design.</p>
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<p>Parking point design.</p>
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<p>Vertiport layout on open ground or transportation hub.</p>
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<p>Vertiport layout on building roof.</p>
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<p>Terminal area approach and departure layout. (<b>a</b>) Layout one, (<b>b</b>) Layout two.</p>
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<p>Terminal area approach and departure layout. (<b>a</b>) Layout one, (<b>b</b>) Layout two.</p>
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<p>Number and location of approach and departure positioning points. (<b>a</b>) Layout one, (<b>b</b>) Layout two, (<b>c</b>) Layout three, (<b>d</b>) Layout four.</p>
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<p>Approach and departure route. (<b>a</b>) Approach process, (<b>b</b>) Departure process.</p>
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<p>Top view of verification site.</p>
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<p>eVTOL aircraft for traffic rule verification. (<b>a</b>) DJI M300 RTK, (<b>b</b>) JOUAV CW-15.</p>
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<p>Simulation trajectory diagram of eVTOL aircraft leaving or entering route. (<b>a</b>) Leaving route, (<b>b</b>) entering route.</p>
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<p>Collision avoidance rule simulation.</p>
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<p>Altitude profiles of collision avoidance rule simulation.</p>
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<p>Turning rule simulation. (<b>a</b>) Cross intersection, (<b>b</b>) roundabout intersection.</p>
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<p>Altitude transition simulation.</p>
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<p>Terminal area approach and departure simulation.</p>
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18 pages, 1056 KiB  
Article
Preserving Privacy of Classified Authentic Satellite Lane Imagery Using Proxy Re-Encryption and UAV Technologies
by Yarajarla Nagasree, Chiramdasu Rupa, Ponugumati Akshitha, Gautam Srivastava, Thippa Reddy Gadekallu and Kuruva Lakshmanna
Drones 2023, 7(1), 53; https://doi.org/10.3390/drones7010053 - 12 Jan 2023
Cited by 22 | Viewed by 2985
Abstract
Privacy preservation of image data has been a top priority for many applications. The rapid growth of technology has increased the possibility of creating fake images using social media as a platform. However, many people, including researchers, rely on image data for various [...] Read more.
Privacy preservation of image data has been a top priority for many applications. The rapid growth of technology has increased the possibility of creating fake images using social media as a platform. However, many people, including researchers, rely on image data for various purposes. In rural areas, lane images have a high level of importance, as this data can be used for analyzing various lane conditions. However, this data is also being forged. To overcome this and to improve the privacy of lane image data, a real-time solution is proposed in this work. The proposed methodology assumes lane images as input, which are further classified as fake or bona fide images with the help of Error Level Analysis (ELA) and artificial neural network (ANN) algorithms. The U-Net model ensures lane detection for bona fide lane images, which helps in the easy identification of lanes in rural areas. The final images obtained are secured by using the proxy re-encryption technique which uses RSA and ECC algorithms. This helps in ensuring the privacy of lane images. The cipher images are maintained using fog computing and processed with integrity. The proposed methodology is necessary for protecting genuine satellite lane images in rural areas, which are further used by forecasters, and researchers for making interpretations and predictions on data. Full article
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<p>Proposed architecture.</p>
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<p>ANN network model.</p>
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<p>U-Net Model System Architecture.</p>
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<p>Fake image.</p>
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<p>Authentic image.</p>
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<p>Proxy re-encryption-based cipher image.</p>
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<p>Lane-predicted image.</p>
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<p>Parameters used in the ANN model.</p>
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<p>Confusion matrix of ANN model.</p>
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<p>Loss curves.</p>
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<p>Training gist curves.</p>
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<p>Comparison of encryption times.</p>
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<p>Comparison analysis for various image formats.</p>
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17 pages, 2932 KiB  
Article
Strapdown Celestial Attitude Estimation from Long Exposure Images for UAV Navigation
by Samuel Teague and Javaan Chahl
Drones 2023, 7(1), 52; https://doi.org/10.3390/drones7010052 - 12 Jan 2023
Cited by 3 | Viewed by 2969
Abstract
Strapdown celestial imaging sensors provide a compact, lightweight alternative to their gimbaled counterparts. Strapdown imaging systems typically require a wider field of view, and consequently longer exposure intervals, leading to significant motion blur. The motion blur for a constellation of stars results in [...] Read more.
Strapdown celestial imaging sensors provide a compact, lightweight alternative to their gimbaled counterparts. Strapdown imaging systems typically require a wider field of view, and consequently longer exposure intervals, leading to significant motion blur. The motion blur for a constellation of stars results in a constellation of trails on the image plane. We present a method that extracts the path of these star trails, and uses a linearized weighted least squares approach to correct noisy inertial attitude measurements. We demonstrate the validity of this method through its application to synthetically generated images, and subsequently observe its relative performance by using real images. The findings of this study indicate that the motion blur present in strapdown celestial imagery yields an a posteriori mean absolute attitude error of less than 0.13 degrees in the yaw axis, and 0.06 degrees in the pitch and roll axes (3 σ) for a calibrated wide-angle camera lens. These findings demonstrate the viability of low-cost, wide-angle, strapdown celestial attitude sensors on lightweight UAV hardware. Full article
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<p>A region of interest containing a single star trail, captured from a strapdown celestial imaging sensor (Pi Camera HQ, 500 ms exposure interval). The shape of the star trail indicates that the camera was subjected to significant changes in attitude throughout the exposure interval.</p>
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<p>Flow diagram of image processing chain, with example images (black and white images converted to a perceptually uniform colour scale).</p>
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<p>An example of attitude correction, displaying a region of interest for a single star. Greyscale images are overlaid onto a three-channel image. <b>Left</b>: mean-only alignment, <b>Right</b>: fine attitude alignment. Green, real image; blue, synthetic image from INS; red, reprojection after corrections.</p>
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<p>Zeta Science FX61 airframe used for capturing in-flight imagery.</p>
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<p>An example of Perlin gradient-based noise generation across various octaves (frequencies).</p>
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<p>Histogram of mean absolute errors from each simulated image containing <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>14</mn> </mrow> </semantics></math> attitude references. (<b>a</b>) Yaw. (<b>b</b>) Pitch. (<b>c</b>) Roll.</p>
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<p>An example of simulation attitude correction, displaying superimposed regions of interest. Green channel, baseline simulation image; blue channel, synthetic image from noisy INS; red channel, synthetic image after corrections. Max yaw error: 0.0727<math display="inline"><semantics> <msup> <mrow/> <mo>∘</mo> </msup> </semantics></math>, max pitch error: 0.0286<math display="inline"><semantics> <msup> <mrow/> <mo>∘</mo> </msup> </semantics></math>, max roll error: 0.0226<math display="inline"><semantics> <msup> <mrow/> <mo>∘</mo> </msup> </semantics></math>.</p>
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<p>ROIs of stars used for attitude correction on a real image. Green channel, real image; blue channel, synthetic image from raw INS data; red channel, synthetic image from corrected INS data. The intensity of each ROI is amplified such that the peak pixel intensity is 255.</p>
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<p>ROIs of stars used for attitude correction on a real image. Green channel, real image; blue channel, synthetic image from raw INS data; red channel, synthetic image from corrected INS data. The intensity of each ROI is amplified such that the peak pixel intensity is 255.</p>
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31 pages, 9153 KiB  
Article
Narrating Ancient Roman Heritage through Drawings and Digital Architectural Representation: From Historical Archives, UAV and LIDAR to Virtual-Visual Storytelling and HBIM Projects
by Fabrizio Banfi, Stefano Roascio, Alessandro Mandelli and Chiara Stanga
Drones 2023, 7(1), 51; https://doi.org/10.3390/drones7010051 - 11 Jan 2023
Cited by 15 | Viewed by 4588
Abstract
One of the main objectives of today’s archaeological sites and museums is the development of research, understood as the interpretation and contextualisation of tangible and intangible cultural heritage to broaden the knowledge and accessibility of archaeological parks often unknown to visitors and the [...] Read more.
One of the main objectives of today’s archaeological sites and museums is the development of research, understood as the interpretation and contextualisation of tangible and intangible cultural heritage to broaden the knowledge and accessibility of archaeological parks often unknown to visitors and the public on a large scale. In this perspective, the Appia Antica Archaeological Park aims to support research in digitising infrastructures and archaeological contexts of high historical and cultural value to plan short- and medium-term preservation and maintenance projects. In this context, unmanned aerial vehicles (UAVs) are tools with enormous potential in survey, inspection and digitisation, providing the basis for the subsequent phases of data interpretation, representation and material analysis. Thanks to the photorealistic reconstruction of dense structure from motion (DSfM) in the application of structural inspections, today it is possible to intercept the geometry and material conditions of small, medium and large structures, reducing the costs of inspections, limiting the interruption of the public and providing professionals and visitors with a better volumetric understanding of the system. However, inserting information that gradually accumulates throughout the process requires advanced 3D digital representation techniques, such as HBIM (historic building information modelling), scan-to-BIM approach and interactive forms, such as virtual and augmented reality (VR-AR). For these reasons, this study summarises the experience and lessons learned from the UAV inspection of three research case studies at archaeological, architectural, and infrastructure scales to increase awareness of the Roman-built heritage. Full article
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<p>The Research case studies: the Appian way and its mausoleums (top) and Castrum Caetani: San Nicola Church, (the Mausoleum of Caecilia Metella and Caetani Palace (bottom).</p>
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<p>The proposed research method for multiple representation scales: from historical archives, UAV and LIDAR to AR, VR and HBIM projects.</p>
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<p>The Appian way: the mausoleums, and the pavement realised with polygonal blocks of mafic lava (Top). Giovanni Battista Piranesi, the pavement and the crepidines (blocks that delimit the road) of the Appian Way towards Rome shortly after the city of Albano, engraving. The Appian Way pavement is engraving on the right (<span class="html-italic">Antichità Romane</span>, 1756—source: Europeana, <a href="https://www.europeana.eu/it" target="_blank">https://www.europeana.eu/it</a>, accessed on 22 November 2022) (Bottom).</p>
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<p>On the left is Giovanni Battista Piranesi’s perspective view of the Appian Way: ruins of an ancient tomb (outside Albano). On the right: ruins of the monuments outside Porta S. Sebastiano (<span class="html-italic">Antichità Romane</span>, 1756—source: Europeana, <a href="https://www.europeana.eu/it" target="_blank">https://www.europeana.eu/it</a>, (accessed on 22 November 2022).</p>
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<p>On the left: Luigi Canina, Monuments after the IV mile, plate XXI, <span class="html-italic">La prima parte della Via Appia dalla Porta Capena a Boville</span>, 1853. On the right: Monuments after the IV mile and detail of the Tomb of Tiberio Claudio Secondo, plate XXII, <span class="html-italic">La prima parte della Via Appia dalla Porta Capena a Boville</span>, 1853.</p>
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<p>The landscape of the Appian Way: from archaeological and architectural scales to the aerial infrastructure views.</p>
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<p>Drawings by Luigi Canina depicting the plan, the ruins of the mausoleum of Caecilia Metella and the reconstruction of the mausoleum. At the bottom right: aerial image of the Castrum Caetani composed by the Cecilia Metella Mausoleum (a); (b) Palace Caetani; and (c) St. Nicola Church.</p>
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<p>Main 3D Survey instruments (from left to right: Leica TPS1200, ZEB Horizon and DJI Mavic Mini 3) and point clouds from laser scanning of St. Nicola Church and Castrum Caetani.</p>
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<p>D-Flight Map, image centred on St. Nicola Church, including also the Appian Way, with restriction areas highlighted. Each colour refers to a height limit. (Source: <a href="http://www.d-flight.it/newportal" target="_blank">www.d-flight.it/newportal</a>, accessed on 1 December 2022).</p>
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<p>The research case studies are characterised by elements that make acquisition difficult. The DJI Mavic Mini 3 was decisive for the three-way detection of obstacles and the acquisition of architectural and structural elements from multiple angles.</p>
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<p>Drones and radio control comparison, DJI Mini 3 Pro on the left with its camera’s vertical axis, reaching 90 degrees and DJI Mini 2 on the right.</p>
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<p>Terrestrial and Aerial acquisition: in blue nadiral and inclined images of St. Nicola Church, Mausoleum of Caecilia Metella and Caetani Palace, dense cloud, mesh and textured model.</p>
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<p>Final measured drawings and cutaway textured 3D models of Caetani Palace.</p>
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<p>Final measured drawings and high-resolution textured 3D models of St. Nicola Church.</p>
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<p>The Appian Way’s mausoleums (IV mile): (<b>a</b>) the Funerary temple with a columbarium; (<b>b</b>) the Tomb of Tiberio Claudio Secondo; and (<b>c</b>) the brick columbarium with a vault.</p>
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<p>Multilevel representation of the Appian Way: 3D models, plan (left) and the section (right): (a) Brick columbarium with a vault, (b) Tomb of Tiberio Claudio Secondo, (c) Funerary temple with colombarium.</p>
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<p>Geometric reliability check of digital models: (<b>a</b>) the NURBS model of the Tomb of Tiberio Claudio Secondo; (<b>b</b>) dense point cloud; (<b>c</b>) standard deviation: the grade of accuracy (GOA) achieved is 0.01 m (<b>d</b>).</p>
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<p>The HBIM project of the brick columbarium: (<b>a</b>) NURBS models; (<b>b</b>) material superficial analysis; (c) HBIM objects; (d) HBIM objects corresponding to each identified area; (e) automatic area quantification; (<b>f</b>) GOA; (<b>g</b>) measured drawings.</p>
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<p>AR projects of the Appian Way (IV mile): the Tomb of Tiberio Claudio Secondo.</p>
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<p>The restitutive hypothesis of both the interior and the exterior, Leporini (1958).</p>
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<p>The 3D restitutive hypothesis of St. Nicola Church: (<b>a</b>) 3D drawings and NURBS model; (<b>b</b>) floor; (<b>c</b>) arches; (<b>d</b>) exterior walls; (<b>e</b>) timber framing system; (<b>f</b>) roof covering; and (<b>g</b>) cutaway 3D models.</p>
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<p>The VR project of St. Nicola Church.</p>
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18 pages, 4596 KiB  
Article
Research on Adaptive Prescribed Performance Control Method Based on Online Aerodynamics Identification
by Shuaibin An, Jianwen Zang, Ming Yan, Baiyang Zhu and Jun Liu
Drones 2023, 7(1), 50; https://doi.org/10.3390/drones7010050 - 11 Jan 2023
Cited by 4 | Viewed by 1935
Abstract
Wide-speed-range vehicles are characterized by high flight altitude and high speed, with significant changes in the flight environment. Due to the strong uncertainty of its aerodynamic characteristics, higher requirements are imposed on attitude control. In this paper, an adaptive prescribed performance control method [...] Read more.
Wide-speed-range vehicles are characterized by high flight altitude and high speed, with significant changes in the flight environment. Due to the strong uncertainty of its aerodynamic characteristics, higher requirements are imposed on attitude control. In this paper, an adaptive prescribed performance control method based on online aerodynamic identification is proposed, which consists of two parts: an online aerodynamic parameter identification method and an adaptive attitude control method based on the pre-defined parameters of the control system. The aerodynamic parameter identification is divided into offline design and online design. In the offline design, neural networks are used to fit nonlinear aerodynamic characteristics. In the online design, a nonlinear recursive identification method is used to correct the errors of the offline fitted model. The adaptive attitude control is based on the conventional control method and updates the control gain in real time according to the desired system parameters to enhance the robustness of the controller. Finally, the effectiveness of the offline neural network and online discrimination correction is verified by mathematical simulations, and the effectiveness and robustness of the adaptive control proposed in this paper are verified by comparative simulation. Full article
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<p>Schematic diagram of multi-layer neural network structure.</p>
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<p>Schematic diagram of multi-layer neural network structure.</p>
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<p>Adaptive control block diagram based on online aerodynamic identification.</p>
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<p>Fitting result graph of neural network verification set.</p>
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<p>Error result of neural network verification set fitting.</p>
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<p>Online aerodynamic parameter identification of flight state curve.</p>
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<p>Identification curve of pitching moment coefficient, static stability coefficient, and controllability coefficient.</p>
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<p>Comparison curve of pitch angle command tracking control.</p>
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<p>Comparison curve of pitch angle command tracking control.</p>
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<p>(<b>a</b>) Comparison curve of pitch angle control under random uncertainty; (<b>b</b>) Comparison curve of pitch rate response under random uncertain interference; (<b>c</b>) Elevator control comparison curve under random uncertainty disturbance; (<b>d</b>) Comparison curve of attack angle response under random uncertain interference.</p>
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<p>Comparison curve of pitch angle command tracking control.</p>
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42 pages, 16735 KiB  
Article
Aero-Propulsive Interactions between UAV Wing and Distributed Propellers Due to Their Relative Position
by Danilo Ciliberti, Pierluigi Della Vecchia, Vincenzo Orticalco and Fabrizio Nicolosi
Drones 2023, 7(1), 49; https://doi.org/10.3390/drones7010049 - 11 Jan 2023
Cited by 5 | Viewed by 3539
Abstract
The purpose of this paper is the evaluation of the aero-propulsive effects on a UAV wing model with distributed propulsion. An array of three propellers is placed ahead of the leading edge of a rectangular wing with flap. The investigation was performed with [...] Read more.
The purpose of this paper is the evaluation of the aero-propulsive effects on a UAV wing model with distributed propulsion. An array of three propellers is placed ahead of the leading edge of a rectangular wing with flap. The investigation was performed with high-fidelity numerical analyses to provide insights into the phenomenology and to screen the interesting positions to be validated in the wind tunnel. The propellers’ array is moved into twelve different positions, allowing longitudinal and vertical translations. The wing has an untwisted and constant section profile, with a single slot trailing-edge flap that is deflected into three positions. The flap span is entirely covered by the propellers’ blowing. Results show an increment of lift, drag, and pitching moment coefficients with distributed propellers enabled. For a given thrust level, the magnitude of such increments depends on the propellers’ positions, the flap configuration, and the angle of attack. The lift enhancement sought in distributed propulsion applications comes at the expense of a significant increase in drag and pitching moment magnitude. In some combinations, the wing’s contribution to the aircraft longitudinal stability is severely affected. Conversely, the propellers’ inflow is altered such that thrust is increased in all the investigated configurations, with a small reduction of propulsive efficiency. Full article
(This article belongs to the Section Drone Design and Development)
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<p>Drawing of the starboard half-wing model with propellers’ disks. Units in mm.</p>
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<p>Positions of the propellers’ array. The black circle is the baseline location.</p>
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<p>Two-dimensional fine mesh around the airfoil. A conical-shaped refinement has been applied to capture the wake.</p>
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<p>Definitions of flap deflection <math display="inline"><semantics> <msub> <mi>δ</mi> <mi mathvariant="normal">f</mi> </msub> </semantics></math>, gap, overlap, and hinge line.</p>
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<p>Two-dimensional design exploration for flap position at <math display="inline"><semantics> <mrow> <mi>R</mi> <msub> <mi>e</mi> <mo>∞</mo> </msub> <mo>=</mo> <mn>5.3</mn> <mo>×</mo> <msup> <mn>10</mn> <mn>5</mn> </msup> </mrow> </semantics></math>: (<b>a</b>) lift coefficient in take-off; (<b>b</b>) lift coefficient in landing; (<b>c</b>) drag coefficient in take-off; (<b>d</b>) drag coefficient in landing; (<b>e</b>) pitching moment coefficient in take-off; (<b>f</b>) pitching moment coefficient in landing.</p>
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<p>Computational domain.</p>
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<p>Top view of the finest mesh on the wing model with flap.</p>
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<p>Grid convergence investigation on the three-dimensional half-wing model with flap. <span class="html-italic">N</span> is the number of cells. The chosen mesh has <math display="inline"><semantics> <mrow> <mi>N</mi> <mo>≈</mo> <mn>8</mn> <mo>·</mo> <msup> <mn>10</mn> <mn>6</mn> </msup> </mrow> </semantics></math>. The related data points are enclosed by gray rectangles.</p>
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<p>High-lift propeller designed with XROTOR: (<b>a</b>) propeller planform; (<b>b</b>) propeller characteristics.</p>
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<p>Aerodynamic coefficients for the clean wing: (<b>a</b>) lift curves; (<b>b</b>) drag polars; (<b>c</b>) pitching moment curves; (<b>d</b>) aerodynamic efficiency curves.</p>
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<p>Effects of DEP array positions on the lift characteristics of the clean wing: (<b>a</b>) lift increment; (<b>b</b>) lift gradient increment; (<b>c</b>) maximum lift increment; (<b>d</b>) stall angle change.</p>
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<p>Effects of DEP array positions on the drag and pitching moment characteristics of the clean wing: (<b>a</b>) minimum drag increment; (<b>b</b>) maximum aerodynamic efficiency change; (<b>c</b>) pitching moment increment; (<b>d</b>) pitching moment gradient change.</p>
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<p>Spanwise section lift distributions for the clean wing: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>0</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>4</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>c</b>) vertical velocity component in the disk plane.</p>
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<p>Chordwise pressure distributions for the clean wing around the mid propeller: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>0</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>4</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>.</p>
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<p>Chordwise skin friction distributions for the clean wing: (<b>a</b>) configuration xFzU at <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>4</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) configuration xAzB at <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>4</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>.</p>
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<p>Effects of the wing on propeller performance with STAR-CCM+ virtual disk model: (<b>a</b>) propellers advance ratio; (<b>b</b>) propellers’ thrust coefficient; (<b>c</b>) propellers’ power coefficient; (<b>d</b>) propellers’ efficiency. Design data is taken from <a href="#drones-07-00049-t006" class="html-table">Table 6</a>, which are the assigned coefficients for the isolated propeller.</p>
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<p>Effects of the wing on propeller performance with STAR-CCM+ virtual disk model: (<b>a</b>) propellers advance ratio; (<b>b</b>) propellers’ thrust coefficient; (<b>c</b>) propellers’ power coefficient; (<b>d</b>) propellers’ efficiency. Design data is taken from <a href="#drones-07-00049-t006" class="html-table">Table 6</a>, which are the assigned coefficients for the isolated propeller.</p>
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<p>Aerodynamic coefficients for the wing with flap deflected for take-off: (<b>a</b>) lift curves; (<b>b</b>) drag polars; (<b>c</b>) pitching moment curves; (<b>d</b>) aerodynamic efficiency curves.</p>
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<p>Effects of DEP array positions on the lift characteristics of the wing with flap deflected for take-off: (<b>a</b>) lift increment; (<b>b</b>) lift gradient increment; (<b>c</b>) maximum lift increment; (<b>d</b>) stall angle change.</p>
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<p>Effects of DEP array positions on the drag and pitching moment characteristics of the wing with flap deflected for take-off: (<b>a</b>) minimum drag increment; (<b>b</b>) maximum aerodynamic efficiency change; (<b>c</b>) pitching moment increment; (<b>d</b>) pitching moment gradient change.</p>
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<p>Spanwise section lift distributions for the wing with flap deflected for take-off: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>4</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>8</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>c</b>) vertical velocity component in the disk plane.</p>
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<p>Chordwise pressure distributions around the mid propeller for the wing with flap deflected for take-off: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>4</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>8</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>.</p>
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<p>Chordwise skin friction distributions for the wing with flap deflected for take-off: (<b>a</b>) configuration xFzC at <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>8</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) configuration xAzB at <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>8</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>.</p>
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<p>Effects of the wing with flap deflected for take-off on propellers’ performance with STAR-CCM+ virtual disk model: (<b>a</b>) propellers’ advance ratio; (<b>b</b>) propellers’ thrust coefficient; (<b>c</b>) propellers power coefficient; (<b>d</b>) propellers’ efficiency. Design data are taken from <a href="#drones-07-00049-t006" class="html-table">Table 6</a>, which are the assigned coefficients for the isolated propeller.</p>
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<p>Effects of the wing with flap deflected for take-off on propellers’ performance with STAR-CCM+ virtual disk model: (<b>a</b>) propellers’ advance ratio; (<b>b</b>) propellers’ thrust coefficient; (<b>c</b>) propellers power coefficient; (<b>d</b>) propellers’ efficiency. Design data are taken from <a href="#drones-07-00049-t006" class="html-table">Table 6</a>, which are the assigned coefficients for the isolated propeller.</p>
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<p>Aerodynamic coefficients for the wing with flap deflected for landing: (<b>a</b>) lift curves; (<b>b</b>) drag polars; (<b>c</b>) pitching moment curves; (<b>d</b>) aerodynamic efficiency curves.</p>
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<p>Effects of DEP array positions on the lift characteristics of the wing with flap deflected for landing: (<b>a</b>) lift increment; (<b>b</b>) lift gradient increment; (<b>c</b>) maximum lift increment; (<b>d</b>) stall angle change.</p>
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<p>Effects of DEP array positions on the drag and pitching moment characteristics of the wing with flap deflected for landing: (<b>a</b>) minimum drag increment; (<b>b</b>) maximum aerodynamic efficiency change; (<b>c</b>) pitching moment increment; (<b>d</b>) pitching moment gradient change.</p>
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<p>Spanwise section lift distributions for the wing with flap deflected for landing: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>8</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>12</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>c</b>) vertical velocity component in the disk plane.</p>
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<p>Chordwise pressure distributions for the wing with flap deflected for landing: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>8</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>12</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>.</p>
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<p>Chordwise skin friction distributions for the wing with flap deflected for landing: (<b>a</b>) configuration xFzU at <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>12</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>; (<b>b</b>) configuration: xAzD at <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>12</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>.</p>
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<p>Effects of the wing with flap deflected for landing on propellers’ performance with STAR-CCM+ virtual disk model: (<b>a</b>) propellers’ advance ratio; (<b>b</b>) propellers’ thrust coefficient; (<b>c</b>) propellers power coefficient; (<b>d</b>) propellers’ efficiency. Design data is taken from <a href="#drones-07-00049-t006" class="html-table">Table 6</a>, which are the assigned coefficients for the isolated propeller.</p>
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<p>Effects of the wing with flap deflected for landing on propellers’ performance with STAR-CCM+ virtual disk model: (<b>a</b>) propellers’ advance ratio; (<b>b</b>) propellers’ thrust coefficient; (<b>c</b>) propellers power coefficient; (<b>d</b>) propellers’ efficiency. Design data is taken from <a href="#drones-07-00049-t006" class="html-table">Table 6</a>, which are the assigned coefficients for the isolated propeller.</p>
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18 pages, 2023 KiB  
Article
Dual Observer Based Adaptive Controller for Hybrid Drones
by Nihal Dalwadi, Dipankar Deb and Stepan Ozana
Drones 2023, 7(1), 48; https://doi.org/10.3390/drones7010048 - 11 Jan 2023
Cited by 6 | Viewed by 2519
Abstract
A biplane quadrotor (hybrid vehicle) benefits from rotary-wing and fixed-wing structures. We design a dual observer-based autonomous trajectory tracking controller for the biplane quadrotor. Extended state observer (ESO) is designed for the state estimation, and based on this estimation, a Backstepping controller (BSC), [...] Read more.
A biplane quadrotor (hybrid vehicle) benefits from rotary-wing and fixed-wing structures. We design a dual observer-based autonomous trajectory tracking controller for the biplane quadrotor. Extended state observer (ESO) is designed for the state estimation, and based on this estimation, a Backstepping controller (BSC), Integral Terminal Sliding Mode Controller (ITSMC), and Hybrid Controller (HC) that is a combination of ITSMC + BSC are designed for the trajectory tracking. Further, a Nonlinear disturbance observer (DO) is designed and combined with ESO based controller to estimate external disturbances. In this simulation study, These ESO-based controllers with and without DO are applied for trajectory tracking, and results are evaluated. An ESO-based Adaptive Backstepping Controller (ABSC) and Adaptive Hybrid controller (AHC) with DO are designed, and performance is evaluated to handle the mass change during the flight despite wind gusts. Simulation results reveal the effectiveness of ESO-based HC with DO compared to ESO-based BSC and ITSMC with DO. Furthermore, an ESO-based AHC with DO is more efficient than an ESO-based ABSC with DO. Full article
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<p>Animated picture of biplane quadrotor.</p>
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<p>Dual observer-based control architecture.</p>
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<p>The Block Diagram of an adaptive hybrid controller.</p>
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<p>Position subsystem tracking by ESO-based BSC with and without DO.</p>
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<p>Position tracking by ESO-based ITSMC with and without DO.</p>
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<p>Position tracking by different ESO-based controllers with DO.</p>
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<p>Attitude tracking by different ESO-based controllers with DO.</p>
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<p><math display="inline"><semantics> <mrow> <mi>x</mi> <mo>−</mo> <mi>y</mi> </mrow> </semantics></math> position trajectory tracking by the ESO-based ABSC and AHC with DO.</p>
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<p>Altitude tracking by the ESO-based ABSC and AHC and DO.</p>
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<p>Attitude tracking by the ESO-based ABSC and AHC with DO.</p>
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34 pages, 1115 KiB  
Article
Autonomous Unmanned Aerial Vehicles in Bushfire Management: Challenges and Opportunities
by Shouthiri Partheepan, Farzad Sanati and Jahan Hassan
Drones 2023, 7(1), 47; https://doi.org/10.3390/drones7010047 - 10 Jan 2023
Cited by 38 | Viewed by 13989
Abstract
The intensity and frequency of bushfires have increased significantly, destroying property and living species in recent years. Presently, unmanned aerial vehicle (UAV) technology advancements are becoming increasingly popular in bushfire management systems because of their fundamental characteristics, such as manoeuvrability, autonomy, ease of [...] Read more.
The intensity and frequency of bushfires have increased significantly, destroying property and living species in recent years. Presently, unmanned aerial vehicle (UAV) technology advancements are becoming increasingly popular in bushfire management systems because of their fundamental characteristics, such as manoeuvrability, autonomy, ease of deployment, and low cost. UAVs with remote-sensing capabilities are used with artificial intelligence, machine learning, and deep-learning algorithms to detect fire regions, make predictions, make decisions, and optimize fire-monitoring tasks. Moreover, UAVs equipped with various advanced sensors, including LIDAR, visual, infrared (IR), and monocular cameras, have been used to monitor bushfires due to their potential to provide new approaches and research opportunities. This review focuses on the use of UAVs in bushfire management for fire detection, fire prediction, autonomous navigation, obstacle avoidance, and search and rescue to improve the accuracy of fire prediction and minimize their impacts on people and nature. The objective of this paper is to provide valuable information on various UAV-based bushfire management systems and machine-learning approaches to predict and effectively respond to bushfires in inaccessible areas using intelligent autonomous UAVs. This paper aims to assemble information about the use of UAVs in bushfire management and to examine the benefits and limitations of existing techniques of UAVs related to bushfire handling. However, we conclude that, despite the potential benefits of UAVs for bushfire management, there are shortcomings in accuracy, and solutions need to be optimized for effective bushfire management. Full article
(This article belongs to the Section Drones in Agriculture and Forestry)
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<p>Solutions to reduce impacts of bushfires and the challenges they pose.</p>
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<p>Statistical analysis of experiments on different types of UAV-based operations in bushfire management systems.</p>
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<p>Structure of the reviewed work.</p>
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<p>Components of a UAV-based bushfire management system.</p>
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<p>Different categories of frequently used UAV models in bushfire management.</p>
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15 pages, 2111 KiB  
Article
Civilian UAV Deployment Framework in Qatar
by Khalifa AL-Dosari, Ziad Hunaiti and Wamadeva Balachandran
Drones 2023, 7(1), 46; https://doi.org/10.3390/drones7010046 - 10 Jan 2023
Cited by 6 | Viewed by 3177
Abstract
Drone deployment in Qatar has been lagging behind that in other countries due to a wide range of reported challenges. This study developed a framework to address these operational gaps and serve as a roadmap for different stakeholders to enable drone applications for [...] Read more.
Drone deployment in Qatar has been lagging behind that in other countries due to a wide range of reported challenges. This study developed a framework to address these operational gaps and serve as a roadmap for different stakeholders to enable drone applications for successful, safe, accountable and sustainable development. Moreover, the framework could help overcome key challenges and lay the groundwork for addressing other challenges facing UAV deployment in Qatar, thereby enabling Qatar to join the global efforts in this technological evolution. The framework was based on an analysis of the available data from previous guidelines for UAV operation and the identification of the challenges facing drone deployment in Qatar. The proposed framework was evaluated through interviews with key stakeholders in the Qatari drone steering committee. The outcomes from this evaluation supported the implementation of the framework with minor amendments and are ready to be put into practice by policymakers. In addition, it could be helpful for Gulf Cooperation Council (GCC) countries and other countries in the region to consider this framework in their efforts to facilitate drone deployment. Full article
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<p>Top five challenges facing UAV deployment in Qatar. Source: the authors.</p>
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<p>Research design logframe. Source: the authors.</p>
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<p>Framework development method. Source: the authors.</p>
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<p>Proposed framework.</p>
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<p>The degree of satisfaction with the DFQ by work sector. Source: the authors.</p>
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<p>Aligned framework. Source: the authors.</p>
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23 pages, 2306 KiB  
Article
Impediments to Construction Site Digitalisation Using Unmanned Aerial Vehicles (UAVs)
by Adetayo Olugbenga Onososen, Innocent Musonda, Damilola Onatayo, Motheo Meta Tjebane, Abdullahi Babatunde Saka and Rasaki Kolawole Fagbenro
Drones 2023, 7(1), 45; https://doi.org/10.3390/drones7010045 - 9 Jan 2023
Cited by 15 | Viewed by 4990
Abstract
Utilising emerging innovative technologies and systems to improve construction processes in an effort towards digitalisation has been earmarked as critical to delivering resilience and responsive infrastructure. However, successful implementation is hindered by several challenges. Hence, this study evaluates the challenges facing the adoption [...] Read more.
Utilising emerging innovative technologies and systems to improve construction processes in an effort towards digitalisation has been earmarked as critical to delivering resilience and responsive infrastructure. However, successful implementation is hindered by several challenges. Hence, this study evaluates the challenges facing the adoption of unmanned aerial vehicles towards the digitalisation of the built environment. The study adopted a quantitative survey of built environment stakeholders in developed and developing economies. A total of 161 completely filled forms were received after the survey, and the data were analysed using descriptive analysis and inferential statistics. The study’s findings show that there are different barriers experienced between developed and developing countries in the adoption of drones towards digitalising construction processes in the built environment. Moreover, economic/cost-related factors were identified as the most critical barriers to the adoption of drones, followed by technical/regulatory factors and education/organisation-related factors. The findings can assist the built environment in reducing the impact of these barriers and could serve as a policy instrument and helpful guidelines for governmental organisations, stakeholders, and others. Full article
(This article belongs to the Special Issue Application of UAS in Construction)
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<p>Countries of survey respondents.</p>
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<p>Professional disciplines.</p>
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<p>Level of awareness.</p>
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<p>Organisational setup.</p>
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<p>Application of drones in construction process.</p>
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<p>Factor scale ranking of impediments.</p>
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23 pages, 33353 KiB  
Article
Intrinsically Safe Drone Propulsion System for Underground Coal Mining Applications: Computational and Experimental Studies
by Ahmed Aboelezz, David Wetz, Jane Lehr, Pedram Roghanchi and Mostafa Hassanalian
Drones 2023, 7(1), 44; https://doi.org/10.3390/drones7010044 - 8 Jan 2023
Cited by 5 | Viewed by 3846
Abstract
The mining industry has recently shown increased interest in drones for routine activities in underground and surface mines. Designing a drone for coal mines is extremely complicated since the Mine Safety and Health Administration (MSHA) has tight guidelines for any equipment that can [...] Read more.
The mining industry has recently shown increased interest in drones for routine activities in underground and surface mines. Designing a drone for coal mines is extremely complicated since the Mine Safety and Health Administration (MSHA) has tight guidelines for any equipment that can be used in underground coal mines. Due to these criteria, designing a drone for underground coal mining is exceedingly difficult. This paper explores the challenges of creating an intrinsically safe drone propulsion system. To address the challenges of designing an intrinsically safe drone’s propulsion system for an underground coal mine, this work aims to investigate the potential approaches to enhance efficiency and mitigate the heat. The study begins with the drone’s sizing approach before moving on to the experimental setup that is utilized to test the drone’s propulsion system. Finally, answers to numerous issues arising during the inquiry are offered, and these solutions are empirically explored. Full article
(This article belongs to the Section Drone Design and Development)
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<p>Sizing procedure of an intrinsically safe/permissible drone for underground mines.</p>
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<p>Multirotor propulsion chain diagram [<a href="#B24-drones-07-00044" class="html-bibr">24</a>].</p>
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<p>Propulsion system design methodology.</p>
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<p>The permissible drone design and its propulsion system.</p>
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<p>Drone propulsion system design and performance measurements flowchart.</p>
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<p>Drone propulsion system performance test rig.</p>
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<p>Mechanical coupler installation.</p>
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<p>Performance measurements for the system with and without the mechanical coupler.</p>
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<p>Performance measurements for the system with and without motor casings.</p>
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<p>Heat-sink coordinates.</p>
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<p>Heat-sink fin temperature distribution for <span class="html-italic">T<sub>w</sub></span> = 393.15 K and various <span class="html-italic">T<sub>inf</sub></span>, 15 mm fin (<b>left</b>) and 30 mm fin (<b>right</b>).</p>
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<p>Heat-sink fin temperature distribution for <span class="html-italic">T<sub>w</sub></span> = 393.15 K and various <span class="html-italic">T<sub>inf</sub></span>, 15 mm fin (<b>left</b>) and 30 mm fin (<b>right</b>).</p>
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<p>Heat-sink fin temperature distribution for <span class="html-italic">T<sub>inf</sub></span> = 298.15 K and various <span class="html-italic">T<sub>w</sub></span>, 15 mm fin (<b>left</b>) and 30 mm fin (<b>right</b>).</p>
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<p>Heat-sink fin temperature distribution for <span class="html-italic">T<sub>inf</sub></span> = 298.15 K and various <span class="html-italic">T<sub>w</sub></span>, 15 mm fin (<b>left</b>) and 30 mm fin (<b>right</b>).</p>
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<p>Heat-sink installation.</p>
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<p>Performance measurements for the system with and without a heat sink.</p>
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<p>Performance measurements for the system with and without a heat sink.</p>
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<p>Heat-sink cooling air direction.</p>
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<p>Smoke-visualization setup.</p>
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<p>Spinner added to the propulsion system.</p>
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<p>Spinner geometry.</p>
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<p>View of spinners’ different geometry.</p>
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<p>Views of 3d-printed spinners.</p>
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<p>View of balancing system.</p>
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<p>Thrust for the different spinners.</p>
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<p>Torque for the different spinners.</p>
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<p>Slipstream airspeed for the different spinners.</p>
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<p>Propeller efficiency for the different spinners.</p>
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<p>System efficiency for the different spinners.</p>
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<p>System vibration for the different spinners.</p>
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<p>View of flow visualization for the system with spinner and without a spinner.</p>
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15 pages, 3293 KiB  
Article
Retrieval of Fractional Vegetation Cover from Remote Sensing Image of Unmanned Aerial Vehicle Based on Mixed Pixel Decomposition Method
by Mengmeng Du, Minzan Li, Noboru Noguchi, Jiangtao Ji and Mengchao (George) Ye
Drones 2023, 7(1), 43; https://doi.org/10.3390/drones7010043 - 7 Jan 2023
Cited by 9 | Viewed by 3137
Abstract
FVC (fractional vegetation cover) is highly correlated with wheat plant density in the reviving period, which is an important indicator for conducting variable-rate nitrogenous topdressing. In this study, with the objective of improving inversion accuracy of wheat plant density, an innovative approach of [...] Read more.
FVC (fractional vegetation cover) is highly correlated with wheat plant density in the reviving period, which is an important indicator for conducting variable-rate nitrogenous topdressing. In this study, with the objective of improving inversion accuracy of wheat plant density, an innovative approach of retrieval of FVC values from remote sensing images of a UAV (unmanned aerial vehicle) was proposed based on the mixed pixel decomposition method. Firstly, remote sensing images of an experimental wheat field were acquired by using a DJI Mini UAV and endmembers in the image were identified. Subsequently, a linear unmixing model was used to subdivide mixed pixels into components of vegetation and soil, and an abundance map of vegetation was acquired. Based on the abundance map of vegetation, FVC was calculated. Consequently, a linear regression model between the ground truth data of wheat plant density and FVC was established. The coefficient of determination (R2), RMSE (root mean square error), and RRMSE (Relative-RMSE) of the inversion model were calculated as 0.97, 1.86 plants/m2, and 0.677%, which indicates strong correlation between the FVC of mixed pixel decomposition method and wheat plant density. Therefore, we can conclude that the mixed pixel decomposition model of the remote sensing image of a UAV significantly improved the inversion accuracy of wheat plant density from FVC values, which provides method support and basic data for variable-rate nitrogenous fertilization in the wheat reviving period in the manner of precision agriculture. Full article
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<p>Plots of experimental wheat field.</p>
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<p>Identification of vegetation endmembers (pixels in green color) and soil endmembers (pixels in red color).</p>
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<p>Spectral characteristics of vegetation endmembers (in green color) and soil endmembers (in red color).</p>
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<p>Abundance map of vegetation.</p>
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<p>Bimodal characteristics of the green–red difference index map.</p>
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<p>Image segmentation results:(<b>a</b>) image thresholding method; (<b>b</b>) support vector machine method.</p>
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<p>Wheat plant density inversion models based on FVC values calculated by using different methods. Note: FVC<sub>MPD</sub>, FVC<sub>SVM</sub>, and FVC<sub>IT</sub> indicate the FVC (fractional vegetation cover) calculated by using mixed pixel decomposition, image thresholding, and the SVM method. <span class="html-italic">y<sub>1</sub>, y<sub>2</sub></span>, and <span class="html-italic">y<sub>3</sub></span> indicate the predicted wheat plant density from FVC<sub>MPD</sub>, FVC<sub>SVM</sub>, and FVC<sub>IT</sub>, respectively.</p>
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<p>Residue plots of predicted wheat plant densities by using different inversion models. Note: MPD, SVM, and IT indicate the methods of mixed pixel decomposition, support vector machine, and image thresholding.</p>
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<p>Map of estimated wheat plant density.</p>
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15 pages, 930 KiB  
Article
Distributed Model Predictive Consensus Control of Unmanned Surface Vehicles with Post-Verification
by Weilin Yang, Tianjing Shen, Tinglong Pan, Guanyang Hu and Dezhi Xu
Drones 2023, 7(1), 42; https://doi.org/10.3390/drones7010042 - 6 Jan 2023
Cited by 6 | Viewed by 2196
Abstract
In this paper, the consensus control of unmanned surface vehicles (USVs) is investigated by employing a distributed model predictive control approach. A hierarchical control structure is considered during the controller design, where the upper layer determines the reference signals of USV velocities while [...] Read more.
In this paper, the consensus control of unmanned surface vehicles (USVs) is investigated by employing a distributed model predictive control approach. A hierarchical control structure is considered during the controller design, where the upper layer determines the reference signals of USV velocities while the lower layer optimizes the control inputs of each USV. The main feature of this work is that a post-verification procedure is proposed to address the failure states caused by local errors or cyberattacks. Each USV compares the actual state and the predicted one obtained at the previous moment. This allows the estimation of local perturbations. In addition, the failure state of the USV can also be determined if a preset condition is satisfied, thus forcing a change in the communication topology and avoiding further impact. Simulations show that the proposed method is effective in USV formation control. Compared with the method without post-verification, the proposed approach is more robust when failure states occur. Full article
(This article belongs to the Section Drone Design and Development)
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<p>Illustration of a desired formation motion.</p>
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<p>Control structure.</p>
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<p>Illustration of the upper-layer DMPC algorithm.</p>
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<p>Communication topologies. (<b>a</b>) Topology1 is a normal state. (<b>b</b>,<b>c</b>) Topology2 and Topology3 are failure states and red circles represent the faulty ships.</p>
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<p>Output trajectory.</p>
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<p>Upper−layer error.</p>
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<p>Upper−layer input.</p>
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<p>Lower−layer output.</p>
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<p>Lower−layer input.</p>
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<p>Output trajectory of Algorithm 1.</p>
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<p>Output trajectory of Algorithm 2.</p>
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<p>Output trajectory of Algorithm 3.</p>
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15 pages, 896 KiB  
Article
NOMA and UAV Scheduling for Ultra-Reliable and Low-Latency Communications
by Xiaowu Liu, Xihan Xu and Kan Yu
Drones 2023, 7(1), 41; https://doi.org/10.3390/drones7010041 - 6 Jan 2023
Cited by 3 | Viewed by 2392
Abstract
Ultra-reliable and low-latency communications (uRLLC) has received great attention in the study of wireless communication for it can provide high network performance in terms of reliability and latency. However, the reliability requirements of uRLLC require further investigation due to the inherent openness of [...] Read more.
Ultra-reliable and low-latency communications (uRLLC) has received great attention in the study of wireless communication for it can provide high network performance in terms of reliability and latency. However, the reliability requirements of uRLLC require further investigation due to the inherent openness of the wireless channel. Different from the previous reliable contributions that focused on the retransmission mechanism, in this paper, we consider scenarios with the interference of multiple UAVs. We establish an analytical framework of the packet error rate (PER) for an air-to-ground (A2G) channel. In this framework, the cellular users are allocated to different UAVs according to their minimum path loss with the aim of minimizing the PER. Furthermore, a wireless link scheduling algorithm is proposed to enhance the reliability between the UAV and cellular user. Simulated results show that, under the same power and channel block length level, our proposed non-orthogonal multiple access (NOMA) scheduling scheme has the best performance. Full article
(This article belongs to the Special Issue UAVs Communications for 6G)
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<p>Network model.</p>
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<p>The scheduling performance effects of the number of links.</p>
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<p>The effects of path-loss exponent on scheduling performance.</p>
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<p>SINR threshold and link-size effects on scheduling performance.</p>
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<p>The overall error probability <math display="inline"><semantics> <msub> <mi>ε</mi> <mrow> <mi>BS</mi> <mo>,</mo> <msub> <mi>CU</mi> <mn>1</mn> </msub> </mrow> </msub> </semantics></math> versus the power, when M = 100 symbols.</p>
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<p>The overall error probability <math display="inline"><semantics> <msub> <mi>ε</mi> <mrow> <mi>BS</mi> <mo>,</mo> <msub> <mi>CU</mi> <mn>1</mn> </msub> </mrow> </msub> </semantics></math> versus the channel blocklength, when P = 40 mW.</p>
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20 pages, 5814 KiB  
Article
Attitude Determination for Unmanned Cooperative Navigation Swarm Based on Multivectors in Covisibility Graph
by Yilin Liu, Ruochen Liu, Ruihang Yu, Zhiming Xiong, Yan Guo, Shaokun Cai and Pengfei Jiang
Drones 2023, 7(1), 40; https://doi.org/10.3390/drones7010040 - 6 Jan 2023
Cited by 4 | Viewed by 2366
Abstract
To reduce costs, an unmanned swarm usually consists of nodes with high-accuracy navigation sensors (HAN) and nodes with low-accuracy navigation sensors (LAN). Transmitting and fusing the navigation information obtained by HANs enables LANs to improve their positioning accuracy, which in general is called [...] Read more.
To reduce costs, an unmanned swarm usually consists of nodes with high-accuracy navigation sensors (HAN) and nodes with low-accuracy navigation sensors (LAN). Transmitting and fusing the navigation information obtained by HANs enables LANs to improve their positioning accuracy, which in general is called cooperative navigation (CN). In this method, the accuracy of relative observation between platforms in the swarm have dramatic effects on the positioning results. In the popular research, constructing constraints in three-dimensional (3D) frame could only optimize the position and velocity of LANs but neglected the attitude estimation so LANs cannot maintain a high attitude accuracy when utilizing navigation information obtained by sensors installed during maneuvers over long periods. Considering the performance of the inertial measurement unit (IMU) and other common sensors, this paper advances a new method to estimate the attitude of LANs in a swarm. Because the small unmanned nodes are strictly limited by relevant practical engineering problems such as size, weight and power, the method proposed could compensate for the attitude error caused by strapdown gyroscopic drift, which only use visual vectors built by the targets detected by cameras with the function of range finding. In our method, the coordinates of targets are mainly given by the You Only Look Once (YOLO) algorithm, then the visual vectors are built by connecting the targets in the covisibility graph of the nodes in the swarm. The attitude transformation matrices between each camera frame are calculated using the multivector attitude determination algorithm. Finally, we design an information filter (IF) to determine the attitude of LANs based on the observation of HANs. Considering the problem of positioning reference, the field test was conducted in the open air and we chose to use two-wheeled robots and one UAV to carry out the experiment. The results show that the relative attitude error between nodes is less than 4 degrees using the visual vector. After filtering, the attitude divergence of LANs’ installed low precision IMU can be effectively constrained, and the high-precision attitude estimation in an unmanned CN swarm can be realized. Full article
(This article belongs to the Special Issue Drone-Based Information Fusion to Improve Autonomous Navigation)
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<p>Method to compensate for the error of attitude for LANs in CN swarm.</p>
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<p>Method to construct a visual vector.</p>
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<p>Construct visual vectors by targets in the overlap (covisibility graph).</p>
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<p>The trajectory of the unmanned vehicle in the Frame-N.</p>
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<p>The yaw of the platform: (<b>a</b>) The true value of yaw; (<b>b</b>) The yaw of the platform after compensation.</p>
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<p>The error of attitude angle of the platform after compensation: (<b>a</b>) yaw; (<b>b</b>) roll and pitch.</p>
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<p>Experimental platforms and major sensors installed. (<b>a</b>) Node 1: HAN; (<b>b</b>) Node 2: LAN; (<b>c</b>) Node 3: drone; (<b>d</b>) High-precision INS.</p>
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<p>Full view of the experimental site.</p>
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<p>Target recognition by YOLO and coordinate calculation.</p>
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<p>The observation result of HAN: (<b>a</b>) Roll, pitch and yaw obtained by visual vectors; (<b>b</b>) Yaw of the HAN observed by IMU output and by visual vectors during the movement.</p>
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<p>Error of attitude angle observed by visual vectors, which act as the observation in the IF.</p>
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<p>Error of attitude angle observed after the compensation of IF.</p>
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26 pages, 8913 KiB  
Article
Small Fixed-Wing UAV Radar Cross-Section Signature Investigation and Detection and Classification of Distance Estimation Using Realistic Parameters of a Commercial Anti-Drone System
by Ioannis K. Kapoulas, Antonios Hatziefremidis, A. K. Baldoukas, Evangelos S. Valamontes and J. C. Statharas
Drones 2023, 7(1), 39; https://doi.org/10.3390/drones7010039 - 6 Jan 2023
Cited by 11 | Viewed by 11171
Abstract
Various types of small drones constitute a modern threat for infrastructure and hardware, as well as for humans; thus, special-purpose radar has been developed in the last years in order to identify such drones. When studying the radar signatures, we observed that the [...] Read more.
Various types of small drones constitute a modern threat for infrastructure and hardware, as well as for humans; thus, special-purpose radar has been developed in the last years in order to identify such drones. When studying the radar signatures, we observed that the majority of the scientific studies refer to multirotor aerial vehicles; there is a significant gap regarding small, fixed-wing Unmanned Aerial Vehicles (UAVs). Driven by the security principle, we conducted a series of Radar Cross Section (RCS) simulations on the Euclid fixed-wing UAV, which has a wingspan of 2 m and is being developed by our University. The purpose of this study is to partially fill the gap that exists regarding the RCS signatures and identification distances of fixed-wing UAVs of the same wingspan as the Euclid. The software used for the simulations was POFACETS (v.4.1). Two different scenarios were carried out. In scenario A, the RCS of the Euclid fixed-wing UAV, with a 2 m wingspan, was analytically studied. Robin radar systems’ Elvira Anti Drone System is the simulated radar, operating at 8.7 to 9.65 GHz; θ angle is set at 85° for this scenario. Scenario B studies the Euclid RCS within the broader 3 to 16 Ghz spectrum at the same θ = 85° angle. The results indicated that the Euclid UAV presents a mean RCS value (σ ¯) of −17.62 dBsm for scenario A, and a mean RCS value (σ ¯) of −22.77 dBsm for scenario B. These values are much smaller than the values of a typical commercial quadcopter, such as DJI Inspire 1, which presents −9.75 dBsm and −13.92 dBsm for the same exact scenarios, respectively. As calculated in the study, the Euclid UAV can penetrate up to a distance of 1784 m close to the Elvira Anti Drone System, while the DJI Inspire 1 will be detected at 2768 m. This finding is of great importance, as the obviously larger fixed-wing Euclid UAV will be detected about one kilometer closer to the anti-drone system. Full article
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<p>A typical identification process of a radar system for drones.</p>
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<p>Elvira Anti Drone System’s main lobe for the DJI Inspire 1 detection case. All lengths are in meters.</p>
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<p>Elvira Anti Drone System’s main lobe for the DJI Inspire 1 classification case. All lengths are in meters.</p>
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<p>RCS measurements of some common commercial multicopters.</p>
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<p>The two targets analyzed in this research and the overall validation methodology for the Euclid results.</p>
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<p>θ angle clarification in POFACETS software.</p>
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<p>Proper placing of a target in POFACETS software.</p>
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<p>Check for normal for the Euclid UAV.</p>
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<p>Graphical representation of the simulation parameters for the two scenarios.</p>
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<p>DJI Inspire 1 RCS results for θ = 85°, φ = 0°–360° and f = 8.7 Ghz.</p>
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<p>Euclid UAV RCS results for θ = 85°, φ = 0°–360° and f = 8.7 Ghz.</p>
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<p>DJI Inspire 1 RCS results for θ = 85°, φ = 0°–360° and f = 9.175 Ghz.</p>
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<p>Euclid UAV RCS results for θ = 85°, φ = 0°–360° and f = 9.175 Ghz.</p>
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<p>DJI Inspire 1 RCS results for θ = 85°, φ = 0°–360° and f = 9.65 Ghz.</p>
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<p>Euclid UAV RCS results for θ = 85°, φ = 0°–360° and f = 9.65 Ghz.</p>
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<p>DJI Inspire 1 RCS signature for θ = 85° and φ = 45° within the 3 to 16 Ghz spectrum.</p>
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<p>Euclid UAV RCS signature for θ = 85° and φ = 45° within the 3 to 16 Ghz spectrum.</p>
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24 pages, 26715 KiB  
Article
A New Image Encryption Algorithm Based on DNA State Machine for UAV Data Encryption
by Moatsum Alawida, Je Sen Teh and Wafa’ Hamdan Alshoura
Drones 2023, 7(1), 38; https://doi.org/10.3390/drones7010038 - 5 Jan 2023
Cited by 35 | Viewed by 4567
Abstract
Drone-based surveillance has become widespread due to its flexibility and ability to access hazardous areas, particularly in industrial complexes. As digital camera capabilities improve, more visual information can be stored in high-resolution images, resulting in larger image sizes. Therefore, algorithms for encrypting digital [...] Read more.
Drone-based surveillance has become widespread due to its flexibility and ability to access hazardous areas, particularly in industrial complexes. As digital camera capabilities improve, more visual information can be stored in high-resolution images, resulting in larger image sizes. Therefore, algorithms for encrypting digital images sent from drones must be both secure and highly efficient. This paper presents a novel algorithm based on DNA computing and a finite state machine (FSM). DNA and FSM are combined to design a key schedule with high flexibility and statistical randomness. The image encryption algorithm is designed to achieve both confusion and diffusion properties simultaneously. The DNA bases themselves provide diffusion, while the random integers extracted from the DNA bases contribute to confusion. The proposed algorithm underwent a thorough set of statistical analyses to demonstrate its security. Experimental findings show that the proposed algorithm can resist many well-known attacks and encrypt large-sized images at a higher throughput compared to other algorithms. High experimental results for the proposed algorithm include correlation coefficients of 0.0001 and Shannon entropy of 7.999. Overall, the proposed image encryption algorithm meets the requirements for use in drone-based surveillance applications. Full article
(This article belongs to the Special Issue Advances in Drone Communications, State-of-the-Art and Architectures)
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<p>Secure surveillance drone framework.</p>
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<p>FSM with two states and its state transition rule.</p>
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<p>FSM of four states and its state transition rule.</p>
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<p>Key sensitivity of DNA-FSM.</p>
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<p>Histogram of 128 DNA bases after five iterations.</p>
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<p>Fuzzy entropy analysis of DNA-FSM.</p>
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<p>Correlation values of 50 round keys.</p>
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<p>Overview of encryption steps.</p>
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<p>Round key generation.</p>
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<p>Four processes of the proposed image encryption scheme: (<b>a</b>) Oil rig (1) image size <math display="inline"><semantics> <mrow> <mn>7998</mn> <mo>×</mo> <mn>5332</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math>, (<b>b</b>) encrypted image, (<b>c</b>) decrypted image. (<b>d</b>) Oil rig (2) image size <math display="inline"><semantics> <mrow> <mn>6431</mn> <mo>×</mo> <mn>4272</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math>, (<b>e</b>) encrypted image, (<b>f</b>) decrypted image. (<b>g</b>) Lena image size <math display="inline"><semantics> <mrow> <mn>512</mn> <mo>×</mo> <mn>512</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math>, (<b>h</b>) encrypted Lena image, (<b>i</b>) decrypted Lena image.</p>
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<p>Drone DJI Mavic Air 2.</p>
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<p>Histogram of different images.</p>
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<p>CC of Oil rig (1) image for red channel. (<b>a</b>) Horizontal cipherimage, (<b>b</b>) horizontal plainimage, (<b>c</b>) vertical cipherimage, (<b>d</b>) vertical plainimage, (<b>e</b>) diagonal plainimage, (<b>f</b>) diagonal cipherimage.</p>
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<p>Encryption results of black and white images.</p>
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<p>Drone images captured in various locations.</p>
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19 pages, 2909 KiB  
Article
Repurposing Existing Infrastructure for Urban Air Mobility: A Scenario Analysis in Southern California
by Xiangyu Li
Drones 2023, 7(1), 37; https://doi.org/10.3390/drones7010037 - 5 Jan 2023
Cited by 7 | Viewed by 4693
Abstract
The deployment of urban air mobility in built-out metropolitan regions is constrained by infrastructure opportunities, land use, and airspace zoning designations. Meanwhile, the availability and spatial distribution of infrastructure opportunities influence the travel demand that can be potentially captured by UAM services. The [...] Read more.
The deployment of urban air mobility in built-out metropolitan regions is constrained by infrastructure opportunities, land use, and airspace zoning designations. Meanwhile, the availability and spatial distribution of infrastructure opportunities influence the travel demand that can be potentially captured by UAM services. The purpose of this study is to provide an initial assessment of the infrastructure opportunities of UAM in southern California with different mixes of spatial constraints, such as noise levels, school buffer zones, and airspace zones. The corresponding travel demand that can be potentially captured under each scenario is estimated with a home–workplace trip table. The results of the analyses indicate that supply-side infrastructure opportunities, such as heliports and elevated parking structures, are widely available to accommodate the regional deployment of UAM services. However, current spatial constraints can significantly limit the scope of vertiport location choices. Furthermore, the low-income population, blue-collar workers, and young people live farther away from supply-side opportunities than the general population. Moreover, this study proposes a network of UAM based on the top home-based and workplace-based stations for long-distance trips. Full article
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<p>Examples of UAM landing sites. (<b>a</b>) UAM landing site design by repurposing underutilized parking structure rooftops [<a href="#B29-drones-07-00037" class="html-bibr">29</a>]. (<b>b</b>) Lilium UAM vertiport in Lake Nona, Florida [<a href="#B30-drones-07-00037" class="html-bibr">30</a>]. (<b>c</b>) Archetypes of UAM infrastructure [<a href="#B31-drones-07-00037" class="html-bibr">31</a>].</p>
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<p>Study area.</p>
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<p>Scenario analysis framework.</p>
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<p>(<b>a</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the best scenario. (<b>b</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the median scenario. (<b>c</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the strictest scenario.</p>
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<p>(<b>a</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the best scenario. (<b>b</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the median scenario. (<b>c</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the strictest scenario.</p>
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<p>(<b>a</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the best scenario. (<b>b</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the median scenario. (<b>c</b>) Spatial distribution of supply-side opportunities and demand-side coverage by user groups based on the strictest scenario.</p>
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<p>A proposed UAM network based on the top home-based and workplace-based stations for residents having commuting trips over 10 miles and living within 10 min driving distance of vertiports.</p>
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19 pages, 3065 KiB  
Article
Visual-Inertial Odometry Using High Flying Altitude Drone Datasets
by Anand George, Niko Koivumäki, Teemu Hakala, Juha Suomalainen and Eija Honkavaara
Drones 2023, 7(1), 36; https://doi.org/10.3390/drones7010036 - 4 Jan 2023
Cited by 14 | Viewed by 9623
Abstract
Positioning of unoccupied aerial systems (UAS, drones) is predominantly based on Global Navigation Satellite Systems (GNSS). Due to potential signal disruptions, redundant positioning systems are needed for reliable operation. The objective of this study was to implement and assess a redundant positioning system [...] Read more.
Positioning of unoccupied aerial systems (UAS, drones) is predominantly based on Global Navigation Satellite Systems (GNSS). Due to potential signal disruptions, redundant positioning systems are needed for reliable operation. The objective of this study was to implement and assess a redundant positioning system for high flying altitude drone operation based on visual-inertial odometry (VIO). A new sensor suite with stereo cameras and an inertial measurement unit (IMU) was developed, and a state-of-the-art VIO algorithm, VINS-Fusion, was used for localisation. Empirical testing of the system was carried out at flying altitudes of 40–100 m, which cover the common flight altitude range of outdoor drone operations. The performance of various implementations was studied, including stereo-visual-odometry (stereo-VO), monocular-visual-inertial-odometry (mono-VIO) and stereo-visual-inertial-odometry (stereo-VIO). The stereo-VIO provided the best results; the flight altitude of 40–60 m was the most optimal for the stereo baseline of 30 cm. The best positioning accuracy was 2.186 m for a 800 m-long trajectory. The performance of the stereo-VO degraded with the increasing flight altitude due to the degrading base-to-height ratio. The mono-VIO provided acceptable results, although it did not reach the performance level of the stereo-VIO. This work presented new hardware and research results on localisation algorithms for high flying altitude drones that are of great importance since the use of autonomous drones and beyond visual line-of-sight flying are increasing and will require redundant positioning solutions that compensate for potential disruptions in GNSS positioning. The data collected in this study are published for analysis and further studies. Full article
(This article belongs to the Special Issue Resilient UAV Autonomy and Remote Sensing)
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<p>Pipeline of VINS-Fusion. Adapted from [<a href="#B20-drones-07-00036" class="html-bibr">20</a>].</p>
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<p>Stereo camera and IMU setup connected to the Intel NUC mini computer.</p>
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<p>Sensor suite and the mini computer mounted on the drone.</p>
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<p>The area above which the datasets were collected. This image was reconstructed using the images from the 60 m, 2 m/s dataset in Agisoft Metashape software. The flight path is marked in the image.</p>
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<p>Sample images from collected datasets. Images in each dataset has different illumination due to different lighting conditions during data collection (<b>a</b>) Dataset 1—normal exposure. (<b>b</b>) Dataset 2—overexposed. (<b>c</b>) Dataset 3—underexposed. (<b>d</b>) Dataset 4—underexposed.</p>
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<p>Trajectory estimation by VINS-Fusion plotted along with the ground truth for different altitudes at a speed of 3 m/s. (<b>a</b>) Stereo visual odometry estimation. (<b>b</b>) Mono visual-inertial odometry estimation.</p>
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<p>Scale errors of estimations at flying altitude 60 m and speed 4 m/s. (<b>a</b>) stereo-VO. (<b>b</b>) mono-VIO. (<b>c</b>) stereo-VIO.</p>
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<p>Stereo visual inertial odometry estimation by VINS-Fusion plotted along with the ground truth for different altitudes at a speed of 4 m/s.</p>
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<p>Absolute rotation errors at flying speed 2 m/s. (<b>a</b>) 40 m flying altitude (<b>b</b>) 60 m flying altitude.</p>
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22 pages, 8198 KiB  
Article
Software Aging Effects on Kubernetes in Container Orchestration Systems for Digital Twin Cloud Infrastructures of Urban Air Mobility
by Jackson Costa, Rubens Matos, Jean Araujo, Jueying Li, Eunmi Choi, Tuan Anh Nguyen, Jae-Woo Lee and Dugki Min
Drones 2023, 7(1), 35; https://doi.org/10.3390/drones7010035 - 3 Jan 2023
Cited by 12 | Viewed by 4325
Abstract
It is necessary to develop a vehicle digital twin (DT) for urban air mobility (UAM) that uses an accurate, physics-based emulator to model the statics and dynamics of a vehicle. This is because the use of digital twins in the operation and control [...] Read more.
It is necessary to develop a vehicle digital twin (DT) for urban air mobility (UAM) that uses an accurate, physics-based emulator to model the statics and dynamics of a vehicle. This is because the use of digital twins in the operation and control of UAM vehicles is essential for the UAM operational digital twin infrastructure (UAM-ODT). There are several issues that need to be addressed in this process: (i) the lack of digital twin engines for the digitalization (twinization) of the dynamics and control of UAM vehicles at the core of UAM-ODT systems; (ii) the lack of back-end system engineering in the development of UAM vehicle DTs; and (iii) the lack of fault-tolerant mechanisms for the DT cloud back-end system to run uninterrupted operations 24/7. On the other hand, software aging and rejuvenation are becoming increasingly important in a variety of computing scenarios as the demand for reliable and available services increases. With the increasing use of containerized systems, there is also a need for an orchestrator to support easy management and reduce operational costs. In this paper, an operational digital twin (ODT) of a typical urban air mobility (UAM) infrastructure is developed on a private cloud system based on Kubernetes using a proposed cloud-in-the-loop simulation approach. To ensure the ODT can provide uninterrupted operational control and services in UAM around the clock, we propose a methodology for investigating software aging in Kubernetes-based containerized clouds. We evaluate the behavior of Kubernetes software using the Nginx and K3S tools while they manage pods in an accelerated lifetime experiment. We continuously execute operations for creating and terminating pods, allowing us to observe the utilization of computing resources (e.g., CPU, memory, and I/O), the performance of the Nginx and K3S environments, and the response time of an application hosted in those environments. In some conditions and for specific metrics, such as virtual memory usage, we observed the effects of software aging, including a memory leak that is not fully cleared when the cluster is stopped. These issues could lead to system performance degradation and eventually compromise the reliability and availability of the system when it crashes due to memory space exhaustion or full utilization of swap space on the hard disk. This study helps with the deployment and maintenance of virtualized environments from the standpoint of system dependability in digital twin computing infrastructures where a large number of services are running under strict continuity requirements. Full article
(This article belongs to the Special Issue Urban Air Mobility (UAM))
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<p>Operational Digital Twin for Urban Air Mobility (UAM-ODT).</p>
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<p>A digital replica of UAM vehicle in UAM-ODT infrastructure.</p>
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<p>A visualization of UAM-ODT infrastructure. (The figures are excerpts from a video at <a href="https://blog.naver.com/yy8661" target="_blank">https://blog.naver.com/yy8661</a> provided by Hyeon Jun Lee, Konkuk Aerospace Design-Trustworthiness Institute, Konkuk University, Seoul, Republic of Korea (<a href="mailto:rain9138@gmail.com">rain9138@gmail.com</a>)).</p>
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<p>Cloud in the loop simulation framework.</p>
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<p>Cloud provisioning hardware system architecture.</p>
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<p>Virtual cluster image provisioning technology.</p>
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<p>Methodology of the software aging measurement and assessment in <tt>Kubernetes</tt> environment.</p>
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<p>Diagram for cycles of operations performed by the experiment script.</p>
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<p>Cluster and Client Interaction Overview.</p>
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<p><tt>CPU</tt> utilization in <tt>Minikube</tt>.</p>
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<p><tt>CPU</tt> utilization on <tt>K3S</tt>.</p>
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<p>Disk-related metrics in <tt>Minikube</tt>.</p>
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<p>Disk usage in <tt>K3S</tt>.</p>
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<p>Memory consumption in <tt>Minikube</tt>.</p>
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<p>Memory consumption on <tt>K3S</tt>.</p>
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