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Search Results (2,221)

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Keywords = computer-aided design

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40 pages, 6767 KiB  
Review
Modeling, Design, and Optimization of Loop Heat Pipes
by Yihang Zhao, Mingshan Wei and Dan Dan
Energies 2024, 17(16), 3971; https://doi.org/10.3390/en17163971 (registering DOI) - 10 Aug 2024
Viewed by 194
Abstract
Thermal management technology based on loop heat pipes (LHPs) has broad application prospects in heat transfer control for aerospace and new energy vehicles. LHPs offer excellent heat transfer performance, reliability, and flexibility, making them suitable for high-heat flux density, high-power heat dissipation, and [...] Read more.
Thermal management technology based on loop heat pipes (LHPs) has broad application prospects in heat transfer control for aerospace and new energy vehicles. LHPs offer excellent heat transfer performance, reliability, and flexibility, making them suitable for high-heat flux density, high-power heat dissipation, and complex thermal management scenarios. However, due to limitations in heat source temperature and heat transfer power range, LHP-based thermal management systems still face challenges, especially in thermohydraulic modeling, component design, and optimization. Steady-state models improve computational efficiency and accuracy, while transient models capture dynamic behavior under various conditions, aiding performance evaluation during start-up and non-steady-state scenarios. Designs for single/multi-evaporators, compensation chambers, and wick materials are also reviewed. Single-evaporator designs offer compact and efficient start-up, while multi-evaporator designs handle complex thermal environments with multiple heat sources. Innovations in wick materials, such as porous metals, composites, and 3D printing, enhance capillary driving force and heat transfer performance. A comprehensive summary of working fluid selection criteria is conducted, and the effects of selecting organic, inorganic, and nanofluid working fluids on the performance of LHPs are evaluated. The selection process should consider thermodynamic properties, safety, and environmental friendliness to ensure optimal performance. Additionally, the mechanism and optimization methods of the start-up behavior, temperature oscillation, and non-condensable gas on the operating characteristics of LHPs were summarized. Optimizing vapor/liquid distribution, heat load, and sink temperature enhances start-up efficiency and minimizes temperature overshoot. Improved capillary structures and working fluids reduce temperature oscillations. Addressing non-condensable gases with materials like titanium and thermoelectric coolers ensures long-term stability and reliability. This review comprehensively discusses the development trends and prospects of LHP technology, aiming to guide the design and optimization of LHP. Full article
13 pages, 2670 KiB  
Review
Advances in Regenerative and Reconstructive Medicine in the Prevention and Treatment of Bone Infections
by Leticia Ramos Dantas, Gabriel Burato Ortis, Paula Hansen Suss and Felipe Francisco Tuon
Biology 2024, 13(8), 605; https://doi.org/10.3390/biology13080605 (registering DOI) - 10 Aug 2024
Viewed by 198
Abstract
Reconstructive and regenerative medicine are critical disciplines dedicated to restoring tissues and organs affected by injury, disease, or congenital anomalies. These fields rely on biomaterials like synthetic polymers, metals, ceramics, and biological tissues to create substitutes that integrate seamlessly with the body. Personalized [...] Read more.
Reconstructive and regenerative medicine are critical disciplines dedicated to restoring tissues and organs affected by injury, disease, or congenital anomalies. These fields rely on biomaterials like synthetic polymers, metals, ceramics, and biological tissues to create substitutes that integrate seamlessly with the body. Personalized implants and prosthetics, designed using advanced imaging and computer-assisted techniques, ensure optimal functionality and fit. Regenerative medicine focuses on stimulating natural healing mechanisms through cellular therapies and biomaterial scaffolds, enhancing tissue regeneration. In bone repair, addressing defects requires advanced solutions such as bone grafts, essential in medical and dental practices worldwide. Bovine bone scaffolds offer advantages over autogenous grafts, reducing surgical risks and costs. Incorporating antimicrobial properties into bone substitutes, particularly with metals like zinc, copper, and silver, shows promise in preventing infections associated with graft procedures. Silver nanoparticles exhibit robust antimicrobial efficacy, while zinc nanoparticles aid in infection prevention and support bone healing; 3D printing technology facilitates the production of customized implants and scaffolds, revolutionizing treatment approaches across medical disciplines. In this review, we discuss the primary biomaterials and their association with antimicrobial agents. Full article
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<p>A diagram demonstrating multiple options for doping bone grafts or polymers for 3D printing using metal nanoparticles or antibiotics in bone reconstruction.</p>
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<p>Silver nanoparticles on bone surface used for orthopedic graft.</p>
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<p>Antibiotic-impregnated PLA models with <span class="html-italic">Staphylococcus aureus</span> test.</p>
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<p>Implants with PLA impregnated with antibiotics tested during surgery for hip replacement.</p>
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27 pages, 8168 KiB  
Review
Affordances of Technology for Sustainability-Oriented K–12 Informal Engineering Education
by Mobina Beheshti, Sheikh Ahmad Shah, Helen Zhang, Michael Barnett and Avneet Hira
Sustainability 2024, 16(16), 6719; https://doi.org/10.3390/su16166719 - 6 Aug 2024
Viewed by 546
Abstract
The need for sustainability-oriented K–12 engineering education that expands beyond the classroom and the increased accessibility of educational technologies create an opportunity for examining the affordances of educational technologies in low-stakes informal engineering education settings. In this paper, we share our experiences of [...] Read more.
The need for sustainability-oriented K–12 engineering education that expands beyond the classroom and the increased accessibility of educational technologies create an opportunity for examining the affordances of educational technologies in low-stakes informal engineering education settings. In this paper, we share our experiences of using novel technologies to develop sustainability-oriented mental models in K–12 informal engineering education. Through the use of technologies including Augmented Reality (AR), Virtual Reality (VR), Minecraft video games, Tinkercad (browser-based application for computer-aided design (CAD)), and physical computing, we have designed and tested approaches to introduce students to engineering design and engineering habits of mind with an overarching theme of developing sustainability-oriented mental models among K–12 youth in informal engineering education spaces. In this paper, we share our approaches, and lessons learned, and outline directions for future research. Full article
(This article belongs to the Special Issue Advances in Engineering Education and Sustainable Development)
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<p>Affordances of different technologies for sustainability-oriented engineering education.</p>
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<p>CoSpaces Edu environment.</p>
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<p>MERGE Cube.</p>
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<p>Sample sustainable city design.</p>
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<p>Point system instruction [<a href="#B70-sustainability-16-06719" class="html-bibr">70</a>].</p>
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<p>Sample sustainable city design with coded items using CoBlocks.</p>
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<p>Sustainable City and Farming educational games in Minecraft.</p>
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<p>Sample farm design.</p>
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<p>The Tinkercad environment.</p>
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<p>The activity of sustainable city design.</p>
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<p>Sample sustainable city design by a student.</p>
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<p>Physical computing.</p>
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26 pages, 72430 KiB  
Article
Interactive Mesh Sculpting with Arbitrary Topologies in Head-Mounted VR Environments
by Xiaoqiang Zhu and Yifei Yang
Mathematics 2024, 12(15), 2428; https://doi.org/10.3390/math12152428 - 5 Aug 2024
Viewed by 417
Abstract
Shape modeling is a dynamic area in computer graphics with significant applications in computer-aided design, animation, architecture, and entertainment. Virtual sculpting, a key paradigm in free-form modeling, has traditionally been performed on desktop computers where users manipulate meshes with controllers and view the [...] Read more.
Shape modeling is a dynamic area in computer graphics with significant applications in computer-aided design, animation, architecture, and entertainment. Virtual sculpting, a key paradigm in free-form modeling, has traditionally been performed on desktop computers where users manipulate meshes with controllers and view the models on two-dimensional displays. However, the advent of Extended Reality (XR) technology has ushered in immersive interactive experiences, expanding the possibilities for virtual sculpting across various environments. A real-time virtual sculpting system implemented in a Virtual Reality (VR) setting is introduced in this paper, utilizing quasi-uniform meshes as the foundational structure. In our innovative sculpting system, we design an integrated framework encompassing a surface selection algorithm, mesh optimization technique, mesh deformation strategy, and topology fusion methodology, which are all tailored to meet the needs of the sculpting process. The universal, user-friendly sculpting tools designed to support free-form topology are offered in this system, ensuring that the meshes remain watertight, manifold, and free from self-intersections throughout the sculpting process. The models produced are versatile and suitable for use in diverse fields such as gaming, art, and education. Experimental results confirm the system’s real-time performance and universality, highlighting its user-centric design. Full article
(This article belongs to the Section Mathematics and Computer Science)
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<p>Two brush modes. The pink sphere in (<b>a</b>) is a spherical brush with its points selection strategy based on the Euclidean distance. The pink ray in (<b>b</b>) is a ray-shaped brush with its points selection strategy based on the geodesic distance. These brushes are oriented toward the negative direction of the Z-axis. Additionally, the green ray points toward the positive direction of the Y-axis, and the red ray points toward the positive direction of the X-axis.</p>
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<p>The process of dividing the octree structure and the schematic diagram of its structure.</p>
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<p>The geodesic distance and Euclidean distance between two points on the surface.</p>
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<p>Points selection scenarios for two brush modes. (<b>a</b>,<b>d</b>) is the origin dog model; the area in the red wireframe is the section we intend to sculpt. (<b>b</b>,<b>c</b>), respectively, correspond to the sculpting outcomes of the spherical brush and the ray-shaped brush on simple surfaces. (<b>e</b>,<b>f</b>), on the other hand, represent the sculpting results of the spherical brush and the ray-shaped brush in more complex area.</p>
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<p>Edge split. As the pink edge splits into two equal segments, the four created green edges are smaller than the largest initial edge.</p>
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<p>Edge collapse. The orange edge shorter than <span class="html-italic">d</span> will be collapsed, and the four pink edges will become two green edges.</p>
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<p>The illegal collapse operation. The collapse of the orange edge results in the original two adjacent green triangles becoming self-intersecting.</p>
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<p>Operation menu for switching between sculpting modes. (<b>a</b>) Pull. (<b>b</b>) Push. (<b>c</b>) Flatten. (<b>d</b>) Smooth.</p>
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<p>Pull and Push operations on spherical shape. (<b>a</b>) Original shape. (<b>b</b>) Pull (+) and Push (−).</p>
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<p>Position update in Laplacian smoothing. The gray points are the adjacent vertices of the yellow point, and the yellow point will be relocated to the position of the pink point.</p>
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<p>Different operations on the same part of the mesh. (<b>a</b>) shows the result obtained by the Pull operation, and (<b>b</b>) shows the result of the Push operation. While these two operations may appear similar to the union and difference operations in Boolean operations, the deformations are gradual processes that can be halted at any time to obtain intermediate results, unlike Boolean operations which directly yield final outcomes. (<b>c</b>) represents the result of the Flatten operation, and (<b>d</b>) shows the result of the Smooth operation.</p>
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<p>Topology fusion induced during the mesh deformation. (<b>a</b>) is the mesh before topology fusion, and (<b>c</b>) is the corresponding wireframe. (<b>b</b>) is the mesh before topology fusion, and (<b>d</b>) is the corresponding wireframe.</p>
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<p>Merge the neighborhoods of two non-adjacent vertices if the distance between them is less than the threshold <math display="inline"><semantics> <msub> <mi>d</mi> <mrow> <mi>t</mi> <mi>h</mi> <mi>i</mi> <mi>c</mi> <mi>k</mi> <mi>n</mi> <mi>e</mi> <mi>s</mi> <mi>s</mi> </mrow> </msub> </semantics></math>.</p>
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<p>The interface of two controllers. (<b>a</b>) is the left-hand controller operation interface, and (<b>b</b>) is the right-hand controller operation interface. (<b>c</b>,<b>d</b>) denote the left-hand and right-hand touchpad partitions, respectively.</p>
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<p>The case of mesh with and without the topological auto-fusion mechanism. (<b>a</b>) is the case where intersections appear as can be seen from the inside of the mesh without the topology auto-fusion mechanism. We can see that the outer mesh appears misaligned in (<b>b</b>), and the zoomed-in case can be seen in (<b>c</b>). Correspondingly, (<b>d</b>) corresponds to the case of the interior of the mesh with the topological auto-fusion mechanism. As can be seen in (<b>e</b>), the outer mesh maintains good properties, and the zoomed-in case can be seen in (<b>f</b>).</p>
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<p>Illegal and legal model adding operations. (<b>a</b>) presents the illegal operation, and the resulting broken mesh is shown in (<b>b</b>). (<b>c</b>) shows the legal operation, and it does not affect the subsequent sculpting as shown in (<b>d</b>).</p>
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<p>Scores of the two compared systems in six evaluation dimensions, including system ease of use, functional completeness, modeling robustness, detail implementation, topological freedom, and overall evaluation.</p>
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<p>Models created by novice users based on existing models. (<b>a</b>,<b>b</b>) are origin models. (<b>c</b>) is a rabbit with horns based on (<b>a</b>), and (<b>d</b>) is a dog with wings and collar based on (<b>b</b>).</p>
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<p>Models created by novice users from scratch. (<b>a</b>) is a monster head, and (<b>b</b>) is a fantasy arthropod.</p>
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<p>Sculpted colored models. (<b>a</b>) is a bunch of grapes, and (<b>b</b>) is a magic broom.</p>
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<p>Sculpting sequence of a vase model. (<b>a</b>) is the basic shape of the model. A ring is created with holes as shown in (<b>b</b>), and the connection between the ring and the model’s body is established in (<b>c</b>). In (<b>d</b>), the handles are added, and then we add the undulating motifs around the surface in (<b>e</b>). Finally, we sculpt some symmetrical textures for the visual impact as shown in (<b>f</b>).</p>
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<p>Three-dimensional (3D) printing model entities. (<b>a</b>) is the entity of vase, and (<b>b</b>) is the entity of fantasy arthropod.</p>
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12 pages, 2869 KiB  
Article
Toward Automated Structural Design for Controlled Vibration Characteristics Using Topology Optimization and Computer Vision in Space Missions
by Musaddiq Al Ali, Masatoshi Shimoda and Marc Naguib
Appl. Sci. 2024, 14(15), 6786; https://doi.org/10.3390/app14156786 - 3 Aug 2024
Viewed by 429
Abstract
This study explores the integration of computer vision with topology optimization for additive manufacturing, with a focus on maximizing eigenfrequency in a design domain. Utilizing custom-developed photogrammetry software, high-resolution images are processed to generate detailed 3D models, which are subsequently converted to STL [...] Read more.
This study explores the integration of computer vision with topology optimization for additive manufacturing, with a focus on maximizing eigenfrequency in a design domain. Utilizing custom-developed photogrammetry software, high-resolution images are processed to generate detailed 3D models, which are subsequently converted to STL files with precision. Adaptive meshing in COMSOL 5.3 Multiphysics, controlled through a MATLAB 2023 API, ensures optimal mesh resolution. Prioritizing resource conservation in extraterrestrial environments, the original volume is reduced by 50% while preserving structural integrity. The design domain undergoes rigorous topology optimization in MATLAB, supported by COMSOL’s advanced FEM simulation. The optimized design exhibits a 57% performance improvement and a 50% weight reduction, maintaining the desired vibration characteristics, validating the efficacy of the modifications. Moreover, the case with an eccentric mass shows a significant 64% increase in eigenfrequency. Full article
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<p>Three-dimensional object simulation using photogrammetry.</p>
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<p>The design domain for a pillar.</p>
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<p>The computer vision-based design domain includes the following configurations: (<b>a</b>) a pillar with a central mass, and (<b>b</b>) a pillar with an eccentric mass, where the center of gravity is positioned on the left side of the top surface.</p>
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<p>Topology optimization designs of central mass shown from multiple perspectives: (<b>a</b>) isometric projection of the design, (<b>b</b>) middle-section view, (<b>c</b>) front view, (<b>d</b>) rear view, (<b>e</b>) top view, and (<b>f</b>) side view.</p>
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<p>Eigen frequency history of the pillar design domain with central mass.</p>
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<p>Topology optimization designs of eccentric mass shown from multiple perspectives: (<b>a</b>) isometric projection of the design, (<b>b</b>) middle-section view, (<b>c</b>) front view, (<b>d</b>) rear view, (<b>e</b>) top view, and (<b>f</b>) side view.</p>
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<p>Eigen frequency history of the pillar design domain with eccentric mass.</p>
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29 pages, 6373 KiB  
Article
Semiactive Car-Seat System for Rear-End Collisions
by Ali Gunes Kaya and Selcuk Himmetoglu
Machines 2024, 12(8), 530; https://doi.org/10.3390/machines12080530 - 3 Aug 2024
Viewed by 288
Abstract
This study proposes and simulates a smart system that can be used in production car seats to decrease whiplash risk in rear-end crashes. A sliding seat incorporating a semiactively controlled magnetorheological (MR) damper model positioned under the seat-pan is simulated with a validated [...] Read more.
This study proposes and simulates a smart system that can be used in production car seats to decrease whiplash risk in rear-end crashes. A sliding seat incorporating a semiactively controlled magnetorheological (MR) damper model positioned under the seat-pan is simulated with a validated biofidelic human body model. Since this is the first study that demonstrates a computer controlled anti-whiplash car seat system to the best of the authors’ knowledge, a benchmark analysis is carried out to compare the proposed semiactive seat with a state-of-the-art passive anti-whiplash car seat using 23 different crash pulses, including the moderate and high severity crash pulses within the European New Car Assessment Program (EuroNCAP) whiplash risk assessment framework. The proposed semiactive design outperforms the passive seat design by further reducing the values of the critical EuroNCAP whiplash criteria, such as NIC and Nkm, together with the loads acting on the upper neck. The semiactive seat lowers the upper-neck shear force by an amount of 4 kg and 7 kg while lessening the NIC by 10% and 21% and Nkm by 9% and 56% for the EuroNCAP crash pulses, having a delta-V of 16 km/h and 24 km/h, respectively. The findings presented in this paper can aid in the design of car seats to further mitigate whiplash risk in rear-end crashes. Full article
(This article belongs to the Special Issue Recent Analysis and Research in the Field of Vehicle Traffic Safety)
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<p>Semiactive whiplash mitigation system architecture, including labelled data flow through the interface between MATLAB SIMULINK and VISUAL NASTRAN. Grey and green colored curved boxes represent System Controllers, blue colored curved box represents MR damper controller. Effective mass adaptation is highlighted with pink colored curved box in the System Controller block.</p>
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<p>Mechanical properties of (<b>a</b>) Recliner and (<b>b</b>) Kelvin element in the passive anti-whiplash car seat.</p>
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<p>Sketch of the Modified Bouc-Wen MR damper model.</p>
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<p>Control flow chart for the Adaptive Kinematics Profile Controller.</p>
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<p>Block diagram for the system sub-controller with effective mass.</p>
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<p>Block diagram for the damper controller.</p>
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<p>The crash pulses applied in the simulations. The name of the crash pulse is given on the upper right-hand side, whereas the corresponding crash pulse number is given on the lower right-hand side of the sub-plots.</p>
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<p>Cumulative performance of the semiactive and passive seats against all of the crash pulses considered (pulse #1 to pulse #23) based on the EuroNCAP whiplash assessment criteria. Results are presented as percentages of the capping limit of the corresponding criterion stated in <a href="#machines-12-00530-t005" class="html-table">Table 5</a>. Median performance of the seats for each criterion is sketched with a vertical thick line inside the rectangular boxes. Left and right edges of these boxes represent the lower and upper quartiles respectively. Endpoints of the dotted lines correspond to the lowest and highest values obtained for all crash pulses.</p>
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<p>Upper neck shear force for the crash pulse SN16.</p>
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<p>Upper neck shear force for the crash pulse TR24.</p>
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<p>Velocity profiles after crash pulse SN16 is applied on the car floor.</p>
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<p>Velocity profiles after crash pulse TR24 is applied on the car floor.</p>
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<p>Control voltage (<span class="html-italic">u</span>), actual voltage <math display="inline"><semantics> <mrow> <mi>V</mi> </mrow> </semantics></math>, and the applied actual force after crash pulse SN16 is applied on the car floor.</p>
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<p>Control voltage (<span class="html-italic">u</span>), actual voltage <math display="inline"><semantics> <mrow> <mi>V</mi> </mrow> </semantics></math>, and the applied actual force after crash pulse TR24 is applied on the car floor.</p>
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<p>The motion of the semiactive seat and occupant for the crash pulse TR24.</p>
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<p>The motion of the passive seat and occupant for the crash pulse TR24.</p>
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18 pages, 1584 KiB  
Article
Computer Simulation-Based Multi-Objective Optimisation of Additively Manufactured Cranial Implants
by Brian J. Moya, Marcelino Rivas, Ramón Quiza and J. Paulo Davim
Technologies 2024, 12(8), 125; https://doi.org/10.3390/technologies12080125 - 2 Aug 2024
Viewed by 476
Abstract
Driven by the growing interest of the scientific community and the proliferation of research in this field, cranial implants have seen significant advancements in recent years regarding design techniques, structural optimisation, appropriate material selection and fixation system method. Custom implants not only enhance [...] Read more.
Driven by the growing interest of the scientific community and the proliferation of research in this field, cranial implants have seen significant advancements in recent years regarding design techniques, structural optimisation, appropriate material selection and fixation system method. Custom implants not only enhance aesthetics and functionality, but are also crucial for achieving proper biological integration and optimal blood irrigation, critical aspects in bone regeneration and tissue health. This research aims to optimize the properties of implants designed from triply periodic minimal surface structures. The gyroid architecture is employed for its balance between mechanical and biological properties. Experimental samples were designed varying three parameters of the surface model: cell size, isovalue and shape factor. Computational simulation tools were used for determining the relationship between those parameters and the response variables: the surface area, permeability, porosity and Young modulus. These tools include computer aided design, finite element method and computational fluid dynamics. With the simulated values, the corresponding regression models were fitted. Using the NSGA-II, a multi-objective optimisation was carried out, finding the Pareto set which includes surface area and permeability as targets, and fulfil the constraints related with the porosity and Young modulus. From these non-dominated solutions, the most convenient for a given application was chosen, and an optimal implant was designed, from a patient computed tomography scan. An implant prototype was additively manufactured for validating the proposed approach. Full article
(This article belongs to the Section Manufacturing Technology)
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Graphical abstract
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<p>Constructed scaffolds keeping a constant block size.</p>
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<p>Finite element analysis setup.</p>
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<p>CFD analysis setup.</p>
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<p>Example of the deformation and stress profiles obtained by FEM-based simulation.</p>
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<p>Example of the pressure profiles obtained by CFD-based simulation.</p>
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<p>Graphical representation of the regression models.</p>
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<p>Outcomes of the optimisation.</p>
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<p>Cranial implant example.</p>
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<p>Additively manufactured implant.</p>
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17 pages, 2265 KiB  
Review
Frequency-Modulated Continuous-Wave Radar Perspectives on Unmanned Aerial Vehicle Detection and Classification: A Primer for Researchers with Comprehensive Machine Learning Review and Emphasis on Full-Wave Electromagnetic Computer-Aided Design Tools
by Ahmed N. Sayed, Omar M. Ramahi and George Shaker
Drones 2024, 8(8), 370; https://doi.org/10.3390/drones8080370 - 2 Aug 2024
Viewed by 542
Abstract
Unmanned Aerial Vehicles (UAVs) represent a rapidly increasing technology with profound implications for various domains, including surveillance, security, and commercial applications. Among the number of detection and classification methodologies, radar technology stands as a cornerstone due to its versatility and reliability. This paper [...] Read more.
Unmanned Aerial Vehicles (UAVs) represent a rapidly increasing technology with profound implications for various domains, including surveillance, security, and commercial applications. Among the number of detection and classification methodologies, radar technology stands as a cornerstone due to its versatility and reliability. This paper presents a comprehensive primer written specifically for researchers starting on investigations into UAV detection and classification, with a distinct emphasis on the integration of full-wave electromagnetic computer-aided design (EM CAD) tools. Commencing with an elucidation of radar’s pivotal role within the UAV detection paradigm, this primer systematically navigates through fundamental Frequency-Modulated Continuous-Wave (FMCW) radar principles, elucidating their intricate interplay with UAV characteristics and signatures. Methodologies pertaining to signal processing, detection, and tracking are examined, with particular emphasis placed on the pivotal role of full-wave EM CAD tools in system design and optimization. Through an exposition of relevant case studies and applications, this paper underscores successful implementations of radar-based UAV detection and classification systems while elucidating encountered challenges and insights obtained. Anticipating future trajectories, the paper contemplates emerging trends and potential research directions, accentuating the indispensable nature of full-wave EM CAD tools in propelling radar techniques forward. In essence, this primer serves as an indispensable roadmap, empowering researchers to navigate the complex terrain of radar-based UAV detection and classification, thereby fostering advancements in aerial surveillance and security systems. Full article
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<p>Procedural steps involved in radar-based UAV detection and classification.</p>
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<p>Range-Doppler maps generation for FMCW radars.</p>
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<p>(<b>a</b>) DJI S900 standard [<a href="#B57-drones-08-00370" class="html-bibr">57</a>]. (<b>b</b>) Its Ansys HFSS model. (<b>c</b>) Three-time stamps showing the rotation of its blades separated by 1 ms.</p>
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13 pages, 5037 KiB  
Case Report
Three Dimensional-Printed Gingivectomy and Tooth Reduction Guides Prior Ceramic Restorations: A Case Report
by Carlos A. Jurado, Jose Villalobos-Tinoco, Mark A. Lackey, Silvia Rojas-Rueda, Manuel Robles and Akimasa Tsujimoto
Dent. J. 2024, 12(8), 245; https://doi.org/10.3390/dj12080245 - 1 Aug 2024
Viewed by 295
Abstract
Computer-aided design and computer-aided manufacturing (CAD/CAM) dentistry have significantly changed workflows in recent years. Restorations and devices can now be digitally designed and 3D-printed for dental care purposes. This clinical case report provides straightforward protocols for the digital design and 3D manufacture of [...] Read more.
Computer-aided design and computer-aided manufacturing (CAD/CAM) dentistry have significantly changed workflows in recent years. Restorations and devices can now be digitally designed and 3D-printed for dental care purposes. This clinical case report provides straightforward protocols for the digital design and 3D manufacture of gingivectomy and tooth preparation guides. These types of guides improved the gingival architecture of the anterior teeth and provided controllable tooth preparations prior to labial ceramic veneers. Thoughtful clinical evaluation started with listening to the patient’s chief complaint and extra- and intra-oral evaluations. Then a digital wax-up was performed, followed by an intra-oral mock-up, to evaluate the shape of the proposed restorations. After patient acceptance, the clinical procedure started with the gingivectomy and tooth preparation. Hand-crafted porcelain veneers were bonded under rubber dam isolation to avoid any contamination and maximize the bonding protocol. The esthetic and functional demands were fully satisfied. Predictable outcomes can be obtained whenever a meticulous evaluation and execution of all the steps are performed. Three dimensional printing technology allows the fabrication of devices such as gingivectomy and tooth reduction guides that help accomplish the desired results. Full article
(This article belongs to the Special Issue 3D Printing and Restorative Dentistry)
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<p>Initial extra-oral situation. (<b>A</b>) Face smiling, (<b>B</b>) close-up of the smile, and (<b>C</b>) patient disliking to smile.</p>
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<p>Initial intra-oral situation. (<b>A</b>) Frontal view, (<b>B</b>) right side view and (<b>C</b>) left side view.</p>
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<p>Digital design of the 3D-printed gingivectomy and tooth reduction guide; (<b>A</b>) initial situation; (<b>B</b>) digital wax-up; (<b>C</b>) gingivectomy guide design over the digital wax-up; (<b>D</b>) gingivectomy guide alone frontal view; (<b>E</b>) cross-shaped tooth reduction guide over the digital wax-up; and (<b>F</b>) cross-shaped guide alone frontal view.</p>
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<p>Gingivectomy procedure. (<b>A</b>) Placement of the printed guide, (<b>B</b>) gingivectomy procedure, (<b>C</b>) measuring with periodontal probe, and (<b>D</b>) result of the gingivectomy frontal view.</p>
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<p>Tooth preparation with reduction guide. (<b>A</b>) Placement of the tooth reduction guide, (<b>B</b>) tooth preparation with the reduction guide in place, (<b>C</b>) measuring with periodontal probe at the gingival third and (<b>D</b>) at the incisal edge.</p>
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<p>Finishing final tooth preparations. (<b>A</b>) Refining with fine diamond bur, (<b>B</b>) polishing with fine grift disc, (<b>C</b>) polishing with super fine grift disc, and (<b>D</b>) final polished preparations.</p>
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<p>Final impression. (<b>A</b>) lateral view of final preps, (<b>B</b>) second cord packing process, (<b>C</b>) second cord packed, and (<b>D</b>) final impression.</p>
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<p>Fabrication of ceramic veneers. (<b>A</b>) Placement of body porcelain, (<b>B</b>) placement of translucent porcelain, (<b>C</b>) placement of porcelain with different shades, (<b>D</b>) final restorations right side view, (<b>E</b>) final restorations left side view, and (<b>F</b>) final restorations frontal view.</p>
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<p>Bonding of the final restorations. (<b>A</b>) Rubber dam placement, (<b>B</b>) bonding of veneers for central incisors, (<b>C</b>) removing excess with blade, (<b>D</b>) final restoration’s lateral view, and (<b>E</b>) final restoration’s frontal view.</p>
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<p>Intra-oral view of final restorations. (<b>A</b>) Frontal view (<b>B</b>) right side view, and (<b>C</b>) left side view.</p>
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<p>Extra-oral view of final restorations. (<b>A</b>) Full-face smile, (<b>B</b>) smile and (<b>C</b>) patient liking to smile.</p>
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<p>Three-year follow-up. (<b>A</b>) Face smiling, (<b>B</b>) smile, and (<b>C</b>) intra-oral frontal view.</p>
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<p>Flowchart describing the clinical workflow implemented for this dental treatment.</p>
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21 pages, 6137 KiB  
Article
Development of Ballistic Protection Soft Panels According to Regulatory Documents
by Dana Barkane, Marianna Grecka, Dana Almli, Viktorija Mecnika and Inese Ziemele
Designs 2024, 8(4), 76; https://doi.org/10.3390/designs8040076 - 31 Jul 2024
Viewed by 396
Abstract
The development of Ballistic Protection Vests (BPVs) has gained significant attention, particularly focusing on the design of Ballistic Protection Soft Panels (BPSPs), which are crucial to the overall size and configuration of these vests. Despite their critical role, there is a noticeable lack [...] Read more.
The development of Ballistic Protection Vests (BPVs) has gained significant attention, particularly focusing on the design of Ballistic Protection Soft Panels (BPSPs), which are crucial to the overall size and configuration of these vests. Despite their critical role, there is a noticeable lack of a standardized design method for surface area patterns of BPSPs in the existing literature. The findings indicate that the National Institute of Justice (NIJ) standard 0101.06 Ballistic Test Templates (BTTs) are only partially applicable to the design of BPSP patterns. While the NIJ standard 0101.06 provides a useful framework, it requires adaptation to meet the specific needs of regional body types and the practicalities of BPV manufacturing. This research aims to address this gap by assessing the suitability of NIJ BTTs for the design of BPSPs and BPVs and to develop a standardized pattern design methodology along with a method for calculating the surface area of the soft amour prior to its creation. Results have to be achieved ready for the production of BPSP patterns tailored to the body types of regional soldiers while adhering to relevant standards and soldier’s physical comfort, thereby saving time and resources for manufacturers and researchers. In this study, we evaluated the applicability of the NIJ standard 0101.06 BTT for configuring these templates into the cutting patterns of BPSPs. To achieve this, patterns for BPSPs were designed and the feasibility of using NIJ BTTs for their configuration was analyzed. The research process involved a comprehensive literature review, an analysis of the dimensions of existing BPV soft panels, and a comparison with NIJ standard 0101.06 BTT. The design and scaling of the panel patterns were executed using computer-aided design (CAD) systems and evaluated through both physical fitting on mannequins and virtual fitting using the Clo3D program. The developed pattern-making methodology includes size specifications tailored to regional covers, incorporating a coefficient K identified to calculate the BPSP surface area prior to design. This approach not only ensures better fitting for the physical comfort and protection of soldiers but also saves time and resources in the manufacturing process of BPSPs. The proposed design methodology offers a significant step forward in standardizing BPSP patterns, promising enhanced protection and efficiency in BPV manufacturing. Full article
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<p>BPV design criteria and tasks (author’s image).</p>
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<p>NIJ C3 test template [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] for soft panels with the main dimensions marked, where A is the panel’s width, B is the panel’s height, C is the panel’s upper part width, and D is the panel’s upper part height. The blue line indicates the test template’s minimal parameters, while the red line indicates the maximum.</p>
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<p>Comparison of the width (A) of the BPSP samples with the corresponding NIJ standard [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] test templates.</p>
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<p>Comparison of the height B for BPSP samples with the NIJ-C3 and NIJ-C4 test templates [<a href="#B6-designs-08-00076" class="html-bibr">6</a>]: (<b>a</b>) outer garment and (<b>b</b>) undergarment.</p>
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<p>Comparison of the upper part width (C) of BPSP samples with the NIJ-C3 and NIJ-C4 test template [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] limits.</p>
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<p>Allowed obliquity (E) of the BPSP upper part width (C) of NIJ standard test templates [<a href="#B6-designs-08-00076" class="html-bibr">6</a>].</p>
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<p>Comparison of “Company B” LL-size undergarment BPV soft panels’ configuration (black line) with the NIJ-C3 test template [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] configuration (blue lines).</p>
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<p>National sizes coverage for BPVs.</p>
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<p>An increase in the circumference of layers of clothing worn under the outer garment BPV at chest and waist level.</p>
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<p>Version 1 of the back panel pattern of M regular size (developed in CAD Grafis).</p>
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<p>Version 2 comparison between the M and L regular size BPSP configuration with the corresponding NIJ-C3 test template [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] (developed in CAD Grafis).</p>
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<p>Comparison of Version 3 M regular-sized soft panel configuration with the equivalent NIJ-C3 test template [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] (developed in CAD Grafis).</p>
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<p>Fitting of the size M regular BPSP mock-up on an appropriately sized mannequin.</p>
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<p>Displacement of the front and back BPSP patterns in the sideline for the M regular size (developed in CAD Grafis).</p>
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<p>Virtual fitting of the BPSP patterns for M regular size in the Clo3D program.</p>
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<p>Outer garment BPV’s first fitting for size M regular.</p>
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<p>The issues created with the soft panel’s dimensions (marked red) if body height gradation is not performed.</p>
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<p>Obtaining the coefficient K for the calculation of the surface area for the designed BPSP patterns.</p>
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<p>Calculation of the coefficient K for the NIJ-C3 [<a href="#B6-designs-08-00076" class="html-bibr">6</a>] test template’s surface area.</p>
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<p>Design algorithm of BPSP patterns.</p>
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20 pages, 7109 KiB  
Article
Time-Series Feature Extraction by Return Map Analysis and Its Application to Bearing-Fault Detection
by Veronika Ponomareva, Olga Druzhina, Oleg Logunov, Anna Rudnitskaya, Yulia Bobrova, Valery Andreev and Timur Karimov
Big Data Cogn. Comput. 2024, 8(8), 82; https://doi.org/10.3390/bdcc8080082 - 29 Jul 2024
Viewed by 298
Abstract
Developing new features for time-series characterization is a current challenge in data science and machine learning. In this paper, we propose a new metric based on a simple and efficient algorithm, namely, the return map. The return map analysis is well established in [...] Read more.
Developing new features for time-series characterization is a current challenge in data science and machine learning. In this paper, we propose a new metric based on a simple and efficient algorithm, namely, the return map. The return map analysis is well established in the field of non-linear dynamics, in particular, for fitting the parameters of a chaotic system from a waveform, or to attack a chaotic communication channel. We show that our metrics work well for both non-linear dynamics and time-series feature extraction problems in the field of machine learning. In an experiment aiming to classify vibration signals of normal and damaged bearings, we compare our method with two other methods that reported to have excellent accuracy, based on entropy and statistical feature distribution, respectively. We show that our method achieves higher accuracy with almost the lowest time costs, which was confirmed in experiments with two different datasets containing three main classes of bearings: normal, with inner race faults, and with outer race faults, having different damage origins and recorded in various conditions. In particular, for the dataset supplied by Case Western Reserve University, our method reached an accuracy of 100% at signals of 5000 sample points length, with a total time of 0.4 s required for feature estimation, while the entropy-based method reached an accuracy of 95% with a time of 100 s, and a statistical feature distribution method reached an accuracy of 93% with a total time of 1.9 s. Results show that the developed method is better suited to real-time bearing condition monitoring applications than most of the methods reported to date. Full article
(This article belongs to the Special Issue Industrial Data Mining and Machine Learning Applications)
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<p>Time series with marked peaks and valleys, and distances which are used to find amplitude and amplitude-phase return maps.</p>
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<p>Visualization of distance calculation between the RMA points in the return map plane.</p>
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<p>Unified system attractors with different <math display="inline"><semantics> <mi>α</mi> </semantics></math> values.</p>
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<p>Gokyildirim system attractors with different parameter <span class="html-italic">a</span> values.</p>
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<p>Flowchart of the entire analytic process, including proposed (right branch, colored blue) and competitive algorithms.</p>
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<p>Schematic of an electric motor with a bearing affected by inner and outer race faults and a diagnostic accelerometer.</p>
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<p>Bifurcation diagram, LLE, and dRMA features plotted for Unified system.</p>
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<p>Bifurcation diagram, LLE, and dRMA features plotted for Gokyildirim system.</p>
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<p>The distance-RMA algorithm results with added noise for the Unified system. Basic <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.575</mn> </mrow> </semantics></math>.</p>
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<p>The distance-RMA algorithm results with added noise for the Gokyildirim system. Basic <math display="inline"><semantics> <mrow> <mi>a</mi> <mo>=</mo> <mn>0.088</mn> </mrow> </semantics></math>.</p>
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<p>EMD of healthy bearing vibration signal.</p>
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<p>Distribution of data samples in dRMA features space.</p>
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<p>Averaged values of dRMA features for bearings of different classes. Normal—healthy bearings, OR—outer race faults, IR—inner race faults.</p>
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<p>Time and accuracy of bearing-fault classification with the compared methods. SampEn and ApEn stand for methods based on sample and approximate entropy, DWT and GGD are the methods based on discrete wavelet decomposition with subsequent approximation of wavelet coefficient histograms using a generalized Gaussian distribution, and EMD and dRMA are the proposed methods based on empirical mode decomposition and subsequent characterization of intrinsic mode functions with the dRMA algorithm.</p>
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<p>Time and accuracy of bearing-fault classification with the compared methods. SampEn and ApEn stand for methods based on sample and approximate entropy, DWT and GGD are the methods based on discrete wavelet decomposition with subsequent approximation of wavelet coefficient histograms using a generalized Gaussian distribution, and EMD and dRMA are the proposed methods based on empirical mode decomposition and subsequent characterization of intrinsic mode functions with the dRMA algorithm.</p>
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14 pages, 6659 KiB  
Article
Studying Biomolecular Protein Complexes via Origami and 3D-Printed Models
by Hay Azulay, Inbar Benyunes, Gershon Elber and Nir Qvit
Int. J. Mol. Sci. 2024, 25(15), 8271; https://doi.org/10.3390/ijms25158271 - 29 Jul 2024
Viewed by 405
Abstract
Living organisms are constructed from proteins that assemble into biomolecular complexes, each with a unique shape and function. Our knowledge about the structure–activity relationship of these complexes is still limited, mainly because of their small size, complex structure, fast processes, and changing environment. [...] Read more.
Living organisms are constructed from proteins that assemble into biomolecular complexes, each with a unique shape and function. Our knowledge about the structure–activity relationship of these complexes is still limited, mainly because of their small size, complex structure, fast processes, and changing environment. Furthermore, the constraints of current microscopic tools and the difficulty in applying molecular dynamic simulations to capture the dynamic response of biomolecular complexes and long-term phenomena call for new supplementary tools and approaches that can help bridge this gap. In this paper, we present an approach to comparing biomolecular and origami hierarchical structures and apply it to comparing bacterial microcompartments (BMCs) with spiral-based origami models. Our first analysis compares proteins that assemble the BMC with an origami model called “flasher”, which is the unit cell of an assembled origami model. Then, the BMC structure is compared with the assembled origami model and based on the similarity, a physical scaled-up origami model, which is analogous to the BMC, is constructed. The origami model is translated into a computer-aided design model and manufactured via 3D-printing technology. Finite element analysis and physical experiments of the origami model and 3D-printed parts reveal trends in the mechanical response of the icosahedron, which is constructed from tiled-chiral elements. The chiral elements rotate as the icosahedron expands and we deduce that it allows the BMC to open gates for transmembrane passage of materials. Full article
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Graphical abstract

Graphical abstract
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<p>BMC proteins and origami models: (<b>A</b>) BMC structure (PDB: 6MZX), (<b>B</b>) top view cartoon model of a BMC-H protein, with cartoon marks for α-helices (red coils) and for β-strands (yellow flat shapes). (PBD: 3GFH). (<b>C</b>) origami flasher model with six flaps, (<b>D</b>) top view cartoon model of a BMC-P protein (PDB: 4N8F), (<b>E</b>) origami flasher model with five flaps, and (<b>F</b>) top view cartoon model of the BMC-T<sup>D</sup> protein (PDB: 2A1B).</p>
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<p>Dome top changes as the structure rotates: (<b>A</b>) top open, and (<b>B</b>) top closes after rotation.</p>
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<p>Folding an origami icosahedron: (<b>A</b>) Folding triangular planes on a sheet into an icosahedron (the figure is reprinted and revised from reference [<a href="#B27-ijms-25-08271" class="html-bibr">27</a>] under the terms of the Creative Commons Attribution 4.0 International License), (<b>B</b>) A tessellation of six-flap spiral folded flashers, and (<b>C</b>) An icosahedron that is constructed from assembly of origami flashers.</p>
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<p>The BMC and the origami tessellation model: (<b>A</b>) The BMC structure with the hexameric BMC-H (blue), which is the main unit cell that constructs the panels, the hexameric BMC-T<sup>D</sup> (green), which is located at the center of the planes and the pentameric BMC-P (yellow), which is located at the vertices (the figure is reprinted and revised from reference [<a href="#B17-ijms-25-08271" class="html-bibr">17</a>] under the terms of the Creative Commons Attribution 4.0 International License), and (<b>B</b>) an origami-based compartment, with a hexameric flasher as the main unit cell, and a pentameric flasher at the corners.</p>
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<p>Dynamic experiment with icosahedron origami models—inflating the structure with air. The folding lines of a flasher that are marked in red show how it changes as the model expands.</p>
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<p>FEA results—deformation of (<b>A</b>) an icosahedron with elements with six ligaments that tile the planes, and elements with five ligaments at the corners. (<b>B</b>) Sphere with elements with six ligaments that tile the planes and elements with five ligaments at the corners. (<b>C</b>) FEA results—deformation of the elements due to internal pressure.</p>
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<p>From an icosahedron to a sphere—(left column)—structures with different curvatures, from an icosahedron (<b>A1</b>) to a sphere (<b>C1</b>). In the FEA simulations, a vertex tile is fixed, and internal pressure is applied to the tiles. The FEA deformation results of the models are shown in the center and right columns (<b>A2</b>–<b>C3</b>). The deformation of the silhouette is marked by a red line that follows the plane and the corners. The color map represents the relative deformation of the elements due to the applied force, where green represents deformation and blue no deformation.</p>
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<p>Parts with chiral elements that were 3D-printed with Stratasys<sup>®</sup> J55: (<b>A</b>) Sphere. (<b>B</b>) Icosahedron.</p>
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<p>An experiment with a 3D-printed icosahedron. A chiral element and part of the silhouette are marked in red to demonstrate how the structure changes during expansion (from left to right).</p>
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<p>The hierarchical bottom-up arrangement of a layered bio-structure, from building blocks to function.</p>
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<p>A workflow of the approach to comparing bimolecular complexes and origami models.</p>
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19 pages, 5731 KiB  
Article
MSCAC: A Multi-Scale Swin–CNN Framework for Progressive Remote Sensing Scene Classification
by A. Arun Solomon and S. Akila Agnes
Geographies 2024, 4(3), 462-480; https://doi.org/10.3390/geographies4030025 - 29 Jul 2024
Viewed by 272
Abstract
Recent advancements in deep learning have significantly improved the performance of remote sensing scene classification, a critical task in remote sensing applications. This study presents a new aerial scene classification model, the Multi-Scale Swin–CNN Aerial Classifier (MSCAC), which employs the Swin Transformer, an [...] Read more.
Recent advancements in deep learning have significantly improved the performance of remote sensing scene classification, a critical task in remote sensing applications. This study presents a new aerial scene classification model, the Multi-Scale Swin–CNN Aerial Classifier (MSCAC), which employs the Swin Transformer, an advanced architecture that has demonstrated exceptional performance in a range of computer vision applications. The Swin Transformer leverages shifted window mechanisms to efficiently model long-range dependencies and local features in images, making it particularly suitable for the complex and varied textures in aerial imagery. The model is designed to capture intricate spatial hierarchies and diverse scene characteristics at multiple scales. A framework is developed that integrates the Swin Transformer with a multi-scale strategy, enabling the extraction of robust features from aerial images of different resolutions and contexts. This approach allows the model to effectively learn from both global structures and fine-grained details, which is crucial for accurate scene classification. The model’s performance is evaluated on several benchmark datasets, including UC-Merced, WHU-RS19, RSSCN7, and AID, where it demonstrates a superior or comparable accuracy to state-of-the-art models. The MSCAC model’s adaptability to varying amounts of training data and its ability to improve with increased data make it a promising tool for real-world remote sensing applications. This study highlights the potential of integrating advanced deep-learning architectures like the Swin Transformer into aerial scene classification, paving the way for more sophisticated and accurate remote sensing systems. The findings suggest that the proposed model has significant potential for various remote sensing applications, including land cover mapping, urban planning, and environmental monitoring. Full article
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<p>Overview of the proposed framework for remote sensing scene classification.</p>
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<p>Architecture of the Multi-Scale Swin–CNN Aerial Classifier for scene classification.</p>
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<p>Flowchart for Multi-Head Self-Attention (MHSA) block mechanism.</p>
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<p>Representative samples from the UC-Merced Land Use Dataset, illustrate the dataset’s diversity.</p>
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<p>Confusion matrix obtained by the proposed MSCAC model on the UC-Merced dataset.</p>
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<p>Representative samples from the WHU-RS19 dataset.</p>
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<p>Confusion matrix obtained by proposed MSCAC model on the WHU-RS19 dataset.</p>
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<p>Sample images from the RSSCN7 dataset.</p>
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<p>Confusion matrix obtained by the proposed MSCAC model on the RSSCN7 dataset.</p>
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<p>Sample images from the AID dataset.</p>
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<p>Confusion matrix obtained by proposed MSCAC model on the AID dataset.</p>
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26 pages, 2617 KiB  
Article
Fixed-Wing UAV Pose Estimation Using a Self-Organizing Map and Deep Learning
by Nuno Pessanha Santos
Robotics 2024, 13(8), 114; https://doi.org/10.3390/robotics13080114 - 27 Jul 2024
Viewed by 411
Abstract
In many Unmanned Aerial Vehicle (UAV) operations, accurately estimating the UAV’s position and orientation over time is crucial for controlling its trajectory. This is especially important when considering the landing maneuver, where a ground-based camera system can estimate the UAV’s 3D position and [...] Read more.
In many Unmanned Aerial Vehicle (UAV) operations, accurately estimating the UAV’s position and orientation over time is crucial for controlling its trajectory. This is especially important when considering the landing maneuver, where a ground-based camera system can estimate the UAV’s 3D position and orientation. A Red, Green, and Blue (RGB) ground-based monocular approach can be used for this purpose, allowing for more complex algorithms and higher processing power. The proposed method uses a hybrid Artificial Neural Network (ANN) model, incorporating a Kohonen Neural Network (KNN) or Self-Organizing Map (SOM) to identify feature points representing a cluster obtained from a binary image containing the UAV. A Deep Neural Network (DNN) architecture is then used to estimate the actual UAV pose based on a single frame, including translation and orientation. Utilizing the UAV Computer-Aided Design (CAD) model, the network structure can be easily trained using a synthetic dataset, and then fine-tuning can be done to perform transfer learning to deal with real data. The experimental results demonstrate that the system achieves high accuracy, characterized by low errors in UAV pose estimation. This implementation paves the way for automating operational tasks like autonomous landing, which is especially hazardous and prone to failure. Full article
(This article belongs to the Special Issue UAV Systems and Swarm Robotics)
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<p>Standard mission profile (<b>left</b>) and typical trajectory state machine (<b>right</b>) [<a href="#B24-robotics-13-00114" class="html-bibr">24</a>].</p>
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<p>Simplified system architecture.</p>
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<p>System architecture with a representation of the used variables.</p>
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<p>Used UAV CAD model illustration.</p>
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<p>Camera and UAV reference frames.</p>
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<p>Example of generated UAV binary images.</p>
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<p>Example I of obtained clustering maps using SOM after 250 iterations: <math display="inline"><semantics> <mrow> <mn>2</mn> <mo>×</mo> <mn>2</mn> </mrow> </semantics></math> grid (<b>left</b>), <math display="inline"><semantics> <mrow> <mn>3</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math> grid (<b>center</b>) and <math display="inline"><semantics> <mrow> <mn>4</mn> <mo>×</mo> <mn>4</mn> </mrow> </semantics></math> grid (<b>right</b>). The dots represent the neuron positions according to their weights <math display="inline"><semantics> <mi mathvariant="bold">W</mi> </semantics></math> (output space).</p>
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<p>Example II of obtained clustering maps using SOM after 250 iterations: <math display="inline"><semantics> <mrow> <mn>2</mn> <mo>×</mo> <mn>2</mn> </mrow> </semantics></math> grid (<b>left</b>), <math display="inline"><semantics> <mrow> <mn>3</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math> grid (<b>center</b>) and <math display="inline"><semantics> <mrow> <mn>4</mn> <mo>×</mo> <mn>4</mn> </mrow> </semantics></math> grid (<b>right</b>). The dots represent the neuron positions according to their weights <math display="inline"><semantics> <mi mathvariant="bold">W</mi> </semantics></math> (output space).</p>
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<p>Example of the obtained sample hits (<b>left</b>), where the numbers indicate the number of input vectors, and neighbor distances (<b>right</b>), where the red lines depict the connections between neighboring neurons for the <math display="inline"><semantics> <mrow> <mn>3</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math> grid shown in <a href="#robotics-13-00114-f007" class="html-fig">Figure 7</a> center. The colors indicate the distances, with darker colors representing larger distances and lighter colors representing smaller distances.</p>
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<p>Used translation estimation DNN structure.</p>
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<p>Used orientation estimation DNN structure.</p>
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<p>Example of a similar topology shown by a UAV symmetric pose.</p>
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<p>Translation error boxplot in meters.</p>
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<p>Orientation error histogram in degrees.</p>
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<p>Examples of pose estimation using the proposed architecture—Original image (<b>left</b>), SOM output (<b>center</b>), and pose estimation (<b>right</b>). The orientation error for (A3) was 30.6 degrees, for (B3) 3.3 degrees, for (C3) 22.2 degrees, and for (D3) 14.4 degrees.</p>
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<p>Orientation error histogram at 5 m when varying the Gaussian noise SD (degrees).</p>
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<p>Obtained loss during the translation DNN training when removing network layers, as described in <a href="#robotics-13-00114-t007" class="html-table">Table 7</a>.</p>
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<p>Obtained loss during the orientation DNN training when removing network layers, as described in <a href="#robotics-13-00114-t008" class="html-table">Table 8</a>.</p>
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<p>Qualitative analysis example: Real captured frame (<b>left</b>) and BS obtained frame (<b>right</b>).</p>
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<p>Real captured frames obtained clustering maps using SOM with 9 neurons (<math display="inline"><semantics> <mrow> <mn>3</mn> <mo>×</mo> <mn>3</mn> </mrow> </semantics></math> grid) after 250 iterations (<b>left</b>) and obtained estimation pose rendering using the network trained after 50,000 iterations (<b>right</b>).</p>
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15 pages, 3553 KiB  
Article
Business Models Definition for Next-Generation Vision Inspection Systems
by Francesco Lupi, Antonio Maffei and Michele Lanzetta
J. Manuf. Mater. Process. 2024, 8(4), 161; https://doi.org/10.3390/jmmp8040161 - 27 Jul 2024
Viewed by 365
Abstract
Automated industrial Visual Inspection Systems (VIS) are predominantly designed for specific use cases, resulting in constrained adaptability, high setup requirements, substantial capital investments, and significant knowledge barriers. This paper explores the business potential of recent alternative architectures proposed in the literature for the [...] Read more.
Automated industrial Visual Inspection Systems (VIS) are predominantly designed for specific use cases, resulting in constrained adaptability, high setup requirements, substantial capital investments, and significant knowledge barriers. This paper explores the business potential of recent alternative architectures proposed in the literature for the visual inspection of individual products or complex assemblies within highly variable production environments, utilizing next-generation VIS. These advanced VIS exhibit significant technical (hardware and software) enhancements, such as increased flexibility, reconfigurability, Computer Aided Design (CAD)-based integration, self-X capabilities, and autonomy, as well as economic improvements, including cost-effectiveness, non-invasiveness, and plug-and-produce capabilities. The new trends in VIS have the potential to revolutionize business models by enabling as-a-service approaches and facilitating a paradigm shift towards more sustainable manufacturing and human-centric practices. We extend the discussion to examine how these technological innovations, which reduce the need for extensive coding skills and lengthy reconfiguration activities for operators, can be implemented as a shared resource within a circular lifecycle. This analysis includes detailing the underlying business model that supports shared utilization among different stakeholders, promoting a circular economy in manufacturing by leveraging the capabilities of next-generation VIS. Such an approach not only enhances the sustainability of manufacturing processes but also democratizes access to state-of-the-art inspection technologies, thereby expanding the possibilities for autonomous manufacturing ecosystems. Full article
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Figure 1

Figure 1
<p>The main properties and related aspects of next-generation VIS. The dotted arrows highlight how autonomy is enabled by certain aspects inherited from the other properties.</p>
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<p>The schematical representation of the pioneering framework proposing the utilization of CAD information for reconfiguring the ReCo file via user-friendly reconfiguration support system (RSS). Image reprinted from Lupi et al., 2023 [<a href="#B6-jmmp-08-00161" class="html-bibr">6</a>] under CC BY 4.0 license.</p>
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<p>The framework for Autonomous-VIS, highlighted within the light gray dotted box. Input/output is shown by light-dotted arrows, while squared boxes represent activities. Module_1 (yellow box) refers to the initial hardware configuration and calibration, which is performed outside of the inspection loop. Modules_2-5 (green boxes) are part of the inspection loop and are connected to other activities outside the scope of the current study (depicted within boxes). Image reprinted from Lupi et al., 2024 [<a href="#B5-jmmp-08-00161" class="html-bibr">5</a>] under CC BY 4.0 license.</p>
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<p>The final version of the next-generation VIS framework, as reprinted from Lupi et al., 2024 [<a href="#B4-jmmp-08-00161" class="html-bibr">4</a>] under CC BY 4.0 license. The red-dotted area denotes the evolution of the framework previously described in <a href="#jmmp-08-00161-f003" class="html-fig">Figure 3</a>. The green area is the CAD-to-ReCo file pipeline.</p>
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<p>Graphical summary of the methodology used in this work to analyze and synthesize the BMs for the next-generation VIS.</p>
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