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9 pages, 1392 KiB  
Article
Clinical Evaluation of an Electronic Guidance System for Optimizing the Ultrasound Screening for Developmental Hip Dysplasia in Newborns
by Stephan Heisinger, Catharina Chiari, Madeleine Willegger, Reinhard Windhager and Alexander Kolb
J. Clin. Med. 2024, 13(24), 7656; https://doi.org/10.3390/jcm13247656 (registering DOI) - 16 Dec 2024
Abstract
Background: Graf ultrasound screening is considered an established method for early detection of developmental dysplasia of the hip (DDH). Although characterized by a high degree of standardization to allow for good reproducibility of results, examination-related factors may still affect sonographic measurements. The relative [...] Read more.
Background: Graf ultrasound screening is considered an established method for early detection of developmental dysplasia of the hip (DDH). Although characterized by a high degree of standardization to allow for good reproducibility of results, examination-related factors may still affect sonographic measurements. The relative tilt angle between the hip and the probe is a potential pitfall as it significantly influences sonographic measurements and consequently classification of DDH according to Graf. Objectives: Evaluation of an electronic guidance system developed to reduce relative tilt angles and increase reliability and comparability in ultrasound screening of DDH. Materials and Methods: Twenty-five newborns were examined using a prototype guidance system, which tracks the position of the transducer and the pelvis to calculate the relative tilt angles. Two ultrasound images were obtained, one conventionally and the other one using the guidance system. Subsequently, relative roll and pitch angles and sonographic measurements were determined and analyzed. Results: The relative inclination angles in the conventional group ranged from −12.6° to 14.3° (frontal plane) and −23.8° to 32.5° (axial plane). vs. −3.7° to 3.0° and −3.2° to 4.5° in the guidance system group. The variances were significantly lower in the guidance system-assisted group for both planes (p < 0.001 and p < 0.001, respectively). The optimized transducer position showed significant effects and consequently significantly reduced alpha angles were observed (p = 0.001, and p = 0.003). Conclusions: The guidance system allowed a significant reduction in the relative tilt angles, supporting optimal positioning of the transducer, resulting in significant effects on Graf sonographic measurements. This technique shows great potential for enhancing the reproducibility and reliability of ultrasound screening for DDH. Full article
(This article belongs to the Section Orthopedics)
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Figure 1
<p>Illustration of the 3D position sensors: detection of the pelvic position by an epicutaneous sensor placed dorsally over the sacrum (arrowhead) and of the transducer position by a sensor fixed by a 3D printed adapter (thin arrow); (<b>a</b>) starting position: the coordination system is shown at the bottom left (normal vector of the frontal (F), axial (A) and sagittal (S) planes); (<b>b</b>) alignment of transducer and pelvis using the guidance system in the axial and frontal plane: note the tilted pelvic position and the different orientation rotation of the sensors in the sagittal plane.</p>
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<p>Relative roll and pitch angles: (<b>a</b>) conventional group according to Graf’s sonographic criteria [<a href="#B8-jcm-13-07656" class="html-bibr">8</a>], (<b>b</b>) guidance system assisted group in which the developed system was used to optimize relative transducer position in addition to Graf’s criteria [<a href="#B10-jcm-13-07656" class="html-bibr">10</a>].</p>
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<p>Illustration of the effects of correction of tilt angles on alpha angles. The average reduction in the alpha angle is color coded and inserted as a number.</p>
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20 pages, 5882 KiB  
Article
Contact Parameter Calibration for Discrete Element Potato Minituber Seed Simulation
by Kai Chen, Xiang Yin, Wenpeng Ma, Chengqian Jin and Yangyang Liao
Agriculture 2024, 14(12), 2298; https://doi.org/10.3390/agriculture14122298 (registering DOI) - 14 Dec 2024
Viewed by 423
Abstract
The discrete element method (DEM) has been widely applied as a vital auxiliary technique in the design and optimization processes of agricultural equipment, especially for simulating the behavior of granular materials. In this study, the focus is placed on accurately calibrating the simulation [...] Read more.
The discrete element method (DEM) has been widely applied as a vital auxiliary technique in the design and optimization processes of agricultural equipment, especially for simulating the behavior of granular materials. In this study, the focus is placed on accurately calibrating the simulation contact parameters necessary for the V7 potato minituber seed DEM simulation. Firstly, three mechanical tests are conducted, and through a combination of actual tests and simulation tests, the collision recovery coefficient between the seed and rubber material is determined to be 0.469, the static friction coefficient is 0.474, and the rolling friction coefficient is 0.0062. Subsequently, two repose angle tests are carried out by employing the box side plates lifting method and the cylinder lifting method. With the application of the response surface method and a search algorithm based on Matlab 2019, the optimal combination of seed-to-seed contact parameters, namely, the collision recovery coefficient, static friction coefficient, and rolling friction coefficient, is obtained, which are 0.500, 0.476, and 0.043, respectively. Finally, the calibration results are verified by a seed-falling device that combines collisions and accumulation, and it is shown that the relative error between the simulation result and the actual result in the verification test is small. Thus, the calibration results can provide assistance for the design and optimization of the potato minituber seed planter. Full article
(This article belongs to the Section Agricultural Technology)
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<p>Potato minituber seed triaxial size.</p>
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<p>Miniature potato compression test.</p>
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<p>Potato minituber seed simulation model. (<b>a</b>) ellipsoidal model, (<b>b</b>) spherical model.</p>
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<p>Potato minituber seed—rubber plate free fall test. (<b>a</b>) actual test, (<b>b</b>) simulation test.</p>
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<p>Collision recovery coefficient fits the curve.</p>
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<p>Slope sliding test. (<b>a</b>) actual test, (<b>b</b>) simulation test.</p>
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<p>Static friction coefficient fitting curve.</p>
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<p>Inclined plane rolling test. (<b>a</b>) actual test, (<b>b</b>) simulation test.</p>
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<p>Rolling friction coefficient fitting curve.</p>
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<p>Repose angle test device. (<b>a</b>) box side plates lifting method, (<b>b</b>) cylinder lifting method.</p>
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<p>Simulation test of box side plates lifting method. (<b>a</b>) initial state, (<b>b</b>) side plates lifting, (<b>c</b>) test completed.</p>
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<p>Simulation test of cylinder lifting method. (<b>a</b>) initial state, (<b>b</b>) cylinder lifting, (<b>c</b>) test completed.</p>
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<p>Repose angle image processing and angle acquisition. (<b>a</b>) initial image, (<b>b</b>) binarization, (<b>c</b>) boundary extraction, (<b>d</b>) linear fitting.</p>
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<p>3D response surface diagram of interaction term BC. (<b>a</b>) interaction terms AB, (<b>b</b>) interaction terms AC, (<b>c</b>) interaction terms BC.</p>
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<p>Test verification device physical drawing.</p>
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<p>Simulation seed drop test. (<b>a</b>) seeds began to pile up, (<b>b</b>) seed pile is almost complete.</p>
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18 pages, 4484 KiB  
Article
One-Step Fabrication Process of Silica–Titania Superhydrophobic UV-Blocking Thin Coatings onto Polymeric Films
by Sharon Hayne, Naftali Kanovsky and Shlomo Margel
Biomimetics 2024, 9(12), 756; https://doi.org/10.3390/biomimetics9120756 - 12 Dec 2024
Viewed by 398
Abstract
Developing a durable multifunctional superhydrophobic coating on polymeric films that can be industrially scalable is a challenge in the field of surface engineering. This article presents a novel method for a scalable technology using a simple single-step fabrication of a superhydrophobic coating on [...] Read more.
Developing a durable multifunctional superhydrophobic coating on polymeric films that can be industrially scalable is a challenge in the field of surface engineering. This article presents a novel method for a scalable technology using a simple single-step fabrication of a superhydrophobic coating on polymeric films that exhibits excellent water-repelling and UV-blocking properties, along with impressive wear resistance and chemical robustness. A mixture of titanium precursors, tetraethylorthosilicate (TEOS), hydrophobic silanes and silica nano/micro-particles is polymerized directly on a corona-treated polymeric film which reacts with the surface via siloxane chemistry. The mixture is then spread on polymeric films using a Mayer rod, which eliminates the need for expensive equipment or multistep processes. The incorporation of silica nanoparticles along with titanium precursor and TEOS results in the formation of a silica–titania network around the silica nanoparticles. This chemically binds them to the activated surface, forming a unique dual-scale surface morphology depending on the size of the silica nanoparticles used in the coating mixture. The coated films were shown to be superhydrophobic with a high water contact angle of over 180° and a rolling angle of 0°. This is due to the combination of dual-scale micro/nano roughness with fluorinated hydrocarbons that lowered the surface free energy. The coatings exhibited excellent chemical and mechanical durability, as well as UV-blocking capabilities. The results show that the coatings remain superhydrophobic even after a sandpaper abrasion test under a pressure of 2.5 kPa for a distance of 30 m. Full article
(This article belongs to the Special Issue Superhydrophobic Surfaces: Challenges, Solutions and Applications)
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Figure 1
<p>SEM images of coated PP films at several magnifications—coated samples 1–4 with increased magnification of each sample. The scale bars of images (<b>a</b>–<b>c</b>) are 50 µm, 5 µm and 1 µm, respectively.</p>
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<p>SEM image high magnification of sample 3: hierarchically structured surface composed of composite of 250 nm SiO<sub>2</sub> particles with titania–silica structures, forming raspberry-like particles.</p>
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<p>FTIR absorbance spectra (<b>a</b>) and UV transmission spectra (<b>b</b>) for PP films, samples 1 (TiO<sub>2</sub> coating) and 4 (TiO<sub>2</sub>-SiO<sub>2_500</sub> coating).</p>
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<p>XPS spectra of samples 1–4 (<b>a</b>), HR-XPS spectra of samples 1–4 of Si 2p (<b>b</b>) and of Ti 2p (<b>c</b>).</p>
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<p>XPS spectra of samples 1–4 (<b>a</b>), HR-XPS spectra of samples 1–4 of Si 2p (<b>b</b>) and of Ti 2p (<b>c</b>).</p>
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<p>Water contact angle measurements for samples 1–4. The droplet is being forced onto the surface using the needle, which yields a perfectly spherical droplet with 180° WCA.</p>
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<p>Samples 1–4 contaminated with soil (<b>column a</b>) and after self-cleaning test (<b>column b</b>).</p>
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<p>Water contact angles of coatings 1–4 after (<b>a</b>) 3000 m of the sandpaper abrasion test and (<b>b</b>) zoom in on the WCA results up to 600 m.</p>
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<p>Water contact angle of samples 1–4 before (control) and after soaking in various solutions.</p>
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15 pages, 7101 KiB  
Article
Fatigue Crack Propagation Analysis of Rail Surface Under Mixed Initial Crack Patterns
by Jianhua Liu, Weiqi Yang and Zhongmei Wang
Appl. Sci. 2024, 14(23), 11454; https://doi.org/10.3390/app142311454 - 9 Dec 2024
Viewed by 473
Abstract
Prolonged rolling contact fatigue between wheels and rails results in the formation of surface cracks on the rail and accurately analyzing the crack expansion behavior is essential to ensuring the safe operation of the train. Drawing upon the principles of fracture mechanics and [...] Read more.
Prolonged rolling contact fatigue between wheels and rails results in the formation of surface cracks on the rail and accurately analyzing the crack expansion behavior is essential to ensuring the safe operation of the train. Drawing upon the principles of fracture mechanics and finite element theory, this study establishes a finite element model of wheel–rail rolling contact that incorporates the presence of cracks. The method utilizes an interaction integral to calculate the stress intensity factors at the leading edge of the crack; then, the Paris formula is used to solve the crack spreading rate. It systematically examines the effects of the initial crack angle, the coefficient of friction of wheels to rails, and crack size on the behavior of fatigue crack propagation. The results indicate that the cracks primarily extend in the depth direction of the rail, transforming the semi-circular surface cracks into elliptical cracks with the major axis oriented along the rail’s width. Crack propagation is primarily driven by model II and III composite crack propagation, with their expansion rates influenced by operating conditions. In contrast, mode-I expansion is less sensitive to these conditions. Under single-variable loading conditions, a smaller initial crack angle results in a faster crack growth rate. Increasing crack length accelerates crack growth, while a higher friction coefficient inhibits it. Full article
(This article belongs to the Section Materials Science and Engineering)
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<p>Microcracks on the surface of the rail.</p>
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<p>Schematic of the 3D wheel track finite element model; (<b>a</b>) model of track; (<b>b</b>) Refinement of the grid in the contact patch; (<b>c</b>) schematic of the cracked interface insertion. (See red circle for crack location).</p>
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<p>Rail flaw detection vehicle.</p>
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<p>Ultrasonic flaw detection system; (<b>a</b>) ultrasonic flaw detection equipment; (<b>b</b>) B-image data.</p>
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<p>Comparison of simulated crack extension and ultrasonic flaw crack extension angles: (<b>a</b>) crack shape evolution; (<b>b</b>) simulated crack extension angle (see protractor); (<b>c</b>) B-image rail head crack extension angle (see protractor).</p>
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<p>Comparison of simulated crack extension and ultrasonic flaw crack extension angles: (<b>a</b>) crack shape evolution; (<b>b</b>) simulated crack extension angle (see protractor); (<b>c</b>) B-image rail head crack extension angle (see protractor).</p>
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<p>Distribution of Von Mises in rails under varying axle loads: (<b>a</b>) axle load 20 T; (<b>b</b>) axle load 25 T; (<b>c</b>) axle load 30 T; (<b>d</b>) the stress distribution of 20 T, 25 T, and 30 T axle loads with depth.</p>
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<p>The shear stress distribution varies with differing axle weights: (<b>a</b>) axle load 20 T; (<b>b</b>) axle load 25 T; (<b>c</b>) axle load 30 T.</p>
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<p>Crack tip stress intensity factor at various initial cracked angles: (<b>a</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mi mathvariant="normal">I</mi> </msub> <mi>,</mi> <mo> </mo> <msub> <mi>K</mi> <mi>II</mi> </msub> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mi>III</mi> </msub> </mrow> </semantics></math>; (<b>c</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Expansion of cracks at various initial crack angles: (<b>a</b>) extension length of cracks; (<b>b</b>) extension rate of cracks.</p>
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<p>Crack tip stress intensity factor at various initial crack lengths: (<b>a</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mi mathvariant="normal">I</mi> </msub> <mi>,</mi> <mo> </mo> <msub> <mi>K</mi> <mi>II</mi> </msub> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mi>III</mi> </msub> </mrow> </semantics></math>; (<b>c</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Crack propagation at different initial crack lengths: (<b>a</b>) crack propagation length; (<b>b</b>) crack propagation rate.</p>
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<p>Crack tip stress intensity factor at various friction coefficients: (<b>a</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mi mathvariant="normal">I</mi> </msub> <mi>,</mi> <mo> </mo> <msub> <mi>K</mi> <mi>II</mi> </msub> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mi>III</mi> </msub> </mrow> </semantics></math>; (<b>c</b>) <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mrow> <mi>e</mi> <mi>q</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Crack propagation at different initial crack friction coefficients: (<b>a</b>) crack propagation length; (<b>b</b>) crack propagation rate.</p>
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19 pages, 1265 KiB  
Article
Neural Network-Based Descent Control for Landers with Sloshing and Mass Variation: A Cascade and Adaptive PID Strategy
by Angel Guillermo Ortega and Afroza Shirin
Aerospace 2024, 11(12), 1009; https://doi.org/10.3390/aerospace11121009 - 8 Dec 2024
Viewed by 413
Abstract
Autonomous control of lunar landers is essential for successful space missions, where precision and efficiency are crucial. This study presents a novel control strategy that leverages proportional, integral, and derivative (PID) controllers to manage the altitude, attitude, and position of a lunar lander, [...] Read more.
Autonomous control of lunar landers is essential for successful space missions, where precision and efficiency are crucial. This study presents a novel control strategy that leverages proportional, integral, and derivative (PID) controllers to manage the altitude, attitude, and position of a lunar lander, considering time-varying mass and sloshing behavior. Additionally, neural network models are developed, to approximate the lander’s mass properties as they change during descent. The challenge lies in the significant mass variations due to fuel, oxidizer, and pressurant consumption, which affect the lander’s inertia and sloshing behavior and complicate control efforts. We have developed a control-oriented model incorporating these mass dynamics, employing multiple PID controllers to linearize the system and enhance control precision. Altitude is maintained by one PID controller, while two others adjust the thrust vector control (TVC) gimbal angles to manage pitch and roll, with a fourth controller governing yaw via a reaction control system (RCS). A cascade PD controller further manages position by feeding commands to the attitude controllers, ensuring the lander reaches its target location. The lander’s TVC mechanism, equipped with a spherical gimbal, provides thrust in the desired direction, with control angles α and β regulated by the PID controllers. To improve the model’s accuracy, we have introduced time delays caused by fluid dynamics and actuator response, modeled via computational fluid dynamics (CFD). Fluid sloshing effects are also simulated as external forces acting on the lander. The neural networks are trained using data derived from computer-aided design (CAD) simulations of the lander vehicle, specifically the inertia tensor and the center of mass (COM) based on the varying mass levels in the tanks. The trained neural networks (NNs) can then use lander tank levels and orientation to inform and accurately predict the lander’s COM and inertia tensor in real time during the mission. The implications of this research are significant for future lunar missions, offering enhanced safety and efficiency in vehicle descent and landing operations. Our approach allows for real-time estimation of the lander’s state and for precise execution of maneuvers, verified through complex numerical simulations of the descent, hover, and landing phases. Full article
(This article belongs to the Section Astronautics & Space Science)
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<p>Propellant fluid sloshing forces in <span class="html-italic">x</span> and <span class="html-italic">y</span> directions.</p>
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<p>Propellant fluid sloshing moments in <span class="html-italic">x</span> and <span class="html-italic">y</span> directions.</p>
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<p>Block diagram of the lunar lander system with a time-delayed TVC controller and instantaneous RCS controller.</p>
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<p>Trajectory interpolation plot for multiple <math display="inline"><semantics> <mrow> <mo>(</mo> <mi>x</mi> <mo>,</mo> <mi>y</mi> <mo>)</mo> </mrow> </semantics></math> positions.</p>
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<p>Visualization of desired mission maneuvers separated by phases.</p>
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<p>Mission control with variable desired altitude.</p>
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<p>Mission control with variable desired orientation.</p>
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<p>Altitude control with commanded and response altitude along with the commanded thrust for the maneuver.</p>
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<p>Lander velocity responses <math display="inline"><semantics> <mrow> <mo>[</mo> <msub> <mi>v</mi> <mi>x</mi> </msub> <mo>,</mo> <msub> <mi>v</mi> <mi>y</mi> </msub> <mo>,</mo> <msub> <mi>v</mi> <mi>z</mi> </msub> <mo>]</mo> </mrow> </semantics></math> with and without active sloshing.</p>
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<p>Consumption of lander propellant mass over time.</p>
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<p>The roll-commanded and TVC gimbal response as mass, inertia, and COM change with time. The responses show disabled and enabled sloshing.</p>
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<p>The pitch-commanded and TVC gimbal response as mass, inertia, and COM change with time. The responses show disabled and enabled sloshing.</p>
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<p>The yaw-commanded and RCS moment response as mass, inertia, and COM change with time. The responses show disabled and enabled sloshing.</p>
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<p>Inertia <span class="html-italic">x</span> terms with mass change over time. The responses show the disabled and enabled sloshing and the polynomial approximation.</p>
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<p>Inertia <span class="html-italic">y</span> terms with mass change over time. The responses show the disabled and enabled sloshing and the polynomial approximation.</p>
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<p>Inertia <span class="html-italic">z</span> terms with mass change over time. The responses show the disabled and enabled sloshing and the polynomial approximation.</p>
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<p>COM change with mass change over time.</p>
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15 pages, 7203 KiB  
Article
Rectangular Improvement Method for Plan View Pattern of Plates During the Angular Rolling Process
by Chunyu He, Junyi Luo, Zhipeng Xu, Zhiqiang Wang, Zhong Zhao, Zhiqiang Wu and Zhijie Jiao
Materials 2024, 17(23), 5964; https://doi.org/10.3390/ma17235964 - 5 Dec 2024
Viewed by 371
Abstract
The effect of the angular rolling process on the plan view pattern of a plate was studied, and the rectangular influencing factors and improvement methods for this process were proposed in this paper. DEFORM (v11.0) finite element software was used to simulate the [...] Read more.
The effect of the angular rolling process on the plan view pattern of a plate was studied, and the rectangular influencing factors and improvement methods for this process were proposed in this paper. DEFORM (v11.0) finite element software was used to simulate the processes of conventional rolling and angular rolling, and the degree of rectangularity of plates under different rolling process conditions was compared. A formula to characterize the degree of rectangularity of plates was established; the closer this value is to one, the better the degree of rectangularity. Considering the actual rolling process conditions, the range of theoretically calculated rectangular rotation angles was extended to obtain the optimum rectangular rotation angle using the finite element simulation method. In the two-pass angular rolling process, the optimal rectangular angle of the second pass was 14.275° when the first pass was 15°. The optimal rectangular angle of the plate was 19.008° when the first pass’ angle was 20°. Two-pass angular rolling is different to four-pass rolling, and the simulation results showed that J 15° 4 (1.0012) was less than J 15° 2 (1.0015) and J 20° 4 (1.0034) was less than J 20° 2 (1.0055). The rectangularity degree of the four-pass process was better than the two-pass process. Angular rolling experiments were carried out, and the actual data show that the characteristic rectangular value of the rolled piece was 1.003 during the four-pass process and 1.014 during the two-pass process. This verified that separating the one-group two-pass angular rolling process from the one-group four-pass angular rolling process can improve the rectangular degree of the rolled plate, thereby increasing the yield rate. This provides a theoretical basis for industrial applications. Full article
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Graphical abstract

Graphical abstract
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<p>Schematic diagram of two-pass angular rolling.</p>
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<p>Schematic diagram of four-pass angular rolling: (<b>a</b>) first pass; (<b>b</b>) second pass; (<b>c</b>) third pass; (<b>d</b>) fourth pass.</p>
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<p>Schematic diagram of the geometric model.</p>
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<p>Lower right corner after rolling: (<b>a</b>) lower right corner three-dimensional (3D) view; (<b>b</b>) lower right corner x–z view; (<b>c</b>) lower right corner y–z view; (<b>d</b>) lower right corner x–y view.</p>
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<p>Pointing diagram for angular rolled parameters: (<b>a</b>) before the first pass and (<b>b</b>) after the first pass.</p>
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<p>Conventional rolling deformation diagram: (<b>a</b>) plan view pattern after rolling and (<b>b</b>) comparison of the plan view pattern of the head and tail along the center line after rolling.</p>
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<p>Stress diagram for conventional rolling biting and throwing stages: (<b>a</b>) rolling biting stage and (<b>b</b>) rolling throwing stage.</p>
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<p>Evolution of the plan view pattern of the rolled piece by two-pass angular rolling.</p>
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<p>Evolution of the plan view pattern of the rolled piece by four-pass angular rolling.</p>
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<p>Characteristic rectangular values of two-pass angular rolling: (<b>a</b>) first pass rotated by 15° and (<b>b</b>) first pass rotated by 20°.</p>
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<p>Experimental rolling mill.</p>
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<p>Plan view pattern after angular rolling (<span class="html-fig-inline" id="materials-17-05964-i001"><img alt="Materials 17 05964 i001" src="/materials/materials-17-05964/article_deploy/html/images/materials-17-05964-i001.png"/></span>–reference points, <span class="html-fig-inline" id="materials-17-05964-i002"><img alt="Materials 17 05964 i002" src="/materials/materials-17-05964/article_deploy/html/images/materials-17-05964-i002.png"/></span>–edge points): (<b>a</b>) two-pass angular rolling and (<b>b</b>) four-pass angular rolling.</p>
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<p>Comparison of the characteristic rectangular values of the two processes.</p>
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24 pages, 12686 KiB  
Article
Research on the Optimization of TP2 Copper Tube Drawing Process Parameters Based on Particle Swarm Algorithm and Radial Basis Neural Network
by Fengli Yue, Zhuo Sha, Hongyun Sun, Dayong Chen and Jinsong Liu
Appl. Sci. 2024, 14(23), 11203; https://doi.org/10.3390/app142311203 - 1 Dec 2024
Viewed by 465
Abstract
After rolling, TP2 copper tubes exhibit defects such as sawtooth marks, cracks, and uneven wall thickness after joint drawing, which severely affects the quality of the finished copper tubes. To study the effect of drawing process parameters on wall thickness uniformity, an ultrasonic [...] Read more.
After rolling, TP2 copper tubes exhibit defects such as sawtooth marks, cracks, and uneven wall thickness after joint drawing, which severely affects the quality of the finished copper tubes. To study the effect of drawing process parameters on wall thickness uniformity, an ultrasonic detection platform for measuring the wall thickness of rolled copper tubes was constructed to verify the accuracy of the experimental equipment. Using the detected data, a finite element model of drawn copper tubes was established, and numerical simulation studies were conducted to analyze the influence of parameters such as outer die taper angle, drawing speed, and friction coefficient on drawing force, maximum temperature, average wall thickness, and wall thickness uniformity. To address the problem of the large number of finite element model meshes and low solution efficiency, the wall thickness uniformity was predicted using a radial basis function (RBF) neural network, and parameter optimization was performed using the particle swarm optimization (PSO) algorithm. The research results show that the RBF neural network can accurately predict wall thickness uniformity, and using the PSO optimization algorithm, the best parameter combination can reduce the wall thickness uniformity after drawing in finite element simulation. Full article
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<p>TP2 copper tube process flow.</p>
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<p>Equilibrium condition of forces.</p>
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<p>Single probe water immersion longitudinal wave pulse emission method.</p>
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<p>Ultrasonic thickness test bench.</p>
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<p>Thickness detection probe: (<b>a</b>) Lower thickness detection probe group; (<b>b</b>) upper thickness detection probe group.</p>
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<p>Thickness probe detection software.</p>
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<p>Detection software offline authentication. (<b>a</b>) Ultrasonic offline detection; (<b>b</b>) test results.</p>
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<p>Mean absolute error.</p>
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<p>Initial finite element model of the pipe.</p>
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<p>(<b>a</b>) Tensile specimen. (<b>b</b>) Real stress–strain curve at room temperature.</p>
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<p>Drawing force change rule. (<b>a</b>) Drawing speed; (<b>b</b>) friction coefficient.</p>
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<p>Temperature change rule. (<b>a</b>) Drawing speed; (<b>b</b>) friction coefficient.</p>
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<p>Wall thickness variation. (<b>a</b>) Drawing speed; (<b>b</b>) friction coefficient.</p>
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<p>Wall thickness uniformity change rule. (<b>a</b>) Drawing speed; (<b>b</b>) friction coefficient.</p>
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<p>Tube wall thickness test. (<b>a</b>) Take point; (<b>b</b>) measurement.</p>
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<p>Simulation parameter combinations.</p>
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<p>RBF neural network topology.</p>
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<p>The flow chart of the PSO algorithm for parameter combination optimization.</p>
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<p>RBF prediction accuracy. (<b>a</b>) Training set prediction accuracy; (<b>b</b>) test set training accuracy.</p>
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<p>The relationship between fitness function and iteration times of the particle swarm optimization algorithm. (<b>a</b>) <span class="html-italic">ω</span> optimal value, (<b>b</b>) <span class="html-italic">c</span><sub>1</sub> optimal value, (<b>c</b>) <span class="html-italic">c</span><sub>2</sub> optimal value, and (<b>d</b>) optimal results.</p>
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<p>Distribution cloud. (<b>a</b>) Temperature distribution results; (<b>b</b>) thickness distribution results.</p>
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<p>Change curve. (<b>a</b>) Drawing force changes with time; (<b>b</b>) temperature changes with time.</p>
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12 pages, 3203 KiB  
Article
Comparative Study of Electrospun Polydimethylsiloxane Fibers as a Substitute for Fluorine-Based Polymeric Coatings for Hydrophobic and Icephobic Applications
by Adrián Vicente, Pedro J. Rivero, Cleis Santos, Nadine Rehfeld and Rafael Rodríguez
Polymers 2024, 16(23), 3386; https://doi.org/10.3390/polym16233386 - 30 Nov 2024
Viewed by 500
Abstract
The development of superhydrophobic, waterproof, and breathable membranes, as well as icephobic surfaces, has attracted growing interest. Fluorinated polymers like PTFE or PVDF are highly effective, and previous research by the authors has shown that combining these polymers with electrospinning-induced roughness enhances their [...] Read more.
The development of superhydrophobic, waterproof, and breathable membranes, as well as icephobic surfaces, has attracted growing interest. Fluorinated polymers like PTFE or PVDF are highly effective, and previous research by the authors has shown that combining these polymers with electrospinning-induced roughness enhances their hydro- and ice-phobicity. The infusion of these electrospun mats with lubricant oil further improves their icephobic properties, achieving a slippery liquid-infused porous surface (SLIPS). However, their environmental impact has motivated the search for fluorine-free alternatives. This study explores polydimethylsiloxane (PDMS) as an ideal candidate because of its intrinsic properties, such as low surface energy and high flexibility, even at very low temperatures. While some published results have considered this polymer for icephobic applications, in this work, the electrospinning technique has been used for the first time for the fabrication of 95% pure PDMS fibers to obtain hydrophobic porous coatings as well as breathable and waterproof membranes. Moreover, the properties of PDMS made it difficult to process, but these limitations were overcome by adding a very small amount of polyethylene oxide (PEO) followed by a heat treatment process that provides a mat of uniform fibers. The experimental results for the PDMS porous coating confirm a hydrophobic behavior with a water contact angle (WCA) ≈ 118° and roll-off angle (αroll-off) ≈ 55°. In addition, the permeability properties of the fibrous PDMS membrane show a high transmission rate (WVD) ≈ 51.58 g∙m−2∙d−1, providing breathability and waterproofing. Finally, an ice adhesion centrifuge test showed a low ice adhesion value of 46 kPa. These results highlight the potential of PDMS for effective icephobic and waterproof applications. Full article
(This article belongs to the Section Polymer Fibers)
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<p>Schematic illustration of the fabrication methods used to produce F(PDMS) and F(SLIPS) samples through the following steps: (<b>i</b>) electrospinning corresponding to PEO-PDMS fibrous coating and HT<sub>0</sub>; (<b>ii</b>) membrane cleaning + silicon oil infusion.</p>
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<p>Scanning electron microscopy (SEM) images of the sample surface morphology F(PDMS) before (<b>a</b>) and after (<b>b</b>) thermal treatment.</p>
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<p>Histograms of the diameter distribution (<b>a</b>) and particle size (<b>b</b>) of the fiber sample F(PDMS).</p>
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<p>TGA curve of PDMS-PEO composite fibers with a weight ratio of 95:5.</p>
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<p>ATR-FTIR spectra of the samples F(PDMS) and PEO.</p>
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<p>Ice adhesion centrifuge test results for electrospun fibrous icephobic coatings and commercial references based on static ice formation.</p>
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15 pages, 2715 KiB  
Article
Modeling and Parameter Calibration of Morchella Seed Based on Discrete Element Method
by Min Li, Xiaowei He, Guansan Zhu, Jinxiu Liu, Kangcheng Gou and Xufeng Wang
Appl. Sci. 2024, 14(23), 11134; https://doi.org/10.3390/app142311134 - 29 Nov 2024
Viewed by 444
Abstract
Studies on the discrete element method (DEM) parameters of Morchella seeds are limited due to their high moisture content and weak inter-particle adhesion. However, accurate DEM simulations are crucial for the design of agricultural machinery. Physical experiments were conducted to measure the fundamental [...] Read more.
Studies on the discrete element method (DEM) parameters of Morchella seeds are limited due to their high moisture content and weak inter-particle adhesion. However, accurate DEM simulations are crucial for the design of agricultural machinery. Physical experiments were conducted to measure the fundamental properties of Morchella seeds, and a DEM model was established using the Hertz–Mindlin with JKR contact model. Subsequently, Plackett–Burman, steepest ascent, and Box–Behnken experiments were employed. They were used to analyze the significance of key contact parameters. A second-order polynomial regression model for the repose angle was developed, and significant contact parameters were optimized and calibrated. The results showed that the seed-to-seed rolling friction coefficient, seed-to-seed surface energy, and seed-to-steel rolling friction coefficient significantly impacted the repose angle. The simulation results using the optimized contact parameters closely matched the repose angle measured in physical experiments. The relative error was only 0.16%, validating the accuracy of the parameter calibration. Full article
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<p>(<b>a</b>) Schematic diagram of three-dimensional sizes. (<b>b</b>) Electric hot blower dry box (Shanghai Boxun Medical Biological Instrument Corp, Shanghai, China).</p>
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<p>Determination of the repose angle.</p>
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<p>Determination of the friction coefficient. (<b>a</b>) Actual test. (<b>b</b>) Test principle (Dongguan Huaguo Precision Instrument Co., Ltd., Dongguan, China).</p>
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<p>(<b>a</b>) Compression test of seed. (<b>b</b>) Texture lab (force).</p>
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<p>(<b>a</b>) The three-dimensional model used for simulations of the seed particles. (<b>b</b>) The simulation process of the angle repose.</p>
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<p>Response surface of the interaction between factors on the repose angle: (<b>a</b>) <span class="html-italic">BA</span> interaction; (<b>b</b>) <span class="html-italic">CB</span> interaction.</p>
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<p>Test results: (<b>a</b>) Measured repose angle. (<b>b</b>) Simulated repose angle.</p>
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14 pages, 4503 KiB  
Article
Personality Traits Estimation Based on Job Interview Video Analysis: Importance of Human Nonverbal Cues Detection
by Kenan Kassab and Alexey Kashevnik
Big Data Cogn. Comput. 2024, 8(12), 173; https://doi.org/10.3390/bdcc8120173 - 28 Nov 2024
Viewed by 494
Abstract
In this research, we delve into the analysis of non-verbal cues and their impact on evaluating job performance estimation and hireability by analyzing video interviews. We study a variety of non-verbal cues, which can be extracted from video interviews and can provide a [...] Read more.
In this research, we delve into the analysis of non-verbal cues and their impact on evaluating job performance estimation and hireability by analyzing video interviews. We study a variety of non-verbal cues, which can be extracted from video interviews and can provide a framework that utilizes the extracted features, and we combine them with personality traits to estimate sales abilities. Experimenting on the (Human Face Video Dataset for Personality Traits Detection) VPTD dataset, we proved the importance of smiling as a valid indicator for estimating extraversion and sales abilities. We also examined the role of head movements (represented by the rotation angles, roll, pitch, and yaw) since they play a crucial role in evaluating personality traits in general and extraversion and neuroticism in particular. The testing results show how these non-verbal cues can be used as assisting features in the proposed approach to provide a valid, reliable, and accurate estimation of sales abilities and job performance. Full article
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<p>The importance of the nonverbal cues obtained from analyzing previous articles.</p>
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<p>The proposed framework for job performance and sales abilities estimation.</p>
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<p>The heat map (correlation coefficient) for personality traits and sales estimation (E—extroversion, A—Agreeableness, C—Conscientiousness, N—neuroticism, O—Openness, and SE—sales estimation).</p>
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<p>The heat map (correlation coefficient and <span class="html-italic">p</span>-value) with the smiling features (E—extroversion, A—Agreeableness, C—Conscientiousness, N—neuroticism, O—Openness, SE—sales estimation, FWS—Frame with Smile, and R_RWS—Ratio of Frame with Smile).</p>
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<p>The scatter of the dataset with high extraversion scores.</p>
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<p>Three-dimensional representation for the rotation angles.</p>
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<p>Visualizing the significant movements through the video.</p>
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<p>The correlation matrix between personality traits and head movements.</p>
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18 pages, 6632 KiB  
Article
Efficient and Accurate Calibration of Discrete Element Method Parameters for Black Beans
by Xuezhen Wang, Qinghang Zhai, Shihao Zhang, Qianwen Li and Hanmi Zhou
Agronomy 2024, 14(12), 2803; https://doi.org/10.3390/agronomy14122803 - 25 Nov 2024
Viewed by 329
Abstract
Discrete element parameters of the black bean (BLB) are key to developing high-performance BLB machineries (e.g., seeders and shellers), which are still lacking in previous literature. In this study, the effects of the radius and lifting speed of cylinder-in-cylinder lifting method (CLM) simulations [...] Read more.
Discrete element parameters of the black bean (BLB) are key to developing high-performance BLB machineries (e.g., seeders and shellers), which are still lacking in previous literature. In this study, the effects of the radius and lifting speed of cylinder-in-cylinder lifting method (CLM) simulations were investigated to efficiently and accurately obtain the repose angle. Discrete element method (DEM) parameters of the BLB were determined by combining the Plackett–Burman Design test, the steepest ascent design test, and the central composite design test. The results show that the measurement moment (i.e., 12 s) of repose angles should be determined when kinetic energy reaches the minimal threshold (1 × 10−6 J) to efficiently and accurately obtain repose angles; too early or too late a measurement can result in inaccurate repose angles or excessive computation time of the computer, respectively. The lifting speed and cylinder radius affected the lateral displacements of BLBs and came at the cost of higher computation time and memory usage. A lifting speed of 0.015 m·s−1 and a radius of 40 mm of the cylinder were determined in CLM simulations. The static friction coefficient and rolling friction coefficient between BLBs significantly affected the repose angles. A static friction coefficient of 0.202 and rolling friction coefficient of 0.0104 between BLBs were obtained based on the optimization results. A low relative error (0.74%) and insignificant difference (p > 0.05) between the simulated and measured repose angles were found. The suggested method can be potentially used to calibrate the DEM parameters of BLBs with good accuracy. The results from this study can provide implications for investigating interactions of BLBs and various BLB processing machines and for the efficient and accurate determination of DEM parameters of crop grains. Full article
(This article belongs to the Section Precision and Digital Agriculture)
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<p>The geometrical measurement positions of the black bean (BLB) (<span class="html-italic">L</span> = length; <span class="html-italic">W</span> = width; <span class="html-italic">T</span> = thickness).</p>
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<p>Experimental principle for determining the coefficient of restitution (BLB, H, and h represent black bean, initial height, and the largest rebound height of the black bean, respectively).</p>
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<p>Test principle for measuring the static friction coefficient (BLB and <span class="html-italic">α</span> represent black bean and the angle between the inclined plane and horizontal plane, respectively).</p>
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<p>Test principle for measuring the rolling friction coefficient (x, β, and L represent the distance from the black bean (BLB) to the base edge of the inclined plane, the inclination angle of the plate, and the rolling distance of the BLB on the horizontal plexiglass plate, respectively).</p>
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<p>Cone image from laboratory repose angle test.</p>
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<p>Discrete element modeling of black beans (BLBs): (<b>a</b>) 3D DEM model of a BLB; (<b>b</b>) lifting process model of the cylinder filled with BLBs.</p>
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<p>Dimension distributions of the black bean (BLB): (<b>a</b>) BLB length distribution (i.e., <span class="html-italic">L</span>); (<b>b</b>) BLB width distribution (i.e., <span class="html-italic">W</span>); (<b>c</b>) BLB thickness distribution (i.e., <span class="html-italic">T</span>).</p>
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<p>Laboratory repose angle results of black bean: (<b>a</b>) fit line from the left side; (<b>b</b>) fit line from the right side.</p>
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<p>BLB accumulation forms from lifting speeds of (<b>a</b>) 0.005 m/s, (<b>b</b>) 0.015 m/s, (<b>c</b>) 0.025 m/s, (<b>d</b>) 0.035 m/s, (<b>e</b>) 0.045 m/s, and (<b>f</b>) 0.055 m/s, and (<b>g</b>) effects of the lifting speed on the solution time of the computer and memory usage (i.e., space occupied by simulation data).</p>
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<p>BLB accumulation forms from lifting speeds of (<b>a</b>) 0.005 m/s, (<b>b</b>) 0.015 m/s, (<b>c</b>) 0.025 m/s, (<b>d</b>) 0.035 m/s, (<b>e</b>) 0.045 m/s, and (<b>f</b>) 0.055 m/s, and (<b>g</b>) effects of the lifting speed on the solution time of the computer and memory usage (i.e., space occupied by simulation data).</p>
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<p>The bean particle cones with cylinder radii of (<b>a</b>) 20 mm, (<b>b</b>) 30 mm, (<b>c</b>) 40 mm, (<b>d</b>) 50 mm, and (<b>e</b>) 60 mm, and (<b>f</b>) the effects of the cylinder radius on the number of bean particles and memory usage.</p>
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<p>The bean particle cones with cylinder radii of (<b>a</b>) 20 mm, (<b>b</b>) 30 mm, (<b>c</b>) 40 mm, (<b>d</b>) 50 mm, and (<b>e</b>) 60 mm, and (<b>f</b>) the effects of the cylinder radius on the number of bean particles and memory usage.</p>
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<p>The change in energy during the formation of the repose angle. (<b>a</b>) Particle energy vs. time. (<b>b</b>) Kinetic energy change of the BLB pile after cylinder separation.</p>
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<p>Accumulation angle formation process in releasing stage of bean particles: (<b>a</b>) 4 s; (<b>b</b>) 5 s; (<b>c</b>) 6 s; (<b>d</b>) 7 s; (<b>e</b>) 8 s.</p>
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<p>Change in accumulation angle during 8–15 s.</p>
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<p>Pareto chart.</p>
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<p>Response surface analysis on the effects of static friction and rolling friction coefficients of black beans (BLBs) on the simulated repose angle θx.</p>
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<p>Verification of optimized DEM parameters: (<b>a</b>) repose angle measured in the laboratory. (<b>b</b>) Repose angle from the DEM simulation.</p>
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18 pages, 15595 KiB  
Article
Vehicle Attitude Control of Magnetorheological Semi-Active Suspension Based on Multi-Objective Intelligent Optimization Algorithm
by Kailiang Han, Yiming Hu, Dequan Zeng, Yinquan Yu, Lei Xiao, Jinwen Yang, Weidong Liu and Letian Gao
Actuators 2024, 13(12), 466; https://doi.org/10.3390/act13120466 - 21 Nov 2024
Viewed by 316
Abstract
A multi-objective intelligent optimization algorithm-based attitude control strategy for magnetorheological semi-active suspension is proposed to address the vehicle attitude imbalance generated during steering and braking. Firstly, the mechanical properties of the magnetorheological damper (MRD) are tested, and the parameters in the hyperbolic tangent [...] Read more.
A multi-objective intelligent optimization algorithm-based attitude control strategy for magnetorheological semi-active suspension is proposed to address the vehicle attitude imbalance generated during steering and braking. Firstly, the mechanical properties of the magnetorheological damper (MRD) are tested, and the parameters in the hyperbolic tangent model of the magnetorheological damper are identified through experiments. Secondly, a simulation model of the whole vehicle multi-degree-of-freedom vehicle dynamics including magnetorheological damper is established, and the whole-vehicle Linear Quadratic Regulator (LQR) controller is designed. Then, the optimization design model of the joint vehicle controller and vehicle dynamics is established to design the optimization fitness function oriented to the body attitude control performance, and the attitude optimal controller is calculated with the help of multi-objective intelligent optimization algorithm. Simulation results show that the proposed control method is able to improve the body roll angle, body pitch angle, and suspension dynamic deflection well on the basis of ensuring no deterioration in other performance indexes, ensuring good attitude control capability of the vehicle and verifying the feasibility of the control strategy. Full article
(This article belongs to the Special Issue Magnetorheological Actuators and Dampers)
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<p>a1-I curve.</p>
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<p>Damping force–displacement curve.</p>
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<p>Damping force–velocity curve.</p>
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<p>Multi-degree-of-freedom dynamics model.</p>
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<p>Flowchart of multi-objective particle swarm algorithm.</p>
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<p>Pareto front viewable view.</p>
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<p>Dominance value of each solution.</p>
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<p>Damping force comparison: (<b>a</b>) damping force of the left front tire; (<b>b</b>) damping force of the left rear tire; (<b>c</b>) damping force of the right front tire; and (<b>d</b>) damping force of the right rear tire.</p>
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<p>Time domain response curve of body attitude: (<b>a</b>) body roll angle; (<b>b</b>) body pitch angle; (<b>c</b>) left front suspension deflection; (<b>d</b>) left rear suspension deflection; (<b>e</b>) right front suspension deflection; and (<b>f</b>) right rear suspension deflection.</p>
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<p>Time domain response curves of vertical acceleration and tire dynamic deformation: (<b>a</b>) body vertical acceleration; (<b>b</b>) dynamic deformation of the left front tire; (<b>c</b>) dynamic deformation of the left rear tire; (<b>d</b>) dynamic deformation of the right front tire; and (<b>e</b>) dynamic deformation of the right rear tire.</p>
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<p>Frequency domain curve of road input against typical output: (<b>a</b>) road input to body vertical acceleration; (<b>b</b>) road input to suspension dynamic deflection; and (<b>c</b>) road input to tire dynamic deformation.</p>
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<p>Frequency domain curve of lateral acceleration against typical outputs: (<b>a</b>) lateral acceleration to body roll angle; (<b>b</b>) lateral acceleration to suspension dynamic deflection; and (<b>c</b>) lateral acceleration to tire dynamic deformation.</p>
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<p>Frequency domain curves of longitudinal acceleration against typical outputs: (<b>a</b>) longitudinal acceleration to body pitch angle; (<b>b</b>) longitudinal acceleration to suspension deflection; and (<b>c</b>) longitudinal acceleration to tire dynamic deformation.</p>
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16 pages, 4963 KiB  
Article
Simultaneous Localization and Mapping Methods for Snake-like Robots Based on Gait Adjustment
by Chaoquan Tang, Zhipeng Zhang, Meng Sun, Menggang Li, Hongwei Tang and Deen Bai
Biomimetics 2024, 9(11), 710; https://doi.org/10.3390/biomimetics9110710 - 19 Nov 2024
Viewed by 514
Abstract
Snake robots require autonomous localization and mapping capabilities for field applications. However, the characteristics of their motion, such as large turning angles and fast rotation speeds, can lead to issues like drift or even failure in positioning and map building. In response to [...] Read more.
Snake robots require autonomous localization and mapping capabilities for field applications. However, the characteristics of their motion, such as large turning angles and fast rotation speeds, can lead to issues like drift or even failure in positioning and map building. In response to this situation, this paper starts from the gait motion characteristics of the snake robot itself, proposing an improved gait motion method and a tightly coupled method based on IMU and visual information to solve the problem of poor algorithm convergence caused by head-shaking in snake robot SLAM. Firstly, the adaptability of several typical gaits of the snake robot to SLAM methods was evaluated. Secondly, the serpentine gait was selected as the object of gait improvement, and a head stability control method for the snake robot was proposed, thereby reducing the interference of the snake robot’s motion on the sensors. Thirdly, a visual–inertial tightly coupled SLAM method for the snake robot’s serpentine gait and Arc-Rolling gait was proposed, and the method was verified to enhance the robustness of the visual SLAM algorithm and improve the positioning and mapping accuracy of the snake robot. Finally, experiments proved that the methods proposed in this paper can effectively improve the accuracy of positioning and map building for snake robots. Full article
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<p>Principle of head stability control.</p>
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<p>Angular differential variation.</p>
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<p>Comparison of SLAM simulation under the serpentine gait.</p>
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<p>Comparison of SLAM simulation under the arc-rolling gait.</p>
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<p>The experimental system of the snake robot.</p>
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<p>Comparison of localization and mapping under the serpentine gait.</p>
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<p>Comparison of localization and mapping under the two methods.</p>
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<p>Comparison of localization and mapping under the arc-rolling gait.</p>
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<p>Localization and mapping results under the arc-rolling gait.</p>
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26 pages, 16654 KiB  
Article
Adaptive Fast Smooth Second-Order Sliding Mode Fault-Tolerant Control for Hypersonic Vehicles
by Lijia Cao, Lei Liu, Pengfei Ji and Chuandong Guo
Aerospace 2024, 11(11), 951; https://doi.org/10.3390/aerospace11110951 - 18 Nov 2024
Viewed by 415
Abstract
In response to control issues in hypersonic vehicles under external disturbances, model uncertainties, and actuator failures, this paper proposes an adaptive fast smooth second-order sliding mode fault-tolerant control scheme. First, a system separation approach is adopted, dividing the hypersonic vehicle model into fast [...] Read more.
In response to control issues in hypersonic vehicles under external disturbances, model uncertainties, and actuator failures, this paper proposes an adaptive fast smooth second-order sliding mode fault-tolerant control scheme. First, a system separation approach is adopted, dividing the hypersonic vehicle model into fast and slow loops for independent design. This ensures that the airflow angle tracking error and sliding mode variables converge to the vicinity of the origin within a finite time. A fixed-time disturbance observer is then designed to estimate and compensate for the effects of model uncertainties, external disturbances, and actuator failures. The controller parameters are dynamically adjusted through an adaptive term to enhance robustness. Furthermore, first-order differentiation is used to estimate differential terms, effectively avoiding the issue of complexity explosion. Finally, the convergence of the controller within a finite time is rigorously proven using the Lyapunov method, and the perturbation of aerodynamic parameters is tested using the Monte Carlo method. Simulation results under various scenarios show that compared with the terminal sliding mode method, the proposed method outperforms control accuracy and convergence speed. The root mean square errors for the angle of attack, sideslip angle, and roll angle are reduced by 65.11%, 86.71%, and 45.51%, respectively, while the standard deviation is reduced by 81.78%, 86.80%, and 45.51%, demonstrating that the proposed controller has faster convergence, higher control accuracy, and smoother output than the terminal sliding mode controller. Full article
(This article belongs to the Section Aeronautics)
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<p>Geometric parameters of the HSV model.</p>
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<p>The structure diagram of the control system.</p>
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<p>Angle of bank.</p>
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<p>Angle of attack.</p>
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<p>Sideslip angle and error.</p>
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<p>Error of bank angle.</p>
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<p>Error of attack.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>a</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>e</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>r</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Angle of bank.</p>
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<p>Angle of attack.</p>
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<p>Sideslip angle and error.</p>
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<p>Error of bank angle.</p>
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<p>Error of attack.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>a</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>e</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>r</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Aerodynamic uncertainty scatter plot.</p>
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<p>Bank angle of TSMFTC.</p>
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<p>Attack angle of TSMFTC.</p>
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<p>Sideslip angle of TSMFTC.</p>
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<p>Bank angle of AFSSOSMFTC.</p>
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<p>Attack angle of AFSSOSMFTC.</p>
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<p>Sideslip angle of AFSSOSMFTC.</p>
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<p>Angle of bank.</p>
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<p>Angle of attack.</p>
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<p>Sideslip angle and error.</p>
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<p>Error of bank angle.</p>
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<p>Error of attack.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>a</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>e</mi> </msub> </mrow> </semantics></math>.</p>
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<p>Variation of <math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>r</mi> </msub> </mrow> </semantics></math>.</p>
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20 pages, 6736 KiB  
Article
Enhanced Anti-Rollover Control for Commercial Vehicles Under Dynamic Lateral Interferences
by Jin Rong, Tong Wu, Junnian Wang, Jing Peng, Xiaojun Yang, Yang Meng and Liang Chu
Designs 2024, 8(6), 121; https://doi.org/10.3390/designs8060121 - 15 Nov 2024
Viewed by 496
Abstract
Commercial vehicles frequently experience lateral interferences, such as crosswinds or side slopes, during extreme maneuvers like emergency steering and high-speed driving due to their high centroid. These interferences reduce vehicle stability and increase the risk of rollover. Therefore, this study takes a bus [...] Read more.
Commercial vehicles frequently experience lateral interferences, such as crosswinds or side slopes, during extreme maneuvers like emergency steering and high-speed driving due to their high centroid. These interferences reduce vehicle stability and increase the risk of rollover. Therefore, this study takes a bus as the carrier and designs an anti-rollover control strategy based on mixed-sensitivity and robust H controller. Specifically, a 7-DOF vehicle dynamics model is introduced, and the factors influencing vehicle rollover are analyzed. Based on this, to minimize excessive intervention in the vehicle’s dynamic characteristics, the lateral velocity, roll angle, and roll rate are recorded at the vehicle’s rollover threshold as desired values. The lateral load transfer rate (LTR) is chosen as the evaluation index, and the required additional yaw moment is determined and distributed to the wheels for anti-rollover control. Furthermore, to verify the effectiveness of the proposed anti-rollover control strategy, a co-simulation platform based on MATLAB/Simulink and TruckSim is developed. Various dynamic lateral interferences (side winds with different changing trends and wind speeds) are introduced, and the fishhook and J-turn maneuvers are selected to analyze and compare the proposed control strategy with a fuzzy logic algorithm. The results indicate that the maximum LTR of the vehicle is reduced by 0.11. Additionally, the lateral acceleration and yaw rate in the steady state are reduced by more than 1.8 m/s² and 15°, respectively, enhancing the vehicle’s lateral stability. Full article
(This article belongs to the Topic Vehicle Dynamics and Control, 2nd Edition)
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Figure 1
<p>7-DOF vehicle dynamics model: (<b>a</b>) the lateral motion and yaw of the vehicle body and (<b>b</b>) the roll motion of the vehicle body.</p>
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<p>Vehicle dynamics comparison validation: (<b>a</b>) steering angle, (<b>b</b>) slip angle, (<b>c</b>) yaw rate, and (<b>d</b>) roll angle.</p>
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<p>Simulation curves under different wheel angles: (<b>a</b>) lateral velocity, (<b>b</b>) yaw rate, (<b>c</b>) roll angle, and (<b>d</b>) roll rate.</p>
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<p>Simulation curves at different vehicle speeds: (<b>a</b>) lateral velocity, (<b>b</b>) yaw rate, (<b>c</b>) roll angle, and (<b>d</b>) roll rate.</p>
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<p>Structure of anti-rollover control strategy. Where, <math display="inline"><semantics> <mrow> <msup> <mrow> <msub> <mi>ω</mi> <mrow> <mi>r</mi> <mi>d</mi> </mrow> </msub> </mrow> <mo>∗</mo> </msup> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msup> <mrow> <msub> <mi>v</mi> <mi>y</mi> </msub> </mrow> <mo>∗</mo> </msup> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msup> <mi>φ</mi> <mo>∗</mo> </msup> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msup> <mover accent="true"> <mi>φ</mi> <mo>˙</mo> </mover> <mo>∗</mo> </msup> </mrow> </semantics></math> are the desired value of yaw rate, lateral velocity, roll angle and roll rate, respectively.</p>
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<p>Generalized system.</p>
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<p>Relationship between wheel braking force and vehicle yaw moment.</p>
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<p>Relationship between cylinder pressure and wheel braking torque.</p>
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<p>Co-simulation platform.</p>
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<p>The membership function of inputs and output: (<b>a</b>) input and (<b>b</b>) output.</p>
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<p>Simulation results of fishhook maneuver: (<b>a</b>) steering wheel angle, (<b>b</b>) lateral velocity, (<b>c</b>) yaw rate, (<b>d</b>) roll angle, (<b>e</b>) roll rate, and (<b>f</b>) vehicle velocity.</p>
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<p>Simulation results of fishhook maneuver considering lateral interference: (<b>a</b>) wind speed, (<b>b</b>) lateral velocity, (<b>c</b>) yaw rate, (<b>d</b>) roll angle, (<b>e</b>) roll rate, and (<b>f</b>) vehicle velocity.</p>
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<p>Simulation diagram of J-turn working maneuver: (<b>a</b>) steering wheel angle, (<b>b</b>) lateral velocity, (<b>c</b>) yaw rate, (<b>d</b>) roll angle, (<b>e</b>) roll rate, and (<b>f</b>) vehicle velocity.</p>
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<p>Simulation diagram of lateral interference intervention under J-turn maneuver: (<b>a</b>) wind speed, (<b>b</b>) lateral velocity, (<b>c</b>) yaw rate, (<b>d</b>) roll angle, (<b>e</b>) roll rate, and (<b>f</b>) vehicle velocity.</p>
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