[go: up one dir, main page]
More Web Proxy on the site http://driver.im/
You seem to have javascript disabled. Please note that many of the page functionalities won't work as expected without javascript enabled.
 
 
Sign in to use this feature.

Years

Between: -

Subjects

remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline

Journals

remove_circle_outline
remove_circle_outline
remove_circle_outline

Article Types

Countries / Regions

remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline

Search Results (797)

Search Parameters:
Keywords = fault-tolerant-control

Order results
Result details
Results per page
Select all
Export citation of selected articles as:
15 pages, 2986 KiB  
Article
Fault-Tolerant Control of Multi-Clamp Disc Elevator Brakes with Fixed-Time Convergence
by Yefeng Jiang, Wanbin Su, Ke Li, Yuan Zhou and Jing Zhou
Actuators 2025, 14(3), 123; https://doi.org/10.3390/act14030123 - 4 Mar 2025
Viewed by 149
Abstract
This paper proposes a passive fault-tolerant control strategy for a multi-caliper disc elevator brake system subject to unknown external disturbances and multiple actuator faults. Initially, a detailed analysis of the dynamic equations of the actuator in a multi-caliper disc elevator brake system with [...] Read more.
This paper proposes a passive fault-tolerant control strategy for a multi-caliper disc elevator brake system subject to unknown external disturbances and multiple actuator faults. Initially, a detailed analysis of the dynamic equations of the actuator in a multi-caliper disc elevator brake system with actuator faults is conducted. Subsequently, a nonsingular terminal sliding mode fault-tolerant control scheme with rapid fixed-time convergence is proposed, where the settling time is independent of the system’s initial state and can be preset through design parameters. The upper bound of the convergence time is derived using Lyapunov theory, ensuring that the faulty elevator brake control system converges within a predetermined fixed time. Ultimately, theoretical analysis and numerical simulation results confirm that the proposed controller can effectively handle the effects of actuator faults, parametric uncertainties, and external disturbances, ensuring satisfactory tracking accuracy. Full article
(This article belongs to the Section Control Systems)
Show Figures

Figure 1

Figure 1
<p>Multi-clamp disc elevator brake.</p>
Full article ">Figure 2
<p>Braking torque analysis diagram for a multi-caliper disc elevator brake.</p>
Full article ">Figure 3
<p>LM1: Position tracking effect of different fault−tolerant control methods. (<b>a</b>) Trajectory tracking comparison: Reference trajectory and actual trajectories. (<b>b</b>) Tracking error dynamics. (<b>c</b>) Control input signals.</p>
Full article ">Figure 4
<p>LM2: Position tracking effect of different fault−tolerant control methods. (<b>a</b>) Trajectory tracking comparison. (<b>b</b>) Tracking error dynamics. (<b>c</b>) Control input signals.</p>
Full article ">Figure 5
<p>LM3: Position tracking effect of different fault−tolerant control methods. (<b>a</b>) Trajectory tracking comparison. (<b>b</b>) Tracking error dynamics. (<b>c</b>) Control input signals.</p>
Full article ">Figure 6
<p>LM4: Position tracking effect of different fault−tolerant control methods. (<b>a</b>) Trajectory tracking comparison. (<b>b</b>) Tracking error dynamics. (<b>c</b>) Control input signals.</p>
Full article ">Figure 7
<p>LM5:Position tracking effect of different fault−tolerant control methods. (<b>a</b>) Trajectory tracking comparison. (<b>b</b>) Tracking error dynamics. (<b>c</b>) Control input signals.</p>
Full article ">Figure 8
<p>RMSE comparison of position tracking for LM1−LM5. Bars represent RMSE values under FNTSMC, CSMC, and NFTSMC.</p>
Full article ">
18 pages, 831 KiB  
Article
Bipartite Fault-Tolerant Consensus Control for Multi-Agent Systems with a Leader of Unknown Input Under a Signed Digraph
by Anning Liu, Wenli Zhang, Dongdong Yue, Chuang Chen and Jiantao Shi
Sensors 2025, 25(5), 1556; https://doi.org/10.3390/s25051556 - 3 Mar 2025
Viewed by 218
Abstract
This paper addresses the bipartite consensus problem of signed directed multi-agent systems (MASs) subject to actuator faults. This problem plays a crucial role in various real-world systems where agents exhibit both cooperative and competitive interactions, such as autonomous vehicle fleets, smart grids, and [...] Read more.
This paper addresses the bipartite consensus problem of signed directed multi-agent systems (MASs) subject to actuator faults. This problem plays a crucial role in various real-world systems where agents exhibit both cooperative and competitive interactions, such as autonomous vehicle fleets, smart grids, and robotic networks. To address this, unlike most existing works, an intermediate observer is designed using newly introduced intermediate variables, enabling simultaneous estimation of both agent states and faults. Furthermore, a distributed adaptive observer is developed to help followers estimate the leader’s state, overcoming limitations of prior bounded-input assumptions. Finally, simulation results demonstrate the method’s effectiveness, showing that consensus tracking errors converge to zero under under various fault scenarios and input uncertainties. Full article
(This article belongs to the Section Fault Diagnosis & Sensors)
Show Figures

Figure 1

Figure 1
<p>Topology of the MASs.</p>
Full article ">Figure 2
<p>Trajectories of <math display="inline"><semantics> <msub> <mi>x</mi> <mn>0</mn> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>x</mi> <mi>i</mi> </msub> </semantics></math>.</p>
Full article ">Figure 3
<p>Faults and its estimations.</p>
Full article ">Figure 4
<p>Trajectories of the leader <math display="inline"><semantics> <msub> <mi>x</mi> <mn>0</mn> </msub> </semantics></math> and observers <math display="inline"><semantics> <msub> <mover accent="true"> <mi>x</mi> <mo stretchy="false">^</mo> </mover> <mrow> <mn>0</mn> <mi>i</mi> </mrow> </msub> </semantics></math>.</p>
Full article ">Figure 5
<p>Trajectories of the error <math display="inline"><semantics> <msub> <mi>e</mi> <mrow> <mi>x</mi> <mi>o</mi> <mi>i</mi> </mrow> </msub> </semantics></math>.</p>
Full article ">Figure 6
<p>Trajectories of the error <math display="inline"><semantics> <msub> <mi>e</mi> <mrow> <mi>x</mi> <mi>i</mi> </mrow> </msub> </semantics></math>.</p>
Full article ">Figure 7
<p>Trajectories of the error <math display="inline"><semantics> <msub> <mi>r</mi> <mi>i</mi> </msub> </semantics></math>.</p>
Full article ">
26 pages, 3217 KiB  
Article
Fault-Tolerant Collaborative Control of Four-Wheel-Drive Electric Vehicle for One or More In-Wheel Motors’ Faults
by Han Feng, Yukun Tao, Jianbo Feng, Yule Zhang, Hongtao Xue, Tiansi Wang, Xing Xu and Peng Chen
Sensors 2025, 25(5), 1540; https://doi.org/10.3390/s25051540 - 1 Mar 2025
Viewed by 410
Abstract
A fault-tolerant collaborative control strategy for four-wheel-drive electric vehicles is proposed to address hidden safety issues caused by one or more in-wheel motor faults; the basic design scheme is that the control system is divided into two layers of motion tracking and torque [...] Read more.
A fault-tolerant collaborative control strategy for four-wheel-drive electric vehicles is proposed to address hidden safety issues caused by one or more in-wheel motor faults; the basic design scheme is that the control system is divided into two layers of motion tracking and torque distribution, and three systems, including driving, braking, and front-wheel steering are controlled collaboratively for four-wheel torque distribution. In the layer of motion tracking, a vehicle model with two-degree-of-freedom is employed to predict the control reference values of the longitudinal force and additional yaw moment required; four types of sensors, such as wheel speed, acceleration, gyroscope, and steering wheel angle, are used to calculate the actual values. At the torque distribution layer, SSOD and MSCD distribution schemes are designed to cope with two operating conditions, namely sufficient and insufficient output capacity after local hub motor failure, respectively, focusing on the objective function, constraints, and control variables of the MSCD control strategy. Finally, two operating environments, a straight-line track, and a DLC track, are set up to verify the effectiveness of the proposed control method. The results indicate that, compared with traditional methods, the average errors of the center of mass sideslip angle and yaw rate are reduced by at least 12.9% and 5.88%, respectively, in the straight-line track environment. In the DLC track environment, the average errors of the center of mass sideslip angle and yaw rate are reduced by at least 6% and 4.5%, respectively. The proposed fault-tolerant controller ensures that the four-wheel-drive electric vehicle meets the requirements of handling stability and safety under one or more hub motor failure conditions. Full article
(This article belongs to the Special Issue Intelligent Maintenance and Fault Diagnosis of Mobility Equipment)
Show Figures

Figure 1

Figure 1
<p>Dynamics model of 4WDEV.</p>
Full article ">Figure 2
<p>Fault-tolerant control policies of 4WDEV with one or more in-wheel motors’ faults.</p>
Full article ">Figure 3
<p>Schematic of the simulation environment.</p>
Full article ">Figure 4
<p>Stability indicators of two torque distribution schemes in the first test scenario: (<b>a</b>) Sideslip angle, (<b>b</b>) Yaw rate.</p>
Full article ">Figure 5
<p>Actual vehicle velocity of 4WDEV in the first test scenario.</p>
Full article ">Figure 6
<p>Actual driving forces of four in-wheel motors in the first test scenario.</p>
Full article ">Figure 7
<p>Vehicle stability indicators of three torque distribution schemes in the second test scenario and a straight-line track: (<b>a</b>) Sideslip angle (<b>b</b>) Yaw rate.</p>
Full article ">Figure 8
<p>Actual vehicle velocity of three torque distribution schemes in the second test scenario and a straight-line track.</p>
Full article ">Figure 9
<p>Actual driving forces of four in-wheel motors in the second test scenario and a straight-line track.</p>
Full article ">Figure 10
<p>Vehicle stability indicators of three torque distribution schemes in the second test scenario and a DLC track: (<b>a</b>) Sideslip angle, (<b>b</b>) Yaw rate.</p>
Full article ">Figure 11
<p>Actual vehicle velocity of three torque distribution schemes in the second test scenario and a DLC track.</p>
Full article ">Figure 12
<p>Actual driving forces of four in-wheel motors in the second test scenario and a DLC track.</p>
Full article ">
19 pages, 3025 KiB  
Article
Two-Step Robust Fault-Tolerant Controller Design Based on Nonlinear Extended State Observer (NESO) for Unmanned Aerial Vehicles (UAVs) with Actuator Faults and Disturbances
by Wei Wang, Yiming Chen, Zhang Ren and Huanhua Liu
Drones 2025, 9(3), 183; https://doi.org/10.3390/drones9030183 - 1 Mar 2025
Viewed by 215
Abstract
This paper presents a two-step robust fault-tolerant controller of incorporating disturbances and actuator faults rejection for a UAV flight control system, which is challenging due to its complex and nonlinear dynamics. First, the main controller, which is designed separately, considers all the design [...] Read more.
This paper presents a two-step robust fault-tolerant controller of incorporating disturbances and actuator faults rejection for a UAV flight control system, which is challenging due to its complex and nonlinear dynamics. First, the main controller, which is designed separately, considers all the design parameters giving the desired closed loop system response. Second, a method to design a standalone disturbance/fault compensator is suggested, which is integrated into the original system to ensure stability. The degraded system stability and performance are compensated by the compensator, which comes into effect only after the disturbance/fault residual error increases to a certain level. The disturbance/fault compensator is designed based on a nonlinear extended state observer (NESO), which cannot only estimate the system’s states but also the unknown disturbances and fault. In the faultless system, only the main controller is active. When an actuator fault/disturbance occurs, the compensator is automatically activated. This controller scheme solves the traditional control conflict between high performance and robustness. It also guarantees the stability of the system in the presence of the disturbances/faults. A civil fixed-wing unmanned aerial vehicle (UAV) that is equipped with a thrust vector control (TVC) with actuator faults and disturbance is chosen for the simulations, and the results prove the efficacy of the new approach. Full article
Show Figures

Figure 1

Figure 1
<p>Two-step robust fault-tolerant controller design.</p>
Full article ">Figure 2
<p>Structure of altitude control system.</p>
Full article ">Figure 3
<p>Structure of the roll angle control system.</p>
Full article ">Figure 4
<p>UAV state responses of the proposed RFTC (robust fault-tolerant controller) under left elevator stuck at 30 degrees. (<b>a</b>) Roll angular velocity. (<b>b</b>) Pitch angular velocity. (<b>c</b>) Yaw angular velocity. (<b>d</b>) Altitude.</p>
Full article ">Figure 5
<p>Fault and disturbance estimation by NESO. (<b>a</b>) Fault and disturbance estimation of roll angular acceleration. (<b>b</b>) Fault and disturbance estimation of pitch angular acceleration. (<b>c</b>) Fault and disturbance estimation of yaw angular acceleration.</p>
Full article ">Figure 6
<p>Actuator deflection under RFTC. (<b>a</b>) Left elevator and right elevator deflection. (<b>b</b>) Left aileron and right aileron deflection. (<b>c</b>) Rudder deflection. (<b>d</b>) Thrust-vectoring deflection.</p>
Full article ">Figure 7
<p>UAV state response responses of the proposed RFTC under rudder stuck at 7 degrees. (<b>a</b>) Roll angular velocity. (<b>b</b>) Pitch angular velocity. (<b>c</b>) Yaw angular velocity. (<b>d</b>) Yaw angle. (<b>e</b>) Roll angle. (<b>f</b>) Altitude.</p>
Full article ">Figure 8
<p>Fault and disturbance estimation by NESO. (<b>a</b>) Fault and disturbance estimation of roll angular acceleration. (<b>b</b>) Fault and disturbance estimation of pitch angular acceleration. (<b>c</b>) Fault and disturbance estimation of yaw angular acceleration.</p>
Full article ">Figure 9
<p>Actuator deflection under RFTC. (<b>a</b>) Left elevator and right elevator deflection. (<b>b</b>) Left aileron and right aileron deflection. (<b>c</b>) Rudder deflection. (<b>d</b>) Thrust-vectoring deflection.</p>
Full article ">
20 pages, 15890 KiB  
Article
Development and Research of the MOCVD Cleaning Robot
by Yibo Ren and Zengwen Dong
Machines 2025, 13(3), 202; https://doi.org/10.3390/machines13030202 - 28 Feb 2025
Viewed by 217
Abstract
With the wide application of the gallium nitride (GaN) preparation method based on Metal–Organic Chemical Vapor Deposition (MOCVD), the automation of MOCVD equipment has become a research hotspot. This paper explores the automation scheme of MOCVD reaction chamber cleaning to improve productivity and [...] Read more.
With the wide application of the gallium nitride (GaN) preparation method based on Metal–Organic Chemical Vapor Deposition (MOCVD), the automation of MOCVD equipment has become a research hotspot. This paper explores the automation scheme of MOCVD reaction chamber cleaning to improve productivity and reduce labor costs. Firstly, this paper establishes the kinematic solution model of a MOCVD cleaning robot and designs the cleaning robot path planning control algorithm. Considering the error between the initial position of the robot end-effector and the desired initial position in practical applications, this paper further designs a fault-tolerant motion planning algorithm for the initial position error. The simulation results show that the method can effectively reduce the initial position error and make it converge exponentially to zero. Finally, this paper builds the robot control system of the cleaning system and verifies the cleaning effect through tests. The test results show that the system can meet the actual use requirements and realize the reaction chamber cleaning automation goal. Full article
(This article belongs to the Section Robotics, Mechatronics and Intelligent Machines)
Show Figures

Figure 1

Figure 1
<p>Sediment on the reaction chamber.</p>
Full article ">Figure 2
<p>(<b>a</b>) Polishing Robot in UCAS [<a href="#B11-machines-13-00202" class="html-bibr">11</a>]; (<b>b</b>) Polishing Robot in SCU [<a href="#B12-machines-13-00202" class="html-bibr">12</a>].</p>
Full article ">Figure 3
<p>(<b>a</b>) Electric-driven end-effector in JLU [<a href="#B14-machines-13-00202" class="html-bibr">14</a>]; (<b>b</b>) Electric-driven end-effector in SIAT [<a href="#B15-machines-13-00202" class="html-bibr">15</a>].</p>
Full article ">Figure 4
<p>Robot’s structural model.</p>
Full article ">Figure 5
<p>End-effector structure. 1—Vacuuming mechanism, 2—Actuator motor, 3—Support transmission mechanism, 4—Steel brush.</p>
Full article ">Figure 6
<p>Link parameter description.</p>
Full article ">Figure 7
<p>Robot dimension diagram.</p>
Full article ">Figure 8
<p>Forward kinematics error bar chart.</p>
Full article ">Figure 9
<p>Inverse kinematics error bar chart.</p>
Full article ">Figure 10
<p>Overall architecture diagram of the algorithm.</p>
Full article ">Figure 11
<p>RRT algorithm diagram.</p>
Full article ">Figure 12
<p>RRT algorithm wireframe.</p>
Full article ">Figure 13
<p>Results of RRT.</p>
Full article ">Figure 14
<p>Pruning optimization principle diagram.</p>
Full article ">Figure 15
<p>Results of post-processing.</p>
Full article ">Figure 16
<p>Test route.</p>
Full article ">Figure 17
<p>(<b>a</b>) Displacement simulation results; (<b>b</b>) Displacement experiment results.</p>
Full article ">Figure 18
<p>(<b>a</b>) Velocity simulation results; (<b>b</b>) Velocity experiment results.</p>
Full article ">Figure 19
<p>Simulation test trajectory.</p>
Full article ">Figure 20
<p>Robot end error curve.</p>
Full article ">Figure 21
<p>Robot control system hardware.</p>
Full article ">Figure 22
<p>Communication framework.</p>
Full article ">Figure 23
<p>(<b>a</b>) MOCVD reaction chamber to be cleaned; (<b>b</b>) MOCVD reaction chamber being cleaned.</p>
Full article ">Figure 24
<p>Trajectory of the cleaning task.</p>
Full article ">Figure 25
<p>(<b>a</b>) Robot displacement in the cleaning phase; (<b>b</b>) Robot velocity in the cleaning phase.</p>
Full article ">Figure 26
<p>(<b>a</b>) Pre-cleaning; (<b>b</b>) Post-cleaning.</p>
Full article ">
20 pages, 3322 KiB  
Article
Consensus-Based Formation Control for Heterogeneous Multi-Agent Systems in Complex Environments
by Xiaofei Chang, Yiming Yang, Zhuo Zhang, Jiayue Jiao, Haoyu Cheng and Wenxing Fu
Drones 2025, 9(3), 175; https://doi.org/10.3390/drones9030175 - 26 Feb 2025
Viewed by 190
Abstract
The purpose of this paper is to develop formation control strategies for heterogeneous multi-intelligent-agent systems in complex environments, with the goal of enhancing their performance, reliability, and stability. Complex flight conditions, such as navigating narrow gaps in urban high-rise buildings, pose considerable challenges [...] Read more.
The purpose of this paper is to develop formation control strategies for heterogeneous multi-intelligent-agent systems in complex environments, with the goal of enhancing their performance, reliability, and stability. Complex flight conditions, such as navigating narrow gaps in urban high-rise buildings, pose considerable challenges for agent control. To address these challenges, this paper proposes a consensus-based formation strategy that integrates graph theory and multi-consensus algorithms. This approach incorporates time-varying group consistency to strengthen fault tolerance and reduce interference while ensuring obstacle avoidance and formation maintenance in dynamic environments. Through a Lyapunov stability analysis, combined with minimum dwell time constraints and the LaSalle invariance principle, this work proves the convergence of the proposed control scheme under changing network topologies. Simulation results confirm that the proposed strategy significantly improves system performance, mission execution capability, autonomy, synergy, and robustness, thereby enabling agents to successfully maintain formation and avoid obstacles in both homogeneous and heterogeneous clusters in complex environments. Full article
(This article belongs to the Special Issue Swarm Intelligence in Multi-UAVs)
Show Figures

Figure 1

Figure 1
<p>First-order agent consensus state trajectory.</p>
Full article ">Figure 2
<p>Velocity of first-order intelligences over time.</p>
Full article ">Figure 3
<p>Position of second-order intelligences over time.</p>
Full article ">Figure 4
<p>Velocity versus time for second-order intelligences.</p>
Full article ">Figure 5
<p>Acceleration versus time for second-order intelligences.</p>
Full article ">Figure 6
<p>Simulated multi-intelligent-agent formation.</p>
Full article ">Figure 7
<p>Simulation results of formation grouping control for multi-intelligent-agent system.</p>
Full article ">Figure 8
<p>Real-time change curves of one-order and two-order multi-consensus results.</p>
Full article ">Figure 9
<p>Simulation results of formation control for 25 multi-intelligent body systems.</p>
Full article ">
19 pages, 6583 KiB  
Article
Multiple Fault-Tolerant Control of DC Microgrids Based on Sliding Mode Observer
by Jian Sun, Zewen Li and Minsheng Yang
Electronics 2025, 14(5), 931; https://doi.org/10.3390/electronics14050931 - 26 Feb 2025
Viewed by 120
Abstract
Different locations and types of faults affect the safe and reliable operation of DC microgrids. Therefore, this paper proposes a secondary multiple fault-tolerant control scheme for a DC microgrid based on a sliding mode observer to ensure the voltage is restored to the [...] Read more.
Different locations and types of faults affect the safe and reliable operation of DC microgrids. Therefore, this paper proposes a secondary multiple fault-tolerant control scheme for a DC microgrid based on a sliding mode observer to ensure the voltage is restored to the rated value and realize the proportional current sharing of all sources. Firstly, the secondary control model of the DC microgrid is established, considering the multiple faults of actuators and sensors simultaneously. Secondly, the system model is transformed into two subsystems by bilinear coordinate transformation, and multiple faults decoupling between the sensor and actuator is realized. Then, two sliding mode observers are designed for the two transformed subsystems. The sliding mode variable structure equivalent principle is used to reconstruct the faults at different positions without knowing the fault models in advance, which is convenient for subsequent processing. Then, the fault-tolerant controller based on the sliding mode observer is designed, which uses the reconstructed value to offset the influence of sensor and actuator faults on the DC microgrid and realizes the fault-tolerant control of the DC microgrid. Finally, the effectiveness of the proposed control strategy is verified by experiments. Full article
Show Figures

Figure 1

Figure 1
<p>Secondary control architecture of DC microgrid.</p>
Full article ">Figure 2
<p>Fault-tolerant control structure.</p>
Full article ">Figure 3
<p>System configuration process.</p>
Full article ">Figure 4
<p>DC microgrid structure.</p>
Full article ">Figure 5
<p>Performance of secondary strategy without fault condition. (<b>a</b>) Current. (<b>b</b>) Voltage.</p>
Full article ">Figure 6
<p>Performance of secondary strategy with faults condition. (<b>a</b>) Current. (<b>b</b>) Voltage.</p>
Full article ">Figure 7
<p>Performance of proposed strategy with faults condition. (<b>a</b>) Current. (<b>b</b>) Voltage.</p>
Full article ">Figure 8
<p>Performance of proposed strategy with faults condition under scenarios 2, 3. (<b>a</b>) Current. (<b>b</b>) Voltage.</p>
Full article ">Figure 9
<p>Existing control strategies. (<b>a</b>) Current. (<b>b</b>) Voltage.</p>
Full article ">Figure 10
<p>Actuator fault 1. (<b>a</b>) Observation. (<b>b</b>) Error.</p>
Full article ">Figure 11
<p>Actuator fault 2. (<b>a</b>) Observation. (<b>b</b>) Error.</p>
Full article ">Figure 12
<p>Sensor fault 1. (<b>a</b>) Observation. (<b>b</b>) Error.</p>
Full article ">Figure 13
<p>Sensor fault 2. (<b>a</b>) Observation. (<b>b</b>) Error.</p>
Full article ">
17 pages, 10830 KiB  
Article
Fault-Tolerant Control of a Multiphase Series Capacitor Buck Converter in a Master–Slave Configuration for Powering a Particle Accelerator Electromagnet
by Edorta Ibarra, Antoni Arias, Iñigo Martínez de Alegría, Alberto Otero-Olavarrieta, Asier Matallana and Louis de Mallac
Electronics 2025, 14(5), 924; https://doi.org/10.3390/electronics14050924 - 26 Feb 2025
Viewed by 158
Abstract
Multiphase DC/DC power converter architectures have recently been investigated for powering the superconducting electromagnets in the High-Luminosity (HL) upgrade of the Large Hadron Collider (LHC) at CERN, targeting high-performance figures and reliability. In terms of control, a master–slave voltage/current regulation configuration was previously [...] Read more.
Multiphase DC/DC power converter architectures have recently been investigated for powering the superconducting electromagnets in the High-Luminosity (HL) upgrade of the Large Hadron Collider (LHC) at CERN, targeting high-performance figures and reliability. In terms of control, a master–slave voltage/current regulation configuration was previously proposed by the authors as an alternative to other well-known cascaded options. In this work, fault-tolerant features (i.e., diagnosis and reconfiguration under open-circuit switch faults) are incorporated into the aforementioned proposal. These features are highly desirable, as physics experiments—which can last for several hours—should not be interrupted in the event of a recoverable fault in the powering system. Simulation and experimental results are provided, demonstrating the correctness of the proposed fault-tolerant scheme. Full article
Show Figures

Figure 1

Figure 1
<p>Sub-converter buck architectures for electromagnet powering: (<b>a</b>) standard buck stage sub-converter. (<b>b</b>) SC-based buck stage sub-converter.</p>
Full article ">Figure 2
<p>Cascaded multiphase DC/DC control architectures: (<b>a</b>) conventional cascaded configuration; (<b>b</b>) cascaded configuration with current sharing regulation loop.</p>
Full article ">Figure 3
<p>Master–slave multiphase buck converter control approach based on the application of decoupling matrix <math display="inline"><semantics> <mi mathvariant="bold">T</mi> </semantics></math>.</p>
Full article ">Figure 4
<p>Block diagram of the proposed controller: (<b>a</b>) fault detection and diagnosis algorithm; (<b>b</b>) fault-tolerant voltage and current balancing algorithm including the fault detection block.</p>
Full article ">Figure 5
<p>Oversampling pattern for the sub-converter’s output current with a sampling time of <math display="inline"><semantics> <mrow> <msub> <mi>T</mi> <mrow> <mi>s</mi> <mi>w</mi> </mrow> </msub> <mo>/</mo> <mn>4</mn> </mrow> </semantics></math> to obtain their averaged values at each <span class="html-italic">k</span>-th instant.</p>
Full article ">Figure 6
<p>Simplified diagram of the interconnection layout between the SC buck cells.</p>
Full article ">Figure 7
<p>Performance of the proposed fault-tolerant algorithm (simulation results) with an open-circuit fault in a master (voltage-regulated) cell: (<b>a</b>) output voltage response; (<b>b</b>) current response; (<b>c</b>) per-cell fault detection flags.</p>
Full article ">Figure 7 Cont.
<p>Performance of the proposed fault-tolerant algorithm (simulation results) with an open-circuit fault in a master (voltage-regulated) cell: (<b>a</b>) output voltage response; (<b>b</b>) current response; (<b>c</b>) per-cell fault detection flags.</p>
Full article ">Figure 8
<p>Performance of the proposed fault-tolerant algorithm (simulation results) with an open-circuit fault in slave (current-regulated) cell: (<b>a</b>) output voltage response; (<b>b</b>) current response; (<b>c</b>) per-cell fault detection flags.</p>
Full article ">Figure 9
<p>Total output current for laboratory output inductance of 50 μH (blue line) vs. final circuit inductance of 0.255 H (red line).</p>
Full article ">Figure 10
<p>Prototype of the SC-based multiphase DC/DC used to validate the proposed fault detection and fault-tolerant algorithms.</p>
Full article ">Figure 11
<p>Operation of the multiphase DC/DC converter during start-up and step-up and step-down transients when working in healthy mode: (<b>a</b>) output voltage vs. reference voltage; (<b>b</b>) per-phase currents; (<b>c</b>) fault flags.</p>
Full article ">Figure 12
<p>Experimental results (II): power converter operation under the occurrence of two consecutive open-circuit faults at current-controlled cell number four (<math display="inline"><semantics> <mrow> <mi>t</mi> <mo>≃</mo> <mn>1</mn> </mrow> </semantics></math> s) and voltage-controlled cell number one (<math display="inline"><semantics> <mrow> <mi>t</mi> <mo>≃</mo> <mn>2.25</mn> </mrow> </semantics></math> s): (<b>a</b>) output voltage vs. reference voltage; (<b>b</b>) per-phase currents; (<b>c</b>) fault flags; (<b>d</b>) details of per-phase current evolution under an open-phase fault in slave sub-converter number four [zoomed area 1 of subfigure (<b>b</b>)]; (<b>e</b>) details of per-phase current evolution under an open-phase fault in master sub-converter [zoomed area 2 of subfigure (<b>b</b>)].</p>
Full article ">Figure 13
<p>Experimental results (and III): oscilloscope capture of the two consecutive open-circuit fault scenarios.</p>
Full article ">
27 pages, 4776 KiB  
Review
Technical Roadmaps of Electric Motor Technology for Next Generation Electric Vehicles
by Adil Usman and Anchal Saxena
Machines 2025, 13(2), 156; https://doi.org/10.3390/machines13020156 - 17 Feb 2025
Viewed by 346
Abstract
This paper provides a consolidated discussion and proposes significant measures in improving and advancing the performance of synchronous machines employed in electric traction applications designed for passenger electric vehicles (EVs). The paper quantifies the discussion on improving the power density (kW/kg) and efficiency [...] Read more.
This paper provides a consolidated discussion and proposes significant measures in improving and advancing the performance of synchronous machines employed in electric traction applications designed for passenger electric vehicles (EVs). The paper quantifies the discussion on improving the power density (kW/kg) and efficiency (%η) of the machine with the commercially available solutions in terms of new design architectures, advanced emerging materials, and adoption of additive manufacturing (AM) technologies. New challenges and opportunities are identified for the optimized machine designs having the potential to meet the global standards while keeping the cost under control. This paper provides an overview of current trends, an introduction to innovative technologies, and changes in existing manufacturing practices to achieve high-performance electrical machines with improved fault tolerance capabilities and reliability. Thereby meeting the standards for the next generation of electric vehicles. Full article
(This article belongs to the Special Issue Fault Diagnostics and Fault Tolerance of Synchronous Electric Drives)
Show Figures

Figure 1

Figure 1
<p>Component of electric traction drive system (ETDS) [<a href="#B7-machines-13-00156" class="html-bibr">7</a>].</p>
Full article ">Figure 2
<p>IPM- and SPM-type synchronous traction motors used in EV applications. (The motor pictures are taken from the research laboratory of Varroc Engineering Limited (VEL), Pune, India).</p>
Full article ">Figure 3
<p>Basic structure of a rare earth barium copper oxide (REBCO)—high-temperature superconducting (HTS) tape [<a href="#B30-machines-13-00156" class="html-bibr">30</a>].</p>
Full article ">Figure 4
<p>(<b>a</b>) Magnetic field (B-H) characteristics of Hiperco-50. (<b>b</b>) Iron losses of Hiperco-50 soft iron material at different frequencies [<a href="#B22-machines-13-00156" class="html-bibr">22</a>].</p>
Full article ">Figure 5
<p>Concept of CNT-Cu composite conductor used for motor windings [<a href="#B50-machines-13-00156" class="html-bibr">50</a>,<a href="#B51-machines-13-00156" class="html-bibr">51</a>].</p>
Full article ">Figure 6
<p>Concept of graphene-based CNT composite conductor developed for motor windings at <span class="html-italic">PNNL</span> [<a href="#B54-machines-13-00156" class="html-bibr">54</a>].</p>
Full article ">Figure 7
<p>Traction motor showing (<b>a</b>) distributed and (<b>b</b>) concentrated windings used in e-mobility systems (the motor pictures are taken from the research laboratory of Varroc Engineering Limited (VEL), Pune, India).</p>
Full article ">Figure 8
<p>Comparison between round wire motor windings with hairpin-shaped windings [<a href="#B59-machines-13-00156" class="html-bibr">59</a>,<a href="#B60-machines-13-00156" class="html-bibr">60</a>,<a href="#B61-machines-13-00156" class="html-bibr">61</a>]. The latter provides more slot fill factors.</p>
Full article ">Figure 9
<p>Ranking of magnetic materials (alternatives and supplements to rare earth materials) [<a href="#B5-machines-13-00156" class="html-bibr">5</a>].</p>
Full article ">Figure 10
<p>(<b>a</b>) Physical geometry of V-shaped rotor design. (<b>b</b>) V-shaped rotor with magnets (the motor pictures are taken from the research laboratory of Varroc Engineering Limited (VEL), Pune, India).</p>
Full article ">Figure 11
<p>Commercially available laminated piece of an 8-pole SRM rotor (left-hand side) and identical 3D-printed/AM-built rotor (right-hand side) [<a href="#B86-machines-13-00156" class="html-bibr">86</a>]—(image taken from [<a href="#B86-machines-13-00156" class="html-bibr">86</a>] under the creative commons (CC) redistribution license).</p>
Full article ">Figure 12
<p>Concept of hollow conductors [<a href="#B37-machines-13-00156" class="html-bibr">37</a>,<a href="#B38-machines-13-00156" class="html-bibr">38</a>,<a href="#B90-machines-13-00156" class="html-bibr">90</a>,<a href="#B91-machines-13-00156" class="html-bibr">91</a>].</p>
Full article ">Figure 13
<p>Process of producing polymer-bonded magnets using AM technology [<a href="#B73-machines-13-00156" class="html-bibr">73</a>,<a href="#B74-machines-13-00156" class="html-bibr">74</a>,<a href="#B75-machines-13-00156" class="html-bibr">75</a>,<a href="#B76-machines-13-00156" class="html-bibr">76</a>,<a href="#B77-machines-13-00156" class="html-bibr">77</a>,<a href="#B78-machines-13-00156" class="html-bibr">78</a>,<a href="#B95-machines-13-00156" class="html-bibr">95</a>,<a href="#B96-machines-13-00156" class="html-bibr">96</a>,<a href="#B97-machines-13-00156" class="html-bibr">97</a>].</p>
Full article ">
28 pages, 2083 KiB  
Article
Pipe Routing with Topology Control for Decentralized and Autonomous UAV Networks
by Shreyas Devaraju, Shivam Garg, Alexander Ihler, Elizabeth Serena Bentley and Sunil Kumar
Drones 2025, 9(2), 140; https://doi.org/10.3390/drones9020140 - 13 Feb 2025
Viewed by 663
Abstract
This paper considers a decentralized and autonomous wireless network of low SWaP (size, weight, and power) fixed-wing UAVs (unmanned aerial vehicles) used for remote exploration and monitoring of targets in an inaccessible area lacking communication infrastructure. Here, the UAVs collaborate to find target(s) [...] Read more.
This paper considers a decentralized and autonomous wireless network of low SWaP (size, weight, and power) fixed-wing UAVs (unmanned aerial vehicles) used for remote exploration and monitoring of targets in an inaccessible area lacking communication infrastructure. Here, the UAVs collaborate to find target(s) and use routing protocols to forward the sensed data of target(s) to an aerial base station (BS) in real-time through multihop communication, which can then transmit the data to a control center. However, the unpredictability of target locations and the highly dynamic nature of autonomous, decentralized UAV networks result in frequent route breaks or traffic disruptions. Traditional routing schemes cannot quickly adapt to dynamic UAV networks and can incur large control overhead and delays. In addition, their performance suffers from poor network connectivity in sparse networks with multiple objectives (exploration and monitoring of targets), which results in frequent route unavailability. To address these challenges, we propose two routing schemes: Pipe routing and TC-Pipe routing. Pipe routing is a mobility-, congestion-, and energy-aware scheme that discovers routes to the BS on-demand and proactively switches to alternate high-quality routes within a limited region around the routes (referred to as the “pipe”) when needed. TC-Pipe routing extends this approach by incorporating a decentralized topology control mechanism to help maintain robust connectivity in the pipe region around the routes, resulting in improved route stability and availability. The proposed schemes adopt a novel approach by integrating the topology control with routing protocol and mobility model, and rely only on local information in a distributed manner. Comprehensive evaluations under diverse network and traffic conditions—including UAV density and speed, number of targets, and fault tolerance—show that the proposed schemes improve throughput by reducing flow interruptions and packet drops caused by mobility, congestion, and node failures. At the same time, the impact on coverage performance (measured in terms of coverage and coverage fairness) is minimal, even with multiple targets. Additionally, the performance of both schemes degrades gracefully as the percentage of UAV failures in the network increases. Compared to schemes that use dedicated UAVs as relay nodes to establish a route to the BS when the UAV density is low, Pipe and TC-Pipe routing offer better coverage and connectivity trade-offs, with the TC-Pipe providing the best trade-off. Full article
Show Figures

Figure 1

Figure 1
<p>Illustration of a decentralized and autonomous UAV network for remote monitoring of an inaccessible area where a communication infrastructure is not available. Here, the UAVs collaborate to provide robust routes for transmitting the sensed information of ground-based targets to a base station while performing fast area coverage.</p>
Full article ">Figure 2
<p>Challenges in a decentralized and autonomous UAV network, where low SWaP UAVs are tasked to provide fast area coverage while maintaining strong network connectivity, and assist in reliably forwarding sensed data of multiple target UAVs to the BS within the latency constraints.</p>
Full article ">Figure 3
<p>Modules used in our proposed Pipe and TC-Pipe routing schemes.</p>
Full article ">Figure 4
<p>Illustration of a pipe around the current route (red links) from the target UAV to BS. The pipe consists of nodes (green nodes) that are up to 2-hop from the nodes along the route (red nodes).</p>
Full article ">Figure 5
<p>Illustration of pipe thinning problem, where the node <math display="inline"><semantics> <msup> <mi>N</mi> <mo>′</mo> </msup> </semantics></math> has no one-hop neighbors except the upstream and downstream nodes on the current route.</p>
Full article ">Figure 6
<p>Applying a pheromone mask to attract UAVs.</p>
Full article ">Figure 7
<p>The target locations in a 6 × 6 <math display="inline"><semantics> <mrow> <msup> <mi>km</mi> <mn>2</mn> </msup> </mrow> </semantics></math> map. Three different target locations are shown for a single target in (<b>a</b>–<b>c</b>) and for a group of 3-targets in (<b>d</b>–<b>f</b>).</p>
Full article ">Figure 8
<p>Average route length for three-target locations.</p>
Full article ">Figure 9
<p>Routing Performance: PDR for single-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>1</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>2</mn> </msub> </semantics></math>, and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>3</mn> </msub> </semantics></math>. Suffix “-20” (e.g., TC-Pipe-20, AODV-20) indicate UAVs at 20 m/s, while “-40” indicates UAVs at 40 m/s speeds.</p>
Full article ">Figure 10
<p>Routing Performance: PDR for three-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>4</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math>, and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>6</mn> </msub> </semantics></math>.</p>
Full article ">Figure 11
<p>Routing Performance: Route Up for three-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>4</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math>, and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>6</mn> </msub> </semantics></math>.</p>
Full article ">Figure 12
<p>Routing Performance: Route Breaks for three-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>4</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>6</mn> </msub> </semantics></math>.</p>
Full article ">Figure 13
<p>Coverage vs. Time plots for three-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>4</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>6</mn> </msub> </semantics></math>.</p>
Full article ">Figure 14
<p>Coverage Performance: <math display="inline"><semantics> <msub> <mi>C</mi> <mi>v</mi> </msub> </semantics></math> for three-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>4</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>6</mn> </msub> </semantics></math></p>
Full article ">Figure 15
<p>Coverage performance: Fairness for three-target settings <math display="inline"><semantics> <msub> <mi>C</mi> <mn>4</mn> </msub> </semantics></math>, <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math> and <math display="inline"><semantics> <msub> <mi>C</mi> <mn>6</mn> </msub> </semantics></math>.</p>
Full article ">Figure 16
<p>PDR values for UAV speed of 40 m/s with 30 and 50 UAVs, for single-target setting <math display="inline"><semantics> <msub> <mi>C</mi> <mn>2</mn> </msub> </semantics></math> and three-target setting <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math>.</p>
Full article ">Figure 17
<p>Routing and Coverage metrics for UAV speed of 40 m/s, with 30 and 50 UAVs, for single-target setting <math display="inline"><semantics> <msub> <mi>C</mi> <mn>2</mn> </msub> </semantics></math> and three-target setting <math display="inline"><semantics> <msub> <mi>C</mi> <mn>5</mn> </msub> </semantics></math>.</p>
Full article ">
20 pages, 4851 KiB  
Article
Research on a Network Diagnosis Method for a Train Control Center and Interlocking Integrated System Based on a Fuzzy Broad Learning System Model
by Lei Yuan, Yinghui Li, Guodong Wei and Wenzhang Guo
Electronics 2025, 14(4), 691; https://doi.org/10.3390/electronics14040691 - 10 Feb 2025
Viewed by 352
Abstract
In high-speed railway signaling systems, the network structure of the Train Control Center and Inter-locking Integrated System (TIS) is highly complex, with a large number of interfaces, numerous redundant channels, and forwarding components such as switches. These factors result in challenges such as [...] Read more.
In high-speed railway signaling systems, the network structure of the Train Control Center and Inter-locking Integrated System (TIS) is highly complex, with a large number of interfaces, numerous redundant channels, and forwarding components such as switches. These factors result in challenges such as insufficient accuracy, low efficiency, and poor real-time performance in terms of network monitoring and fault diagnosis. As the scale of railway yards continues to expand, these issues are becoming increasingly prominent. To address these challenges, this paper proposes a network fault propagation model based on the Fuzzy Broad Learning System (FBLS). By leveraging nonlinear transformations and feature mapping techniques, FBLS can efficiently extract and analyze network fault features, even with a relatively small amount of data. Experimental results show that the FBLS-based diagnostic model achieves higher accuracy and faster response speed in fault identification and propagation path analysis compared to traditional graph theory and fuzzy reasoning methods. Further comparisons with existing methods validate the advantages of FBLS in handling multi-source data, improving noise tolerance, and adapting to large-scale railway yard network systems, demonstrating its broad application prospects in railway signaling systems. Full article
Show Figures

Figure 1

Figure 1
<p>FBLS Basic Architecture.</p>
Full article ">Figure 2
<p>Structure of the <math display="inline"><semantics> <mrow> <mi>i</mi> </mrow> </semantics></math>-th fuzzy subsystem in a fuzzy BLS.</p>
Full article ">Figure 3
<p>Typical TIS Structure Diagram.</p>
Full article ">Figure 4
<p>TIS System Network Monitoring Physical Interface.</p>
Full article ">Figure 5
<p>The Overall Framework of the Network Fault Diagnosis Model Based on FBLS.</p>
Full article ">Figure 6
<p>Accuracy Analysis of the FBLS Model with NumRule and NumFuzz Parameters. (<b>a</b>) Training accuracy of the FBLS model as a function of NumRule, with NumFuzz values indicated by color; (<b>b</b>) Testing accuracy of the FBLS model as a function of NumRule, with NumFuzz values indicated by color.</p>
Full article ">Figure 7
<p>3D Visualization of Training and Testing Accuracy Based on NumRule and NumFuzz. (<b>a</b>) Training accuracy of the model based on NumRule and NumFuzz values; (<b>b</b>) Testing accuracy of the model based on NumRule and NumFuzz values.</p>
Full article ">Figure 8
<p>Scatter plot of true labels and predicted labels under the FBLS model and the fuzzy inference model. (<b>a</b>) Accuracy of the fuzzy inference model; (<b>b</b>) Accuracy of the FBLS method.</p>
Full article ">Figure 9
<p>The fault propagation path display effect of the TIS system. Green indicates normal, orange indicates partial failure, red indicates failure, and gray indicates unknown.</p>
Full article ">Figure 10
<p>Readable language fuzzy rules (ILFR) display effect.</p>
Full article ">
27 pages, 892 KiB  
Article
A Blockchain Solution for the Internet of Vehicles with Better Filtering and Adaptive Capabilities
by Xueli Shen and Runyu Ma
Sensors 2025, 25(4), 1030; https://doi.org/10.3390/s25041030 - 9 Feb 2025
Viewed by 560
Abstract
The traditional consensus algorithm based on the Internet of Vehicles (IoV) system has the disadvantages of high latency, low reliability, and weak fault tolerance, and it cannot make real-time adjustments according to the actual environment, making the system vulnerable to malicious control, inefficiency, [...] Read more.
The traditional consensus algorithm based on the Internet of Vehicles (IoV) system has the disadvantages of high latency, low reliability, and weak fault tolerance, and it cannot make real-time adjustments according to the actual environment, making the system vulnerable to malicious control, inefficiency, and poor environmental adaptability. To solve this problem, we propose a gradually accelerating environment adaptive consensus algorithm, AE-PBFT, that can be applied to IoV. It includes a trust management model that achieves gradual acceleration by recording the historical continuous behavior of nodes, thereby improving the efficiency of screening nodes with different intentions, accelerating the consensus process, and reducing latency. At the same time, we introduce a dynamic consensus group division mechanism based on environmental adaptive changes, which can adaptively adjust the number of nodes participating in the consensus process according to the needs of the operating environment, to deal with extreme situations, thereby improving the reliability and fault tolerance of the system. Experiments confirm that the performance of our proposed solution is superior to current solutions in terms of consensus latency and fault tolerance and is more suitable for the operating environment of IoV. Full article
(This article belongs to the Section Internet of Things)
Show Figures

Figure 1

Figure 1
<p>Consensus process of PBFT algorithm.</p>
Full article ">Figure 2
<p>Consensus process of AE-PBFT algorithm.</p>
Full article ">Figure 3
<p>Model training speed under different learning rates.</p>
Full article ">Figure 4
<p>Trust management model based on gradual acceleration mechanism.</p>
Full article ">Figure 5
<p>Recording semaphore mechanism.</p>
Full article ">Figure 6
<p>Simulated mutex semaphore mechanism.</p>
Full article ">Figure 7
<p>Construction of IoV system.</p>
Full article ">Figure 8
<p>Consensus latency.</p>
Full article ">Figure 9
<p>Throughput.</p>
Full article ">Figure 10
<p>Communication overhead.</p>
Full article ">Figure 11
<p>Consensus latency under malicious nodes.</p>
Full article ">Figure 12
<p>Fault-tolerance ability.</p>
Full article ">
16 pages, 704 KiB  
Article
Time-Synchronized Fault-Tolerant Control for Robotic Manipulators
by Duansong Wang, Gang Zhang, Rui Chen, Jinzhong Zhang and Tan Zhang
Mathematics 2025, 13(3), 507; https://doi.org/10.3390/math13030507 - 3 Feb 2025
Viewed by 420
Abstract
This article proposes a time-synchronized fault-tolerant convergence control method for n-degree-of-freedom robotic manipulators. The main challenge lies in driving the tracking errors of all joints to converge simultaneously, especially in the presence of system faults, external disturbances, and model uncertainties. We introduce a [...] Read more.
This article proposes a time-synchronized fault-tolerant convergence control method for n-degree-of-freedom robotic manipulators. The main challenge lies in driving the tracking errors of all joints to converge simultaneously, especially in the presence of system faults, external disturbances, and model uncertainties. We introduce a normalized sign function that guarantees the property of ratio persistence for all joints and plays a crucial role in time-synchronized convergence control. A time-synchronized convergence observer is proposed that not only adopts a time-synchronized convergence control framework but also overcomes the lumped uncertainty term, which includes the system fault components, external disturbances, and system uncertainties. A salient feature of this method is that, regardless of the initial state and various uncertainties, each component of the robot manipulator system can simultaneously converge to an equilibrium point. Simulations conducted on a two-link robotic manipulator demonstrate the notable benefits of the designed time-synchronized control method, as evidenced by the comparative results. Full article
Show Figures

Figure 1

Figure 1
<p>Model of a knee rehabilitation robotic manipulator. (<b>a</b>) Physical Structure Diagram (<b>b</b>) Description of each variable.</p>
Full article ">Figure 2
<p>The tracking performance of joint 1.</p>
Full article ">Figure 3
<p>The tracking performance of joint 2.</p>
Full article ">Figure 4
<p>Tracking errors of two joints: (<b>a</b>) time-synchronized convergence curves; (<b>b</b>) enlarged time-synchronized convergence curves; (<b>c</b>) tracking error curves for controller 1; (<b>d</b>) tracking error curves for controller 2.</p>
Full article ">Figure 5
<p>Three-dimensional bar chart comparing the controllers’ tracking errors.</p>
Full article ">
20 pages, 2464 KiB  
Article
z-Ary Compression Event-Triggered Control for Spacecraft with Adhesive-Resilient Prescribed Performance
by Ze Yang, Baoqing Yang, Ruihang Ji, Tong Wang and Jie Ma
Mathematics 2025, 13(3), 386; https://doi.org/10.3390/math13030386 - 24 Jan 2025
Viewed by 452
Abstract
The attitude tracking control for spacecraft with limited communication and actuator faults is investigated in this paper by employing event-trigger-based prescribed control. Traditional methods struggle to address arbitrary initial conditions and fault-induced saturation, which both lead to prescribed control singularities, limiting practical deployment. [...] Read more.
The attitude tracking control for spacecraft with limited communication and actuator faults is investigated in this paper by employing event-trigger-based prescribed control. Traditional methods struggle to address arbitrary initial conditions and fault-induced saturation, which both lead to prescribed control singularities, limiting practical deployment. This paper proposes the adhesive-resilient prescribed control (ARPC), which dynamically adjusts the performance envelope by sensing fault and error trends through resilient correction and an adhesive mechanism, respectively. This approach significantly enhances conservatism and robustness, particularly under actuator faults that exceed the saturation level. Additionally, the challenge of balancing high performance with low communication burden under limited resources is addressed. To mitigate communication frequency and bit consumption without sacrificing performance, a z-ary compression event-triggered scheme (CES) is introduced. Compared to existing methods, this work provides substantial improvements in fault tolerance, communication efficiency, and performance adaptability. Numerical experiments demonstrate the superiority of our method in regulating tracking error within a custom envelope and appointed time, regardless of initial conditions, while minimizing communication usage. Full article
Show Figures

Figure 1

Figure 1
<p>Structural relationship of ARPC and CES.</p>
Full article ">Figure 2
<p>Calculate <math display="inline"><semantics> <msub> <mi>z</mi> <mi>i</mi> </msub> </semantics></math> based on performance function properties.</p>
Full article ">Figure 3
<p>Comparison between traditional PPC and ARPC.</p>
Full article ">Figure 4
<p>CET update strategy.</p>
Full article ">Figure 5
<p>Lumped faults and actuator saturation.</p>
Full article ">Figure 6
<p>Time response of Euler angles under the proposed ARPC with CES.</p>
Full article ">Figure 7
<p>Time response of <math display="inline"><semantics> <mrow> <msub> <mi>q</mi> <mrow> <mi>e</mi> <mi>v</mi> </mrow> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> under the proposed ARPC with CES.</p>
Full article ">Figure 8
<p>Response comparison about ARPC and existing methods.</p>
Full article ">Figure 9
<p>Response of <math display="inline"><semantics> <mrow> <msub> <mi>v</mi> <mi>a</mi> </msub> <mrow> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> under CES.</p>
Full article ">Figure 10
<p>Trigger levels at different times under CES.</p>
Full article ">Figure 11
<p>Performance comparison of CES with other ET schemes.</p>
Full article ">
36 pages, 15476 KiB  
Article
Hybrid System for Fault Tolerance in Selective Compliance Assembly Robot Arm: Integration of Differential Gears and Coordination Algorithms
by Claudio Urrea, Pablo Sari and John Kern
Technologies 2025, 13(2), 47; https://doi.org/10.3390/technologies13020047 - 24 Jan 2025
Viewed by 1060
Abstract
This study presents a fault-tolerant control system for Selective Compliance Assembly Robot Arm (SCARA) robots, ensuring operational continuity in cooperative tasks. It is evaluated in five scenarios: normal operation, failures without reconfiguration, and with active reconfiguration. The system employs redundant actuators, differential gears, [...] Read more.
This study presents a fault-tolerant control system for Selective Compliance Assembly Robot Arm (SCARA) robots, ensuring operational continuity in cooperative tasks. It is evaluated in five scenarios: normal operation, failures without reconfiguration, and with active reconfiguration. The system employs redundant actuators, differential gears, torque limiters, and rapid detection and reconfiguration algorithms. Simulations in MATLAB R2024a demonstrated reconfiguration times of 0.5 s and reduced trajectory errors (0.0042 m on the X-axis for Robot 1), achieving efficiency above 99%. Nonlinear Model Predictive Controllers (NLMPCs) and Adaptive Sliding Mode Control (ASMC) were compared, with NLMPC excelling in stability and ASMC in precision. The system showcased high productivity in pick-and-place tasks, even under critical failures, establishing itself as a robust solution for industrial environments requiring high reliability and advanced automation. Full article
(This article belongs to the Section Assistive Technologies)
Show Figures

Figure 1

Figure 1
<p>Fault-tolerant system diagram for the cooperative SCARA system.</p>
Full article ">Figure 2
<p>Arrangement of primary and redundant actuators in SCARA robots.</p>
Full article ">Figure 3
<p>SCARA robot components: (<b>a</b>) base; (<b>b</b>) first arm; (<b>c</b>) second arm; (<b>d</b>) shaft.</p>
Full article ">Figure 4
<p>SCARA system prototype.</p>
Full article ">Figure 5
<p>Kinematic diagram of the SCARA robot.</p>
Full article ">Figure 6
<p>Fault detection in the SCARA system.</p>
Full article ">Figure 7
<p>Fault diagnosis SCARA system.</p>
Full article ">Figure 8
<p>System reconfiguration.</p>
Full article ">Figure 9
<p>Differential gear system.</p>
Full article ">Figure 10
<p>Servomotor prototype: (<b>a</b>) front view; (<b>b</b>) isometric view.</p>
Full article ">Figure 11
<p>Differential gear system prototype.</p>
Full article ">Figure 12
<p>Torque limiter prototype: (<b>a</b>) front view; (<b>b</b>) isometric view.</p>
Full article ">Figure 13
<p>Electromechanical circuit of the differential system.</p>
Full article ">Figure 14
<p>Working area of Robot 1 and Robot 2.</p>
Full article ">Figure 15
<p>Cooperative system in collision: (<b>a</b>) position collision; (<b>b</b>) orientation collision.</p>
Full article ">Figure 16
<p>Algorithm for coordinating the robots when performing cooperative tasks.</p>
Full article ">Figure 17
<p>Virtual environment of the SCARA cooperative system.</p>
Full article ">Figure 18
<p>Cooperative object manipulation process by the SCARA robots: (<b>a</b>) movement of green objects; (<b>b</b>) movement of red objects; (<b>c</b>) movement of blue objects; (<b>d</b>) completion of the cooperative task.</p>
Full article ">Figure 19
<p>Cooperative object manipulation process by the SCARA robots with a failure in Actuator 1 of Robot 1: (<b>a</b>) movement of green objects; (<b>b</b>) the robots transport red objects with the first actuator of Robot 1 defective; (<b>c</b>) movement of blue objects with the first actuator of Robot 1 defective; (<b>d</b>) completion of the inefficient cooperative task.</p>
Full article ">Figure 20
<p>Cooperative object manipulation process by the SCARA robots with a failure in actuator 2 of Robot 2: (<b>a</b>) movement of red objects; (<b>b</b>) the robots hold blue objects; (<b>c</b>) movement of blue objects with the second primary actuator of Robot 2 defective; (<b>d</b>) completion of the inefficient cooperative task.</p>
Full article ">Figure 20 Cont.
<p>Cooperative object manipulation process by the SCARA robots with a failure in actuator 2 of Robot 2: (<b>a</b>) movement of red objects; (<b>b</b>) the robots hold blue objects; (<b>c</b>) movement of blue objects with the second primary actuator of Robot 2 defective; (<b>d</b>) completion of the inefficient cooperative task.</p>
Full article ">Figure 21
<p>Positions in the primary and redundant actuators of the SCARA robots with a failure in Actuator 1 of Robot 1: (<b>a</b>) Robot 1; (<b>b</b>) Robot 2.</p>
Full article ">Figure 22
<p>Positions in the primary and redundant actuators of the SCARA robots with a failure in the second primary actuator of Robot 2: (<b>a</b>) Robot 1; (<b>b</b>) Robot 2.</p>
Full article ">Figure 23
<p>Desired and measured trajectories of the SCARA robots.</p>
Full article ">Figure 24
<p>Positions in the primary and redundant actuators of the SCARA robots with a failure in the first primary actuator of Robot 1 and the second primary actuator of Robot 2: (<b>a</b>) Robot 1; (<b>b</b>) Robot 2.</p>
Full article ">Figure 25
<p>Desired and measured trajectories of the SCARA robots with multiple actuator failures.</p>
Full article ">Figure 26
<p>Joint positions of the robots with multiple failures: (<b>a</b>) Robot 1; (<b>b</b>) Robot 2.</p>
Full article ">Figure 27
<p>Cooperative process for transporting a table between both robots: (<b>a</b>) robots hold the table; (<b>b</b>) robots lift the table; (<b>c</b>) robots transport the table; (<b>d</b>) completion of the cooperative task.</p>
Full article ">Figure 28
<p>Trajectories performed by the robots in the presence of a failure in Actuator 1 of Robot 1 and Actuator 2 of Robot 2.</p>
Full article ">Figure 29
<p>Position errors in the trajectories performed by the robots in the presence of failures in the primary Actuator 1 of Robot 1 and Actuator 2 of Robot 2: (<b>a</b>) Robot 1; (<b>b</b>) Robot 2.</p>
Full article ">Figure 30
<p>Trajectory errors when an actuator failure occurs in Robot 1 and Robot 2.</p>
Full article ">Figure 31
<p>Bar chart of the trajectory errors of the robots on the X, Y, and Z axes using the fault-tolerant system and NLMPC and ASMC controllers.</p>
Full article ">Figure 32
<p>Bar chart of the percentage efficiency in the cooperative task for robots using NLMPC and ASMC controllers.</p>
Full article ">
Back to TopTop