A5040630828- Vehicle Dynamics and Control Systems
- Hydraulic and Pneumatic Systems
- Manufacturing Process and Optimization
- Simulation and Modeling Applications
- Autonomous Vehicle Technology and Safety
- Traffic control and management
- Real-time simulation and control systems
- Brake Systems and Friction Analysis
- Advanced machining processes and optimization
- Engineering and Test Systems
- Product Development and Customization
- Industrial Automation and Control Systems
- Advanced Numerical Analysis Techniques
- Aerodynamics and Fluid Dynamics Research
- Control Systems and Identification
- Advanced Measurement and Detection Methods
- Electric and Hybrid Vehicle Technologies
- Engineering Technology and Methodologies
- Advanced Sensor and Control Systems
- Control Systems in Engineering
- Design Education and Practice
Beihang University
2016-2021
Guizhou Institute of Technology
2018
Guizhou University
2018
Radio, Film & TV Design and Research Institute
2010
Beijing Institute of Technology
2004
Shaanxi Research Association for Women and Family
2004
Hsin Sheng College of Medical Care and Management
2002
The aircraft antiskid braking system is an important hydraulic for preventing tire bursts and ensuring safe take-off landing. brake adjusts the force applied on discs by controlling pressure. Traditional systems achieve performance pressure with electrohydraulic servo valve. Because pilot stage of valve easily blocked carbonized oil, would become a dangerous weak point safety. This paper proposes new approach that uses on-off array to replace control. Based this control component, efficient...
This article proposes a real-time maximum tire–road friction tracking control method with disturbance compensation for aircraft antiskid braking system (ABS). Conventional ABS cannot accurately set the optimal slip ratio in real time runways different characteristics, resulting not being completely utilized time. To address this problem, first, runway identification is developed to determine of initial runway. Then, an update algorithm based on Burckhardt model proposed according...
Reliability and efficiency under complex working conditions are the ultimate goal of aircraft wheel brake system. In order to ensure safety different conditions, traditional control methods for braking tend be conservative in parameter adjustment, resulting loss efficiency. this article, an antiskid algorithm based on reinforcement learning (RL) is designed, which takes both into consideration. Meanwhile, solve problems generalization difficulty designing reward function high failure rate...
Affected by the mutation of runway condition, crosswind, unbalance load and different performance brake device on both sides wheels, there will generally appear yaw angle lateral offset while unmanned aerial vehicle (UAV) is taxiing. The UAV would skid off cause serious accident if are not corrected in time. In this paper, a dynamic allocation algorithm for gain nose wheel steering differential braking based decomposition control proposed to correct these departures make turning back center...
This article has been retracted by the publisher.
Aiming to solute low efficiency in sorting and packaging process of non-conventional type cigarette, a steady rapid automatic palletizing tray institution was designed this paper.Based on the three-dimensional model established by software SolidWorks, mechanical properties were analyzed.The results showed that most obvious deformation occurred top right-hand corner pushing board, but it does not affect actual work effect cigarette mechanism.The largest stress point is connection rod, value...
The aircraft brake system is one of the most important airborne subsystems, which determines braking distance and safety. efficiency parameters system. How to match based on always a difficult problem. In this paper, method matching constraint proposed for large aircraft. First, an accurate model whole plane are established. Secondly, simulation performance test each component carried out. Finally, integral system, design obtained. in paper can proceed from carry out parameter thus...