Shiyu Hao

ORCID: 0009-0004-8078-805X
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About
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Research Areas
  • Fusion materials and technologies
  • Fault Detection and Control Systems
  • Robotic Path Planning Algorithms
  • Metal and Thin Film Mechanics
  • Real-time simulation and control systems
  • Electromagnetic Launch and Propulsion Technology
  • Electromagnetic Effects on Materials
  • Diamond and Carbon-based Materials Research
  • Mechanical Engineering and Vibrations Research
  • Aerospace Engineering and Energy Systems
  • Combustion and Detonation Processes
  • Soil Mechanics and Vehicle Dynamics
  • Energetic Materials and Combustion
  • Advanced Sensor and Control Systems
  • Intermetallics and Advanced Alloy Properties
  • Agriculture and Farm Safety
  • Adaptive Control of Nonlinear Systems
  • Electric and Hybrid Vehicle Technologies
  • Nuclear Materials and Properties
  • Vehicle emissions and performance
  • Hydraulic and Pneumatic Systems
  • Aerospace and Aviation Technology
  • Metal Alloys Wear and Properties
  • Vacuum and Plasma Arcs
  • Spacecraft Dynamics and Control

Xi'an Jiaotong University
2000-2024

Civil Aviation University of China
2024

State Key Laboratory of Electrical Insulation and Power Equipment
2023-2024

Northwestern Polytechnical University
2023-2024

The modular augmented staged electromagnetic launcher can save electric current through the armature and increase projectile acceleration, helping to miniaturize system. First, predict performance, an improved simulation method considering rail coil structure as well coupling magnetic field action is proposed. proposed then used compare equal-length equal-time segment ways of two-stage launcher. It demonstrated that former holds a higher muzzle velocity segment-by-segment rise in efficiency....

10.1109/tps.2023.3297733 article EN IEEE Transactions on Plasma Science 2023-08-01

Limited research has been conducted on the interaction forces between clamping and lifting mechanism front landing gear wheel during overall turning of towbarless aircraft tractors aircraft. To address this issue, Adams software was utilized to model along with for dynamic simulation. Subsequently, an analysis simulation results conducted. The indicate that turning, shifts in aircraft's center gravity result fluctuating horizontal acting mechanism. Furthermore, angle plane is much more...

10.1117/12.3039473 article EN 2024-08-28

The geometry nonlinear aeroelastic problems of the high-aspect-ratio unmanned aerial vehicles (UAV) are prominent, which will bring many adverse factors to flight control. A UAV controller design technique in accordance with L1 adaptive control algorithm is therefore suggested increase system's robustness. First, effects brought by aerodynamic lift surface model static problem analyzed. Then, a longitudinal channel designed, including law, and state observer. Next, stability designed...

10.1109/rcae59706.2023.10398852 article EN 2023-11-03

Abstract: The performance of the gaseous fuel supply and its influence on hydrocarbon (HC) emissions dual-fuel engines have been investigated. A new design manifold respirators with mixers is also presented in paper. system has a great HC engine at light load. problem scavenging discussed solved by using engine. It performs function retarding entry timing from moment intake valve opening, delaying effects measured tested. Experimental results show that respirator gives best reducing compared...

10.1177/095440700021400815 article EN Proceedings of the Institution of Mechanical Engineers Part D Journal of Automobile Engineering 2000-08-01

A set of hardware in the loop simulation methods based on UAV model is proposed to create fault data, which used judge parts where faults happen. Actual flight experimental data utilized prove reliability Simulink models. Then a series typical with various amplitudes are injected into different channels platform. Fault created this way, and effect task/control can be obtained through damage analysis. Typical characters extracted, those that have analyzed judged. We also know trend will...

10.48550/arxiv.2309.03462 preprint EN other-oa arXiv (Cornell University) 2023-01-01

A set of hardware in the loop simulation methods based on UAV model is proposed to create fault data, which used judge parts where faults happen. Actual flight experimental data utilized prove reliability Simulink models. Then a series typical with various amplitudes are injected into different channels platform. Fault created this way, and effect task/control can be obtained through damage analysis. Typical characters extracted, those that have analyzed judged. We also know trend will...

10.1109/frse58934.2023.00024 article EN 2023-06-01
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