Yang Chao

ORCID: 0000-0001-7146-3545
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About
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Research Areas
  • Adaptive Control of Nonlinear Systems
  • Aerospace and Aviation Technology
  • Aeroelasticity and Vibration Control
  • Computational Fluid Dynamics and Aerodynamics
  • Advanced Sensor and Control Systems
  • Underwater Vehicles and Communication Systems
  • Aerospace Engineering and Control Systems
  • Advanced Algorithms and Applications
  • Advanced Control Systems Optimization
  • Hydraulic and Pneumatic Systems
  • Iterative Learning Control Systems
  • Wind and Air Flow Studies
  • Aerospace Engineering and Energy Systems
  • Aerodynamics and Fluid Dynamics Research
  • Mechanical Engineering and Vibrations Research
  • Atmospheric chemistry and aerosols
  • Plasma and Flow Control in Aerodynamics
  • Industrial Technology and Control Systems
  • Stability and Control of Uncertain Systems
  • Control and Dynamics of Mobile Robots
  • Industrial Automation and Control Systems
  • Robotic Mechanisms and Dynamics
  • Biomimetic flight and propulsion mechanisms
  • Distributed Control Multi-Agent Systems
  • VLSI and FPGA Design Techniques

Jiaxing University
2020-2025

Harbin Engineering University
2017-2025

China Academy of Engineering Physics
2020-2024

China Huadian Corporation (China)
2020

Beijing Aerospace Flight Control Center
2016

Beihang University
2003-2015

Northwest Normal University
2014

Guizhou University
2010

Abstract Establishing a microelastic deformation (micro-deformation) model of end-point parallel manipulators (PMs) in the gravity field is great significance for improving calibration accuracy. Gravity affects limb constraint wrenches space and micro-deformation PMs, which leads to decrease precision end effector. A modeling method was proposed analysis PMs with consideration flexibility rods actuators based on screw theory fix this issue. First, mechanism considered an open-loop by cutting...

10.1115/1.4067720 article EN Journal of Mechanisms and Robotics 2025-01-23

Abstract In the present paper, we study well-posedness of solution to initial boundary value problem for damped Kirchhoff-type wave equation with fractional Laplacian. First, existence and uniqueness local are established by Banach fixed point theorem. Then, global finite time blowup derived at subcritical critical energy levels. Finally, upper bound lower estimate given arbitrarily positive level.

10.1515/ans-2023-0172 article EN cc-by-nc-nd Advanced Nonlinear Studies 2025-03-13

Due to the growing interest using model predictive control (MPC), there are more and researches about applications of MPC on autonomous underwater vehicle (AUV), these mainly focused simulation simple application AUV. This paper focuses improvement based state space an Unlike previous approaches a fixed weighting matrix, in this paper, coefficient, varied with error, is introduced adjust increment vector matrix reduce settling time. Then, analysis effect adjustment stability given. In...

10.3390/s18072321 article EN cc-by Sensors 2018-07-17

The trajectory tracking control problem is addressed for autonomous underwater vehicle (AUV) in marine environment, with presence of the influence uncertain factors including ocean current disturbance, dynamic modeling uncertainty, and thrust model errors. To improve accuracy AUV, an adaptive backstepping terminal sliding mode based on recurrent neural networks (RNN) proposed. Firstly, considering inaccurate thruster, a Taylor's polynomial used to obtain And then, uncertainty errors are...

10.1186/s10033-018-0307-5 article EN cc-by Chinese Journal of Mechanical Engineering 2018-12-01

The joint control problem of the underwater manipulator is addressed in this paper, under influence uncertainty factors such as model uncertainty, external disturbance, and lag. In general, for factors, it usually approximated online, but difficult to select a reasonable value approximation error boundary, too conservative estimated values would cause chattering easily. And lag on should be considered actual work. Unlike most previous method, function technique (FAT), which uses Legendre...

10.3390/app10051728 article EN cc-by Applied Sciences 2020-03-03

For long-term missions in complex seas, the onboard energy resources of autonomous underwater vehicles (AUVs) are limited. Thus, consumption reduction is an important aspect study AUVs. This paper addresses using model predictive control (MPC) based on state space AUVs for trajectory tracking control. Unlike previous approaches, which use a cost function that consists quadratic deviations predicted controlled output from reference and input changes, term (i.e., input) introduced into this...

10.3390/s19010162 article EN cc-by Sensors 2019-01-04

A novel underwater long-arm manipulator (ULAM) and its improved small-flow hydraulic driving system (SHDS) are presented in this article for small autonomous vehicle (AUV). In the process of design, a joint device consisting linear cylinder, three-bar linkage, four-bar linkage mechanism is developed to allow be folded. Since much long, angle deviation would result large end-effector's position deviation. To solve problem, with circulation closed loop proposed. And manipulator,...

10.1177/1729881417747104 article EN cc-by International Journal of Advanced Robotic Systems 2017-11-01

This paper investigates the finite-time tracking problem for autonomous underwater vehicles (AUVs) in presence of external disturbance and modelling uncertainty. A control scheme is proposed based on an improved non-singular terminal sliding mode manifold. Firstly, order to achieve stability avoid singular problem, a continuous smooth manifold designed piecewise function. And then law by indirectly estimating bound general uncertainty, compensate Based Lyapunov analysis, it verified that...

10.1080/00207179.2020.1825818 article EN International Journal of Control 2020-09-21

An optimization design method in the preliminary stage using aeroelastic performance indexes as constraints is proposed to wing stiffness and build primary model. A beam-frame structure model with a high aspect ratio an example built. Stiffness distribution of main beam designed by engineering estimation obtain Because comparative precise, three-dimensional introduced reference for comparison two methods. Static responses are calculated, advantage our verified through comparing analyzing....

10.2514/6.2010-2719 article EN 2010-04-12

<p indent="0mm">As dynamic growth engine of the economy China, Yangtze River Delta (YRD) region is one most densely populated regions around globe with advanced industrial cluster and developed transportation network, which has brought problem high intensity air pollutant emissions including nitrogen oxides (NO<sub><italic>x</italic></sub>), volatile organic compounds (VOCs), etc. Although PM<sub>2.5</sub> quality tremendously improved in recent years, ozone concentration showed an...

10.1360/tb-2021-0774 article EN Chinese Science Bulletin (Chinese Version) 2021-11-17

10.1109/icarcv63323.2024.10821564 article EN 2022 17th International Conference on Control, Automation, Robotics and Vision (ICARCV) 2024-12-12

In this paper, an adaptive multiple-model controller is developed for nonlinear systems in parametric-strict-feedback form.Unlike the previous results, a switching scheme not required here to switch most appropriate model into design.The new reduces number of identification models and uses information provided by all more efficiently than results using convex combination estimates parameters.The method guarantees parameter convergence global asymptotic stability closed-loop system.The...

10.2991/jrnal.2015.2.2.1 article EN Journal of Robotics Networking and Artificial Life 2015-01-01

Digital PID control is one of the most widely used methods in manufacturing process. Based on analysis algorithm, system has designed and simulated incremental controller using LPM macro module built-in FPGA,and also PWM module. The combination two modules can be for a variety applications. results show that design feasible correct.

10.4028/www.scientific.net/amm.602-605.830 article EN Applied Mechanics and Materials 2014-08-11

10.13700/j.bh.1001-5965.2014.0025 article EN Beijing Hangkong Hangtian Daxue xuebao 2015-01-20

Multi-body aircraft is a new concept consisting of multiple small unmanned aerial vehicles hinged-connected by wing tips. This can integrate the performance and advantages two types flying platforms: high-altitude long endurance vehicles. It has great development potential. Based on Newton-Euler equation lifting line method, it establishes multi-body flight dynamics model, analyzes trim stability characteristics system that allowing relative degree freedom rolling motion with dual-aircraft...

10.6052/j.issn.1000-4750.2020.11.0820 article EN 工程力学 2021-11-25
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