Rongwei Guo

ORCID: 0000-0001-8836-0964
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Research Areas
  • Computational Fluid Dynamics and Aerodynamics
  • Nonlinear Dynamics and Pattern Formation
  • Chaos control and synchronization
  • Stability and Control of Uncertain Systems
  • Plasma and Flow Control in Aerodynamics
  • Neural Networks Stability and Synchronization
  • Adaptive Control of Nonlinear Systems
  • Fluid Dynamics and Turbulent Flows
  • Gas Dynamics and Kinetic Theory
  • Heat Transfer and Boiling Studies
  • Innovative Microfluidic and Catalytic Techniques Innovation
  • Distributed Control Multi-Agent Systems
  • Quantum chaos and dynamical systems
  • Rocket and propulsion systems research
  • Stability and Controllability of Differential Equations
  • Aerodynamics and Fluid Dynamics Research
  • Aerospace and Aviation Technology
  • Control and Stability of Dynamical Systems
  • Advanced Control Systems Optimization
  • Fault Detection and Control Systems
  • Aerodynamics and Acoustics in Jet Flows
  • Vibration and Dynamic Analysis
  • Guidance and Control Systems
  • Turbomachinery Performance and Optimization
  • Hydraulic flow and structures

Qilu University of Technology
2015-2025

Shandong Academy of Sciences
2020-2025

State Key Laboratory of Chemical Engineering
2018-2023

Tianjin University
2018-2023

Shandong University
2011-2017

Nanjing University of Aeronautics and Astronautics
2006-2015

Chinese People's Liberation Army
2009-2012

Fujian Research Institute of Light Industry
2011

China Aerodynamics Research and Development Center
2007

Shanghai University
2003-2005

To solve abruptly occurrence of parameters jumping and directed communication topologies changing in the control process networked manipulators, this paper, distributed switched consensus algorithms are formulated for a group robot manipulators realizing cooperative performance. In fact, Lagrange systems modeled as regarding different topologies. Namely, dynamic models switch when system or topology structures change. The strategy is constructed by resorting to (improved) average dwell time...

10.1109/access.2021.3049261 article EN cc-by IEEE Access 2021-01-01

Wind-tunnel tests were conducted to better understand the flow pattern of a hypersonic inlet at an unstable-unstarted condition that is caused by downstream mass choking. High-speed shadowgraph visualization and instantaneous pressure measurements are employed reveal oscillations shock system unsteady process duct flow. Results show both inside in front oscillates intermittently when unstarted. With increase throttling ratio, fundamental frequency goes up shock-on-lip time down, but whereby...

10.2514/1.28039 article EN Journal of Propulsion and Power 2007-06-25

ABSTRACT This paper presents a novel robust consensus control method for multiple nonholonomic wheeled mobile robots (MNWMRs). The involves developing dynamic sliding mode tracker based on the Average Dwell Time (ADT) technique, which tracks velocity state onto kinematic auxiliary vector through torque control. While communication topologies are randomly switched to achieve of virtual trajectories by controlled robots. Furthermore, considering influence strong external disturbances and...

10.1002/rnc.7863 article EN International Journal of Robust and Nonlinear Control 2025-01-30

Abstract This paper investigates the adaptive finite‐time robust control problem of a class nonlinear time‐delay Hamiltonian systems via Lyapunov‐Krasovskii (L‐K) method, and proposes some delay‐dependent results on issue. Different from existing works, this first presents time‐varying stability (FTS) criterion an L‐K functional approach, obtains two FTS conditions by constructing specific functionals. Then, is investigated for port‐controlled (PCH) systems, design procedure presented....

10.1002/asjc.1556 article EN Asian Journal of Control 2017-06-29

This paper investigates the stabilization problem of fractional order systems with both model uncertainty and external disturbance. By combining linear feedback control method, dynamic disturbance estimator (UDE)-based respectively, two new UDE-based methods are developed. Using these methods, can be stabilized by three steps. In first step, controllers designed to stabilize nominal systems. The second step is design a controller estimate third combined into realize those Finally, numerical...

10.1109/access.2021.3060093 article EN cc-by IEEE Access 2021-01-01

In this paper, parameters of a given (chaotic) dynamical system are estimated from time series by using identical synchronization between two different systems. This technique is based on the invariance principle differential equations, i.e., Lyapunov function involving error and estimation parameters. The control used in consists feedback adaptive loop associated with update law Our process indicates that one may identify dynamically all unknown as long available. Lorenz Rössler systems to...

10.1063/1.1635095 article EN Chaos An Interdisciplinary Journal of Nonlinear Science 2003-12-31

Summary The paper presents the results of measurement static pressure, total pressure and swirl in flow through an S-shaped duct typical air intake proportions mounted a wind tunnel tested at different incidences through-flow ratios. In order to reduce magnitude high incidence, two methods have been studied - one, change distribution pressures by means spoiler two, re-energize separated with inflow free stream auxiliary inlets. Measurements were also made, 0° perforated intended simulate...

10.1017/s0001925900009641 article EN Aeronautical Quarterly 1983-05-01

Abstract This paper investigates the stability of a class switched linear systems, and proposes number new results on analysis. A novel analysis method is developed by using 2‐norm technique, then several are obtained based method. It shown that main in this not only guarantee systems under arbitrary switching, but also provide an algorithm to find minimum dwell time (MDT) with which switches make stable. Finally, illustrative examples numerical simulations studied paper. The study shows our...

10.1002/asjc.365 article EN Asian Journal of Control 2011-02-25

Summary This paper proposes a sliding‐mode control (SMC) method to achieve practical cooperative consensus tracking for network of multiple nonholonomic wheeled mobile robots (MNWMRs) with input disturbances. A novel SMC surface under the constraints is first formulated characterize communication interactions among networked framework polar coordinates. unified distributed strategy then proposed by systematically combining position controller and direction controller. Furthermore, simple yet...

10.1002/rnc.4967 article EN International Journal of Robust and Nonlinear Control 2020-04-05

The impulse and self starting characteristics of a mixed-compression hypersonic inlet designed at Mach number 6.5 are studied by applying the unsteady computational fluid dynamics (CFD) method. full Navier–Stokes equations solved with assumption viscous perfect gas model, shear-stress transport (SST) k–ω two-equation Reynolds averaged (RANS) model is used for turbulence modeling. Results indicate that during starting, flow field divided into three zones different aerodynamic parameters...

10.1016/j.cja.2013.04.018 article EN cc-by-nc-nd Chinese Journal of Aeronautics 2013-05-02

Summary As part of a series investigations the swirl in S-ducts, present paper gives results tests on duct with both horizontal and vertical offsets, for comparison earlier work ducts offset only. Results obtained bear similarity to those Reference 2, which had same cross-sectional shapes areas, but addition magnifies resultant considerably. before, is found be sensitive entry conditions, that solid spoiler, blocking off 15% width from inside wall, reverses sense final swirl. Taken overall,...

10.1017/s0001925900009653 article EN Aeronautical Quarterly 1983-05-01

In this paper, a simple adaptive control is proposed for the synchronization of chaotic dynamics resistive–capacitive–inductive-shunted Josephson junctions (RCLSJ). The problem investigated based on drive–response system configuration consisting two identical RCLSJ with and without parameters. addition, when parameters are unknown considered parameter estimation. Sufficient conditions global asymptotic given numerical simulations employed to demonstrate efficiency scheme. presence noise, we...

10.1088/0031-8949/79/03/035801 article EN Physica Scripta 2009-03-01

Hypersonic inlet self-starting ability is of great importance for scramjet engines and hypersonic flight vehicles to operate stably efficiently. However, the prediction limit generally difficult. This paper proposes a flow-based approach limiting internal contraction ratio two-dimensional inlets. The key lies in establishment general approximate expression fluid dynamic blockage, caused by migration primary separation bubble down portion inlet. Formulas blockage are given. predicted results...

10.2514/1.b35703 article EN Journal of Propulsion and Power 2016-02-16

This paper is concerned with the partial anti-synchronization of 4D financial hyper-chaotic system periodically external disturbance. Firstly, existence problem for nominal proven. Then, a suitable filter presented, by which disturbance asymptotically estimated. Moreover, two estimator (DE)-based controllers are designed to realize such system. Finally, numerical simulation verifies effectiveness and correctness proposed results.

10.3390/math10183373 article EN cc-by Mathematics 2022-09-16

For gas–liquid two-phase flow in comb-shaped microchannels, operating conditions could change the pattern and uniformity of distribution further affect mass transfer performance. In this study, hydrodynamics microchannels are investigated. Four patterns observed: single-phase or foam flow, slug-bubbly slug compact flow. When is velocity microchannel ideal, its performance close to that a single microchannel. Before appearance improved with increase ratio rate. After deteriorated

10.1021/acs.iecr.2c03851 article EN Industrial & Engineering Chemistry Research 2023-01-05
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