School of Electrical and Information Engineering
Associate professor
control theory and control engineering
13821113851
douliqian@tju.edu.cn
No.92, Weijin Road, Nankai District, Tianjin, China.
300072
Liqian Dou received his B.Eng. degree form Tianjin University in 1999. He received his M.Sc. degree and the Ph.D. degrees in control science and engineering from Tianjin University in 2005 and 2008. After working as a Lecture for three years in school of Electrical Engineering and Automation,Tianjin University. From 2016 to 2017, he visited, as an academic visitor, The University of Manchester, UK, where he studied nonlinear control methods and application in flight control. Now he is an associate professor with School of Electrical and Information Engineering, Tianjin University. His research interests are focused on modeling and control for hypersonic vehicle, Autonomic cooperation control for multiple UAVs, and Intelligent control technology.
- Master’s Degree| Tianjin University| control science and engineering| 2005
- Bachelor’s Degree| Tianjin University| Industrial Automation| 1999
- Doctoral degree| Tianjin University| control science and engineering| 2008
- Intelligent control system
- Modeling and control of Hypersonic vehicle
- Formation control of multiple UAV
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1999.9-2002.6
Tianjin thermo power company | Assistant Engineer
- Papers
- [1] Attitude controller design for reusable launch vehicles during reentry phase via compound adaptive fuzzy H-infinity control
- [2] Fuzzy disturbance observer-based dynamic surface control for air-breathing hypersonic vehicle with variable geometry inlets
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- [3] Modeling and nonlinear control for air-breathing hypersonic vehicle with variable geometry inlet
- [4] Identification of nonlinear aeroelastic system using fuzzy wavelet neural network
- [5] Iterative Identification andControl Design with Optimal Excitation Signals Based on v-gap
- [6] Identification of nonlinear aeroelastic systems based on neural network
- [7] Trajectory tracking control for underactuated quadrotor UAV based on ESO and backstepping
- [8] Analysis of viscous effects on hypersonic vehicle model characteristics