Dr. Dawei Li
Associate Professor
Address: Unmanned Aerial Vehicle Research Institute, Beihang University (BUAA), Beijing, 100191, P R China
Phone: 010-82317394, 13810026101
Email: david@buaa.edu.cn
Dr. Dawei Li is currently an associate professor in School of Aeronautical Science and Engineering Technology at Beihang University. As a master advisor, Prof. Li has strong academic background and practical experience in the field of aircraft design and flight control. He received his Ph.D degree in Navigation, Guidance and Control from Beihang University in 2013. He has over 10 archival journal papers, conference papers, and technical reports, in the areas of Aircraft Aerodynamics, Inflow control and Flight control. His main research field is in flight vehicle design, Computational fluid dynamics, flight control and adaptive control. He took charge and participated in many scientific research items: the young talent Program Foundation for the Talents by the Ministry of Education of China, the National Natural Science Foundation, etc. His research in Aircraft design got award of science and technology advancement in Beihang University. He is the senior fellow of Chinese Society of Aeronatics and Astronatics. From Oct. 2012 to Present, he was the Depute Director of Aircraft Research Laboratory in the Unmanned Aerial Vehicle Research Institute, and he was responsible for the research programs of key design tech. of UAV.
1. Personal Details
Date of Birth: March 1979
Place of Birth: Qiqihar, Heilongjiang, China
Nationality: Chinese
Languages: Chinese, English
2. Current Research Interests
flight vehicle (especially UAV) design, Computational fluid dynamics, flight control and adaptive control.
3. Education
2013: Ph.D. in Navigation, Guidance and Control, School of Automation Science & Electrical Engineering, Beihang University, Beijing, China (Advisors: Prof. Wang Honglun. Thesis Title: Unmanned Aerial Vehicle Flight Control in Automated Aerial Refueling)
2005: M.Sc in Flight vehicle design, School of Aeronautic Science and Engineering, Beihang University, Beijing, China.
2001: B.Sc in Flight vehicle design, Department of Flying Vehicle Design and Applied Mechanics, Beihang University, Beijing, China.
4. Employment
2013.7-Present: Associate professor, School of Aeronautic Science and Engineering, Beihang University, Beijing, China.
2001-present: Senior Research Scientist, Unmanned Aerial Vehicle Research Institute, Beihang University, Beijing, China.
5. Publication list
Journal Papers:
[1] Li Da-Wei, Zhang Yun-Fei, Ma Dong-Li. Design and numerical investigation of dorsal S-shaped inlet[J]. Journal of Propulsion Technology,2006,27(1):61-65.
[2] Li Dawei, Ma Dongli. Improving dorsal S-shaped inlet performance by vortex flow control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(12): 1456-1459.
[3] LI Dawei, WANG Honglun. Wake vortex effect modeling and simulation in automated aerial refueling[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7): 776-780.
[4] Li Dawei, Ma Dongli1, Chen Xiaolong. Comparison of experimental ground testing and computational fluid dynamics for S-shaped inlet and JT15D-4 engine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(4): 449-452+458.
[5] Li Dawei, Ma Dongli. Numerical investigation of S-shaped inlet performance at different angle of attack with and without vortex generators[J]. Journal of Harbin Institute of Technology, 2013,45(5):114-118.
[6] Li Da-Wei, Yan Wen-Cheng, Jiang Feng. Aerodynamic optimization for short range UAV using vortex lattice method and wind tunnel verification[J]. Journal of Experiments in Fluid Mechanics,2012,26(3):61-65.
[7] LI Da-wei, WANG hong-lun. UAV Flight control in automated aerrial refueling[J]. Journal of System Simulation,2010,22(suppl.1):126-130.
[8] Li Dawei, Wang Honglun, Gai Wendong. L1 adaptive control for automated aerial refueling[J]. Control Theory & Applications,2014,31(5):.
Conferences:
[1] Li Dawei, Wang Honglun, Gai Wendong. Application of a Feedforward Controller with a Disturbance Observer for UAV during Missile Launch. 2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, Zhengzhou, China, 2011: 2811-2815. (EI: 20114014388374)
