WANG Xiangyang  Associate Professor, Master Supervisor

Email: wangxy668@tsinghua.edu.cn

Education Background

2008~2014: Ph.D. in Aerospace Science and Technology, Tsinghua University

2004~2008: Bachelor of Engineering in Engineering Mechanics and Aerospace Engineering, Tsinghua University

Work Experience

December 2021 - Present: Associate Professor, Master Supervisor, Institute for Aero-Engine, Tsinghua University

2019 - Present: Assistant Professor, Master Supervisor, Institute for Aero-Engine, Tsinghua University

2014~2019: Postdoctoral Researcher, Department of Computer Science, Tsinghua University

Research Overview

Main research areas include: Integrated Flight/Propulsion Control, Hybrid Electric Power Systems for Aviation Application, Integrated Flight/Propulsion System Design for Vertical Takeoff and Landing (VTOL) Aircraft.

Awards and Honors

2022: First Prize of Military Invention Award (5/6)

2019: "Top Ten" Excellent Postdoc Award by Tsinghua University

Academic Achievements

[1] Wang X Y, Hybrid Electric Tail-sitter VTOL Aircraft - Integrated Flight/Propulsion System Design and Control, China Science Publishing & Media Ltd., 2023

[2] Yang X, Wang X Y*, Zhu J H, Yan W H. Modelling, Analysis and Experimental Study of the Prop-rotor of V/STOL Aircraft. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering，2022.

[3] Yang Y J, Yang J L, Wang X Y*, Zhu J H. Robust Optimal Transition Maneuvers Control for Tail-sitter Unmanned Aerial Vehicles. International Journal of Robust and Nonlinear Control, 2021, 31(16)：8007-8029.

[4] Yang Y J, Wang X Y*, Zhu J H, Yuan X M. Robust Transition Trajectory Optimization for Tail-Sitter UAVs Considering Uncertainties. SCIENCE CHINA Information Sciences, 2023, 66(6): 169201:1-169201:2

[5] Wang X Y, Zhu B, Zhu J H*, et al. Thrust vectoring control of vertical/short takeoff and landing aircraft. Sci China Inf Sci, 2020, 63(2): 1-3

[6] Wang X Y, Yuan X M, Zhu J H*, Yang Y J. Stability Analysis of Tail-Sitters in Vertical Takeoff and Landing Flights, AIAA Journal of Aircraft, 2019, 56(4):1487-1500

[7] Wang X Y, Zhu J H*, Yang J L, et al. Coordination Control Strategy Based on Characteristic Model for 3-Bearing Swivel Duct Nozzles. Science in China - Series E: Technological Sciences，2014，57（4）：838-848.

[8] Wang X Y, Zhu J H*, Liu K, Zheng Y. Kinematic Modeling and Testing of 3-Bearing Swivel Duct Nozzle．Acta Aeronautica et Astronautica Sinica, 2014, 35(4):911-920.