Shubo Yang Assistant Research Fellow

Email: shubo_yang@tsinghua.edu.cn

Education

Sep. 2014 – Aug. 2020: Ph.D. in Aerospace Propulsion Theory and Engineering, Beihang University

Sep. 2010 – Jun. 2014: B.Eng. in Aircraft Power Engineering, Beihang University

Professional Experience

Mar. 2023 – Present: Assistant Research Fellow, Tsinghua University

Dec. 2020 – Mar. 2023: Postdoctoral Researcher, Beihang University

Research Interests

Modeling and simulation of auxiliary components in aero-engine control systems

Research Overview

His research focuses on aero-engine control, as well as performance modeling and simulation. He has served as a key technical member in several major projects, including fundamental research efforts under the Major Program for Aero Engines and Gas Turbines, sponsored by the Ministry of Industry and Information Technology. His primary research interests include the application of nonlinear control methods in aero-engine control and the dynamic performance modeling of multidisciplinary coupled systems. He has published over ten academic papers as the first or corresponding author, holds one authorized invention patent, and has registered one software copyright.

Academic Service

Youth Member, Engine Control Committee, Third Professional Information Network of China Aerospace

Academic Achievements

Yang S, Long Y, Hu Z. Exploring a category of limit cycle oscillations in aircraft hydraulic systems. Proceedings of ICAS Congress, 2024, ICAS2024-0932.

Long Y, Yang S*, Wang X et al. MoHydroLib: an HMU library for gas turbine control system with Modelica. Symmetry. 2022;14(5):851.

Yang S*, Wang X, Sun P. Design of LPV based sliding mode regulator for limit protection of aero engines, Journal of Dynamic Systems, Measurement, and Control. 2021, 142(1):1-7.

Yang S, Wang X*, Wang H et al. Sliding mode control with system constraints for aircraft engines. ISA Transactions. 2020, 98(1):1-10.

Yang S*, Julaiti A, Wang X et al. A self-tuning model framework using KNN algorithm, Proceedings of ASME Turbo Expo, 2020, GT2020-15262.

Yang S, Wang X*, Yang B. Adaptive sliding mode control for limit protection of aircraft engines. Chinese Journal of Aeronautics. 2018, 31(7):1480-1488.