LIU Jiashuai Assistant Research Fellow

Email:liujiashuai@tsinghua.edu.cn

Address:Tsinghua University, Haidian District, Beijing

Education

Sep. 2018 – Jan. 2024: Doctor of Engineering in Aerospace Propulsion Theory and Engineering, Beihang University

Sep. 2014 – Jun. 2018: Bachelor of Engineering in Automation, Northwestern Polytechnical University

Professional Experience

Aug. 2026 – Present: Assistant Research Fellow, Tsinghua University

Jul. 2024 – Aug. 2026: Postdoctoral Researcher, Tsinghua University

Research Interests

> Control technologies and applications for aero-engines (TBCC, hydrogen-fueled aero-engine, turbo-electric hybrid systems)

> Modeling and control technologies for Altitude Ground Test Facilities

> Nonlinear control theory and applications

Research Overview

I have long been engaged in research on modeling and advanced control technologies for aero-engines and Altitude Ground Test Facilities. I have served as Principal Investigator (PI) of the NSFC Youth Fund (Category C). As a core member, I have participated in more than ten national- and provincial-level research projects. I have published over 20 academic papers, including 11 first/corresponding-author SCI-indexed papers, and hold 12 authorized invention patents and 4 software copyrights.

Academic Achievements

[1] J. Liu, A. He, X. Pei, et al. Pressure and temperature control in hydrogen supply experimental system subject to unknown rate saturation. Aerospace Science and Technology, 2026, 113566.

[2] J. Liu, A. He, X. Pei, et al. Feedforward compensation-based L1 adaptive control for aeropropulsion system test facility and hardware-in-the-loop verification. Chinese Journal of Aeronautics, 2025, 38(3): 103386.

[3] J. Liu, X. Wang, X. Liu, et al. μ-Synthesis control with reference model for aeropropulsion system test facility under dynamic coupling and uncertainty. Chinese Journal of Aeronautics, 2023, 36(10): 246-261.

[4] J. Liu, X. Wang, X. Liu, et al. μ-Synthesis-based robust L1 adaptive control for aeropropulsion system test facility. Aerospace Science and Technology, 2023, 140: 108457.

[5] J. Liu, X. Wang, X. Liu, et al. An anti-windup design with local sector and H2/H∞ optimization for flight environment simulation system. Aerospace Science and Technology, 2022, 128: 107787.

[6] J. Liu, X. Wang, M. Zhu, et al. Multivariable adaptive control method for turbofan engine with dynamic and input uncertainties. Journal of Engineering for Gas Turbines and Power-Transactions of the ASME, 2021, 143: 071027.

[7] J. Liu, X. Wang, X. Pei, et al. Generic modeling method of quasi-one-dimensional flow for aeropropulsion system test facility. Symmetry, 2022, 14(6): 1161.