TY - GEN
T1 - Tube-Based Model Predictive Control for Aero-Engine Transient-State Tracking Problems
AU - Hu, Yonghao
AU - Gou, Linfeng
AU - Huang, Yingzhi
AU - Chen, Yingxue
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - Transient-state control is one of the most important parts in aero-engine design, which determines the performance of an aero-engine. In recent years, MPC has been widely studied due to its excellent ability to handle constraints in control processes. Tube-MPC, as a type of robust MPC, is more suitable for aero-engines by treating the differences between engine models and real engines as uncertainties. Thus, this paper aims to design a Tube-based model predictive controller for aero-engine transient control to ensure good engine performance. A LPV model based on the nonlinear model of the aero-engine will be established in this paper, then construct an engine transition state controller based on the Tube-MPC algorithm. In the end, a numerical simulation example is presented to show the effectiveness of the designed method. The simulation results show that the engine can work safely and stably during acceleration and deceleration, while its control performance can fully meet the expected requirements.
AB - Transient-state control is one of the most important parts in aero-engine design, which determines the performance of an aero-engine. In recent years, MPC has been widely studied due to its excellent ability to handle constraints in control processes. Tube-MPC, as a type of robust MPC, is more suitable for aero-engines by treating the differences between engine models and real engines as uncertainties. Thus, this paper aims to design a Tube-based model predictive controller for aero-engine transient control to ensure good engine performance. A LPV model based on the nonlinear model of the aero-engine will be established in this paper, then construct an engine transition state controller based on the Tube-MPC algorithm. In the end, a numerical simulation example is presented to show the effectiveness of the designed method. The simulation results show that the engine can work safely and stably during acceleration and deceleration, while its control performance can fully meet the expected requirements.
KW - Aero-Engine Control
KW - LPV Model
KW - Tube-MPC
UR - http://www.scopus.com/inward/record.url?scp=85186746575&partnerID=8YFLogxK
U2 - 10.1109/ICMAE59650.2023.10424484
DO - 10.1109/ICMAE59650.2023.10424484
M3 - 会议稿件
AN - SCOPUS:85186746575
T3 - 2023 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
SP - 225
EP - 229
BT - 2023 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
Y2 - 18 July 2023 through 21 July 2023
ER -