Research on Modeling and Control Method of the Mode Transition for High-Flow Variable Cycle Engine

This paper focuses on high-flow dual variable cycle engines, conducting aerodynamic simulations on the mode selection valve. By employing an Extreme Learning Machine (ELM) method, a relationship between the geometric parameters and performance parameters of the mode selection valve is established, which is then coupled to the engine performance calculation model to create a high-confidence coupled model. Compared with the traditional zero-dimensional model, the results indicate that the high-confidence coupled model more accurately reflects the performance changes during mode transition. However, thrust fluctuations were observed during the mode transition. To address this issue, a mode transition thrust controller based on nonlinear model predictive control (NMPC) was designed. Simulation results show that this controller can ensure stable thrust while maintaining normal engine operation.

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Publication Details

Published
2024-09-27
DOI
https://doi.org/10.1109/aaac63570.2024.11027339
Primary Topic
Advanced Combustion Engine Technologies
Type
article
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article

Research on Modeling and Control Method of the Mode Transition for High-Flow Variable Cycle Engine

Xianghua Huang, Runmin Ji, Qiyuan Zhang, Junhao Lei
Advanced Combustion Engine Technologies
article

Research on Modeling and Control Method of the Mode Transition for High-Flow Variable Cycle Engine

Xianghua Huang, Runmin Ji, Qiyuan Zhang, Junhao Lei
article en

Abstract

This paper focuses on high-flow dual variable cycle engines, conducting aerodynamic simulations on the mode selection valve. By employing an Extreme Learning Machine (ELM) method, a relationship between the geometric parameters and performance parameters of the mode selection valve is established, which is then coupled to the engine performance calculation model to create a high-confidence coupled model. Compared with the traditional zero-dimensional model, the results indicate that the high-confidence coupled model more accurately reflects the performance changes during mode transition. However, thrust fluctuations were observed during the mode transition. To address this issue, a mode transition thrust controller based on nonlinear model predictive control (NMPC) was designed. Simulation results show that this controller can ensure stable thrust while maintaining normal engine operation.

Nanjing University of Aeronautics and Astronautics (CN)
Affordable and clean energy
Openalex Percentile: Top 76%
Advanced Combustion Engine Technologies
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Research on Modeling and Control Method of the Mode Transition for High-Flow Variable Cycle Engine — Xianghua Huang, Runmin Ji, et al. · (2024) | TGRS Research Map | TGRS