A hybrid onboard model for aero-engine direct thrust predictive control
Abstract Direct thrust control can markedly enhance thrust regulation accuracy and unlock the full performance potential of aero-engines. To improve both real-time capability and precision, we propose a hybrid adaptive onboard predictive modeling framework, termed DNN-PSM-SVM. In this approach, a deep neural network captures strong nonlinearities to refine accuracy, while steady- and dynamic-deviation models based on PSM and SVM reduce computational complexity. A Kalman filter further enhances adaptability, avoiding heavy nonlinear calculations and significantly improving real-time performance. Leveraging this model within a predictive control scheme, unmeasurable parameters such as thrust and surge margin are estimated in real-time, enabling accurate thrust control even under component degradation. Simulation results show that the method outperforms conventional predictive control, achieving steady-state accuracy below 0.06 % and improving real-time performance by nearly an order of magnitude. Unlike sensor-based control, it maintains precise thrust regulation despite engine degradation.
Authors
- Qiangang Zheng (ORCID: https://orcid.org/0000-0002-8055-5633)
- Dewei Xiang (ORCID: https://orcid.org/0000-0001-5957-1500)
- Liangliang Li (ORCID: https://orcid.org/0000-0002-4104-9148)
- Haibo Zhang (ORCID: https://orcid.org/0000-0002-5134-4167)
- Wei Liu (ORCID: https://orcid.org/0000-0002-3414-1405)
- Fayu Sun
Institutions
- Nanjing University of Aeronautics and Astronautics (CN)
Publication Details
- Journal
- International Journal of Turbo and Jet Engines
- Published
- 2025-11-24
- DOI
- https://doi.org/10.1515/tjj-2025-0090
- Primary Topic
- Advanced Aircraft Design and Technologies
- Type
- article
- Field-Weighted Citation Impact
- 0.00