Volume 40 Issue 4
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BO Lixin, LI Ruichao, LIU Yuan, et al. Research on dynamic real-time modeling of aero engine based on ODENet[J]. Journal of Aerospace Power, 2025, 40(4):20240513 doi: 10.13224/j.cnki.jasp.20240513
Citation: BO Lixin, LI Ruichao, LIU Yuan, et al. Research on dynamic real-time modeling of aero engine based on ODENet[J]. Journal of Aerospace Power, 2025, 40(4):20240513 doi: 10.13224/j.cnki.jasp.20240513

Research on dynamic real-time modeling of aero engine based on ODENet

doi: 10.13224/j.cnki.jasp.20240513
  • Received Date: 2024-07-28
    Available Online: 2025-02-09
  • A new dynamic real-time modeling technique for aircraft engines based on Neural Ordinary Differential Equations (ODENet) was proposed. First, the structure of the ODENet model was determined based on the prior knowledge of engine dynamics. Then, an amplitude-modulated pseudo-random binary sequence signal was designed to collect input-output data from the component-level model of the engine, which was used to train the ODENet model, ensuring to cover the dynamic characteristics across the entire operating envelope. Finally, the model was applied to a mixed-flow turbofan engine with a bypass duct injector to validate its real-time performance, accuracy, and robustness through open-loop and closed-loop simulations. The results show that: in the open-loop simulation, the ODENet model’s running speed was approximately 15 times faster than the component-level model, and the fitting degree of each parameter on both the training and testing datasets was no less than 90%; in the closed-loop simulation, the average steady-state and dynamic errors of the output variables between the ODENet and component-level models did not exceed 4%.

     

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  • [1]
    SIMON D L,LONG T W. Adaptive optimization of aircraft engine performance using neural networks[R]. Washington,US: Symposium on Advanced Aero Engines Concepts and Controls,1995.
    [2]
    黄劲东. 面向预测性维修构建航空发动机综合监控和健康管理系统[J]. 航空动力,2022(5): 74-78. HUANG Jindong. Constructing aero engine integrated monitoring and health management system towards predictive maintenance[J]. Aerospace Power,2022(5): 74-78. (in Chinese

    HUANG Jindong. Constructing aero engine integrated monitoring and health management system towards predictive maintenance[J]. Aerospace Power, 2022(5): 74-78. (in Chinese)
    [3]
    马帅,吴亚锋,郑华,等. 基于飞行过程数据的航空发动机故障诊断方法研究[J]. 推进技术,2023,44(5): 2208041. MA Shuai,WU Yafeng,ZHENG Hua,et al. Aircraft engine fault diagnosis based on flight process data[J]. Journal of Propulsion Technology,2023,44(5): 2208041. (in Chinese

    MA Shuai, WU Yafeng, ZHENG Hua, et al. Aircraft engine fault diagnosis based on flight process data[J]. Journal of Propulsion Technology, 2023, 44(5): 2208041. (in Chinese)
    [4]
    YAN Zhiqi,ZHONG Shisheng,LIN Lin,et al. Adaptive Levenberg-Marquardt algorithm: a new optimization strategy for Levenberg-Marquardt neural networks[J]. Mathematics,2021,9(17): 2176. doi: 10.3390/math9172176
    [5]
    KIDGER P. On neural differential equations[EB/OL]. [2024-04-10]. https://arxiv.org/abs/2202.02435v1.
    [6]
    GU Ziyu,PANG Shuwei,ZHOU Wenxiang,et al. An online data-driven LPV modeling method for turbo-shaft engines[J]. Energies,2022,15(4): 1255. doi: 10.3390/en15041255
    [7]
    CHEN Hongyi,LI Qiuhong,PANG Shuwei,et al. A state space modeling method for aero-engine based on AFOS-ELM[J]. Energies,2022,15(11): 3903. doi: 10.3390/en15113903
    [8]
    CHEN R T Q,RUBANOVA Y,BETTENCOURT J,et al. Neural ordinary differential equations[C]//Proceedings of the 32nd International Conference on Neural Information Processing Systems. New York: ACM,2018: 6572-6583.
    [9]
    RAHMAN A,DRGOŇA J,TUOR A,et al. Neural ordinary differential equations for nonlinear system identification[C]//2022 American Control Conference. Piscataway,US: IEEE,2022: 3979-3984.
    [10]
    BRADLEY W,BOUKOUVALA F. Two-stage approach to parameter estimation of differential equations using neural ODEs[J]. Industrial & Engineering Chemistry Research,2021,60(45): 16330-16344.
    [11]
    CHEE KONG Yao,ANI HSIEH M,MATNI N. Learning-enhanced nonlinear model predictive control using knowledge-based neural ordinary differential equations and deep ensembles[R]. Oxford,UK: Learning for Dynamics and Control Conference,2023.
    [12]
    LINOT A J,BURBY J W,TANG Qi,et al. Stabilized neural ordinary differential equations for long-time forecasting of dynamical systems[J]. Journal of Computational Physics,2023,474: 111838. doi: 10.1016/j.jcp.2022.111838
    [13]
    TRAN G,WARD R. Exact recovery of chaotic systems from highly corrupted data[J]. Multiscale Modeling and Simulation,2017,15(3): 1108-1129. doi: 10.1137/16M1086637
    [14]
    LUO Junwei,CANUSO V,JANG J B,et al. Machine learning-based operational modeling of an electrochemical reactor: handling data variability and improving empirical models[J]. Industrial & Engineering Chemistry Research,2022,61(24): 8399-8410.
    [15]
    GOYAL P,BENNER P. Neural ordinary differential equations with irregular and noisy data[J]. Royal Society Open Science,2023,10(7): 221475. doi: 10.1098/rsos.221475
    [16]
    张书刚,郭迎清,陆军. 基于GasTurb/MATLAB的航空发动机部件级模型研究[J]. 航空动力学报,2012,27(12): 2850-2856. ZHANG Shugang,GUO Yingqing,LU Jun. Research on aircraft engine component-level models based on GasTurb/MATLAB[J]. Journal of Aerospace Power,2012,27(12): 2850-2856. (in Chinese

    ZHANG Shugang, GUO Yingqing, LU Jun. Research on aircraft engine component-level models based on GasTurb/MATLAB[J]. Journal of Aerospace Power, 2012, 27(12): 2850-2856. (in Chinese)
    [17]
    HU Pipi. A note on the adjoint method for neural ordinary differential equation network[EB/OL]. [2024-04-10]. https://arxiv.org/abs/2402.15141v1.
    [18]
    NELLES O. Nonlinear dynamic system identification[M]//Nonlinear System Identification. Cham: Springer International Publishing,2020: 831-891.
    [19]
    MONTAZERI-GH M,RASTI A,JAFARI A,et al. Design and implementation of MPC for turbofan engine control system[J]. Aerospace Science and Technology,2019,92: 99-113. doi: 10.1016/j.ast.2019.05.061
    [20]
    BRUNELL B J,BITMEAD R R,CONNOLLY A J. Nonlinear model predictive control of an aircraft gas turbine engine[C]//Proceedings of the 41st IEEE Conference on Decision and Control. Piscataway,US: IEEE,2002: 4649-4651.
    [21]
    AKPAN V A,HASSAPIS G D. Nonlinear model identification and adaptive model predictive control using neural networks[J]. ISA Transactions,2011,50(2): 177-194. doi: 10.1016/j.isatra.2010.12.007
    [22]
    李睿超,虞超,姚竞豪,等. 基于冗余执行器的航空发动机推力快速响应控制方法研究[J]. 推进技术,2024,45(7): 2307039. LI Ruichao,YU Chao,YAO Jinghao,et al. Rapid thrust modulation control of aeroengines based on redundant actuators[J]. Journal of Propulsion Technology,2024,45(7): 2307039. (in Chinese

    LI Ruichao, YU Chao, YAO Jinghao, et al. Rapid thrust modulation control of aeroengines based on redundant actuators[J]. Journal of Propulsion Technology, 2024, 45(7): 2307039. (in Chinese)
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