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基于粒子群核极限学习机的涡扇发动机加速过程模型辨识
引用本文:赵姝帆,李本威,钱仁军,朱飞翔.基于粒子群核极限学习机的涡扇发动机加速过程模型辨识[J].推进技术,2020,41(10):2358-2366.
作者姓名:赵姝帆  李本威  钱仁军  朱飞翔
作者单位:海军航空大学 航空基础学院,海军航空大学 航空基础学院,海军航空大学 航空基础学院,海军航空大学 航空基础学院
基金项目:国家自然科学基金(51505492);山东省自然科学基金(ZR2016FQ19);泰山学者建设工程专项经费资助。
摘    要:针对解析法建立涡扇发动机加速过程模型精度和实时性不高的问题,提出了一种基于粒子群核极值学习机(PSO-KELM)的涡扇发动机加速过程模型数据驱动辨识方法,构建涡扇发动机加速过程模型,结合加速过程试车数据,利用PSO-KELM方法对该加速模型进行辨识。试验结果表明:低压转子转速、高压转子转速和低压涡轮出口燃气总温都较好地逼近了试车数据,最大相对误差均值分别为1.013%,0.355%和1.055%,平均计算时间为0.04ms。精度和实时性均优于反向传播神经网络和粒子群支持向量回归方法,可用于发动机状态监控和性能优化控制。

关 键 词:涡扇发动机  加速过程  核极限学习机  数据驱动  模型辨识
收稿时间:2019/8/27 0:00:00
修稿时间:2019/9/24 0:00:00

Turbofan Engine Model Identification of Acceleration Process Based on Particle Swarm Optimization Kernel Extreme Learning Machine
ZHAO Shu-fan,LI Ben-wei,QIAN Ren-jun,ZHU Fei-xiang.Turbofan Engine Model Identification of Acceleration Process Based on Particle Swarm Optimization Kernel Extreme Learning Machine[J].Journal of Propulsion Technology,2020,41(10):2358-2366.
Authors:ZHAO Shu-fan  LI Ben-wei  QIAN Ren-jun  ZHU Fei-xiang
Institution:Aviation Foundation College,Naval Aviation University,,,
Abstract:In order to solve the difficulty of establishing the model of turbofan engine acceleration process by analytic method, a data-driven method on identification the turbofan engine acceleration process model based on kernel extreme learning machine (KELM) optimized by particle swarm optimization (PSO) was proposed. Firstly, a turbofan engine acceleration process model was constructed. Then, PSO-KELM was adopted to identify the model using engine acceleration process test data. The results show that identification results of the low-pressure rotor speed, the high-pressure rotor speed and the low-pressure turbine outlet gas temperature are all close to measured data, the mean maximum relative errors are 1.013%, 0.355% and 1.055%, respectively, the mean computing time is 0.04ms. The precision and real-time are better than BP neural network method and PSO-SVR method, which can be used for engine condition monitoring and performance optimization control.
Keywords:Turbofan engine  Acceleration process  Kernel extreme learning machine  Data-driven  Model identification
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