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Aero-engine Thrust Estimation Based on Ensemble of Improved Wavelet Extreme Learning Machine

机译:基于改进的小波极限学习机集成的航空发动机推力估计

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摘要

Aero-engine direct thrust control can not only improve the thrust control precision but also save the oper-ating cost by reducing the reserved margin in design and making full use of aircraft engine potential performance. However,it is a big challenge to estimate engine thrust accurately.To tackle this problem,this paper proposes an ensemble of improved wavelet extreme learning machine(EW-ELM)for aircraft engine thrust estimation.Ex-treme learning machine(ELM)has been proved as an emerging learning technique with high efficiency.Since the combination of ELM and wavelet theory has the both excellent properties,wavelet activation functions are used in the hidden nodes to enhance non-linearity dealing ability.Besides,as original ELM may result in ill-condition and robustness problems due to the random determination of the parameters for hidden nodes,particle swarm optimi-zation(PSO)algorithm is adopted to select the input weights and hidden biases.Furthermore,the ensemble of the improved wavelet ELM is utilized to construct the relationship between the sensor measurements and thrust.The simulation results verify the effectiveness and efficiency of the developed method and show that aero-engine thrust estimation using EW-ELM can satisfy the requirements of direct thrust control in terms of estimation accuracy and computation time.
机译:航空发动机直接推力控制不仅可以提高推力控制精度,而且还通过减少设计中的保留边缘并充分利用飞机发动机潜在性能来节省运营费用。然而,估计发动机准确的挑战是一个很大的挑战。解决这个问题,本文提出了一种改进的小波极限学习机(EW-ELM)的集合,用于飞机发动机推力估计.ex-Treme学习机(ELM)已经存在被证明是具有高效率的新兴学习技术。榆树和小波理论的组合具有优异的性质,小波激活功能用于隐藏节点以增强非线性交易能力。基于原始榆树可能导致生病-Condition和鲁棒性问题由于随机确定隐藏节点的参数,采用粒子群优化Zation(PSO)算法来选择输入权重和隐藏偏差。繁殖,改进的小波ELM的集合用于构建传感器测量与推力之间的关系。仿真结果验证了开发方法的有效性和效率,并显示了航空发动机推力估计使用EW-ELM的AION可以满足估计准确度和计算时间直接推力控制的要求。

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2018年第2期|290-299|共10页
  • 作者

    Zhou Jun; Zhang Tianhong;

  • 作者单位

    Jiangsu Province Key Laboratory of Aerospace Power Systems,College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Jiangsu Province Key Laboratory of Aerospace Power Systems,College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 自动控制系统;
  • 关键词

  • 入库时间 2022-08-18 02:01:02
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