基于改进小波极值学习机集成的航空发动机推力估计

Q4 Engineering
Zhou Jun, Zhang Tianhong
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引用次数: 4

摘要

航空发动机直接推力控制不仅可以提高推力控制精度,而且可以通过减少设计中的预留余地和充分利用航空发动机的潜在性能来节省运行成本。然而,准确估计发动机推力是一个巨大的挑战。为了解决这个问题,本文提出了一种用于飞机发动机推力估计的改进小波极值学习机(EW-ELM)。极限学习机(ELM)已被证明是一种新兴的高效学习技术。由于ELM和小波理论的结合具有这两个优点,因此在隐藏节点中使用小波激活函数来增强非线性处理能力。此外,由于原始ELM可能由于隐藏节点参数的随机确定而导致病态和鲁棒性问题,因此采用粒子群优化算法来选择输入权重和隐藏偏差。此外,利用改进的小波ELM的集合来构建传感器测量值与推力之间的关系。仿真结果验证了所提方法的有效性和有效性,表明采用EW-ELM的航空发动机推力估计在估计精度和计算时间方面能够满足直接推力控制的要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Aero-engine Thrust Estimation Based on Ensemble of Improved Wavelet Extreme Learning Machine
Aero-engine direct thrust control can not only improve the thrust control precision but also save the operating 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. Extreme 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 optimization (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.
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CiteScore
1.20
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0.00%
发文量
3
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