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Neural network-based helicopter gearbox health monitoring system

机译:基于神经网络的直升机变速箱健康监测系统

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The results of two neural hardware implementations of a helicopter gearbox health monitoring system (HMS) are summarized. The first hybrid approach and implementation to fault diagnosis is outlined, and results are summarized using three levels of fault characterization: fault detection (fault or no fault), classification (hear or bearing fault), and identification (fault sub-classes). Initial hardware results compare well with previously published software simulations. The second all-analog implementation exploits the ability of analog neural hardware to compute the discrete Fourier transform (DFT) as a preprocessor to a neural classifier.
机译:总结了直升机齿轮箱健康监测系统(HMS)的两个神经硬件实现的结果。概述了第一种混合方法和对故障诊断的实现,并使用三个故障表征概述结果:故障检测(故障或无故障),分类(听到或轴承故障)和识别(故障子类)。初始硬件结果与先前发布的软件模拟相比很好。第二种全模模拟实现利用模拟神经硬件将离散傅里叶变换(DFT)作为预处理器计算到神经分类器的能力。

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