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Fault Diagnosis and Prognosis of Aerospace Systems Using Growing Recurrent Neural Networks and LSTM

机译:使用生长经常性神经网络和LSTM的航空航天系统故障诊断及预后

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Due to the increase in complexity in aerospace systems, developing a diagnosis, prognosis, and health monitoring (DPHM) framework is a challenge that must be considered to assure the safety of such systems. This paper discusses this problem by proposing an artificial intelligence technique based on two novel neural networks, the growing neural networks (GNN) and variable sequence LSTM (VarLSTM) model to automate the process of DPHM for aerospace systems. For single-unit datasets, the proposed model estimates a Health Index value using the residuals between the measured telemetry data and the one predicted using the GNN algorithm, and then the HI value is extrapolated for prognostics. For multiple-units datasets, the model makes RUL predictions by directly mapping the RUL of the training units to their corresponding measured features at every measured instant. In this paper, the model optimizes the architecture of a recurrent neural network and was used to make RUL predictions for aircraft engines and detect failure for satellite attitude actuators (Reaction Wheels). It was tested on the CMAPSS and PHM08 aircraft engine datasets (multiple-unit datasets) simulated by NASA, and it was able to make RUL predictions with root mean square errors as low as 14 engine cycles. Another application to test the proposed model was on the Kepler Spacecraft's reaction wheels from which two have failed (single-unit datasets). The model detected the failure of the two failed reaction wheels by estimating a HI value which indicates the probability of failure of the reaction wheels using the residuals between the speed predictions made by the model and measured speed values. Failure was detected using the model almost 105 days and 54 days for reaction wheels two and four respectively. Prognostics were also applied on the Kepler Mission reaction wheels and RUL predictions were made with mean absolute errors ranging between 2–13 days depending on how close the reaction wheel is to fail when the prediction is made. The proposed artificial intelligence algorithm shows promising results in system fault diagnosis and prognosis leading to the development of smart systems for aerospace applications.
机译:由于航空航天系统中复杂性的增加,开发诊断,预后和健康监测(DPHM)框架是必须考虑的挑战,以确保这些系统的安全性。本文通过提出基于两种新型神经网络的人工智能技术,生长神经网络(GNN)和可变序列LSTM(VARLSTM)模型来讨论该问题,以自动化航空航天系统DPHM的过程。对于单单元数据集,所提出的模型使用测量的遥测数据与使用GNN算法预测的剩余物的健康指标值,然后将Hi值推断为预后。对于多个单元数据集,该模型通过将训练单元的rul映射到每个测量的瞬间,通过将训练单元的rul映射到它们的相应测量特征来使RUL预测成为RUL预测。在本文中,该模型优化了经常性神经网络的架构,并用于制作飞机发动机的RUL预测,并检测卫星姿态执行器(反应轮)的故障。它在CMAPS和PHM08飞机发动机数据集(MPM08飞机发动机数据集(多单位数据集)上进行了测试,并且能够使RUL预测具有低至14个发动机循环的根均方误差。测试所提出的模型的另一个应用程序位于开普勒航天器的反应车轮上,两个失败(单位数据集)。该模型通过估计使用由模型和测量速度值所产生的速度预测之间的速度预测之间的差值来检测两个失败的反应轮的故障。使用型号近105天和54天的模型检测到失败,分别用于两和四个。预后也应用于开普勒任务反应车轮,并且rul预测由2-13天之间的平均绝对误差进行,这取决于反应轮在预测时的关闭程度。所提出的人工智能算法显示了有希望的系统故障诊断和预后导致航空航天应用智能系统的开发。

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