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LIQUID-PROPELLANT ROCKET ENGINES FAULT DIAGNOSTIC BASED ON DYNAMIC CLOUD BP NETWORKS

机译:基于动态云BP网络的液体推进剂火箭发动机故障诊断

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Fault diagnosis is very important to improve and enhance the reliability and safety of current expendable and next-generation reusable liquid-propellant rocket engines. However, fault diagnosis for liquid-propellant rocket engines often faces a lack of prior knowledge or insufficient sampling data, and thus becomes a decision-making problem with uncertain information sources. In this paper, a method based on dynamic cloud back-propagation (BP) networks is proposed. This uses cloud theory to synthetically combine randomness and fuzziness. In this work, a cloud model and BP neural network are synthetically combined in series. A cloud transformation is used to identify the network structure and extract the features of the cloud model. Simultaneously, a unit-delay step is introduced into the input layer to describe the dynamic behaviour during the engine working process. The proposed fault diagnosis method for liquid-propellant rocket engines is verified using actual data. The results confirm that the proposed method accurately recognizes all three relevant failure modes. Further, randomness associated with the measurement process and ambient noises are simulated by adding random noise to the test conditions. Simulation results demonstrate that the method correctly detects and classifies faults according to the principles of sustainability, indicating a high robustness towards noise. The proposed method has a single-step operating time of 1.24 10-4 s, satisfying the real-time requirements for fault diagnosis in liquid-propellant rocket engines. In addition, the data compression capability of the proposed method, which is due to the function of its fuzzy layer, means that fewer training data are required than in traditional neural networks. This effectively overcomes the issue of a lack of training samples.
机译:故障诊断对于改善和提高电流消耗和下一代可重复使用的可重复使用的液相推进剂火箭发动机的可靠性和安全性非常重要。然而,液体推进剂火箭发动机的故障诊断通常面临缺乏先验知识或采样数据不足,因此成为不确定信息源的决策问题。本文提出了一种基于动态云反向传播(BP)网络的方法。这将云理论合成组合随机性和模糊性。在这项工作中,云模型和BP神经网络串联组合。云转换用于标识网络结构并提取云模型的特征。同时,将单位延迟步骤引入到输入层中以描述发动机工作过程中的动态行为。使用实际数据验证液体推进剂火箭发动机的所提出的故障诊断方法。结果证实,该方法准确地识别所有三种相关的故障模式。此外,通过向测试条件增加随机噪声来模拟与测量过程和环境噪声相关联的随机性。仿真结果表明,该方法根据可持续性原理正确检测和分类故障,表明对噪声的高稳健性。所提出的方法具有1.24 10-4 s的单步工程时间,满足液体推进剂火箭发动机中的故障诊断的实时要求。另外,所提出的方法的数据压缩能力是由于其模糊层的功能,这意味着需要比传统的神经网络更少的训练数据。这有效地克服了缺乏训练样本的问题。

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