首页> 外文会议>Chinese Control Conference vol.2; 20040810-13; Wuxi(CN) >Neural Networks Based Real-Time Fault Detection for A Liquid Rocket Propulsion System
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Neural Networks Based Real-Time Fault Detection for A Liquid Rocket Propulsion System

机译:基于神经网络的液体火箭推进系统实时故障检测

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The real-time fault detection is very crucial in developing the online health monitoring techniques for rocket propulsion systems, particularly when the manned space missions are accompanied. The neural networks based approach provides an alternative solution to the design of model-based fault detection methods for detecting the potential failures of propulsion systems. In this paper, a general framework for neural networks based fault detection is developed for a class of liquid rocket propulsion systems. The design approach consists of system modeling, residual generation, and fault detection. First, feed-forward neural networks are used to model the complicated dynamics of propulsion system for simplifying the modeling process and improving the real-time performance of model-based fault detection. Second, a real-time fault detection architecture using the established neural networks approximator is designed. By using the real measurements from ground firing test, an example is provided for demonstrating the effectiveness of the proposed approach to the real-time fault detection of a liquid rocket propulsion system.
机译:实时故障检测对于开发用于火箭推进系统的在线健康监测技术至关重要,特别是在有人驾驶飞行任务伴随进行时。基于神经网络的方法为基于模型的故障检测方法的设计提供了一种替代解决方案,用于检测推进系统的潜在故障。在本文中,为一类液体火箭推进系统开发了基于神经网络的故障检测的通用框架。设计方法包括系统建模,残差生成和故障检测。首先,前馈神经网络用于对推进系统的复杂动力学建模,以简化建模过程并提高基于模型的故障检测的实时性能。其次,设计了一种使用已建立的神经网络逼近器的实时故障检测架构。通过使用地面射击测试的实际测量结果,提供了一个示例,以证明所提出的方法对液体火箭推进系统的实时故障检测的有效性。

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