首页> 外文会议>58th International Astronautical Congress 2007 >A TEMPORAL-CAUSAL-GRAPH-BASED FAULT DIAGNOSIS METHOD FOR LIQUID-PROPELLANT ROCKET ENGINES
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A TEMPORAL-CAUSAL-GRAPH-BASED FAULT DIAGNOSIS METHOD FOR LIQUID-PROPELLANT ROCKET ENGINES

机译:基于时间因果图的液体火箭发动机故障诊断方法

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Although qualitative model-based methods are simple and quick in the fault diagnosis for complicate systems like liquid-propellant rocket engines (LRE), ambiguity always exists in the final diagnosis results because some important information such as the trend in the change of symptoms, the propagation duration between the nodes in models, the importance of the occurred faults are always neglected by these techniques. So a new diagnosis method for LRE based on the Temporal-Causal-Graph (TCG) is developed in this paper to overcome the above deficiencies. Based on the analysis and clarification of the relation and difference between the TCG and other general causal graphs, the proposed method focuses on the representation of the dynamic behavior of engine operation from the little-deviation dynamical equations. Some techniques including the forward propagation of predicting dynamic behaviors, the backward propagation of generating assumptions of faults, and the progressive monitoring strategy of checking the consistency and producing final diagnosis results are developed. By this way, the generated unreasonable assumptions of faults can be eliminated and the ambiguity of the results can be reduced gradually with the increase of measured information. Simulated results with fault samples of a liquid-propellant rocket engine as example show that the method proposed is effective. It can be available for reference in the design and realization of practical fault diagnosis systems.
机译:尽管基于定性模型的方法在诸如液体推进火箭发动机(LRE)之类的复杂系统的故障诊断中简单快捷,但由于某些重要信息(例如症状变化趋势,在模型中节点之间的传播持续时间中,发生故障的重要性始终被这些技术所忽略。因此,为克​​服上述缺陷,本文提出了一种基于时间因果图(TCG)的LRE诊断新方法。在分析和澄清了TCG与其他一般因果图之间的关系和差异的基础上,提出的方法着重于利用小偏差动力学方程来表示发动机运行的动力学行为。开发了一些技术,包括预测动态行为的正向传播,故障产生假设的向后传播以及检查一致性并产生最终诊断结果的渐进监视策略。通过这种方式,可以消除所产生的不合理的故障假设,并且随着测量信息的增加,可以逐渐减少结果的歧义。以液体火箭发动机故障样品为例的仿真结果表明,该方法是有效的。在实际故障诊断系统的设计和实现中可以参考。

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