基于鲁棒模型的故障诊断方案设计方法及其在飞机液压动力系统中的应用

Felix Mardt, P. Bischof, F. Thielecke
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引用次数: 0

摘要

在系统的设计阶段,对系统的实际行为知之甚少,因此设计一个高效且健壮的系统诊断程序是一项复杂的任务。为了简化这一过程,本文提出了一种基于模型的故障诊断方案设计方法。该方法分析了系统可用行为模型的结构,并提出了满足诊断要求的最小传感器集。为了选择最优的传感器集,该方法从成本和诊断鲁棒性两个方面对传感器集进行评估。所提出的故障检测、隔离和识别方案依赖于使用蒙特卡罗方法和最高密度区域对基于模型的残差进行鲁棒评估,以考虑测量和参数的不确定性。为验证该方法的设计能力,将该方法应用于某型飞机液压动力总成,并在实际试验台上进行了验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design Methodology for Robust Model-Based Fault Diagnosis Schemes and its Application to an Aircraft Hydraulic Power Package
In a system’s design phase, where knowledge about the actual behavior of the system is shallow, the design of an efficient and robust system diagnostics is a complex task. In order to simplify this process, this paper presents a modelbased methodology for the design of fault diagnosis schemes. The methodology analyzes the structure of available behavioral models of the system and proposes minimal sets of sensors to fulfill diagnostic requirements. In order to choose an optimal set of sensors, the method evaluates the sets in terms of costs and diagnostic robustness. The proposed fault detection, isolation and identification schemes rely on the robust evaluation of model-based residuals using Monte-Carlo methods and highest density regions to account for measurement and parameter uncertainty. To show the design capabilities, the presented method is applied to an aircraft hydraulic power package and the resulting schemes are tested on a real test rig.
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