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A Risk Analysis Tool for Estimating the Risk of Electrical Failures Due to Human Induced Defects

机译:风险分析工具,用于估算人为缺陷引起的电气故障的风险

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Aerospace electrical systems are required to withstand and adequately operate in extremely harsh environments that include, for example, high radiation exposure, temperature extremes, intense vibrational stress and drastic temperature cycling. The nature of aerospace electronics also demands high reliability since, with very few exceptions, there is no chance for hardware servicing or repairs. Common risk mitigation techniques for this type of situation are to perform a Reliability Analysis of the system throughout the development cycle, and to use electrical components that are regarded as “high reliability” because of additional controls and requirements applied in their design, manufacturing and testing. Unfortunately, studies have shown that even though these techniques are used, many systems fail to meet mission requirements well before the predicted lifetimes. This paper presents the analysis of failures of electrical parts, experienced during various stages of system development, at NASA Goddard Space Flight Center, Greenbelt MD, between the years 2001 and 2013. One of the results of the analysis was the realization that a surprising proportion of failures experienced during system integration and testing were caused by human error (i.e. human induced defect). Further analysis included the determination of root failure mechanisms and any influencing factors contributing to these failures. The major causes of these defects were attributed to electrostatic damage (ESD), electrical overstress (EOS), mechanical overstress (MOS), and thermal overstress (TOS). Finally, the study proposes a risk analysis tool which incorporates these major causes for component failures. This tool provides system engineers and risk analysts a quantitative tool to manage, and a visual tool to communicate the risk of electrical part failure caused by defects induced by users during system assembly, integration, and testing. The proposed methodology is demonstrated with an example.
机译:航空航天电气系统需要承受并在极端恶劣的环境中正常运行,这些环境包括高辐射,极端温度,强烈的振动应力和剧烈的温度循环。航空电子产品的性质也要求很高的可靠性,因为除了极少数例外,几乎没有机会进行硬件服务或维修。针对此类情况的常见风险缓解技术是在整个开发周期中执行系统的可靠性分析,并使用由于其设计,制造和测试中应用了附加控件和要求而被视为“高可靠性”的电气组件。 。不幸的是,研究表明,即使使用了这些技术,许多系统也无法在预期寿命之前很好地满足任务要求。本文介绍了在2001年至2013年之间在美国宇航局戈达德太空飞行中心(Greenbelt MD)进行的系统开发各个阶段经历的电气部件故障的分析。分析的结果之一是意识到令人惊讶的比例系统集成和测试过程中遇到的故障中,有多少是由人为错误(即人为导致的缺陷)引起的。进一步的分析包括确定根故障机制以及导致这些故障的任何影响因素。这些缺陷的主要原因归因于静电损伤(ESD),电过载(EOS),机械过载(MOS)和热过载(TOS)。最后,该研究提出了一种风险分析工具,其中包含了这些导致组件故障的主要原因。该工具为系统工程师和风险分析人员提供了定量管理工具,以及可视化工具来传达由用户在系统组装,集成和测试过程中引起的缺陷所导致的电气部件故障的风险。举例说明了所提出的方法。

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