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Modeling the Propagation of Failures in Software Driven Hardware Systems to Enable Risk-Informed Design

机译:对软件驱动的硬件系统中的故障传播进行建模,以实现基于风险的设计

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Software-driven hardware configurations account for the majority of modern complex systems. The often costly failures of such systems can be attributed to software specific, hardware specific, or software/hardware interaction failures. The understanding of the propagation of failures in a complex system is critical because, while a software component may not fail in terms of loss of function, a software operational state can cause an associated hardware failure. The least expensive phase of the product life cycle to address failures is during the design stage. This results in a need to evaluate how a combined software/hardware system behaves and how failures propagate from a design stage analysis framework.Historical approaches to modeling the reliability of these systems have analyzed the software and hardware components separately. As a result significant work has been done to model and analyze the reliability of either component individually. Research into interfacing failures between hardware and software has been largely on the software side in modeling the behavior of software operating on failed hardware.This paper proposes the use of high-level system modeling approaches to model failure propagation in combined software/hardware system. Specifically, this paper presents the use of the Function-Failure Identification and Propagation (FFIP) framework for system level analysis. This framework is applied to evaluate nonlinear failure propagation within the Reaction Control System Jet Selection of the NASA space shuttle, specifically, for the redundancy management system. The redundancy management software is a subset of the larger data processing software and is involved in jet selection, warning systems, and pilot control. The software component that monitors for leaks does so by evaluating temperature data from the fuel and oxidizer injectors and flags a jet as having a failure by leak if the temperature data is out of bounds for three or more cycles.The end goal is to identify the most likely and highest cost paths for fault propagation in a complex system as an effective way to enhance the reliability of a system. Through the defining of functional failure propagation modes and path evaluation, a complex system designer can evaluate the effectiveness of system monitors and comparing design configurations.
机译:软件驱动的硬件配置占现代复杂系统的大部分。这样的系统的代价高昂的故障可以归因于特定于软件,特定于硬件或软件/硬件交互故障。了解故障在复杂系统中的传播是至关重要的,因为尽管软件组件可能不会因功能丧失而发生故障,但软件运行状态却可能导致相关的硬件故障。解决故障的产品生命周期中最便宜的阶段是在设计阶段。这导致需要评估组合的软件/硬件系统的行为方式以及从设计阶段分析框架传播故障的方式。 对这些系统的可靠性进行建模的历史方法已经分别分析了软件和硬件组件。结果,已经进行了大量工作来分别建模和分析两个组件的可靠性。在对在故障硬件上运行的软件的行为进行建模时,主要是在软件方面对硬件和软件之间的接口故障进行研究。 本文提出了使用高级系统建模方法来对组合软件/中的故障传播进行建模的方法。 硬件系统。具体来说,本文介绍了使用功能故障识别和传播(FFIP)框架进行系统级分析的方法。该框架用于评估NASA航天飞机反应控制系统喷射选择内的非线性故障传播,特别是对于冗余管理系统。冗余管理软件是较大的数据处理软件的子集,涉及喷射选择,警告系统和飞行员控制。监视泄漏的软件组件通过评估来自燃料和氧化剂喷射器的温度数据来执行此操作,如果温度数据超出三个或更多周期,则将喷嘴标记为因泄漏而失效。 最终目标是确定复杂系统中故障传播的最可能途径和最高成本途径,以此作为增强系统可靠性的有效方法。通过定义功能故障传播模式和路径评估,复杂的系统设计人员可以评估系统监视器的有效性并比较设计配置。

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