Towards an FDIR Software Fault Tree Library for Onboard Computers

S. Müller, K. Höflinger, Michal Smíšek, A. Gerndt
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引用次数: 1

Abstract

The increasing complexity of space missions, their software architectures, and hardware that has to meet the demands for those missions, imposes numerous new challenges for many engineering disciplines such as reliability engineering. Affected by the ever growing demand for more onboard computation power are the onboard computers. They in return require Fault Detection, Isolation, and Recovery (FDIR) architectures to support their fault tolerant operation in the harsh environment of space. Especially high performance commercial processing units face the challenge of dealing with negative radiation effects, which may significantly degrade their operation. To design performant and fault tolerant onboard computers, it is of high interest to assess the effectiveness of the FDIR architecture in the early phase of system design. This can be achieved using Fault Tree Analysis (FTA). However, to create complete fault trees manually is an error prone and labor intensive task. In this paper, the methodology for assessing the FDIR design of onboard computers in space systems, presented in [1], is refined by introducing a library of FDIR routines. The routines are modeled using fault trees and are composed into a software system fault tree using a basic fault model and a design configuration chosen by the reliability engineer. To assess the configurations, we give a heuristic based on a factor-criteria-metric model. We demonstrate the feasability of our approach on the basis of a case study on the rover of the Martian Moons eXploration (MMX) mission. Several FDIR configurations are studied and fault trees are generated for them. For the chosen case study, we obtain a reduction of up to 80% in terms of modeling effort.
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面向板载计算机的FDIR软件故障树库
航天任务日益复杂,其软件架构和硬件必须满足这些任务的需求,这给可靠性工程等许多工程学科带来了许多新的挑战。随着对机载计算能力需求的不断增长,机载计算机应运而生。反过来,它们需要故障检测、隔离和恢复(FDIR)体系结构来支持它们在恶劣的空间环境中的容错操作。特别是高性能商业处理单元面临着处理负辐射效应的挑战,这可能会大大降低其运行。为了设计高性能和容错的板载计算机,在系统设计的早期阶段评估FDIR架构的有效性是非常重要的。这可以使用故障树分析(FTA)来实现。然而,手工创建完整的故障树是一项容易出错且耗费大量人力的任务。本文通过引入一个FDIR例程库,对空间系统中机载计算机FDIR设计的评估方法进行了改进。这些例程使用故障树建模,并使用基本故障模型和可靠性工程师选择的设计组态组成软件系统故障树。为了评估配置,我们给出了一个基于因子-标准-度量模型的启发式方法。我们在火星卫星探测(MMX)任务漫游者的案例研究的基础上证明了我们的方法的可行性。研究了几种FDIR配置,并生成了故障树。对于所选择的案例研究,我们在建模工作方面减少了高达80%。
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