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Case study: safety analysis of the NASA/Boeing fly-by-light airplane using a new reliability tool

机译:案例研究:使用新可靠性工具的NASA /波音飞行飞机的安全性分析

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This paper is a follow-on to a previous paper (Nicol et al., see ibid., 1995), in which a new reliability tool called reliability performance module (RPM) was described. Since that time, RPM has been used to perform a safety analysis trade study of the primary flight control system (PFCS) architectures proposed for the joint NASA/Boeing fly-by-light/power-by-wire (FBL/PBW) airplane. The purposes of this paper are to: relate experiences and lessons learned from using RPM on the FBL/PBW safety analysis; and present the results of the safety analysis. The conclusions are that: RPM is a powerful tool for performing reliability analyses of complex systems; and the proposed FBL/PBW PFCS architectures meet all of the safety requirements except for one related to spoilers.
机译:本文是前一篇论文的后续(Nicol等,参见Ibid。,1995),其中描述了一种名为可靠性性能模块(RPM)的新可靠性工具。从那时起,RPM已被用来对初级飞行控制系统(PFCS)架构进行安全分析贸易研究,该研究为联合NASA /波音飞蝇/逐线(FBL / PBW)飞机。本文的目的是:在FBL / PBW安全分析上使用RPM提供从使用RPM的经验和经验教训;并提出安全分析的结果。结论是:rpm是执行复杂系统可靠性分析的强大工具;拟议的FBL / PBW PFCS架构符合所有与扰流板相关的安全要求。

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