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首页> 外文期刊>IEEE Transactions on Reliability >Design of a fault-tolerant COTS-based bus architecture
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Design of a fault-tolerant COTS-based bus architecture

机译:基于容错COTS的总线体系结构设计

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This paper describes the authors' approach to usingncommercial-off-the-shelf (COTS) products in highly reliable systems. Thenmethodology calls for multilevel fault-protection. The methodologynrealizes that COTS products are often not developed with highnreliability in mind. Nevertheless, by using multi-level faultnprotection, the same level of reliability as the traditional full-customnfault tolerance approach can be achieved. This methodology allows morenfreedom for design trade-offs among the fault-protection levels, whichncan result in less complicated designs than the traditionalnstrictly-enforced fault-containment policy. This paper covers thenauthors' experiences and findings on the design of a fault-tolerantnavionics bus architecture comprised of two COTS buses, the IEEE 1394,nand the I2C, for the avionics system of X2000 program at thenJet Propulsion Laboratory. The X2000 design is judicious about ensuringnthe fault-tolerance provisions do not cause the bus design to deviatenfrom commercial standard specifications, so that the economicnattractiveness of using COTS is preserved. The hardware and softwarendesigns of the X2000 fault-tolerant bus are being implemented, andnflight hardware will be delivered to the Europa Orbiter missions. Thisnwork provides an example of how to construct a highly reliable systemnwith low-cost COTS interfaces
机译:本文介绍了作者在高度可靠的系统中使用商用现货(COTS)产品的方法。然后,方法论要求多层次的故障保护。该方法学认识到,在开发COTS产品时通常不会考虑高可靠性。但是,通过使用多级故障保护,可以实现与传统的全客户故障容忍方法相同的可靠性。这种方法为故障保护级别之间的设计权衡提供了更大的自由度,与传统的严格执行的故障遏制策略相比,这种方法可以简化设计。本文介绍了作者在当时的喷气推进实验室的X2000计划航空电子系统中设计的容错航空电子总线体系结构的经验和发现,该体系结构由两条COTS总线(IEEE 1394和n2C)组成。 X2000设计在确保容错规定不会导致总线设计偏离商业标准规格方面是明智的,从而保留了使用COTS的经济吸引力。 X2000容错总线的硬件和软件设计正在实施,nflight硬件将交付给Europa Orbiter任务。本工作提供了一个示例,说明如何使用低成本的COTS接口构建高度可靠的系统

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