Comparison of RTL fault models for the robustness evaluation of aerospace FPGA devices

Romain Champon, V. Beroulle, Athanasios Papadimitriou, D. Hély, Gilles Genévrier, Frédéric Cézilly
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引用次数: 5

Abstract

Confronted to more and more demanding standards in terms of safety and reliability, aerospace companies are investigating new methodologies to evaluate the robustness of their FPGA designs against energetic particles. In this paper, this evaluation is realized early in the design flow to avoid costly design re-spins. It permits to have a first evaluation of the RTL design robustness and of the design protections efficiency. To deal with the low accuracy of classical RTL fault models, we use a new RTL fault model taking into account the local effects of particles. We compare the fault model characteristics of different high level fault models (RTL) and low level fault models (layout) on a RTL design dedicated to the plane power supply control. These evaluations show that the new RTL fault model have best characteristics than the classical register fault model.
航天FPGA器件鲁棒性评估的RTL故障模型比较
面对越来越苛刻的安全性和可靠性标准,航空航天公司正在研究新的方法来评估他们的FPGA设计对高能粒子的稳健性。在这篇文章中,这个评价是实现在设计流程的早期re-spins避免代价高昂的设计。它允许对RTL设计的稳健性和设计保护效率进行第一次评估。针对经典RTL故障模型精度低的问题,提出了一种考虑粒子局部效应的RTL故障模型。在针对飞机电源控制的RTL设计中,比较了不同的高阶故障模型(RTL)和低阶故障模型(布局)的故障模型特征。结果表明,该故障模型比传统的注册故障模型具有更好的特性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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