近地轨道上M430FR5989SRGCREP、EFM32GG11B820F2048、AT32UC3C0512C和M2S010微控制器SEU灵敏度的质子束测试

S. Damkjar, I. Mann, D. Elliott
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引用次数: 5

摘要

在几个微控制器上进行了质子束测试,质子能量在2.4 MeV到57.6 MeV之间。开发了一个远程操作的机器人测试平台,通过最大限度地减少对辐射库的人工干预来提高测试吞吐量。测定了对SEU、SEL和SEFI故障的敏感性。利用测量到的SEU横截面数据以及NASA的辐射带模型AP8,确定了国际空间站轨道上的在轨SEU率。在改变质子束入射角的情况下也进行了测试,结果表明,随着入射角的减小,SEL和SEFI的失败率显著增加。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Proton Beam Testing of SEU Sensitivity of M430FR5989SRGCREP, EFM32GG11B820F2048, AT32UC3C0512C, and M2S010 Microcontrollers in Low-Earth Orbit
Proton beam testing was performed on several microcontrollers using proton energies between 2.4 MeV and 57.6 MeV. A remotely operated robotic testing platform was developed to improve testing throughput by minimizing the need for human intervention in the radiation vault. Sensitivity to SEU, SEL, and SEFI faults was determined. Using the measured SEU cross-section data along with NASA’s radiation belt model, AP8, in-orbit SEU rates were determined for an ISS orbit. Testing was also done while varying the incidence angle of the proton beam which shows that the rate of SEL and SEFI faults increased significantly with shallower incidence angle.
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