Enhanced Soft Error Rate Estimation Technique for Aerospace Electronics Safety Design via Emulation Fault Injection

Author:

Lee Dongmin1ORCID,Nam Taehyeong2,Park Daeseon2,Kim Yeju3ORCID,Na Jongwhoa3ORCID

Affiliation:

1. School of Smart Air Mobility, Korea Aerospace University, Goyang-si 10540, Republic of Korea

2. Electronics and Telecommunications Research Institute (ETRI), Daejeon 34129, Republic of Korea

3. School of Electronics and Information Engineering, Korea Aerospace University, Goyang-si 10540, Republic of Korea

Abstract

In this paper, we propose Automatic Configuration Memory Fault Injection (ACMFI), a tool that calculates the architectural vulnerability factor (AVF) and soft error rate (SER) using the emulation fault injection technique. SER, which is essential for the safety design of aerospace electronics, can be obtained by experiments (beam tests) performed in a beam facility equipped with high-energy radiation facilities. However, SER calculation using beam tests has the disadvantage of a high cost and a long waiting time, making it difficult to use in the conceptual design stage, which is the aerospace system development stage and the initial HW/SW development stage. Using the emulation fault injection method, it is possible to estimate the SER, which can be used in the system safety design phase. This paper describes the ACMFI tool, which automatically performs emulation fault injection in SRAM-based FPGAs, which are widely used in aerospace electronic hardware. Unlike the existing methods, the proposed method has the advantage of minimizing the side effects by injecting faults into a dedicated SRAM area. In other words, the SER obtained by the proposed method can be estimated more accurately than the SER result obtained by the existing method. To prove the accuracy of the proposed test method, the SER calculated by performing an emulation fault injection test on the same FPGA was compared with the SER results tested at the beam facility. The method of obtaining SER using the proposed ACMFI gave results that were closer to the SER obtained by testing at the beam facility than the method of obtaining SER using the existing EMFI. The proposed method is used to calculate the failure rate, which is a key variable in determining the development assurance level when performing safety design tests in aerospace system development, enabling the development of safer systems and lower cost/higher quality aerospace electronic equipment than before.

Funder

National Research Foundation of Korea

GRRC program of Gyeonggi province

Publisher

MDPI AG

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Algorithms and Software Tools for Evaluating the Design Process of Electronic Components and their Technology for Compliance with the Requirements of IECQ 080000;2024 International Conference on Information Processes and Systems Development and Quality Assurance (IPS);2024-03-19

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