Reliability Evaluation of Integrated Modular Avionics Computational Structures for Different Hardware Configurations

Ekaterina Kniga; Igor Zharinov; Anatolii Shukalov; Vladimir Nechaev

doi:10.4028/www.scientific.net/KEM.685.350

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HomeKey Engineering MaterialsKey Engineering Materials Vol. 685Reliability Evaluation of Integrated Modular...

Reliability Evaluation of Integrated Modular Avionics Computational Structures for Different Hardware Configurations

Abstract:

The problem of designing advanced computing systems of integrated modular avionics is considered in this paper. A unified topology of internal network based on SpaceWire channels and options for its application for a variety of onboard implementations are proposed. Equivalent reliability scheme of each special structure is provided and the fail-safe performance probability of each structure is analyzed.

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High Technology: Research and Applications 2015

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Periodical:

Key Engineering Materials (Volume 685)

Pages:

350-354

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.685.350

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Online since:

February 2016

Authors:

Ekaterina Kniga*, Igor Zharinov, Anatolii Shukalov, Vladimir Nechaev

Keywords:

Computational Systems, Evaluation of Reliability Indicators, Fail-Safe Performance Probability, Integrated Modular Avionics

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References

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