In a joint project with the FAA, NASA Langley is developing a hardware design in accordance with RTCA DO-254: Design Assurance Guidance for Airborne Electronic Hardware. The purpose of the case study is to gain understanding of the new guidance document and generate an example suitable for use in training. For the case study, we have selected a core subsystem of the Scalable Processor-Independent Design for Electromagnetic Resilience (SPIDER). SPIDER is a new fault-tolerant architecture under development at NASA Langley Research Center.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A case-study application of RTCA DO-254: design assurance guidance for airborne electronic hardware


    Contributors:
    Miner, P.S. (author) / Carreno, V.A. (author) / Malekpour, M. (author) / Torres, W. (author)


    Publication date :

    2000-01-01


    Size :

    653207 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    A Case-Study Application of RTCA DO-254: Design Assurance Guidance for Airborne Electronic Hardware

    Miner, P. S. / IEEE / AIAA | British Library Conference Proceedings | 2000


    Airborne electronic hardware design assurance : a practitioner's guide to RTCA/DO-254

    Fulton, Randall / Vandermolen, Roy / RTCA, Inc. et al. | TIBKAT | 2014




    Introduction to DO-254/ED-80 (Design Assurance Guidance for Airborne Electronic Hardware)

    Alderton, I. / Royal Aeronautical society | British Library Conference Proceedings | 2001