Requirements for future advanced tactical aircraft identify the need for flight control system architectures that provide a higher degree of performance with regard to electromagnetic interference immunity, communication bus data rate, propulsion/utility subsystem integration, and affordability. Evolution for highly centralized, digital, fly-by-light flight/propulsion/utility control system is achieved as modular functions are implemented and integrated by serial digital fiberoptic communication links. These adaptable architectures allow the user to configure the fly- by-light system to meet unique safety requirements, system performance, and design-to-cost targets. This paper presents results of the open and closed loop system demonstrations of Fly-By-Light Advanced System Hardware architecture building blocks integrated with SAE AS-1773 communication bus at MDA.


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    Titel :

    Demonstration results of fly-by-light flight control system architectures for tactical military aircraft


    Beteiligte:
    Corrigan, Jack (Autor:in) / Shaw, Brad (Autor:in) / Jones, Jack E. (Autor:in)

    Kongress:

    Fly-by-Light III ; 1996 ; Denver,CO,United States


    Erschienen in:

    Erscheinungsdatum :

    1996-10-14





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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