A new approach to the organization of a reliable aerospace computer system is described in this paper. The organization is based on the use of a multithreading design in which a multiplicity of paths are available, any of which can perform the minimum data processing functions. The combination of all of the multithreading paths comprises a total data processing system which is capable of handling more than the minimum task for which the highest reliability is required. This approach utilizes active redundancy to provide a higher capability for more extensive data processing tasks during that period in which no failures have occurred. Optimum utilization of system weight is achieved through use of a minimum of inactive redundant hardware.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Multithreading Design of a Reliable Aerospace Computer


    Beteiligte:
    Hassett, R. P. (Autor:in) / Miller, E. H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966-11-01


    Format / Umfang :

    1746160 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Reliable rubber for aerospace

    English, L.K. | Tema Archiv | 1989


    LabVIEW 5.0 delivers multithreading, ActiveX

    British Library Online Contents | 1998


    Aerospace Digital Computer Design Trends

    D. O. Baechler | NTIS | 1969


    Aerospace digital computer design trends

    Baechler, D. O. | NTRS | 1969


    The synergy of multithreading and access/execute decoupling

    Parcerisa Bundó, Joan Manuel / González Colás, Antonio María | BASE | 1999

    Freier Zugriff