The computer architecture and components used in the NASA Langley Advanced Real-Time Simulation System (ARTSS) are briefly described and illustrated with diagrams and graphs. Particular attention is given to the advanced Convex C220 processing units, the UNIX-based operating system, the software interface to the fiber-optic-linked Computer Automated Measurement and Control system, configuration-management and real-time supervisor software, ARTSS hardware modifications, and the current implementation status. Simulation applications considered include the Transport Systems Research Vehicle, the Differential Maneuvering Simulator, the General Aviation Simulator, and the Visual Motion Simulator.


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    Titel :

    High performance computing system for flight simulation at NASA Langley


    Beteiligte:

    Kongress:

    AIAA Flight Simulation Technologies Conference ; 1991 ; New Orleans, LA, United States


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    High performance flight simulation at NASA Langley

    Cleveland, Jeff I., II / Sudik, Steven J. / Grove, Randall D. | NTRS | 1992


    High performance flight simulation at NASA Langley

    CLEVELAND, II, JEFF / SUDIK, STEVEN / GROVE, RANDALL | AIAA | 1992


    High-Performance Real-Time Flight Simulation at NASA Langley

    United States; National Aeronautics and Space Administration | British Library Conference Proceedings | 1993


    NASA Langley Flight Test Program

    M. Lewis | NTIS | 1991


    NASA Langley flight test program

    Lewis, Mike | NTRS | 1991