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High Performance Computing System for Flight Simulation at NASA LangleyThe 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.
Document ID
19910063225
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jeff I Cleveland, II
(Langley Research Center Hampton, United States)
Steven J Sudik
(Langley Research Center Hampton, United States)
Randall D Grove
(Langley Research Center Hampton, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Computer Systems
Report/Patent Number
AIAA PAPER 91-2971
Meeting Information
Meeting: AIAA Flight Simulation Technologies Conference
Location: New Orleans, LA
Country: US
Start Date: August 12, 1991
End Date: August 14, 1991
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
91A47848
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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