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A new method for hardware/software integration of strategic systems - Case study of the Space ShuttleAn advanced system integrated self-test has been developed to provide dynamic checkout of all critical subsystems and hardware/software interfaces of the Space Shuttle during pre-launch ground testing. The system modifies hardware sensor data to represent a real flight scenario. This modified data then drives the flight software. The system was sucessfully utilized for three phases of Space Shuttle testing, and will be expanded for use as a maintenance tool.
Document ID
19820030349
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haque, S. I. (Intermetrics, Inc. Cambridge, MA, United States)
Ionescu, T. V. (Intermetrics, Inc. Cambridge, MA, United States)
Henley, G. D. (Intermetrics, Inc. Cambridge, MA, United States)
Date Acquired
August 10, 2013
Publication Date
November 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-2384
Meeting Information
Meeting: Flight Testing Conference
Location: Las Vegas, NV
Start Date: November 11, 1981
End Date: November 13, 1981
Accession Number
82A13884
Funding Number(s)
CONTRACT_GRANT: NAS9-14000
Distribution Limits
Public
Copyright
Other

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