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Rapid development of the X-31 simulation to support flight-testingThe X-31 Enhanced Fighter Maneuverability Program has been recognized to form the International Test Organization, with the NASA Dryden Flight Research Facility (NASA-Dryden) as the responsible test organization. The two X-31 research aircraft and engineering support personnel were colocated at NASA-Dryden, with flight test operations beginning in Apr. 1992. Therefore, rapid development of a hardware-in-the-loop simulation was needed to support the flight test operations at NASA-Dryden, and to perform verification and validation of flight control software. The X-31 simulation system requirements, distributed simulation system architecture, simulation components math models to the visual system, and the advanced capabilities the X-31 simulation provides. In addition, unique software tools and the methods used to rapidly develop this simulation system will be highlighted.
Document ID
19930029319
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mackall, Dale
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Norlin, Kenneth
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Cohen, Dorothea
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Kellogg, Gary
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Schilling, Lawrence
(NASA Flight Research Center Edwards, CA, United States)
Sheen, John
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-4176
Meeting Information
Meeting: AIAA and AHS, Flight Simulation Technologies Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: AHS, AIAA
Accession Number
93A13316
Distribution Limits
Public
Copyright
Other

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