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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 April 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
19920023905
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
External Source(s)
Authors
Dale Mackall
(Dryden Flight Research Facility Edwards, California, United States)
Kenneth Norlin
(Dryden Flight Research Facility Edwards, California, United States)
Dorothea Cohen
(Dryden Flight Research Facility Edwards, California, United States)
Gary Kellogg
(Dryden Flight Research Facility Edwards, California, United States)
Lawrence Schilling
(Dryden Flight Research Facility Edwards, California, United States)
John Sheen
(Rockwell International Corp. Canoga Park, CA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
AIAA PAPER 92-4176
NASA-TM-104256
H-1857
NAS 1.15:104256
Meeting Information
Meeting: AIAA/AHS Flight Simulation Technologies Conference
Location: Hilton Head, SC
Country: US
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
92N33149
Funding Number(s)
PROJECT: RTOP 505-64-30
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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