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Qualitative evaluation of a conformal velocity vector display for use at high angles-of-attack in fighter aircraftA piloted simulation study was conducted to evaluate the utility of a display device designed to illustrate graphically and conformally the approximate location of a fighter aircraft's velocity vector. The display device consisted of two vertical rows of light emitting diodes (LED's) located toward the center of the cockpit instrument panel to each side of the control stick. The light strings provided a logical extension of the head up display (HUD) velocity vector symbol at flight path angles which exceeded the HUD field-of-view. Four test subjects flew a modified F/A-18 model with this display in an air-to-air engagement task against an equally capable opponent. Their responses to a questionnaire indicated that the conformal velocity vector information could not be used during the scenarios investigated due to the inability to visually track a target and view the lights simultaneously.
Document ID
19900016665
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jones, Denise R.
(NASA Langley Research Center Hampton, VA, United States)
Burley, James R., II
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-102629
NAS 1.15:102629
Report Number: NASA-TM-102629
Report Number: NAS 1.15:102629
Accession Number
90N25981
Funding Number(s)
PROJECT: RTOP 505-66-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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