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The effect of perspective displays on altitude and stability control in simulated rotary wing flightThe effect of perspective displays on flight performance is investigated using two simulation experiments. In the first, a perspective grid display was superimposed on computer-generated terrain and subjects attempted to maintain their initial attitude in a simulated hover using terrain and/or one of four grid patterns. Horizontal lines produced the best attitude control performance. In the second experiment, a square grid was studied in combination with various visual display configurations and grid attachment conditions. It was found that performance with the panel-mounted display was significantly worse than with the out-the-window or helmet-mounted displays. The results suggested that the partial grid attachment condition improved hovering performance with the panel-mounted display.
Document ID
19880066440
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
O'Donnell, K. A.
(U.S. Army, Aeroflightdynamics Directorate, Moffett Field CA, United States)
Johnson, W. W.
(Army Aviation Research and Development Command Moffett Field, CA, United States)
Bennett, C. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 88-4634
Report Number: AIAA PAPER 88-4634
Accession Number
88A53667
Distribution Limits
Public
Copyright
Other

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