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Effects of update and refresh rates on flight simulation visual displaysAn experiment was performed to study the effects of update and refresh rates on dynamic calligraphic CRT displays, particularly those used for visual displays in flight simulators. A moving horizontal line was generated on a CRT and observed at various velocities. Observations were made with both one and two refreshes per update. The data gathered from these observations are presented on plots of refresh-update rate as a function of display velocity. The display velocity where picture degradation occurs can be found by using these plots. These velocities are related to actual simulated aircraft angular and linear velocities. Results show that a visual display updated at 30 Hz and refreshed at 60 Hz degrades at very low simulated aircraft angular and linear velocities. These velocities at which degradation occurs can be significantly increased by increasing the update rate of the visual display. Only minor improvements are possible by refreshing the display twice for each uptake. To display rapidly changing flight scenery without degradation, the display update rate must be far in excess of 60 Hz, typically several hundred Hz.
Document ID
19880012649
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kellogg, Gary V.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Wagner, Charles A.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:100415
NASA-TM-100415
H-1439
Accession Number
88N22033
Funding Number(s)
PROJECT: RTOP 922-22-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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