DocumentCode
2593546
Title
Determination of washout performance of various monochrome displays under simulated flight ambient and solar lighting conditions
Author
Batson, Vernon M. ; Robertson, James B. ; Parrish, Russell V.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
fYear
1990
fDate
15-18 Oct 1990
Firstpage
447
Lastpage
452
Abstract
The aircraft cockpit ambient lighting simulation system (ACALSS) has been developed to study display readability and associated pilot/vehicle performance effects in a part-task simulator cockpit. In the study reported, the ACALSS was used to determine the illumination levels at which subjects lose the ability to maintain aircraft states when using three display technologies as display media for primary flight displays: a standard monochrome EL (electroluminescent) flat-panel, a laboratory-class monochrome cathode-ray tube (CRT), and an enhanced-brightness EL flat-panel. The multivariate statistical technique of modified profile analysis was used to test for performance differences between display devices as functions of illumination levels
Keywords
aerospace simulation; aircraft instrumentation; cathode-ray tube displays; electroluminescent displays; flat panel displays; human factors; visual perception; aircraft cockpit; flat panel display; illumination levels; monochrome displays; multivariate statistical technique; pilot/vehicle performance; primary flight displays; profile analysis; readability; simulated flight; solar lighting; Aerospace simulation; Aircraft; Cathode ray tubes; Computer displays; Instruments; Laboratories; Lighting; NASA; Space technology; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location
Virginia Beach, VA
Type
conf
DOI
10.1109/DASC.1990.111330
Filename
111330
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