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
Link To Document :
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