DocumentCode :
2396280
Title :
Wide-angle, gray-scale AMLCD for flight decks with cross-cockpit viewing requirements
Author :
Thomsen, Scott V. ; Fye, Glenn ; Abileah, Adi
Author_Institution :
Satellite Syst. Oper., Honeywell Inc., Glendale, AZ, USA
fYear :
1994
fDate :
30 Oct-3 Nov 1994
Firstpage :
275
Lastpage :
280
Abstract :
A high-resolution, wide-angle view, normally black active matrix liquid crystal display (AMLCD) has been developed for the National Aeronautics and Space Administration (NASA) Space Shuttle glass cockpit upgrade program. With nine 6.71 by 6.71 in. Active area AMLCDs on the front panel, all containing vehicle flight information, the displays must exhibit optimal performance over the entire AMLCD viewing envelope [±60 deg horizontal (H) and -10/+45 deg vertical (V)], under dark and high-ambient flight deck lighting conditions. Cross-cockpit AMLCDs must provide high off-axis contrast ratios; vertical and horizontal gray-level stability, a consistent and predictable mixture of primary colors; saturated colors; low reflectance; sunlight readability; and a dark, achromatic background over all viewing angles
Keywords :
avionics; liquid crystal displays; space vehicle electronics; 6.71 in; NASA; National Aeronautics and Space Administration; Space Shuttle glass cockpit; chromaticity; cross-cockpit AMLCD; cross-cockpit viewing; dark achromatic background; flight deck lighting; flight decks; gray-scale AMLCD; horizontal gray-level stability; low reflectance; primary colors; saturated colors; sunlight readability; vehicle flight information; vertical gray-level stability; Active matrix liquid crystal displays; Aerospace electronics; Chromium; Enterprise resource planning; Gray-scale; Liquid crystal displays; Optical filters; Production; Reflectivity; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1994. 13th DASC., AIAA/IEEE
Conference_Location :
Phoenix, AZ
Print_ISBN :
0-7803-2425-0
Type :
conf
DOI :
10.1109/DASC.1994.369470
Filename :
369470
Link To Document :
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