F-22 cockpit display system

Author

Bailey, David C.

Author_Institution

Lockheed Sanders Avionics, Nashua, NH, USA

fYear

1994

fDate

30 Oct-3 Nov 1994

Firstpage

459

Lastpage

464

Abstract

Through the work of a multi-disciplined integrated product team from several organizations a cockpit display system has evolved that strikes a balance between conflicting requirements to provide an optimal interface for the operator utilizing high performance liquid crystal displays. Among the many requirements competing for display system consideration are limited instrument panel area, many and varied types of information to be displayed, weight power and cost constraints, redundancy, image generation and optical performance, including sunlight readability and night vision goggle compatibility. The keys to the F-22 display performance are the use of active matrix liquid crystal display front end, high intensity fluorescent back lighting, high performance antialiasing drawing engine and embedded and remote processing

Keywords

aircraft computers; aircraft displays; computerised instrumentation; liquid crystal displays; military avionics; F-22 cockpit display; antialiasing drawing engine; cost; embedded remote processing; graphic display; high intensity fluorescent back lighting; image generation; instrument panel area; liquid crystal displays; night vision goggle compatibility; optimal interface; redundancy; sunlight readability; weight; Active matrix liquid crystal displays; Costs; Engines; Eye protection; Fluorescence; Fluorescent lamps; Image generation; Instruments; Liquid crystal displays; Night vision;

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.1994.369439

Filename

369439