DocumentCode
1369186
Title
All-digital jets are taking off: Aboard developmental commercial and military aircraft, digital electronics score high in compactness, control flexibility, and reliability
Author
Spitzer, C.R.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
Volume
23
Issue
9
fYear
1986
Firstpage
51
Lastpage
56
Abstract
The key attributes of second-generation digital avionics systems are discussed. These are: increased integration, allowing more functions in less space; increased reliability through redundancy of components and systems and augmented fault-tolerance capabilities; and an improved man-machine interface, including such features as flat panels and voice controls. Examples of increased integration include more efficient data buses that cut down on wiring and connectors, and an inertial reference system and an air-data computer combined into one line-replacement unit. The author describes several commercial and military aircraft with emphasis on the European Airbus Industrie A-320, which will be the first commercial aircraft to use second-generation digital avionics. This 150-passenger, medium-range airliner is schedule to enter service in the spring of 1988. Issues in fault tolerance and improved aircraft control are included.
Keywords
aerospace computer control; aircraft instrumentation; digital systems; fault tolerant computing; military systems; redundancy; European Airbus Industrie A-320; aerospace computer control; air-data computer; commercial aircraft; data buses; fault-tolerance capabilities; flat panels; inertial reference system; line-replacement unit; man-machine interface; military aircraft; redundancy; second-generation digital avionics systems; voice controls; Aerospace control; Aerospace electronics; Aircraft; Aircraft navigation; Fuels; Military aircraft; Reliability;
fLanguage
English
Journal_Title
Spectrum, IEEE
Publisher
ieee
ISSN
0018-9235
Type
jour
DOI
10.1109/MSPEC.1986.6371088
Filename
6371088
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