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Integrated controls for a new aircraft generationMany of the commercial aircraft now flying will have to be phased out in the early 1980s because of fuel inefficiency and unacceptable noise levels. This paper discusses the role of new digital technology in making aircraft more fuel efficient, more reliable, and quieter. Attention is given to the integration of sensing and control functions in an aircraft in order to provide a simple, lightweight, and high-redundancy system. Technology under development now is expected to come on-line in the 1990s.
Document ID
19780044310
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mace, W. D.
(NASA Langley Research Center Hampton, VA, United States)
Howell, W. E.
(NASA Langley Research Center Flight Electronics Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1978
Publication Information
Publication: Astronautics and Aeronautics
Volume: 16
Subject Category
Aircraft Stability And Control
Accession Number
78A28219
Distribution Limits
Public
Copyright
Other

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