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Development of an active fly-by-wire flight control systemA summary of the YF-16 flight control system is presented. The basic functions of the flight control system are discussed, as well as the unique features such as Relaxed Static Longitudinal Stability (RSS), Fly By Wire (FBW), and Side Stick Pilot's Controller (SSC). In addition, the basic philosophy behind the selection of the flight control system functions and unique features is discussed.
Document ID
19760024050
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, C. A. (General Dynamics/Fort Worth TX, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Stability And Control
Accession Number
76N31138
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760024047Collected WorksAdvanced Control Technology and its Potential for Future Transport Aircraft
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