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Results of recent NASA studies on automatic spin prevention for fighter aircraftA broad based research program was developed to eliminate or minimize inadvertent spins for advanced military aircraft. Recent piloted simulator studies and airplane flight tests have demonstrated that the automatic control systems in use on current fighters can be tailored to provide a high degree of spin resistance for some configurations without restrictions to maneuverability. Such systems result in greatly increased tactical effectiveness, safety, and pilot confidence.
Document ID
19770003439
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chambers, J. R.
(NASA Langley Research Center Hampton, VA, United States)
Nguyen, L. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Advan. in Eng. Sci., Vol. 4
Subject Category
Aircraft Stability And Control
Accession Number
77N10381
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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