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A preliminary analysis of flight data from the AFTI/F-16 airplaneFlight test data from the AFTI/F-16 airplane are analyzed. Two flight control system modes (Independent Backup Unit and Standard Normal Mode) are considered. Estimated stability and control derivatives are compared with values from the wind tunnel and F-16A flight tests. Modeling difficulties are shown to arise due to the near-neutral static stability of the airplane and the number of coordinated control surface movements commanded in the Standard Normal Mode.
Document ID
19840059553
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Batterson, J. G. (NASA Langley Research Center Hampton, VA, United States)
Klein, V. (Joint Institute for Advancement of Flight Sciences Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 84-2085
Accession Number
84A42340
Distribution Limits
Public
Copyright
Other

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