Title: A preliminary analysis of flight data from the AFTI/F-16 airplane
Abstract: Flight 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.
Publication Year: 1984
Publication Date: 1984-08-17
Language: en
Type: article
Indexed In: ['crossref']
Access and Citation
Cited By Count: 2
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