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Precision controllability of the F-15 airplaneA flying qualities evaluation conducted on a preproduction F-15 airplane permitted an assessment to be made of its precision controllability in the high subsonic and low transonic flight regime over the allowable angle of attack range. Precision controllability, or gunsight tracking, studies were conducted in windup turn maneuvers with the gunsight in the caged pipper mode and depressed 70 mils. This evaluation showed the F-15 airplane to experience severe buffet and mild-to-moderate wing rock at the higher angles of attack. It showed the F-15 airplane radial tracking precision to vary from approximately 6 to 20 mils over the load factor range tested. Tracking in the presence of wing rock essentially doubled the radial tracking error generated at the lower angles of attack. The stability augmentation system affected the tracking precision of the F-15 airplane more than it did that of previous aircraft studied.
Document ID
19790015808
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sisk, T. R.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Matheny, N. W.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-72861
H-1073
Accession Number
79N23979
Funding Number(s)
PROJECT: RTOP 505-11-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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