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AFTI/F-16 DFCS development summary - A report to industry multimode control law designThe primary goal of the AFTI/F-16 program is to develop a reliable triplex digital multimode flight control system; this system is to be tailored to optimize fighter performance and capable of six-degree-of-freedom decoupled aircraft control. The multiple digital control law configurations arrived at through flight testing are presented. The changes in these designs from the results of flight tests establish that flight testing is an integral part of the development process. The flight test results are analyzed here from the standpoint of pilot comments and resulting control law design modifications.
Document ID
19840033878
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Toles, R. D.
(General Dynamics Corp. Fort Worth, TX, United States)
Anderson, D. C.
(General Dynamics Corp. Fort Worth, TX, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Stability And Control
Accession Number
84A16665
Distribution Limits
Public
Copyright
Other

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