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Pilot vehicle interface on the advanced fighter technology integration F-16This paper focuses on the work load aspects of the pilot vehicle interface in regard to the new technologies tested during AMAS Phase II. Subjects discussed in this paper include: a wide field-of-view head-up display; automated maneuvering attack system/sensor tracker system; master modes that configure flight controls and mission avionics; a modified helmet mounted sight; improved multifunction display capability; a voice interactive command system; ride qualities during automated weapon delivery; a color moving map; an advanced digital map display; and a g-induced loss-of-consciousness and spatial disorientation autorecovery system.
Document ID
19870029513
Document Type
Conference Paper
Authors
Dana, W. H. (NASA Flight Research Center Edwards AFB, CA, United States)
Smith, W. B. (General Dynamics Corp. Fort Worth, TX, United States)
Howard, J. D. (USAF, Flight Test Center Edwards AFB, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
AIRCRAFT STABILITY AND CONTROL
Distribution Limits
Public
Copyright
Other