This paper describes some emerging technologies in guidance and control which are candidates for future aircraft. It briefly describes an advanced development program which successfully demonstrated Integrated Fire/Flight Control (IFFC) technology to automatically deliver air-to-air and air-to-surface weapons while maneuvering. It describes the advanced cockpit design of the new F-16 C/D aircraft and some of the difficulty encountered during its development. Brief descriptions of normal acceleration of a induced loss of consciousness, anti-g hardware and pilot g tolerance in the F-16 are also covered. Lastly, the angle of attack and load factors limiting features of the F-16 and how they affect the maneuvering of this relaxed static stability, fly-by-wire, high performance aircraft are described in detail.
Implications of Guidance & Control Technology on Human Factors Considerations
1984
13 pages
Report
Keine Angabe
Englisch
Avionics , Human Factors Engineering , Human factors engineering , Military aircraft , Control systems , Man machine systems , Guidance , Integration , Fire control systems , Flight control systems , Weapon delivery , Cockpits , Jet fighters , Acceleration tolerance , Consciousness , Angle of attack , Flight loads , Limitations , Flight maneuvers , Symposia , Component Reports
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