DocumentCode
2817018
Title
Flying qualities lessons learned-1988
Author
Black, G. Thomas ; Thomas, William T.
Author_Institution
USAF Aeronaut. Syst. div., Wright-Patterson AFB, OH, USA
fYear
1989
fDate
22-26 May 1989
Firstpage
299
Abstract
The authors review five major areas of lessons learned in the discipline of flying qualities in 1988. Specifically, they examine flight-control system automatic limiters, the effects of `small´ aerodynamic changes, the effect of thrust increases, the effect of discretization of existing analog systems, and simulator evaluation results of some flight-control modes. Aircraft from which the lessons are drawn are the F-16, a conceptual agile fighter design, the E-8A, YA-7F, F-14A+/D, F-15, F-111, and F-15 S/MTD
Keywords
aerospace computing; aerospace simulation; aircraft control; digital simulation; E-8A; F-111; F-14A+/D; F-15; F-15 S/MTD; F-16; YA-7F; aerodynamic changes; aerospace simulation; analog systems; automatic limiters; discretization; flight-control system; simulator evaluation; thrust increases; Aerodynamics; Aerospace control; Aerospace simulation; Aircraft propulsion; Airplanes; Automatic control; Military aircraft; Protection; Testing; Variable speed drives;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location
Dayton, OH
Type
conf
DOI
10.1109/NAECON.1989.40228
Filename
40228
Link To Document