Some fundamental information on control system effects on controllability of highly-maneuverable aircraft at high angles of attack and techniques for enhancing fighter aircraft departure/spin resistance using control system design is summarized. The discussion includes: (a) a brief review of pertinent high angle-of-attack phenomena including aerodynamics, inertia coupling, and kinematic coupling; (b) effects of conventional stability augmentation systems at high-alpha; (c) high-alpha control system concepts designed to enhance departure/spin resistance; and (d) the outlook for applications of these concepts to future fighters, particularly those designs which incorporate relaxed static stability.
Control system techniques for improved departure/spin resistance for fighter aircraft
Aerospace Meeting ; 1979 ; Los Angeles, CA
1979-12-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Control System Techniques for Improved Departure/Spin Resistance for Fighter Aircraft
SAE Technical Papers | 1979
|MCAIR Design Philosophy for Fighter Aircraft Departure and Spin Resistance
SAE Technical Papers | 1979
|