Some fundamental information on control system effects on controllability of highly maneuverable aircraft at high angles of attack are summarized as well as techniques for enhancing fighter aircraft departure/spin resistance using control system design. The discussion includes: (1) a brief review of pertinent high angle of attack phenomena including aerodynamics, inertia coupling, and kinematic coupling; (2) effects of conventional stability augmentation systems at high angles of attack; (3) high angle of attack control system concepts designed to enhance departure/spin resistance; and (4) 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
1980
69 pages
Report
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
|