Automatic system, designed to provide warning approach to stall condition and protection from entering full stall and possible pitch-up, senses aircraft pitch rate and angle of attack and actuates stick-shaker warning device followed by application of corrective pitch control force if warning is ignored and unsatisfactory conditions persist; techniques developed for evaluation of system performance consisted of flights with lowered system boundary limits, 1-g stall approaches, windup turns, and rapid pull-ups; performance data are presented for several stages of development including final system and preflight and inflight checkout procedures to verify system operation.
Automatic stall prevention control for supersonic fighter aircraft
J Aircraft
Journal of Aircraft ; 2 , n 3
1965
5 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.