Automatic flight control system (AFCS) for A-7A fighter-attack aircraft is production version of prototype system, developed over 3 yr by Lear Siegler Inc; paper presents developmental philosophy that led to selection of final configuration, completely dual, fixed-gain control-augmentation system, using series hydraulic servos and with attitude, altitude, heading-hold, and heading-select capabilities; results of U S Navy flight evaluation in F-8D aircraft showing capabilities of system in providing improved airplane-handling qualities.
A-7A AFCS -- Flight-proved high-gain system
J Aircraft
Journal of Aircraft ; 3 , n 5
1966
8 pages
Aufsatz (Zeitschrift)
Englisch
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A-7A AFCS - A flight-proved high-gain system.
AIAA | 1966
|THE A-7A AFCS: A FLIGHT-PROVED HIGH GAIN SYSTEM
AIAA | 1965
|SAE Technical Papers | 1981
|Digital computation makes AFCS (automatic flight control system) more reliable
Tema Archiv | 1975
|A study of (AFCS) communications measurement program
Tema Archiv | 1973
|