Study of closed loop rate feedback system to determine applicability to high speed, high altitude aircraft; advantages are fully maneuverable aircraft, minimum of programming to obtain desired flying characteristics, reduction of weight over mechanical system, and flexibility previously unobtainable; study of possible ways to improve reliability of control system electronic equipment.
Analysis of electrical flight-control system for interceptor-type aircraft
Aeronautical Eng Rev
Aeronautical Engineering Review ; 16 , n 8
1957
Aufsatz (Zeitschrift)
Englisch
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Integration of navigational flight information for jet interceptor aircraft
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