Aeronautics and astronautics – Aircraft control – Automatic
Patent
1988-12-19
1990-10-23
Jordan, Charles T.
Aeronautics and astronautics
Aircraft control
Automatic
244 311, 244179, 244189, B64C 1320
Patent
active
049645986
ABSTRACT:
A remotely-controlled aircraft comprises a sensor for sensing the actual rate-of-turn of the aircraft and for generating a rate-of-turn signal proportional thereto, which signal, inherently also proportional to the actual bank-angle of the aircraft, is applied to the aileron drive as a negative feedback signal with the bank-angle command signal to thereby stabilize the bank-angle of the aircraft. The aircraft includes a further sensor for sensing the actual rate-of-climb of the aircraft and for generating a rate-of-climb signal proportional thereto, which latter signal, inherently also proportional to the actual pitch-angle of the aircfaft, is applied to the elevator drive as a negative feedback signal with the pitch-angle command signal to thereby stabilize the pitch-angle of the aircraft.
REFERENCES:
patent: 4054254 (1977-10-01), Cole
patent: 4790493 (1988-12-01), Schwarzkopf et al.
Berejik Zacharia
Wallach Allon
B.T.A. Automatic Piloting Systems Ltd.
Barish Benjamin J.
Jordan Charles T.
Lieberman Rochelle
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