Aeronautics and astronautics – Aircraft control – Automatic
Patent
1987-06-22
1989-05-02
Barefoot, Galen
Aeronautics and astronautics
Aircraft control
Automatic
244 76R, 244 78, 318564, 91363A, B64C 1316
Patent
active
048261106
ABSTRACT:
Prevention of actuator oscillation due to failure mode in an aircraft pitch axis control system is provided by an oscillatory failure monitor. The oscillatory failure monitor provides power shutdown of the actuator through inner loop modeling and error signal processing of inner loop disturbances.
REFERENCES:
patent: 3462662 (1969-08-01), Carpenter
patent: 3741073 (1973-06-01), Garjost
patent: 3826174 (1974-07-01), Platt et al.
patent: 4094481 (1978-06-01), DeWalt
patent: 4304375 (1981-12-01), Builta et al.
Barefoot Galen
Donahue B. A.
Gardner Conrad O.
The Boeing Company
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