Aeronautics and astronautics – Aircraft control – Automatic
Patent
1976-08-23
1978-01-31
Blix, Trygve M.
Aeronautics and astronautics
Aircraft control
Automatic
91384, 244 83E, 244 83J, 318621, B64C 1304
Patent
active
040712095
ABSTRACT:
A control system is specifically designed to improve the performance of an aircraft or other vehicle having undesirable dynamic characteristics. For this purpose there is employed a compensator, either hydromechanical or electrical (hydro-electrical) depending upon the basic control system, which is incorporated into that system and modifies command inputs to the directional controls of the vehicle. This compensator is designed and preset to impose predetermined dynamic characteristics on the command inputs so as to create a resulting input which eliminates or substantially diminishes the undesirable dynamic characteristics.
REFERENCES:
patent: 2496391 (1950-02-01), Hall
patent: 2584127 (1952-02-01), Harcum
patent: 2708258 (1955-05-01), Westwood
patent: 2803221 (1957-08-01), Walker
patent: 2903205 (1959-09-01), Borngesser
patent: 3093121 (1963-06-01), Murphy
patent: 3389639 (1968-06-01), Asche
Blix Trygve M.
Corber Billy G.
Eisenzopf Reinhard J.
Lockheed Corporation
Sullivan John J.
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