Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Patent
1975-11-24
1977-01-25
Blix, Trygve M.
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
244182, B64C 1900, G05D 108
Patent
active
040047563
ABSTRACT:
An automatic flight controller for rotary wing aircraft having a setting apparatus for setting the device for the distance from a starting distance signal, a speed signal, and a remaining distance signal corresponding to the remaining distance from the starting spot to the hovering spot whereby the flight of the aircraft can be controlled in accordance with the remaining distance signal. A ground speed signal from a ground speed detecting device is integrated to obtain a signal corresponding to the flight distance from the starting spot and a remaining distance signal is then produced which is equal to the difference between the starting distance signal and the flight distance signal, and, through a function amplifier, a reference speed signal is obtained which corresponds to the remaining distance to be flown at every instance. This reference speed signal is compared with the actual ground speed to provide a speed difference signal which is used as a control signal for controlling the speed of the aircraft. The automatic flight controller may also provide an altitude control system for controlling the collective pitch control mechanism to obtain a desired altitude.
REFERENCES:
patent: 2650046 (1953-08-01), Vanderlip
patent: 3649818 (1972-03-01), Sylvander
patent: 3711042 (1973-01-01), Rempfer
patent: 3816716 (1974-06-01), DeGarmo
Futatsugi Setsuo
Gerstine Milton I.
Goldberg Joshua I.
Iwasaki Koji
Seo Ryozo
Blix Trygve M.
D'Ambrosio F. J.
Eisenzopf Reinhard J.
The Boeing Company
Visek F. J.
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