Flap compensation system for use when controlling the pitch atti

Details Flap compensation system for use when controlling the pitch atti Flap compensation system for use when controlling the pitch atti

1975-12-24

1977-04-12

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft control

Automatic

244178, 318565, G05D 100

Patent

active

040170454

ABSTRACT:
A flap compensation system is provided which reduces the pilot applied force required to hold the pitch attitude of an aircraft within specified limits upon pilot operation of the aircraft flaps by automatically displacing the horizontal stabilizer of the craft as a function of flap displacement.

REFERENCES:
patent: 3215374 (1965-11-01), Olshausen
patent: 3422327 (1969-01-01), McBrayer et al.
patent: 3643146 (1972-02-01), Ferguson et al.

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