Automatic direction stabilization system

Aeronautics and astronautics – Aircraft propulsion and steering on land or water

Patent

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Details

244103W, B64C 2550

Patent

active

042213509

ABSTRACT:
The present system automatically stabilizes the travel direction of an aircraft rolling out after touchdown on a runway. A corrected difference control signal is supplied to the steering mechanisms of the aircraft, including, if desired, the brake system. The control signal is generated in a comparator or transducer which receives at its inputs an actually measured signal representing changes in the travel direction of an aircraft, and a rated signal to produce a combined steering signal which is supplied to the nose wheel steering and/or to the wheel brakes.

REFERENCES:
patent: 2953323 (1960-09-01), Minch
patent: 3711042 (1973-01-01), Rempfer
patent: 3823899 (1974-07-01), Currey
patent: 3919961 (1975-11-01), McDougal
patent: 4006870 (1977-02-01), Boone
patent: 4008868 (1977-02-01), Berg

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