Fuzzy logic autobrake system for aircraft

Details Fuzzy logic autobrake system for aircraft Fuzzy logic autobrake system for aircraft

1995-06-06

1996-07-23

Park, Collin W.

Boots, shoes, and leggings

395900, 244110R, 303126, B60T 1310

Patent

active

055396429

ABSTRACT:
A system for automatically controlling the braking of an aircraft to a desired setting upon landing or during a rejected takeoff. The inputs to the control system are airplane acceleration and airplane pitch. The output from the control system is an electric current which is sent to a hydraulic servo valve. This valve meters hydraulic pressure to the brakes.

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