Aircraft deceleration brake control system

Details Aircraft deceleration brake control system Aircraft deceleration brake control system

1990-02-20

1992-08-04

Chin, Gary

Boots, shoes, and leggings

244111, 303 93, B60T 828

Patent

active

051365103

ABSTRACT:
An aircraft deceleration brake control system receives deceleration command signals from left and right brake pedals of an aircraft. An amplifier generates the difference between the two command signals while an inertial navigation system of the aircraft provides a signal corresponding to the instantaneous deceleration of the aircraft. First and second control signals, corresponding to the respective command signals, are generated as a function of the difference in value between the command signals and the amplitude of the instantaneous deceleration signal.

REFERENCES:
patent: 3937526 (1976-02-01), Ruof
patent: 4022513 (1977-05-01), Hirzel et al.
patent: 4140352 (1979-02-01), Delpech et al.
patent: 4293165 (1981-10-01), Hirzel
patent: 5024491 (1991-06-01), Pease, Jr. et al.

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