Method and device for automatic control of an aircraft...

Fluid-pressure and analogous brake systems – Speed-controlled – Automatic braking including speed governor or hydraulic...

Reexamination Certificate

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Details

C244S111000

Reexamination Certificate

active

06991304

ABSTRACT:
The invention relates to a system to control the deceleration of an aircraft during the taxiing phase on a landing strip, the system has a detector of the current position of the aircraft on the strip, and of the current speed of the aircraft on the strip, a calculator receiving position and speed values from the detector, to define, as a function of the desired final speed of the aircraft at the so-called final position on the strip, a deceleration set-point modification time, after the current time, and a new deceleration set-point to apply from the modification time, to reach the final position at the desired speed.

REFERENCES:
patent: 3920282 (1975-11-01), DeVlieg
patent: 4316252 (1982-02-01), Cooper
patent: 4367529 (1983-01-01), Masclet et al.
patent: 4454582 (1984-06-01), Cleary et al.
patent: 5024491 (1991-06-01), Pease, Jr. et al.
patent: 5142478 (1992-08-01), Crook
patent: 5951122 (1999-09-01), Murphy
patent: 5968106 (1999-10-01), DeVlieg et al.
patent: 6092919 (2000-07-01), Calise et al.
patent: 0 025 614 (1980-07-01), None
patent: 0 505 236 (1992-03-01), None
patent: 0 895 929 (1998-08-01), None

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