Longitudinal piloting system for a taxiing aircraft

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Details

C701S003000

Reexamination Certificate

active

07340327

ABSTRACT:
The system includes a plurality of engines that generate a thrust of an aircraft, each of the engines controlled by a first controllable actuator. A plurality of brakes reduce the speed of the aircraft when it is taxiing, each of the brakes controlled by a second controllable actuator. A control unit generates a piloting setpoint that relates to the longitudinal behavior of the aircraft. A central processing unit automatically determines, from the piloting setpoint, a plurality of individual control commands that are applied automatically to the first and second actuators and used to satisfy the piloting setpoint and a usage objective for the actuators.

REFERENCES:
patent: 4822113 (1989-04-01), Amberg et al.
patent: 5386954 (1995-02-01), Bissey et al.
patent: 6241183 (2001-06-01), Mathieu
patent: 2003/0125848 (2003-07-01), Otake et al.
patent: 2770824 (1999-05-01), None

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