METHOD FOR CONTROLLING AN AIRCRAFT TAXI SYSTEM

The invention relates to a method for controlling an aircraft taxi system, comprising the steps of:generating a traction command (Com) to control an electric motor of a wheel drive actuator;detecting whether or not an external brake command, intended to control braking of the wheel via the brake, is...

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Hauptverfasser: LIEGEOIS, Pierre-Yves, BOISSARD, Laurent, HADJIDJ, Djemouai
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creator LIEGEOIS, Pierre-Yves
BOISSARD, Laurent
HADJIDJ, Djemouai
description The invention relates to a method for controlling an aircraft taxi system, comprising the steps of:generating a traction command (Com) to control an electric motor of a wheel drive actuator;detecting whether or not an external brake command, intended to control braking of the wheel via the brake, is generated;if an external braking command is generated, producing a predetermined minimum command (Cmp) to control the electric motor so that the drive actuator applies a strictly positive predetermined minimum motor torque to the wheel during braking;detecting whether a speed of the aircraft becomes zero and, if so, inhibiting the predetermined minimum command (Cmp) so that the drive actuator applies zero torque to the wheel.
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subjects AEROPLANES
AIRCRAFT
ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES
TRANSPORTING
VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF
VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
VEHICLES IN GENERAL
title METHOD FOR CONTROLLING AN AIRCRAFT TAXI SYSTEM
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