公开(公告)号：US09604719B2

公开(公告)日：2017-03-28

申请号：US14167095

申请日：2014-01-29

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Matthieu Mayolle ,  Caroline Acanfora ,  Louis-Emmanuel Romana ,  Julien Fontan

IPC: B64C25/48 ,  B60T8/17 ,  B64C25/50

CPC classification number: B64C25/48 ,  B60T8/1703 ,  B60T2201/16 ,  B64C25/50

Abstract: A device for lateral control of an aircraft includes a calculating unit for automatically applying, if conditions for turning of the aircraft are met, a symmetrical braking value at a brake assembly. Subsequently, in the course of the turn, the device automatically distributes this symmetrical braking value in differential braking between a braking device of the left main landing gear and a braking device of the right main landing gear of the aircraft. Distribution of the symmetrical breaking is performed as a function of current directional command orders in such a way as to maintain a constant overall braking level for, at least for directional command orders below a predetermined threshold.