Method of managing the braking of an aircraft to limit its pitch
View Patent ↗A method of managing the braking of an aircraft 1 having at least one controllable brake 9 for braking the aircraft 1 when the aircraft 1 is on the ground and as a function of a braking setpoint C. The method includes correcting the braking setpoint as a function of the pitch angle θ of the aircraft 1 during braking.
1. A method of managing the braking of an aircraft having a braking computer and at least one brake controllable by said braking computer for braking the aircraft when the aircraft is on the ground and as a function of a braking setpoint, the method comprising:
correcting the braking setpoint as a function of a pitch angle of the aircraft during braking, and
wherein said correction is performed by subtracting a correction value from the braking setpoint, which correction value is:
calculated by the braking computer as a function of the pitch angle if the aircraft is running at a ground speed less than a threshold speed; and
set to zero if the ground speed is greater than or equal to the threshold speed.
2. A method according to claim 1 , wherein the correction of the braking setpoint includes a step of limiting any variation to the correction of the setpoint.