Braking control method for landed airplane, aiming to optimise its pitching anle.

The method involves correcting an instruction of braking according to a pitching angle (theta) of an aircraft (1) during braking. The correction process is carried out by subtracting the instruction of braking from a breaking setpoint correction value. The breaking setpoint correction value is calculated according to the pitching angle when the aircraft runs at a ground speed (V) with a lower threshold speed (Vseuil). The breaking setpoint correction value is set to zero when the ground speed is greater than or equal to the threshold speed.