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.
Procédé de gestion du freinage d'un aéronef permettant de limiter son tangage
Braking control method for landed airplane, aiming to optimise its pitching anle.
Verfahren zum Steuern das Bremsen eines gelandeten Flugzeugs zur Reduzierung seines Gierwinkels.
2017-08-16
Patent
Electronic Resource
French
PROCEDE DE GESTION DU FREINAGE D'UN AERONEF PERMETTANT DE LIMITER SON TANGAGE
European Patent Office | 2015
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