Method and device for automatic control of an aircraft...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/42 (2006.01)

Patent

CA 2431361

The invention concerns a device for controlling an aircraft deceleration in running phase on a runway, the device comprising: means for input (100) of a current position of the aircraft on the runway; means for input (100) of a current speed of the aircraft on the strip, calculating means (102), receiving the position and speed values derived from the input means, for establishing, on the basis of a desired final speed of the aircraft in a so-called final position on the runway, a time modifying the deceleration set point, subsequent to a current time, and a new deceleration set point to be applied, based on the modifying time, to reach the desired final speed.

L'invention concerne un dispositif de commande de la décélération d'un aéronef en phase de roulement sur une piste d'atterrissage, le dispositif présentant : - des moyens de saisie (100) d'une position actuelle de l'aéronef sur la piste, - des moyens de saisie (100) d'une vitesse actuelle de l'aéronef sur la piste,des moyens de calcul (102), recevant des valeurs de position et de vitesse en provenance des moyens de saisie, pour établir, en fonction d'une vitesse finale souhaitée de l'aéronef en une position dite finale sur la piste, un instant de modification de la consigne de décélération, postérieur ô un instant actuel, et une nouvelle consigne de décélération ô appliquer ô partir de l'instant de modification, pour atteindre la position final ô la vitesse souhaitée.

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