Method of validating a flight plan constraint

G - Physics – 05 – D

Patent

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G05D 1/00 (2006.01)

Patent

CA 2508287

The invention relates to the validation, by the FMS flight management computer on board an aerodyne, of a flight plan (Dpv) constraint, such as altitude, at an imposed fly-by point close to the position of the aerodyne at the moment when the automatic flight plan-following system is activated. According to the invention, one such constraint is validated in advance by looking into the near future using an aerodyne movement forecast (Pt), taking account of the movement of the aerodyne during the transition between the application of the current flying orders before the activation of the automatic following system and the flying orders newly provided by the FMS flight computer (30) at the time of activation.

La présente invention concerne le respect, par le calculateur de gestion de vol FMS équipant un aérodyne, d'une contrainte, notamment d'altitude, du plan de vol (Dpv) en un point imposé de passage proche de la position de l'aérodyne au moment de la mise en route de sa fonction de suivi automatique de plan de vol. Elle consiste à valider àl'avance une telle contrainte en se projetant dans un futur proche au moyen d'une prévision (Pt) du déplacement de l'aérodyne tenant compte du mouvement de l'aérodyne au cours de la transition entre les mises en application des consignes de vol prévalant avant la mise en route de la fonction de suivi automatique et celles nouvellement fournies par le calculateur de vol FMS (30) lors de cette mise en route.

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