The invention relates to a method for controlling an aircraft comprising at least one camera and a guidance system configured to indicate a trajectory (Ta) to the aircraft (A), the method (1) being implemented by a computer and being characterised in that it comprises the following steps: - acquiring (11) a distance (D) between the aircraft (A) and an obstacle (O) on the trajectory (Ta) of the aircraft (A) and a time before the aircraft (A) collides with the obstacle (O) from images of the obstacle (O) obtained by the camera; - estimating (12) at least one radial speed (Vr) of the obstacle (O) using an extended Kalman filter taking as input the distance (D) and the time before the aircraft (A) collides with the obstacle (O); and - modifying (13) the trajectory (Ta) of the aircraft (A) by the guidance system, according to the estimated radial speed value (Vr) of the obstacle (O) and the distance (D) between the aircraft (A) and the obstacle (O), so as to avoid a collision of the aircraft (A) with the obstacle (O).


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    Title :

    PROCÉDÉ DE CONTRÔLE DE LA TRAJECTOIRE D'UN AÉRONEF


    Additional title:

    METHOD FOR CONTROLLING THE TRAJECTORY OF AN AIRCRAFT
    VERFAHREN ZUR STEUERUNG DER FLUGBAHN EINES FLUGZEUGS


    Contributors:

    Publication date :

    2025-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French



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