According to the present disclosure, there is provided a landing system for landing an aerial vehicle at a target location, the landing system comprising: a processor assembly configured to: receive information related to variation in vertical displacement of the target location over time; determine a downward heave phase of the target location based on the received information; control the aerial vehicle to land at the target location during the downward heave phase.

    Selon la présente divulgation, l'invention concerne un système d'atterrissage pour poser un véhicule aérien à un emplacement cible, le système d'atterrissage comprenant : un ensemble processeur configuré pour : recevoir des informations relatives à une variation du déplacement vertical de l'emplacement cible au cours du temps ; déterminer une phase de pilonnement descendant de l'emplacement cible sur la base des informations reçues ; commander le véhicule aérien pour atterrir à l'emplacement cible pendant la phase de pilonnement descendant.


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    Title :

    LAND PLATFORM ASSEMBLY, LANDING SYSTEM, VEHICLE, FLOAT ARRANGEMENT, AERIAL VEHICLE AND ASSOCIATED SYSTEMS AND METHODS


    Additional title:

    ENSEMBLE PLATEFORME TERRESTRE, SYSTÈME D'ATTERRISSAGE, VÉHICULE, AGENCEMENT DE FLOTTEUR, VÉHICULE AÉRIEN ET SYSTÈMES ET PROCÉDÉS ASSOCIÉS



    Publication date :

    2024-12-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge




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