The present invention relates to an unmanned aerial vehicle flight control system for conventional non-guided missile dropping, which designates a target in an image photographed by means of an unmanned aerial vehicle to allow the unmanned aerial vehicle to automatically move and hover vertically above the target, and autonomously corrects a flight position in a hovering flight state, thereby determining an accurate dropping position of a loaded non-guided missile to maximize a dropping effect.

    La présente invention se rapporte à un système de commande de vol de véhicule aérien sans pilote pour un largage de missile non guidé classique, qui désigne une cible dans une image photographiée au moyen d'un véhicule aérien sans pilote pour permettre au véhicule aérien sans pilote de se déplacer et de survoler automatiquement verticalement au-dessus de la cible, et corrige de manière autonome une position de vol dans un état de vol stationnaire, ce qui permet de déterminer une position de largage précise d'un missile non guidé chargé pour maximiser un effet de largage.

    본 발명은 무인비행체를 통해 촬영된 촬영영상에서 표적을 지정하여 무인비행체가 표적의 수직 상방으로 자동 이동 및 정지비행 하도록 하며, 정지비행 상태에서 비행 위치를 자체적으로 보정함으로써 탑재된 무유도탄의 정확한 투하 위치를 판단하여 투하 효과를 극대화할 수 있도록 하는 재래식 무유도탄 투하를 위한 무인비행체 비행 제어 시스템에 관한 것이다.


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    Title :

    UNMANNED AERIAL VEHICLE FLIGHT CONTROL SYSTEM FOR CONVENTIONAL NON-GUIDED MISSILE DROPPING


    Additional title:

    SYSTÈME DE COMMANDE DE VOL DE VÉHICULE AÉRIEN SANS PILOTE POUR UN LARGAGE DE MISSILE NON GUIDÉ CLASSIQUE
    재래식 무유도탄 투하를 위한 무인비행체 비행 제어 시스템


    Contributors:

    Publication date :

    2025-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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