The present invention relates to a flying vehicle, and more specifically to the flying vehicle that is provided with a thrust vectoring control device so that generation of thrust for flight and fine altitude control of a fuselage can be simultaneously implemented, thereby capable of stabilizing the flight altitude by overcoming aerodynamic instability, electronically controlling the thrust vectoring control device in particular, and ensuring flight stability even in emergencies by enabling manual control. The flight vehicle includes a fuselage, a thrust part, and a thrust vectoring control device.

    본 발명은 비행체에 관한 것으로, 보다 상세하게는, 추력 편향 조종장치를 구비하여 비행을 위한 추력의 발생과 동체의 미세한 자세제어를 동시에 구현하여 공기역학적 불안정성을 극복해 비행 자세를 보다 안정화시킬 수 있을 뿐 아니라, 특히, 추력 편향 조종장치의 전자적인 제어 뿐만 아니라, 수동으로의 제어가 가능하도록 하여 유사시에도 비행 안정성을 확보할 수 있도록 하는 비행체에 관한 것이다.


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    Titel :

    Flying object with thrust vector controller


    Weitere Titelangaben:

    추력 편향 조종장치를 구비한 비행체


    Beteiligte:
    LEE BONG SEUB (Autor:in) / HONG CHOL GI (Autor:in)

    Erscheinungsdatum :

    28.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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