This morphing wing (140) comprises: a link structure capable of expanding in a first direction and retracting in a second direction, which is opposite to the first direction; a plurality of front wing covers (180) mounted frontward, which is one side orthogonal to the first direction in the link structure; and a plurality of flight feathers (160) mounted rearward, which is the other side orthogonal to the first direction in the link structure. The front wing covers (180) and the flight feathers (160) are streamlined from front to back, and when the link structure retracts, flight feathers (160) retract inside adjacent flight feathers (160).


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    Title :

    Morphing wing, flight control device, flight control method, and program


    Contributors:
    DAICHI WADA (author)

    Publication date :

    2024-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen



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