The invention discloses an empennage regulation mechanism with pitching and yawing independently regulated and an ornithopter. The regulation mechanism comprises a frame and an empennage. The empennage comprises a horizontal wing panel and a vertical wing panel, wherein the horizontal wing panel achieves pitching regulation through reciprocating rotation of a horizontal shaft and the vertical wing panel achieves yawing regulation through reciprocating rotation of a vertical shaft. The regulation mechanism further comprises a first drive assembly and a second drive assembly. The horizontal shaft and the vertical shaft are two structures moving independently from each other. The first drive assembly is used for driving one of the horizontal wing panel and the vertical wing panel to implement the corresponding regulation movement, and the second drive assembly is used for driving the other of the horizontal wing panel and the vertical wing panel to implement the corresponding regulation movement. According to the invention, pitching regulation and yawing regulation can be completely decoupled, yawing regulation and pitching regulation of the empennage can be achieved through two irrelevant steps, and therefore mutual interference is effectively avoided, the control accuracy can be improved, and the control difficulty can be lowered.


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    Titel :

    Empennage regulation mechanism with pitching and yawing independently regulated and ornithopter


    Beteiligte:
    XU WENFU (Autor:in) / PAN ERZHEN (Autor:in) / LI GUANGMING (Autor:in) / LUO CAN (Autor:in)

    Erscheinungsdatum :

    2015-12-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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