The invention discloses a flight control debugging system of a rotor craft. The flight control debugging system of the rotor craft comprises the rotor craft and a box body. The box body comprises an upper box and a lower box. The rotor craft is arranged in the upper box, the upper box is a perspective box, and a vent hole is formed in at least one in the upper face and the side faces of the upperbox. The lower box is arranged in the lower portion of the upper box and is provided with multiple port portions, and the port portions comprise an AC/DC port and a communication port. The flight control debugging system of the rotor craft is convenient to use, simple in maintenance and high in safety, and the real flight environment can be simulated better.

    本发明公开了一种旋翼飞行器的飞控调试系统,所述旋翼飞行器的飞控调试系统包括:旋翼飞行器和箱体本体,所述箱体本体包括:上箱体和下箱体,所述旋翼飞行器设置在所述上箱体中,所述上箱体为透视箱体,所述上箱体的上面和所述上箱体的侧面中的至少一个设置有透气孔;所述下箱体设置在所述上箱体的下部,所述下箱体设置有多个接口部,所述接口部包括:AC/DC接口和通讯接口。根据本发明的旋翼飞行器的飞控调试系统使用方便、维护简单且安全性强,能够更好地模拟真实的飞行环境。


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    Title :

    Flight control debugging system of rotor craft


    Additional title:

    旋翼飞行器的飞控调试系统


    Contributors:
    JIANG CHEN (author) / WANG HAOWEN (author) / YANG ZHIHONG (author)

    Publication date :

    2020-11-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen





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