The invention provides a wingtip flexible connection fixed wing combined unmanned aerial vehicle and an attitude control method thereof, and the wingtip flexible connection fixed wing combined unmanned aerial vehicle comprises a central single machine and a plurality of non-central single machines; the non-central single machines are symmetrically arranged on the two sides of the central single machine, and the wing tip positions of every two adjacent central single machines and/or the wing tip positions of the non-central single machines are flexibly connected. According to the invention, attitude control of the flexible combined unmanned aerial vehicle can be completed, the system has certain anti-interference performance, the hardware cost is low, the combination mode is flexible, and the control method is simple and easy to implement.

    本公开提供了一种翼尖柔性连接固定翼组合无人机及其姿态控制方法,其翼尖柔性连接固定翼组合无人机包括,一个中心单机和多个非中心单机;所述非中心单机对称设置于所述中心单机两侧,且相邻两个中心单机和/或非中心单机的机翼翼尖位置柔性连接。本公开既能够完成柔性组合体无人机的姿态控制,又能够使系统具有一定的抗干扰性,硬件成本低,组合方式灵活,控制方法简单,易于实现。


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    Title :

    Wingtip flexible connection fixed wing combined unmanned aerial vehicle and attitude control method thereof


    Additional title:

    翼尖柔性连接固定翼组合无人机及其姿态控制方法


    Contributors:
    YUAN ZIWEI (author) / YANG YANPING (author) / ZHAO XINHUI (author) / LI ZIRONG (author) / WANG XIANGYU (author) / MA XIAOPING (author)

    Publication date :

    2020-06-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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