The invention relates to the technical field of unmanned aerial vehicle flying wing layout, in particular to a flying wing layout unmanned aerial vehicle stability augmentation control method which comprises the steps that eight control surfaces are arranged on two wings of an unmanned aerial vehicle, a control surface deflection virtual line is arranged on each wing, and all the control surfaces can deflect upwards and downwards along the corresponding control surface deflection virtual lines; and designing a control law of an unmanned aerial vehicle controller on the basis of a transverse-heading linear trajectory tracking control mode. The technical scheme is designed for course stability augmentation control decoupling of the flying wing layout unmanned aerial vehicle, the problem of course divergence of the flying wing unmanned aerial vehicle can be solved, and compared with an existing control method, the technical scheme is quick, stable and practical.

    本发明涉及无人机飞翼布局技术领域,尤其涉及一种飞翼布局无人机增稳控制方法,包括在无人机的两个机翼上布设八个舵面,并在每个机翼上设置一条舵面偏转虚拟线,所有舵面可沿对应的舵面偏转虚拟线上偏和下偏;以横航向直线轨迹跟踪控制模态为基础,设计无人机控制器的控制律。本技术方案为针对飞翼布局无人机的航向增稳控制解耦设计,能够解决飞翼无人机航向发散的问题,且相对对于现有控制方法而言,本技术方案快速、稳定、实用。


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    Titel :

    Flying wing layout unmanned aerial vehicle stability augmentation control method


    Weitere Titelangaben:

    一种飞翼布局无人机增稳控制方法


    Beteiligte:
    ZOU YANG (Autor:in) / ZHANG QUHUI (Autor:in) / XIAO BEN (Autor:in)

    Erscheinungsdatum :

    2021-07-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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