The invention relates to the field of rotor unmanned aerial vehicles, in particular to a rotor unmanned aerial vehicle power system based on lift force feedback, which replaces traditional motor rotating speed closed-loop control, performs closed-loop control by directly taking lift force generated by a rotor wing as a control object, and designs a force feedback controller. According to the power system, a force sensor is used for directly measuring the lift force, filtering processing is conducted on data output by the sensor, the data serve as feedback signals of force closed-loop control, and closed-loop control over the lift force of the power system is formed by building a force feedback controller. When the power system is applied to the rotor unmanned aerial vehicle, the maneuverability and robustness of the system can be effectively improved.

    本发明涉及旋翼无人机领域,具体涉及一种基于升力反馈的旋翼无人机动力系统,取代传统的电机转速闭环控制,直接以旋翼产生的升力作为控制对象进行闭环控制,并设计力反馈控制器。动力系统使用力传感器直接对升力进行测量并对传感器输出数据进行滤波处理,将其作为力闭环控制的反馈信号,通过搭建力反馈控制器形成动力系统升力的闭环控制。将该动力系统应用于旋翼无人机可以有效提升系统机动性和鲁棒性。


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    Titel :

    Rotor wing unmanned aerial vehicle power system based on lift force feedback


    Weitere Titelangaben:

    一种基于升力反馈的旋翼无人机动力系统


    Beteiligte:
    HE YUQING (Autor:in) / CHANG YANCHUN (Autor:in) / YANG LIYING (Autor:in) / LI SILIANG (Autor:in) / HUANG CHAOXIONG (Autor:in) / SUN MIAO (Autor:in)

    Erscheinungsdatum :

    14.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64C AEROPLANES , Flugzeuge



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