The present invention relates to an unmanned aerial vehicle equipped with a control moment gyro (CMG) for posture stabilization. In particular, a horizontal posture can be maintained while performing position movement without tilting a main body of the unmanned aerial vehicle so that a flight posture of cluster flight can be stabilized and geometric distortion during video recording missions can be prevented. In addition, the unmanned aerial vehicle can greatly improve flight stability and portability through structural improvement of the unmanned aerial vehicle. In particular, battery consumption in the control moment gyro can be minimized by providing a technology for balancing the body of the unmanned aerial vehicle by varying the number of rotations of a flywheel of a control moment gyro according to an air volume. The unmanned aerial vehicle equipped with a CMG for posture stabilization includes a main body, a driving part, a physical information sensing part, at least one inertial body, a control part, and a sensor.

    본 발명은 자세안정정화를 위해 제어 모멘트 자이로(CMG ; control memet gyro)를 구비한 무인비행체에 관한 것으로 상세하게는 무인비행체 본체를 기울이지 않고 수평자세를 유지하면서 위치 이동을 수행하여 군집비행 비행자세를 안정화하고 영상촬영 임무시 기하 왜곡을 방지하고, 또한 무인비행체의 구조 개선을 통해 비행안정성 및 휴대성을 크게 향상시키고자 하는 무인비행체를 제공하되, 특히, 본 발명은 제어 모멘트 자이로의 플라이휠의 회전수를 풍량에 따라 가변시켜 무인비행체의 몸체의 균형을 잡도록 하는 기술을 제공하여 제어 모멘트 자이로에서 소모되는 배터리의 소모를 최소화 하고자 한다.


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    Title :

    control memet gyro base Drone


    Additional title:

    자세안정정화를 위해 제어 모멘트 자이로를 구비한 무인비행체


    Contributors:

    Publication date :

    2022-12-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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