本发明公开一种多旋翼无人机PID调试及抗干扰测试装置,包括圆形底座(1)、多旋翼无人机固定板(2),所述多旋翼无人机固定板(2)的中部通过万向节(3)与所述圆形底座(1)的中心连接;所述多旋翼无人机固定板(2)由圆形中心板(2.1)和沿所述圆形中心板(2.1)径向伸出的两对同轴悬臂(2.2)组成;两对同轴的悬臂(2.2)的轴线相互垂直;所述悬臂(2.2)的底部均设有钕铁硼磁块(4);所述钕铁硼磁块(4)距离所述圆形中心板(2.1)的中心距离相等;本发明能对能对PID调参效果进行简单、安全和高效的抗干扰测试。

    The invention discloses a multi-rotor unmanned aerial vehicle PID debugging and anti-interference testing device, which comprises a circular base (1) and a multi-rotor unmanned aerial vehicle fixing plate (2), and the middle part of the multi-rotor unmanned aerial vehicle fixing plate (2) is connected with the center of the circular base (1) through a universal joint (3); the multi-rotor unmannedaerial vehicle fixing plate (2) is composed of a circular center plate (2.1) and two pairs of coaxial cantilevers (2.2) extending out in the radial direction of the circular center plate (2.1). The axes of the two pairs of coaxial cantilevers (2.2) are perpendicular to each other; neodymium iron boron magnetic blocks (4) are arranged at the bottoms of the cantilevers (2.2); the distances from theneodymium iron boron magnetic blocks (4) to the center of the circular center plate (2.1) are equal; and according to the invention, simple, safe and efficient anti-interference testing can be carriedout on the PID parameter adjusting effect.


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    Titel :

    一种多旋翼无人机PID调试及抗干扰测试装置


    Erscheinungsdatum :

    2024-05-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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