The invention discloses a pan-tilt control method, the pan-tilt and an unmanned aerial vehicle. Wherein the pan-tilt comprises a driving pan-tilt and a driven pan-tilt, the driving pan-tilt and the driven pan-tilt are in a linkage control mode, and the method comprises the following steps: obtaining a target attitude parameter of a target attitude of the driving pan-tilt, the target attitude being an attitude to which the driving pan-tilt is about to move; and sending the target attitude parameter to the driven holder, so that the driven holder is adjusted to the target attitude. After the target attitude parameter of the target attitude of the active pan-tilt is obtained, the target attitude parameter is sent to the driven pan-tilt, so that the attitude difference between the driven pan-tilt and the active pan-tilt can be reduced, and the control precision is improved.

    一种云台的控制方法、云台及无人飞行器。其中,所述云台包括主动云台和从动云台,所述主动云台与所述从动云台处于联动控制模式,所述方法包括:获得所述主动云台的目标姿态的目标姿态参数,所述目标姿态为所述主动云台将要运动到的姿态;向所述从动云台发送所述目标姿态参数,使所述从动云台向所述目标姿态调整。在获得主动云台的目标姿态的目标姿态参数后,发送给从动云台,可以缩小从动云台与主动云台之间的姿态差异,提高控制精度。


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    Titel :

    Pan-tilt control method, pan-tilt and unmanned aerial vehicle


    Weitere Titelangaben:

    云台的控制方法、云台及无人飞行器


    Beteiligte:
    WANG YINGZHI (Autor:in) / LIU SHUAI (Autor:in) / HE CHANGXIN (Autor:in) / YANG YONG (Autor:in) / CHEN HANPING (Autor:in)

    Erscheinungsdatum :

    2022-01-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




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