A method is provided for controlling a gimbal including a mounting member. The method includes determining, through a magnetic sensor, a first deflection angle of the mounting member around a yaw axis in a time period. The method also includes determining, through an inertial measurement unit, a second deflection angle of the mounting member around the yaw axis in the time period. The method also includes determining an angle error of the inertial measurement unit based on the first deflection angle and the second deflection angle. The method further includes controlling attitude of the gimbal based on measurement data of the inertial measurement unit in which the angle error has been corrected.


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    Titel :

    GIMBAL CONTROL METHOD, CONTROL SYSTEM, GIMBAL, AND UNMANNED AIRCRAFT


    Beteiligte:
    WANG YAN (Autor:in)

    Erscheinungsdatum :

    17.10.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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