Abstract: The present invention discloses a motor, a gimbal including the motor and an aircraft including the gimbal. The motor includes a base, a rotation shaft, a stator assembly, a first bearing, a stator bearing and a rotor assembly that is used for driving an external member to rotate. The rotation shaft has a first end portion, a second end portion and a middle portion connecting the first end portion to the second end portion. The base is connected to the first end portion by using the first bearing. The rotor assembly is connected to the middle portion. The stator bearing, the rotor assembly and the first bearing are sequentially arranged along an axial direction of the rotation shaft. The stator assembly is connected to the rotation shaft by using the stator bearing.

Abstract: The present application relates to a gimbal configured to mount a photographing device. The gimbal includes a main body, a mounting shaft connected to the main body and a base disposed on the mounting shaft. The base is configured to fasten the photographing device. The gimbal further includes a fixing plate disposed on the base and a circuit board mounted between the fixing plate and the base. The circuit board is provided with a USB input interface and a USB output interface. The USB input interface is configured to form a data transmission connection to the photographing device. The USB output interface is configured to be connected to an external storage device. The present application further relates to an image photographing apparatus including the foregoing gimbal and an unmanned aerial vehicle including the foregoing image photographing apparatus.

Abstract: The present application relates to a gimbal configured to mount a photographing device. The gimbal includes a main body, a mounting shaft connected to the main body and a base disposed on the mounting shaft. The base is configured to fasten the photographing device. The gimbal further includes a fixing plate disposed on the base and a circuit board mounted between the fixing plate and the base. The circuit board is provided with a USB input interface and a USB output interface. The USB input interface is configured to form a data transmission connection to the photographing device. The USB output interface is configured to be connected to an external storage device. The present application further relates to an image photographing apparatus including the foregoing gimbal and an unmanned aerial vehicle including the foregoing image photographing apparatus.

Abstract: The present application provides a dual-arm gimbal, including a support base, two support arms and two mounting bases. The support base is assembled on a gimbal base and a first motor is assembled in the support base; the two support arms are assembled on the support base and an upper end of each support arm is integrally connected to a first motor rotor of the first motor in the support base, so as to drive the support arm to rotate around the support base; and the two mounting bases are respectively fixedly mounted at lower ends of the support arms and a camera apparatus used to photographing is mounted between the two mounting bases by using a rotary shaft.

Abstract: The present invention discloses a motor, a gimbal including the motor and an aircraft including the gimbal. The motor includes a base, a rotation shaft, a stator assembly, a first bearing, a stator bearing and a rotor assembly that is used for driving an external member to rotate. The rotation shaft has a first end portion, a second end portion and a middle portion connecting the first end portion to the second end portion. The base is connected to the first end portion by using the first bearing. The rotor assembly is connected to the middle portion. The stator bearing, the rotor assembly and the first bearing are sequentially arranged along an axial direction of the rotation shaft. The stator assembly is connected to the rotation shaft by using the stator bearing.

Abstract: Method, device, and apparatus for a gimbal parameter adjustment are provided. An exemplary method includes: controlling a supply of power to a motor upon detection of a gimbal parameter adjustment event, recording rotational angular velocity data of a gimbal axis controlled by the motor at respective time points, calculating angular acceleration data at the respective time points based on the rotational angular velocity data, determining a peak frequency within a predefined frequency band after performing a frequency conversion on the angular acceleration data, and configuring the peak frequency as a trap frequency of the motor to filter out a signal sending to the motor and having a frequency of the trap frequency.

Abstract: Systems and methods are provided for supporting and articulating a payload using stabilization platform. The stabilization platform may be configured to avoid gimbal lock. The stabilization platform may be configured to automatically transition between different modes of orientation.

Abstract: Method, device, and apparatus for a gimbal parameter adjustment are provided. An exemplary method includes: controlling a supply of power to a motor upon detection of a gimbal parameter adjustment event, recording rotational angular velocity data of a gimbal axis controlled by the motor at respective time points, calculating angular acceleration data at the respective time points based on the rotational angular velocity data, determining a peak frequency within a predefined frequency band after performing a frequency conversion on the angular acceleration data, and configuring the peak frequency as a trap frequency of the motor to filter out a signal sending to the motor and having a frequency of the trap frequency.

Abstract: Systems and methods are provided for supporting and articulating a payload using stabilization platform. The stabilization platform may be configured to avoid gimbal lock. The stabilization platform may be configured to automatically transition between different modes of orientation.

Abstract: Systems and methods are provided for supporting and articulating a payload using stabilization platform. The stabilization platform may be configured to avoid gimbal lock. The stabilization platform may be configured to automatically transition between different modes of orientation.