The present disclosure provides a gimbal, a gimbal control device and method implemented in the gimbal and gimbal control device. The method includes obtaining a first angular velocity of a directional device mounted on a gimbal in a first direction; obtaining at least one reference angular velocity in at least one reference direction of the gimbal; obtaining an angular velocity offset in the first direction based on the first angular velocity and the at least one reference velocity; and adjusting an angle of the gimbal in the first direction based on the angular velocity offset. In this way, the posture drift of the gimbal in the yaw direction due to a detection error of the directional device may be eliminated, so that the picture taken by a photographing device provided on gimbal is stable, and the shooting quality is improved.

A gimbal includes a rotation assembly. The rotation assembly includes an axis arm, a lock device, and an electric motor configured to drive the axis arm with a first driving force to rotate to a pre-set position, such that the lock device locks the axis arm at the pre-set position, and when the axis arm is at the pre-set position, drive the axis arm with a second driving force to rotate, such that the lock device unlocks the axis arm.

A stabilizer folding structure and a handheld stabilizer. a stabilizer folding structure for rotationally connecting the motor base and the rocker arm such that the motor base and the rocker arm have an unfolded first state and a stored second state during relative rotation, comprising: an elastic member, applying An elastic force for abutting the motor base and the rocker arm; and a snap structure at a position where the motor base abuts the rocker arm, in the first state and the second state, The snap structure is engaged to restrict relative rotation of the motor base and the rocker arm. In other states, the snap structure is disengaged such that the motor base and the rocker arm are relatively rotatable. The folding structure of aspects of the invention facilitates the folding and storage of the stabilizer, and is convenient for the user to use.

A method for suppressing a vibration of a gimbal includes obtaining state information of the gimbal, determining a vibration frequency of the gimbal according to the state information, and performing an operation of suppressing the vibration of the gimbal according to the vibration frequency of the gimbal.

A stabilizing platform for stabilizing a payload includes a frame assembly, a plurality of actuators, and a plurality of electronic speed control (ESC) units. The frame assembly includes a plurality of frame components movable relative to one another and is configured to support the payload. The plurality of actuators are configured to permit the plurality of frame components to move relative to one another. Each of the plurality of ESC units is electrically coupled to a corresponding actuator of the plurality of actuators and is configured to control actuation of the corresponding actuator. At least one of the plurality of frame components includes a cavity, one of the plurality of actuators allowing the at least one of the frame components that includes the cavity to move relative to the carrier. At least two of the plurality of ESC units are received and sealed in the cavity.

Embodiments of the present disclosure provides a gimbal. The gimbal includes a pitch motor, a coaxial cable, and a first support arm arranged opposite a second support arm. The pitch motor is disposed at a front end of the first support arm, a motor shaft of the pitch motor extending in a direction of the second support arm for connecting with one end of an imaging device; a limiting shaft is disposed at a front end of the second support arm, the limiting shaft extending in a direction of the first arm for connecting with another end of the imaging device; a first wiring space is formed in the limiting shaft and a second wiring space is formed in the second support arm, a first end of the coaxial cable sequentially passing through the second wiring space and the first wiring space for electrically connecting with the imaging device.

The present disclosure provides an imaging system. The imaging system includes an imaging host. The imaging host includes a camera and a host interface connected with the camera. The imaging system includes a wireless communication module. The wireless communication module includes a circuit board, a Bluetooth antenna, and a Wi-Fi antenna, the Bluetooth antenna and Wi-Fi antenna being disposed on the circuit board, and the wireless communication module and the host interface being plugged into the imaging host.

A device for wall mounting television or another display includes a wall mounting portion, a display mounting portion, and an extending/contracting portion. The extending/contracting portion includes a lower arm, an upper arm, a front bracket, a wall mounting bracket, one or more gas springs, and a linear actuator. The one or more gas springs and the linear actuator are arranged selectively to retract and extend the display mounting portion. The lower arm includes protrusions for automatically straightening a display attached to the display mounting portion. The display mounting portion and the extending/contracting portion together include a mechanism for automatically adjusting azimuth of the display mounting portion to a pre-set position when the display mounting portion is lowered into a viewing position. The mechanism for automatically adjusting azimuth may include a set screw and a biasing spring.

A stabilizing platform for stabilizing a payload includes a frame assembly, a plurality of actuators, and a plurality of electronic speed control (ESC) units. The frame assembly includes a plurality of frame components movable relative to one another and is configured to support the payload. The plurality of actuators are configured to permit the plurality of frame components to move relative to one another. Each of the plurality of ESC units is electrically coupled to a corresponding actuator of the plurality of actuators and is configured to control actuation of the corresponding actuator. At least one of the plurality of frame components includes a cavity, one of the plurality of actuators allowing the at least one of the frame components that includes the cavity to move relative to the carrier. At least two of the plurality of ESC units are received and sealed in the cavity.

A stabilizing device for stabilizing a payload includes a handle assembly, a payload stabilization assembly, and a constant force assembly. The handle assembly includes one or more grips configured to permit a user to support the entirety of the stabilizing device using the one or more grips. The payload stabilization assembly is configured to support the payload and permit the payload to rotate about at least one axis of rotation. The constant force assembly is operably connected to the handle assembly and supports the payload stabilization assembly. The constant force assembly is configured to provide a force that equipoises a gravity force of the payload stabilization assembly with the payload in a vertical direction such that a net force of the payload stabilization assembly with the payload in the vertical direction is substantially zero.