Abstract: An electric motor, a gimbal and an unmanned aerial vehicle. The electric motor includes: a stator assembly; and a rotor assembly rotatably connected with the stator assembly. The stator assembly includes a stator housing for installation of a stator, the rotor assembly includes a rotor housing for installation of a rotor, and at least one of the stator housing and the rotor housing has a connecting arm. The gamble includes an electric motor group. At least one electric motor in the electric motor group is the above electric motor.

Abstract: A gimbal and a shooting apparatus are provided. The gimbal includes a motor and an imaging module, the gimbal further includes a case of the imaging module, the imaging module is received in the case, and the imaging module is connected with the motor through the case so that the case serves as a connection member.

Abstract: An unmanned aerial vehicle (UAV), a UAV landing control device and method. The UAV landing control method includes: receiving a trigger command; starting to monitor under control of the trigger command and outputting monitoring information based on a landing platform below the UAV, where the UAV has one or more rotors; and determining whether to control the one or more rotors of the UAV to stop rotation based on the monitoring information.

Abstract: A gimbal assembly and a hand-held device are provided. The gimbal assembly includes a gimbal, an image pick-up device and a light-transmitting cover covering the gimbal and the image pick-up device. The gimbal includes a holding assembly, the holding assembly is configured to drive the image pick-up device to rotate around at least one axis in the light-transmitting cover. The at least one axis passes through a spherical center of the light-transmitting cover, and upon the image pick-up device rotating, an optical axis of a lens of the image pick-up device always coincides with a normal line of a tangent plane at an intersection of the optical axis and the light-transmitting cover.

Abstract: A gimbal and a method for winding a flexible cable on a gimbal are provided. The gimbal includes a first motor and a second motor connected with each other. The flexible cable includes a connection unit and a connection end connected with each other, and the connection end is extended from the connection unit. The gimbal winding method includes winding the connection unit on the first motor while allowing the connection end to be electrically connected with the second motor.

Abstract: A method of winding a flexible cable, a carrying equipment and a gimbal are provided. The method is used for electrical connection in the carrying equipment, and includes winding a multilayer flexible cable provided in layered stack on a carrier device to form a winding structure, and the winding structure includes at least one force offsetting unit including a first bending part and a second bending part bent in opposite directions.

Abstract: An embodiment of the present disclosure provides an unmanned aerial vehicle, An unmanned aerial vehicle, with a double-layered structure formed by stacking a cover and a main component layer, wherein, the main component layer includes a base body and at least one functional component, the base body has a top facing to the cover layer and a bottom opposite to the top, the cover is in direct contact with the top of the base body, and the at least one functional component is mounted on the base body.

Abstract: An arm-airframe connecting structure and an unmanned aerial vehicle are provided by embodiments of the present disclosure. The arm-airframe connecting structure is configured to movably connect an airframe and an arm, and the arm is switchable between an unfolded position and a housed position with respect to the airframe. The arm-airframe connecting structure includes: at least one arm matching part provided on the arm; and at least one airframe matching part provided on the airframe. The at least one arm matching part and the at least one airframe matching part are configured to be bonded with each other so as to maintain at least one of the unfolded position and the housed position of the arm with respect to the airframe.

Abstract: A battery device comprises a housing, an electric core assembly enclosed within the housing, a control circuit board electrically coupled to the electric core assembly and for generating at least one battery parameter indicative of an operation status of the electric core assembly, and a connection port disposed on a front wall of the housing. The connection port comprises a set of power pins coupled to the electric core assembly and for charging or discharging the electric core assembly; and a set of data connection pins coupled to the control circuit board and for outputting the at least one battery parameter from the control circuit board.

Abstract: A method for controlling an unmanned aerial vehicle (UAV) is provided. The UAV comprises at least one rotor. The method includes receiving a take-off signal; initiating the at least one rotor to operate with a first preset rotation acceleration in response to the take-off signal; detecting a take-off status information of the UAV, the take-off status information at least comprising a current height of the UAV; determining whether the detected current height of the UAV is equal to or greater than a threshold; and sending a hover signal to the at least one rotor to enable the UAV to hover in the current height in response to the determination that the detected current height of the UAV is equal to or greater than the threshold.

Abstract: A method for controlling a UAV using a remote terminal. The remote terminal is capable of wirelessly communicating with the UAV. The method comprises detecting, via a physical input device of the remote terminal, at least one user's action applied to the physical input device; generating a control instruction in response to the detected at least one user's action; and transmitting the control instruction to the UAV.

Abstract: A cradle head includes: a yaw support, wherein one end of the yaw support is rotatable around a yaw axis; a pitching support, which is rotatably connected to the yaw support via a pitching axis, wherein a camera device mounting seat is provided on the pitching support; a first casing attached on the pitching support, wherein a first accommodating space is provided within the first casing, wherein the camera device mounting seat is disposed within the first accommodating space, and wherein a camera hole is provided in the first casing; and a third casing, provided on the yaw support, wherein a third accommodating space is provided within the third casing, the yaw support being disposed within the third accommodating space; wherein the third casing and the first casing form a part of a curved outer surface of the cradle head.

Abstract: A positioning method for unmanned aerial vehicle is disclosed. A first photo and a second photo of a predetermined form are first obtained, a first color card image of a color card is recognized from the first photo, and a second color card image of the same color card is recognized from the second photo, wherein the predetermined form includes a number of color cards. A first geometric center point coordinate and a first barycentric point coordinate of the first color card image are calculated. A reference line on the color card is obtained by mapping the first geometric center point coordinate and the first barycentric point coordinate to the color card, and a rotation angle of the UAV based on the reference line is obtained. A positioning method to get the flight speed for the UAV and a positioning device is also disclosed.

Abstract: A moving object tracking apparatus is disclosed. The moving object tracking apparatus includes an image input module, a memory, a coordinate obtainment module, a tracking coordinate filtering module, a displacement vector obtainment module, a similarity integral obtainment module, and a tracking point output module. A moving object tracking method is also provided.

Abstract: A supporting assembly for an unmanned aerial vehicle is disclosed. The supporting assembly includes a base, rotor arms, and rotor shrouds. The rotor arms extend from the base. Each of the rotor arms includes a proximal end secured to the base and a distal end opposite to the proximal end. Each of the rotor shrouds includes a converged end removably engaged with and secured to the distal end, an arc shaped end, and one or more connecting members extending from the arc shaped end to the converged end. An unmanned aerial vehicle and a rotor shroud apparatus are also disclosed.

Abstract: Disclosed is a supporting assembly and an unmanned aerial vehicle using the same, the supporting assembly includes a first base, a second base, a plurality of arms, and a damping element disposed between the first base and the second base. The second base is disposed on the first base. Each of the plurality of arms includes a proximal end and a distal end opposite to the proximal end, the proximal end is secured to the first base, and the distal end is configured for mounting a vibration source.

Abstract: A method for navigating an unmanned aerial vehicle (UAV) from an initial position of the UAV towards a base position comprises A) flying the UAV to a plurality of destination positions each having a first predetermined distance from the initial position of the UAV, wherein the plurality of destination positions correspond to a plurality of trial directions with respect to the initial position, respectively; B) detecting, for each of the plurality of destination positions, a distance from the base position to the destination position when the UAV is at the destination position, thereby to obtain a plurality of detected distances corresponding to the plurality of trial directions, respectively; C) determining a return direction of the UAV on the basis of the plurality of detected distances; and D) flying the UAV a second predetermined distance along the return direction.