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 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 method for controlling an unmanned aerial vehicle (UAV) includes: determining, by a processor, a change in a body portion of a user based on acquired images that include the body portion of the user; determining, by the processor, control data of the UAV based on the change in the body portion; and controlling, by the processor, the UAV based on the control data.

Abstract: An unmanned aerial vehicle arm adjustment device for adjusting an unmanned aerial vehicle arm into a folding state or an extracting state with respect to a fuselage of the aerial vehicle includes: left and right curb plates connected to the fuselage; a rocking arm connected to the unmanned aerial vehicle arm, wherein one end of the rocking arm is articulated with the left and right curb plates, and a first engaging part is provided on the rocking arm; and a locking member articulated with the left and right curb plates, wherein the locking member is provided with a second engaging part for engaging with the first engaging part; wherein the locking member is adapted to rotate in a first direction to force the second engaging part to engage with the first engaging part so as to hold the rocking arm such that the unmanned aerial vehicle arm is in the extracting state; and wherein the locking member is adapted to rotate in a second direction opposite to the first direction to force the second engaging part to dis

Abstract: An image capturing system of an unmanned aerial vehicle is disclosed. The image capturing system includes a camera; a platform carrying the camera; and a platform controller configured to adjust a rotating speed of the camera through the platform based on a rotating instruction information and a current zoom magnification of the camera. The current zoom magnification is substantially real-time obtained from the camera. An image capturing method of an unmanned aerial vehicle is also disclosed. In the method a first instruction information and a rotating instruction information are received. A camera is zoomed based on the first instruction information. A current zoom magnification of the camera is obtained. A rotating speed of the camera is adjusted through a platform based on the rotating instruction information and the current zoom magnification.

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: An unmanned aerial vehicle (UAV) includes an image capturing module disposed on the UAV, and configured to capture image data; and a controller chip coupled to the image capturing module to receive and process the image data; and the controller chip being configured to control the flight of the UAV.

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 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 includes a base and a fixing support rotatably provided on the base, wherein the fixing support includes a first mounting seat and a second mounting seat, and the second mounting seat is provided with an inner cavity therein. An unmanned aerial vehicle including a gimbal is also provided.

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: An image capturing system of an unmanned aerial vehicle is disclosed. The image capturing system includes a camera; a platform carrying the camera; and a platform controller configured to adjust a rotating speed of the camera through the platform based on a rotating instruction information and a current zoom magnification of the camera. The current zoom magnification is substantially real-time obtained from the camera. An image capturing method of an unmanned aerial vehicle is also disclosed. In the method a first instruction information and a rotating instruction information are received. A camera is zoomed based on the first instruction information. A current zoom magnification of the camera is obtained. A rotating speed of the camera is adjusted through a platform based on the rotating instruction information and the current zoom magnification.

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: 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: The disclosure relates to an unmanned aerial vehicle, a motor control device and method for controlling the same. The motor control method includes: acquiring current attitude information of a load, target attitude information of the load and current operation parameter information of one or more motors on the load, and obtaining control information for controlling the one or more motors in accordance with the acquired information above; transmitting the control information to a shared memory for storage; reading the control information from the shared memory, and controlling operation of the one or more motors in accordance with the control information. In one embodiment, the motor control device does not require cable or PCB wiring to connect a main control unit and an execution unit, reducing the size of hardware. Moreover, with the shared memory, the speed and stability of data interaction between the main control unit and the execution unit may be improved.

Abstract: A flight monitoring system comprises a first set of flight-status detecting sensors comprising a first-type sensor A1 for providing a first-type measurement result and a second-type sensor A2 for providing a second-type measurement result; a second set of flight-status detecting sensors comprising a first-type sensor B1 for providing a first-type measurement result and a second-type sensor B2 for providing a second-type measurement result.

Abstract: An unmanned aerial vehicle (UAV), a UAV flight control method and device. The method includes: monitoring a current flight state of the UAV; correcting a flight attitude of the UAV to a preset attitude when the current flight state of the UAV is not consistent with a target flight state; and controlling the flight attitude of the UAV to be a natural hovering attitude when the flight attitude of the UAV fails to be corrected to the preset attitude under a first preset condition.

Abstract: A flight control system is provided. The system includes a primary circuit board, a secondary circuit board electrically connected to the primary circuit board, a system on chip (SOC) integrated chip, a power management chip configured to supply power to the SOC integrated chip, an electronic speed control (ESC) driving circuit module configured to control flight speed in response to an instruction from the SOC integrated chip. In the system, the SOC integrated chip and the power management chip are arranged on the primary circuit board, and the ESC driving circuit module is arranged on the secondary circuit board.