Zerotech (shenzhen) Intelligence Robot Co., Ltd.

Zerotech (beijing) Intelligence Technology Co. Ltd.

Hongtao Sun

Jianjun Yang

Gengpeng Liu

Zhangtao Xie

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.

Method of winding flexible cable, carrying equipment and gimbal

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.

Electric motor and gimbal applied with such electric motor

A dual-redundancy flight control system, comprises a master control system and a secondary control system. The master control system comprises a master controller, and further comprises a first inertial measurement unit (IMU), a first magnetic compass unit, and a first satellite navigation unit, each of which being connected to the master controller respectively. The secondary control system comprises a secondary controller, and further comprises a second IMU, a second magnetic compass unit, and a second satellite navigation unit, each of which being connected to the secondary controller respectively. The secondary controller is connected to the master controller via a data bus, and the master controller is connected to an electronic speed regulator of an aircraft for controlling the flight actions of the aircraft.

Dual-redundancy flight control system

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.

Gimbal and unmanned aerial vehicle including the same

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.

Growing community of inventors

Beijing, China

Hongtao Sun