Sz Dji Technology Co., Ltd.

Shenzhen Zhuoyu Technology Co., Ltd.

Zhimeng Shang

Canlong Lin

Li Wei Wang

Xiaoliang Wang

Jiahang Ying

Ximin Lv

Jianyun Ma

A multi-rotor UAV control method, a multi-rotor UAV, a control apparatus, and a non-volatile computer-readable storage medium are provided. The multi-rotor UAV control method includes: obtaining a power status of each rotor of the UAV; and when it is determined, based on the power status, that the power of any one of the rotors of the UAV fails, controlling the UAV to enter a balance mode. In the balance mode, the UAV rotates at an angular velocity greater than a first threshold, and a displacement of the UAV in the horizontal direction is less than a preset displacement amount.

Multi-rotor unmanned aerial vehicle and control method thereof, control apparatus and computer-readable storage medium

The present disclosure discloses a driving device, a driving device control method and apparatus, and a storage medium. The method includes: determining whether an automatic driving state is currently available; if yes, detecting whether a user operates an acceleration controller; if the user operates the acceleration controller, receiving an output signal of the acceleration controller in real time; and finally, changing a driving speed based on a simulated acceleration control signal. According to the present disclosure, an operation on the acceleration controller can be used as an acceleration/deceleration operation in the automatic driving state, thereby improving user experience and market competitiveness.

Driving device, control method and apparatus, and storage medium

A method for controlling a landing gear of an unmanned aerial vehicle (UAV) includes detecting whether a relative-to-ground height of the UAV is greater than a height threshold, where the relative-to-ground height is a vertical height of the UAV with respect to an object; and in response to the relative-to-ground height being not greater than the height threshold and the UAV having not lowered the landing gear, adjusting the relative-to-ground height to the height threshold or above, and lowering the landing gear.

Unmanned aerial vehicle landing gear control method, apparatus, unmanned aerial vehicle, and system thereof

A control method includes obtaining one or more attitude parameters of a gimbal of a UAV and adjusting one or more attitude parameters of the UAV according to the one or more attitude parameters of the gimbal. The UAV includes a vehicle body, and a power system and the gimbal that are provided at the vehicle body. The power system includes a motor and a propeller and is configured to provide flight power for the UAV. The gimbal is configured to connect a photographing device to the vehicle body. Adjusting the one or more attitude parameters of the UAV includes adjusting a yaw parameter of the UAV according to the yaw parameter of the gimbal. Adjusting the yaw parameter of the UAV includes controlling the UAV to rotate in a yaw direction according to the yaw parameter of the gimbal, to cause the UAV to rotate along with the gimbal.

Control method, apparatus, and device, and UAV

A control method includes obtaining one or more attitude parameters of a gimbal of an unmanned aerial vehicle (UAV) and adjusting one or more attitude parameters of the UAV according to the one or more attitude parameters of the gimbal.

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Shenzhen, China

Zhimeng Shang