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公开(公告)号:US11703886B2
公开(公告)日:2023-07-18
申请号:US17646768
申请日:2022-01-03
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Canlong Lin , Zhimeng Shang
IPC: G05D1/08 , B64C39/02 , B64D47/08 , G05D1/00 , B64U101/30
CPC classification number: G05D1/085 , B64C39/024 , B64D47/08 , G05D1/0094 , B64U2101/30
Abstract: 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.
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公开(公告)号:US11834197B2
公开(公告)日:2023-12-05
申请号:US16515428
申请日:2019-07-18
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Canlong Lin , Li Wang , Zhimeng Shang
CPC classification number: B64D45/04 , B64C25/24 , G01C5/005 , G05D1/0676 , B64U70/00
Abstract: 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.
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公开(公告)号:US11216013B2
公开(公告)日:2022-01-04
申请号:US16457305
申请日:2019-06-28
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Canlong Lin , Zhimeng Shang
Abstract: 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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