-
公开(公告)号：US20220153404A1
公开(公告)日：2022-05-19
申请号：US17590805
申请日：2022-02-01
发明人： Fu-Kai YANG , Chien-Hsun LIAO , Yi-Feng CHENG , Di-Yang WANG , Meng-Yan SHEN
摘要： The present application provides an unmanned aerial vehicle (UAV) for a long duration flight. An exemplary UAV may include a UAV body assembly. The UAV may also include a flight control system (FCS) coupled to the UAV body assembly. The UAV may further include a motor coupled to the UAV body assembly at one end and coupled to a propeller at the other end. The FCS is communicatively connected to the motor. A center of gravity (CG) of the UAV is at a point between 21% and 25% of a mean aerodynamic chord (MAC) of the UAV.
-
公开(公告)号：US20190220038A1
公开(公告)日：2019-07-18
申请号：US16243019
申请日：2019-01-08
发明人： Lung-Shun SHIH , Fu-Kai YANG , Yi-Feng CHENG , Chao-Wen FU , Meng-Yan SHEN
CPC分类号： G05D1/0661 , B64C9/00 , B64C39/024 , B64C2009/005 , B64C2201/08 , B64C2201/12 , G05D1/085
摘要： The present application provides methods and systems for launching an unmanned aerial vehicle (UAV). An exemplary system for launching a UAV includes a detector configured to detect acceleration of the UAV in a launch mode. The exemplary system may also include a memory storing instructions and a processor configured to execute the instructions to cause the system to: obtain a signal configured to notify the UAV to enter the launch mode, determine whether the acceleration of the UAV satisfies a condition corresponding to threshold acceleration in the launch mode, and responsive to the determination that the acceleration of the UAV satisfies the condition, turn on a motor of the UAV.
-
搜索结果
2 条记录 (耗时 0.013 秒)
