Title:
An unmanned aircraft, its control system, a method, and the unmanned aircraft landing control method
Document Type and Number:
Japanese Patent JP6234610
Kind Code:
B2
Abstract:
The present invention relates to an unmanned aerial vehicle (100), an unmanned aerial vehicle control system, an unmanned aerial vehicle control method, and an unmanned aerial vehicle landing control method. The unmanned aerial vehicle includes a fuselage (12), a power device (32) connected onto the fuselage, and a control device and a takeoff and landing device (50) disposed on the fuselage. The power device (32) and the takeoff and landing device are electrically connected with the control device respectively. The control device includes a landing surface detection assembly. The control device is used for controlling operating modes of the power device and the takeoff and landing device when the landing surface detection assembly detects that a landing destination of the unmanned aerial vehicle is a water surface. It may enable the unmanned aerial vehicle to land on the water surface and navigate. The unmanned aerial vehicle can fly in the air and can also navigate in water.
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Inventors:
King name Yu
Application Number:
JP2016558200A
Publication Date:
November 22, 2017
Filing Date:
July 02, 2015
Export Citation:
Assignee:
SZ DJI TECHNOLOGY CO.,LTD
International Classes:
B64C25/54; B64C13/10; B64C25/58; B64C27/08; B64C37/00; B64C39/02; B64D45/00; B64D47/00; B64D47/08
Domestic Patent References:
JP2009514740A | ||||
JP2008203123A | ||||
JP11334698A |
Foreign References:
US20130206915 | ||||
US20030011493 | ||||
CN102815397A | ||||
US20110248118 | ||||
US20100066158 | ||||
CN102424110A |
Attorney, Agent or Firm:
try international patent corporation
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