UNMANNED AERIAL VEHICLE, CONTROL SYSTEM AND METHOD THEREFOR, AND LANDING CONTROL METHOD FOR UNMANNED AERIAL VEHICLE

WIPO Patent Application WO/2017/000304

A1

An unmanned aerial vehicle (100), a control system for an unmanned aerial vehicle, a control method for an unmanned aerial vehicle, and a landing control method for an unmanned aerial vehicle. The unmanned aerial vehicle (100) comprises a vehicle body (10), a power device (30) connected to the vehicle body (10), and a control device (70) and a take-off and landing device (50) disposed on the vehicle body (10). The control device (70) comprises a landing surface detection assembly (74). The control device (70) is used for controlling working modes of the power device (30) and the take-off and landing device (50) when the landing surface detection assembly (74) detects that a landing destination of the unmanned aerial vehicle (100) is a water surface, such that the unmanned aerial vehicle (100) can land and sail on the water surface. The unmanned aerial vehicle (100) can fly in the air and sail in water.

WO/2001/036268	PNEUMATIC FLOAT FOR LIGHT AND ULTRALIGHT AIRCRAFT
JP2020019463	DEPLOYMENT DEVICE FOR PARACHUTE OR PARAGLIDER, AND FLYING OBJECT EQUIPPED WITH SAME
JP2010126008	SHIFT (TELESCOPIC MOTION) TYPE FLOAT SEAPLANE (SEMI-BOAT SEAPLANE OR THE LIKE)

WANG MINGYU (CN)

PCT/CN2015/083171

January 05, 2017

July 02, 2015

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SZ DJI TECHNOLOGY CO LTD (CN)

B64C25/56

CN102815397A	2012-12-12
FI124723B	2014-12-31
CN204368424U	2015-06-03
CN204279934U	2015-04-22
CN102933460A	2013-02-13
CN104199462A	2014-12-10

See also references of EP 3318487A4

SHENZHEN SCIENBIZIP INTELLECTUAL PROPERTY AGENCY CO.,LTD. (CN)

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