Aerial vehicle capable of vertical take-off and landing, vertical and horizontal flight and on-air energy generation버티컬 이착륙, 버티컬 및 호리즌탈 비행 및 비행중 에너지 생성이 가능한 비행체

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An aerial vehicle includes: a main body; two main wings arranged to the main body; two main wing tilting control units coupled to the main wings to control the main wings to tilt independently; two main propulsion units arranged to the main wings; tail wings arranged to a rear side of the main body; a rudder arranged to the tail wing; a rudder tilting control unit to control the rudder to tilt; a tail propulsion unit arranged to the rear side of the main body; a tail tilting control unit to control the tail propulsion unit to tilt; a power unit to provide power to the main and tail propulsion units; and a position control unit to control the main wing tilting control units, the main propulsion units, the rudder tilting control unit, the tail propulsion unit, the tail tilting control unit to adjust position of the aerial vehicle.
Assignee
KAIST
Country
US (United States)
Issue Date
2019-08-27
Application Date
2017-12-22
Application Number
15852444
Registration Date
2019-08-27
Registration Number
10392107
URI
http://hdl.handle.net/10203/267624
Appears in Collection
GT-Patent(특허)
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