-
公开(公告)号:US20170372625A1
公开(公告)日:2017-12-28
申请号:US15699410
申请日:2017-09-08
Inventor: Takashi HORINOUCHI
CPC classification number: G08G5/045 , B64C27/08 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/141 , B64C2201/143 , B64C2201/145 , B64C2201/146 , B64D47/06 , B64D47/08 , G05D1/0027 , G05D1/104 , G06K9/00664 , G06K9/4604 , G08G5/0004 , G08G5/0021 , G08G5/0069 , G08G5/0078
Abstract: An unmanned aerial vehicle according to the present disclosure is an unmanned aerial vehicle that can fly in midair and includes a propulsion unit configured to generate a propulsion force for fly in midair, a laser light source configured to illuminate laser light, an imaging unit configured to generate a captured image by capturing vertically below the unmanned aerial vehicle during flight in midair, and a controller configured to control an operation of the propulsion unit. The controller analyzes a captured image, extracts a light spot formed by laser light, measures a positional relationship with another unmanned aerial vehicle based on the extracted light spot, and executes a collision avoidance operation with respect to another unmanned aerial vehicle based on the measured positional relationship.