公开(公告)号：US20170270808A1

公开(公告)日：2017-09-21

申请号：US15405507

申请日：2017-01-13

申请人： FUJI JUKOGYO KABUSHIKI KAISHA

发明人： Yoichi ONOMURA ,  Shinei TAKAHASHI ,  Yu ITABASHI

IPC分类号： G08G5/04 ,  H04N13/04

CPC分类号： G08G5/04 ,  G01S13/9303 ,  G08G5/0008 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/045 ,  H04N13/302

摘要： A flight hindrance display apparatus includes circuitry. The circuitry is configured to acquire surrounding information of an aircraft. The surrounding information is related to the a hindrance factor which is a possible flight hindrance to the aircraft. The circuitry is configured to determine a spatial range of the flight hindrance factor on a basis of the acquired surrounding information. The circuitry is configured to determine a flight hindrance cross-section that intersects a plane including a vector of a flight direction of the aircraft and is included in the determined spatial range of the flight hindrance factor. The circuitry is configured to cause a display unit to stereoscopically display an own position of the aircraft, the spatial range of the flight hindrance factor, and the flight hindrance cross-section.