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.
FLIGHT HINDRANCE DISPLAY APPARATUS, FLIGHT HINDRANCE DISPLAY METHOD, AND COMPUTER-READABLE MEDIUM
2017-09-21
Patent
Elektronische Ressource
Englisch
Flight hindrance display apparatus, flight hindrance display method, and computer-readable medium
Europäisches Patentamt | 2017
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