Landing point indication system for a rotorcraft

According to one embodiment, a landing point indication system (300) includes an image provider (310), a rotorcraft position provider (330), a pilot image generation system (340), and a display device (350). The image provider (310) is operable to provide a visual representation of an area underneat...

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Bibliographische Detailangaben
Hauptverfasser:	WORSHAM, ROBERT, CAUDILL, TROY S, ARCHER II, THOMAS E, REGNIER, BRADLEY, MCCOLLOUGH, JAMES M, COVINGTON, CHARLES E
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GYROSCOPIC INSTRUMENTS HELICOPTERS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SIGNALLING SURVEYING TESTING TRAFFIC CONTROL SYSTEMS TRANSPORTING
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Beschreibung
Zusammenfassung:	According to one embodiment, a landing point indication system (300) includes an image provider (310), a rotorcraft position provider (330), a pilot image generation system (340), and a display device (350). The image provider (310) is operable to provide a visual representation of an area underneath a rotorcraft. The rotorcraft position provider (330) is operable to provide information indicating a position of the rotorcraft. The pilot image generation system (340) is operable to generate a supplemented visual representation. The supplemented visual representation includes the visual representation of the area underneath the aircraft and information indicating a position of the rotorcraft relative to the visual representation. The display device (350) is operable to display the supplemented visual representation within the rotorcraft.