Method and apparatus for determining aircraft-to-ground distance

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

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342 33, G06F 1900, G08G 502

Patent

active

060120010

ABSTRACT:
A method and apparatus are described for the determination of the height above a landing surface and the rate of descent to the landing surface for a fixed wing or rotary wing aircraft when the aircraft is less than about 100 feet above the landing surface. The invention relies on the time-of-flight measurement of preferably short infrared pulses that are transmitted from the sensing device and reflected back to the sensing device from the landing surface. Multiple sensors can be used for redundancy. For each sensing unit the distance is determined by a conversion of the time-of-flight information into a distance reading. The rate of descent is determined from successive distance determinations. An additional algorithm determines if the rate of descent is excessive for the distance above the landing surface and generates an alarm such as an audible or visual signal.

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