Helicopter warning system

G - Physics – 01 – C

Patent

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Details

343/15, 343/78

G01C 5/00 (2006.01) G01S 13/08 (2006.01)

Patent

CA 1072195

Abstract of the Disclosure To prevent inadvertent ground contact of the tail of a helicopter during a landing operation without providing a continuous warning signal for normal landings the altitude and attitude signals are scaled such that when they are equal and opposite in voltage and phase compared to a ground contact curve the comparator will energize a relay for actuating a pilot warning signal. A rate of descent signal biases the altitude signal upward varying in proportion to rate of descent as to enable the pilot to have sufficient warning time to take corrective action. -1-

239974

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