Warning system for tactical rotary wing aircraft

G - Physics – 08 – G

Patent

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343/15

G08G 5/02 (2006.01) B64D 45/04 (2006.01) G01C 5/00 (2006.01)

Patent

CA 1240771

WARNING SYSTEM FOR TACTICAL ROTARY WING AIRCRAFT Abstract of the Disclosure A warning system for rotary wing aircraft that monitors the altitude above ground of the aircraft and issues a warning when there is insufficient terrain clearance. The warning criteria are optimized for rotary wing aircraft and are altered as a function of landing gear position and airspeed. Two distinct warnings are given. One indicates insufficient terrain clearance and the other warns the pilot if he attempts to land with the landing gear up. Logic circuitry is provided to modify the criteria necessary to gener- ate a warning, and to inhibit certain warnings, as required by the mode of operation of the aircraft.

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