Negative climb after take-off warning system

Details Negative climb after take-off warning system Negative climb after take-off warning system

G - Physics

08

B

340/47

G08B 19/00 (2006.01) G01C 5/00 (2006.01) G01P 1/10 (2006.01)

Patent

CA 1223315

NEGATIVE CLIMB AFTER TAKE-OFF WARNING SYSTEM Abstract of the Disclosure A warning system for aircraft compares the rate of descent of the aircraft with its altitude above ground after take-off, and generates a warning if the aircraft is experiencing an excessive descent condition for the radio altitude at which the air- craft is flying. The position of the landing gear, the speed of the aircraft and the engine power are monitored to enable the system only during the take- off or missed approach phases of operation in order to minimize false warnings during other phases. The relationship between radio altitude and descent rate required to generate a warning is optimized for small, high performance aircraft such as fighter or attack aircraft.

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