Excessive pitch attitude warning system for rotary wing...

Details Excessive pitch attitude warning system for rotary wing... Excessive pitch attitude warning system for rotary wing...

G - Physics

08

B

340/47

G08B 19/00 (2006.01) G01C 5/00 (2006.01)

Patent

CA 1242255

EXCESSIVE PITCH ATTITUDE WARNING SYSTEM FOR ROTARY WING AIRCRAFT Abstract of the Disclosure A system for warning the pilot of a rotary wing aircraft such as a helicopter of a flight condi- tion that, if left uncorrected, would result in the tail of the aircraft striking the ground monitors the alti- tude above ground, descent rate, pitch and pitch rate of the aircraft and provides a warning if the relation- ship between the aforementioned parameters is such that a tail strike is imminent.

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