Configuration responsive descent rate warning system for...

G - Physics – 01 – C

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343/15, 354/18

G01C 21/00 (2006.01) G01C 5/00 (2006.01) G05D 1/08 (2006.01)

Patent

CA 1243405

CONFIGURATION RESPONSIVE DESCENT Warning system that monitor the altitude above ground and descent rate of an aircraft and generate a warning if the descent rate of the aircraft is excessive for the altitude in which the aircraft is flying are well suited to aircraft whose flight and operational characteristics are readily predictable but not as suitable for aircraft, such as tactical aircraft whose operating conditions are not so predict- able. To overcome this problem, the criteria for providing the warnings are altered (30, 32) as a func- tion of flight configuration (16, 18) to optimize the warning for different flight conditions.

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