FIELD: aircraft equipment. SUBSTANCE: device has aircraft position detection system, database, which stores information about runaway, first comparison unit, unit for detection of coordinates of landing point on runaway, units for calculation and output of vectors of real and theoretical inclination angles of aircraft trajectory respectively, and second unit for comparison of said vectors. Second comparison unit outputs calculated vertical and horizontal mismatch values between said vectors and compares produced values to threshold values. EFFECT: prevention of collisions on low altitudes, decreased probability of false triggering. 6 cl, 4 dwg
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Authors
Dates
2000-07-20—Published
1995-03-20—Filed