FIELD: aircraft engineering.
SUBSTANCE: invention relates to a method of aircraft control during land approach at the leveling stage. To implement the method, measurements by a height radio altimeter are made, a predetermined pitch angle value is generated, which is stored at the minimum guaranteed altitude of the radio altimeter operation, stabilization of the stored value of the pitch angle is ensured until the moment of touching the runway.
EFFECT: quality and reliability of the aircraft control system during approach at the leveling stage are improved.
1 cl, 2 dwg
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