FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft control means. Proposed device (1) comprises system (8) designed to assist in aircraft guidance in case control means (11A, 11B, 11n) are activated in both initial stage in compliance with the first guidance mode and final stage in compliance with the second guidance mode. Changing between aforesaid two guidance modes is effected automatically by guidance system (8).
EFFECT: simplified landing approach.
13 cl, 3 dwg
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