FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed method allows computing speed ranges and landing approach angles to realise complete stoppage of aircraft, determining upper and lower thresholds of total power acceptable for aircraft and comparing current aircraft power with thresholds to indicate theoretical possibility of aircraft stoppage on landing strip. Proposed device comprises computation facilities receiving data on current parametres and computing the index indicating total power level, comparators to compare said index with threshold that corresponds to correct and excess level of total power.
EFFECT: adequate data on aircraft power for pilot in landing.
10 cl, 3 dwg
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