FIELD: transport.
SUBSTANCE: proposed method comprises forming decent trajectory by setting aircraft final speed vector at preset point of the Earth surface. Note here that ETA is determined with the help of onboard computer. ETA deviation from computed value is determined. Determined deviation is used to correct required direction of aircraft final speed at preset point of the Earth surface from minimising ETA deviation.
EFFECT: control over aircraft landing at preset location in conditions of disturbing factors.
2 dwg
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