FIELD: aircraft engineering.
SUBSTANCE: invention relates to a method of preventing ingress of an aircraft into a vortex trail of a vortex generator aircraft. To implement the method, information on configuration, location and orientation of aircraft and vortex generator aircraft, as well as information on environment parameters at current time is received, geometrical characteristics of the hazardous zone of the vortex trace are determined, visual information on the risk of falling into the hazardous zone of the vortex trace in a certain way is presented to the crew.
EFFECT: reduced flying load on pilot, higher safety of flights.
1 cl, 2 dwg
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