FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to refueling aircrafts in flight. It is intended to show the pilot current and prognostic information about the future movement of the aircraft relative to the tanker with display of the zone of the minimum and dangerous expected vortex effect, automation of the management of navigating the aircraft into the position for refueling, performing refueling and suppressing the vortex effect on the basis of calculated and measuring information. Further, an effective interactive control method for aircraft navigation is used for aiming at aerial targets.
EFFECT: visual display is provided based on the calculation of prognostic information about the relative movement of the fueling hose funnel of the tanker during air refueling of the aircraft.
1 cl, 1 dwg
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