FIELD: air transport.
SUBSTANCE: invention relates to a method for controlling an aircraft for the implementation of automatic parachute landing of heavy loads. To implement the method in flight in steady mode, the landing target is found, an anti-gravity maneuver is performed, the cargo is moved off and the aircraft is then transferred to the steady flight mode, while the control is carried out automatically in a certain way using data on the mismatch between the set and current flight parameters from sensors of barometric altitude, trajectory angle, vertical speed and angular velocity, as well as data on changes in the mass and balancing of the aircraft after moving the cargo off.
EFFECT: efficiency, quality and safety of heavy cargo landing are improved.
1 cl, 10 dwg
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