FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to multipropeller VTOL aircraft. Multicopter with two-tier arrangement of propeller-driven groups comprises a fuselage, a landing gear, a power supply system, propeller-driven groups with controllers, a flight controller, system of sensors for monitoring and control of flight, avionics and parachute. Propeller-driven groups are located in two parallel planes, horizontal during vertical take-off, located above and below fuselage and forming upper and lower tiers. In each tier there are at least three propeller-driven groups arranged at vertices of flat polygons, said geometrical centers lie on one vertical axis, note here that aircraft center of gravity is located between tiers.
EFFECT: optimum ratio of multicopter stability and maneuverability.
1 cl, 12 dwg
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