FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft control systems. Proposed method relates to control over aircraft (1) with airfoil spinning at high rpm. Said aircraft comprises fuselage (2) at least one rotor (3), at least one pull variable pitch propeller (4) and at least two half-wings (11, 11′) located on both sides of fuselage (2). Besides, it includes, at least one horizontal tail (20) provided with moving surface (21, 21′) and at least one power plant (2) to drive said rotor (3) and every pull propeller (4). Proposed method comprises determination of total lift of aircraft, adjustment of lift of every half-wing (11, 11') by acting at the drive of flaps (12) so that said lift equal the first preset percentage of total lift. Note here that difference in lift between half-wings (11, 11′) allows to compensate for rotor (3) influence on said half-wings.
EFFECT: automatic stabilisation of hybrid copper position.
18 cl, 6 dwg
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