FIELD: aviation.
SUBSTANCE: aircraft features fuselage with a longitudinal axis, power plant, panels of wing lifting plane with front and rear edges, panels of canard wing lifting plane with front and rear edges, and rudder and stabiliser fins. The aircraft has a capsule attached to the fuselage in front of the front edge of lifting plane panels and rotating along the said fuselage axis. Panels of canard wing lifting plane feature ailerons at the rear edge and are attached to the outer surface of the said capsule at opposite sides.
EFFECT: improved maneuverability of an aircraft without impairment to flight stability.
3 cl, 5 dwg
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