FIELD: dynamically supported hovering craft. SUBSTANCE: wing-in-ground effect craft includes fuselage, wing, tail unit straightway tunnel open at bow which is formed by wing or by its center section nix and provided with controllable flap fitted at aft extremity of tunnel; it is provided with tunnel bottom profile corrector made in form of front and rear controllable doors articulated together. They are articulated respectively with fore and aft parts of tunnel bottom. Doors of profile corrector may be retracted flush with tunnel bottom and may be differentially extended into flow forming break of aerodynamic profile whose top is located under CG of wing-in-ground effect craft. Method of longitudinal control of wing-in-ground effect craft consists in differentiated throttling of air flow passing through under-wing tunnel both at its outlet and in area of wing-in-ground effect craft CG. EFFECT: enhanced reliability. 3 cl, 6 dwg
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