FIELD: flying vehicle optical landing systems. SUBSTANCE: system contains indicator unit of flying vehicle landing trajectory mounted on stabilized platform together with flying vehicle attitude sensors. Indicator unit contains two-degree-of-freedom gyroscope and collimating sight optically connected with landing trajectory indicator unit. Optical unit consists of reflectors, light sources, controllable light filter, collimating lens with transparencies mounted in its focal distance, coordinate converters with electromechanical servo drives connected with three attitude sensors of gyroscope and attitude sensors of mechanical unit of sight base. Amplifier of electric drive of movable coordinate system of sight is connected with attitude sensor of movable base of landing trajectory indicator unit made on base of light concentrating forms of light-return coats. Device is used for surface check pneumatic assembly of electric jet engine plant. EFFECT: enhanced efficiency. 3 cl, 8 dwg
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