FIELD: aircraft engineering.
SUBSTANCE: laser semi-automatic landing control system consists of two hemispherical laser radiation transducers with built-in lasers and radio transceivers, four cylindrical laser radiation transducers including built-in radio transceivers, radio transceiver, spherical laser radiation transducer and laser radiator. Two hemispherical laser radiation transducers are arranged along runway at its start and end. Four cylindrical laser radiation transducers are arranged at sides and at the end of runway. Aircraft is equipped with radio transceiver, spherical laser radiation transducer and laser beam radiator. The latter consists of two electromechanical converters with mirror fitted at the ends of the latter, laser controller, and paraboloid of revolution with mirror surface. The latter accommodates vide camera arranged between its focus and vertex while vertex base is rigidly connected with telescopic prop of two-axis table.
EFFECT: higher safety of landing.
11 dwg
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