FIELD: transport.
SUBSTANCE: aircraft landing procedure exploiting standard homing radar and navigation systems, landing laser automatic control system including two hemispherical, spherical laser radiation transducers, four cylindrical laser radiation transducers, laser system controller, laser radiator including laser and two electromechanical converters integrated in two-axis module of high-power laser drive. Stator of electromechanical converters is secured in lengthwise axis perpendicular to aircraft airframe. Laser radiation transducers comprises controller with multiple input, radio transceiver, radio transceiver controller, laser controller, LEDs arranged on transducer surface with discrete spacing in bearing and location angles.
EFFECT: safe landing in extreme weather, reliable homing.
6 dwg
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