FIELD: transport.
SUBSTANCE: invention relates to aircraft instrumentation and permits to perform automatic search for runway and provide automatic control of aircraft landing irrespective to meteorological conditions and time of day. The said technical result is achieved using laser system of aircraft landing automatic control which consists of two hemispheric laser emission sensors having integrated lasers and radio transceivers, and four cylindric laser emission sensors containing integrated radio transceivers, and radio transceiver, spheric laser emission sensor and laser emitter. Two hemispheric laser emission sensors are installed along longitudinal line at the beginning and at the end, and four cylindric laser emission sensors are installed at the beginning and at the end of runway. Aircraft has radio transceiver, spheric laser emission sensor and laser emitter installed on it.
EFFECT: higher accuracy of landing and flight safety.
3 cl, 5 dwg
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