FIELD: transport.
SUBSTANCE: invention relates to aircraft landing integrated automated control systems and can be used to perform safe landing of plane or helicopter in obscured conditions. Integrated system contains on-board equipment of aircraft and external navigation system. On-board equipment includes processor unit to calculate aircraft navigation fix, electronic ground map generator and multifunction display with functions of two-dimensional and three-dimensional imaging, optoelectronic module of orthostereoscopic imaging. Optoelectronic module of orthostereoscopic imaging contains binocular image processing unit and binocular video camera with spectral sensitivity in near and/or far infrared band. Input of binocular video camera is optically interlinked with zone of take-off runway or pad. Output of binocular video camera is connected with input of binocular image processing unit the output of which is connected to the second input of multifunction display.
EFFECT: higher accuracy of pilot orientation in external vision environment.
5 cl, 4 dwg
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