METHOD FOR AUTOMATIC CONTROL OF AIRCRAFT AT LANDING AND SYSTEM THEREFOR Russian patent published in 2016 - IPC G08G5/00 B64C19/00 

FIELD: aviation.

SUBSTANCE: for aircraft landing signals radio altitude, vertical speed, a control signal to elevator and to control engine thrust, addition of corrective signals compensation of influence of wind on elevator and thrust control drive. Correcting signal to elevator is based on measurement of absolute difference and registered speed. Correcting signal to drive thrust regulator is based on measurement of difference of current and rated power of the aircraft, determined based on track and registered speed. System for aircraft landing comprises measurement system of flight parameters, device for generating control signals to elevator and drive engine thrust, respectively. Flight parameters measurement system comprises a radar altimeter, vertical speed transducer, vertical overload sensor, sensor of absolute speed, registered speed sensor. Device for generating control signals to elevator comprises a unit for generating complex exponential signal, two adders, programmer, differentiator, two height correction unit, two non-linear converter. Control signal generating device contains speed setting panel, an adder, non-linear converter, draught stabilisation unit, unit calculating preset energy aircraft computation unit current aircraft power comparator.

EFFECT: providing required accuracy of landing.

2 cl, 1 dwg