FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Aircraft ACS in landing approach comprises landing radio complex including ground glide-path beacon, on-board glide-path beacon and range finder interconnected via radio channel. Besides this system incorporates multiplier, complex control computer and vertical overload transducer, that of pitch angular velocity and angle of attach, steering linkage, integrators, adders and filter connected with aforesaid units. Additionally, this system comprises interconnected filters, adders, six nonlinear units, sensor of pilot interference in aircraft control, bank angle transducer, inverter, two-position switch, three units of signal transmission static factors and aircraft vertical flight speed transducer.
EFFECT: higher efficiency and reliability.
5 dwg
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