AIRCRAFT AUTOMATIC LANDING CONTROL SYSTEM Russian patent published in 1995 - IPC

FIELD: control systems of flying vehicles. SUBSTANCE: aircraft automatic landing control system has radio altimeter, localizer receiver, glide-path channel mechanically linked with respective control actuators, as well as speed setting device and auto-throttle computer connected in series; output of auto-throttle computer is connected with servo actuator of auto-throttle; besides that, control system includes inertial navigation system, satellite navigation system, integral unit, airfield information receiver, unit for determination of landing regime, relative coordinate generating unit, program unit of longitudinal motion, units for indirect measurement of disturbance of lateral banking motion and longitudinal motion, setters of coefficients of lateral motion, banking and longitudinal motion, units of adaptation of lateral motion, banking and longitudinal motion; generators of adaptive program of lateral motion, banking and longitudinal motion; first, second, third, fourth, fifth, sixth and seventh adders, lateral motion control unit and heading control unit connected in series, banking control unit, altitude control unit and pitch control unit connected in series. EFFECT: enhanced efficiency. 1 dwg