COMPLEX SYSTEM FOR CONTROLLING AIRCRAFT TRAJECTORY DURING APPROACH LANDING

摘要

FIELD: physics; control.;SUBSTANCE: invention relates to a complex system for controlling aircraft trajectory during approach landing. The system comprises an inertial navigation system, an air signal system, a landing signal indicator, a complex information processing unit, a satellite navigation system, a memory unit, a landing strip parameter determining unit, a virtual heading-glide beacon location unit, a unit for determining the direction and range of the virtual heading-glide beacon, first and second adders and a unit for determining the elevation angle of the virtual heading-glide beacon.;EFFECT: high reliability and safety of landing aircraft.;7 dwg