FIELD:
SUBSTANCE: invention relates to the field of flight control and landing of aircraft in the airfield area. The landing radar system contains a landing radar (LR), consisting of a heading channel, a glide path channel and data combination and transmission equipment (DCTE) of the LR, a control radar (CR), consisting of a primary channel, a secondary channel and an DCTE of a control radar, a control module (CM), consisting of a workplace (WP) of the head of the near zone, a WP of the head of the landing zone, an objective control system, two radio communication stations and an DCTE of the control module. The system additionally includes broadcast-type automatic dependent surveillance equipment in the LR, an optical-electronic monitoring module in the LR, data transmission equipment in the CR, an automatic radio direction finder in the CM, and an uninterruptible power supply in the CM.
EFFECT: increasing the reliability of aircraft detection in the near aerodrome zone and the landing zone of the radar landing system (RLS), as well as providing the possibility of transmitting data on the parameters of the position and movement of the aircraft to the command control center (CCC) with various options for the performance of the RLS components.
1 cl, 1 dwg
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Authors
Dates
2022-09-05—Published
2021-12-21—Filed