FIELD: transport.
SUBSTANCE: radar incorporates gyro-stabilised antenna system, control unit, signal generation and processing unit, and inertial micro navigation measuring unit. Gyro-stabilised antenna system comprises active phase-aerial consisting of subarrays, distributor, antenna system control unit and radiation direction switchboard. Control, signal generation and processing unit comprise radar controller and exciter-receiver. The latter incorporates intermediate frequency module and superhigh-frequency radiation module, and signal processor. Said signal processor comprises equaliser, preprocessing module, radar image generator module and secondary power supply. Antenna system control unit allows scanning by azimuth and elevation angle and beam stabilising in changes of aircraft attitude.
EFFECT: expanded operating performances.
1 dwg
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