| 摘要 |
FIELD: the invention refers to radiolocation technique and may be used in airborne radars, primarily in pulse-Doppler, installed on aircraft-interceptors attacking air targets. ^ SUBSTANCE: the technical result is in provision of survey of the front hemisphere in a group flight of two interceptors in the flight mode "one after another". The technical result is achieved due to the fact that a controllable attenuator and an attenuator control block is introduced into a known airborne radar having a antenna with drives of displacement of the mirror along the axles of the azimuth and the inclination with sensors shaft-drive code for each axle, an antenna control block, a high-frequency commutator, a transmitting and receiving arrangement, an automatic signal control, Doppler filters, an information processing block, an indicator and a driving generator. ^ EFFECT: provides survey of the front hemisphere. ^ 2 cl, 3 dwg |
