FIELD: rocketry.
SUBSTANCE: invention refers to the mobile anti-aircraft missile systems. Air defense missile system (ADMS) includes the vehicle, on which the two-coordinate rotary device with the azimuth drives and the unit of N anti-aircraft missiles with the homing heads (HH) containing optical-electronic channels, is installed, the aiming head, which is mounted on the anti-aircraft missile unit and contains the opto-electronic channel of the aiming head. ADMS includes the monitor, the control unit, the computing unit, and the image alignment unit. Fields of view of the opto-electronic channels of the HH are designed in order to cover the observed space without omissions, forming the broad field of view in the aggregate. Each HH is made of the opto-electronic channel, the memory device, the control unit for driving the steering planes of the rocket and of the digital correlator. Output of the memory device is connected to the input of the digital correlator. ADMS includes the meteorological unit, the navigation unit, the information exchange unit, the additional computational unit, and the multichannel signal splitter.
EFFECT: technical result of the invention is to ensure the elimination of the effect of the optical interference, which arises at the start of the first missile onto the subsequent launches.
1 cl, 2 dwg
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Authors
Dates
2018-04-19—Published
2017-02-13—Filed