FIELD: weapons and ammunition.
SUBSTANCE: invention can be used in anti-aircraft missile systems (AAMS) for defense of military and industrial objects against low-altitude aircraft, helicopters and other smaller air attach means in the rage of 30 km. Proposed system comprises command station with rotary platform, missiles for volley launch and target detection radar. Said radar is connected to computing station with its one input connected with missile direction-finding channels, while its output is connected with synchronisation and encoding unit. Command station elevating-rotary platform accommodates radar station with phase aerial. Every volley-launch missile is furnished with radio receiver, radio responder and control signal decoder. Said command station additionally comprises missile range univalent determination unit and control signal switching unit.
EFFECT: higher efficiency of guidance system in radar mode.
2 dwg
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