Shipborne Early Warning Aircraft Array Configuration Based on Velocity Constraint of Anti-ship Missile
The characteristic parameters of typical anti-ship missiles are analyzed briefly in view of the problem of array con-figuration of ship-borne early warning and detection aircraft for various types of anti-ship missiles.The factors affecting the array configuration of shipborne early warning aircraft and the whole process of shipborne early warning and detection of anti-ship mis-siles are clarified.The calculation model of array position configuration of ship-borne early warning and detection anti-ship missile is established from the forward distance of ship-borne early warning and detection aircraft,the threat angle of incoming missile and the maximum detection radius of ship-borne early warning and detection aircraft.The effects of radar reflection cross-sectional area(RCS)and the velocity of incoming anti-ship missile on the forward departure distance of shipborne early warning aircraft are simu-lated and analyzed.The results show that the forward departure range of shipborne early warning aircraft against different types of in-coming anti-ship missiles increases as the radar reflection cross-sectional area(RCS)of incoming missiles increases,and the for-ward departure range decreases as the speed of incoming missiles increases.
shipborne early warning aircraftearly warning detectionarray configurationmodeling and simulation
国家科技期刊平台
NSTL
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