火力与指挥控制
火力與指揮控製
화력여지휘공제
FIRE CONTROL & COMMAND CONTROL
2010年
1期
32-34
,共3页
蔡文新%方洋旺%周晓滨%赵亚锋
蔡文新%方洋旺%週曉濱%趙亞鋒
채문신%방양왕%주효빈%조아봉
反辐射导弹%毁伤能力%有源诱偏%多点源
反輻射導彈%燬傷能力%有源誘偏%多點源
반복사도탄%훼상능력%유원유편%다점원
anti-radiation missile%damage degree%active decoy%multi-points source
基于有源诱偏原理,推导出反辐射导弹在有源诱偏条件下的弹落点计算公式;并由已知的导弹毁伤模型,利用计算机仿真获得对目标雷达或其有源诱饵的毁伤效能.通过仿真结果分析不同的攻击角和末速度对导弹毁伤效能的影响,由此获得反辐射导弹在干扰条件下的最佳攻击角和末速度范围,对于在诱偏条件下研究反辐射导弹毁伤能力的有效性和实用性提供一定的理论和实用参考.
基于有源誘偏原理,推導齣反輻射導彈在有源誘偏條件下的彈落點計算公式;併由已知的導彈燬傷模型,利用計算機倣真穫得對目標雷達或其有源誘餌的燬傷效能.通過倣真結果分析不同的攻擊角和末速度對導彈燬傷效能的影響,由此穫得反輻射導彈在榦擾條件下的最佳攻擊角和末速度範圍,對于在誘偏條件下研究反輻射導彈燬傷能力的有效性和實用性提供一定的理論和實用參攷.
기우유원유편원리,추도출반복사도탄재유원유편조건하적탄낙점계산공식;병유이지적도탄훼상모형,이용계산궤방진획득대목표뢰체혹기유원유이적훼상효능.통과방진결과분석불동적공격각화말속도대도탄훼상효능적영향,유차획득반복사도탄재간우조건하적최가공격각화말속도범위,대우재유편조건하연구반복사도탄훼상능력적유효성화실용성제공일정적이론화실용삼고.
Based on the active decoy theory, the formula of fall points for anti-radiation missile was deduced.By known missile damage model, the damage efficiency of radar or add-baits were gotten by computer simulation.Finally, the simulation result analyses the influence of different attack angle and final speed to the missile damage efficiency, and the best attack angle and final speed rang were gained, which provides the high theory and reference value for the validity and practicability of research on the capacity of anti-radiation missile with condition.
