指挥控制与仿真
指揮控製與倣真
지휘공제여방진
Command Control & Simulation
2015年
5期
19-23
,共5页
舰载无人机%舰载预警直升机%反辐射导弹%诱偏
艦載無人機%艦載預警直升機%反輻射導彈%誘偏
함재무인궤%함재예경직승궤%반복사도탄%유편
shipborne UAV%shipborne early-warning helicopter%ARM%tricking
针对反辐射导弹对预警直升机的威胁，给出了舰载无人机携带辐射源诱偏反辐射导弹的基本原理；从反辐射导弹的空间分辨条件和几何运动分析出发，建立了无人机携带辐射源和预警直升机共同组成的两点源诱偏反辐射导弹的数学模型和预警直升机与无人机的最佳间距模型。通过仿真计算，分析了各种因素对诱偏效果的影响。
針對反輻射導彈對預警直升機的威脅，給齣瞭艦載無人機攜帶輻射源誘偏反輻射導彈的基本原理；從反輻射導彈的空間分辨條件和幾何運動分析齣髮，建立瞭無人機攜帶輻射源和預警直升機共同組成的兩點源誘偏反輻射導彈的數學模型和預警直升機與無人機的最佳間距模型。通過倣真計算，分析瞭各種因素對誘偏效果的影響。
침대반복사도탄대예경직승궤적위협，급출료함재무인궤휴대복사원유편반복사도탄적기본원리；종반복사도탄적공간분변조건화궤하운동분석출발，건립료무인궤휴대복사원화예경직승궤공동조성적량점원유편반복사도탄적수학모형화예경직승궤여무인궤적최가간거모형。통과방진계산，분석료각충인소대유편효과적영향。
Aimming at the threat of ARM toward shipborne early?warning helicopter, the principle of shipborne UAV carrying radiation source to trick ARM is proposed. Based on spatial resolution condition and the geometry movement analysis of ARM, the mathematic model of two radiation sources decoy system consisted of UAV carrying radiation source and early?warning helicopter to trick ARM and the best space model between early?warning helicopter and UAV are deduced. Through simulating calculation, various factors influencing on the tricking effect is analyzed.
