指挥控制与仿真
指揮控製與倣真
지휘공제여방진
COMMAND CONTROL & SIMULATION
2015年
4期
21-24,35
,共5页
舰载无人机%预警直升机%雷达干扰%航迹模型
艦載無人機%預警直升機%雷達榦擾%航跡模型
함재무인궤%예경직승궤%뢰체간우%항적모형
shipborne UAV%shipborne early-warning helicopter%radar interfere%model of flight path
针对敌机对舰载预警直升机的威胁，给出了无人机携带雷达干扰载荷干扰敌机载雷达掩护预警直升机的基本原理；从敌机对舰载预警直升机攻击过程的几何运动出发，通过微分方程，建立了干扰情况下敌机攻击预警直升机的飞行航迹模型；通过仿真计算，分析了无人机携带雷达干扰载荷干扰敌机载雷达掩护预警直升机可行性，并给出了无人机掩护预警直升机的基本方法。
針對敵機對艦載預警直升機的威脅，給齣瞭無人機攜帶雷達榦擾載荷榦擾敵機載雷達掩護預警直升機的基本原理；從敵機對艦載預警直升機攻擊過程的幾何運動齣髮，通過微分方程，建立瞭榦擾情況下敵機攻擊預警直升機的飛行航跡模型；通過倣真計算，分析瞭無人機攜帶雷達榦擾載荷榦擾敵機載雷達掩護預警直升機可行性，併給齣瞭無人機掩護預警直升機的基本方法。
침대활궤대함재예경직승궤적위협，급출료무인궤휴대뢰체간우재하간우활궤재뢰체엄호예경직승궤적기본원리；종활궤대함재예경직승궤공격과정적궤하운동출발，통과미분방정，건립료간우정황하활궤공격예경직승궤적비행항적모형；통과방진계산，분석료무인궤휴대뢰체간우재하간우활궤재뢰체엄호예경직승궤가행성，병급출료무인궤엄호예경직승궤적기본방법。
Aimming at the threat of enemy fighter plane against shipborne early?warning helicopter, the principle of UAV carrying radar interference load to interfere radar of enemy aircraft to cover early?warning helicopter is proposed. Based on the geometry movement of enemy aircraft attacking process toward shipborne early?warning helicopter, through differential equa?tion, the flight path model of enemy aircraft attacking early?warning helicopter is established. Through simulation calculation, the possibility and combat effectiveness of UAV carrying radar interference load to interfere radar of enemy aircraft to cover early?warning helicopter is analyzed and the method of UAV covering early?warning helicopter is given.
