飞行器迎面拦截导引仿真  

Simulation of Head-on Intercepting Guidance and Control Law for Aerocraft

作　　者：陈淼[1] 刘晓光[1] 

机构地区：[1]信息系统工程重点实验室,南京210007

出　　处：《舰船电子工程》2015年第7期120-123,共4页Ship Electronic Engineering

摘　　要：以航母编队防空作战推演为背景,基于仿真方法对其中的航空器迎面拦截问题进行了分析研究。针对目标运动态势,限于非军事因素,要求任务单元能够在目标正前方威慑距离外与目标面对面对峙,从而达到威慑拦截效果,旨在迫使对方后退,最大限度避免火力接触,这一点与导弹击毁式拦截不同。迎面拦截分为两个部分,首先在与目标同方向运动过程中,向目标对称靠近,然后再沿圆弧路径飞行更改航向,达到与目标面对面对峙。论文设计了拦截算法,并通过仿真验证了算法的有效性。With the problem of anti-aircraft campaign operation for aircraft carrier formation,the problem of head-on interception against aerocraft is studied in this paper.According to the dynamic statement and trend of the target,and considering many nonmilitary factors,the mission unit is required to head-on intercept the target out of overawed interval space,which can achieve the purpose of overawed interception.This method aims at making the opposed target fall back self,avoiding firepower,which is different from the attacking interception by guided missile.To realized this method,the mission unit lay aboard to the target firstly,and then adjust the orientation self by circular guidance,that can confront each other against the target.The interception method is designed in this paper,and finally the effectiveness of the proposed method is testified by simulation.

关 键 词：威慑 迎面拦截 圆弧导引 

分 类 号：TP391[自动化与计算机技术—计算机应用技术]