摘要
在末制导雷达搜索方式已知的条件下,建立了空舰导弹射前目标指示精度模型。引入误差分析的思想,综合考虑自控终点散布误差引起的末制导雷达有效搜索区域的变化,修正了目标指示精度模型。采用解析算法,在不同末制导雷达搜索扇面角、不同开机距离的情况下,对超音速反舰导弹射前最低目标指示精度模型进行了仿真,验证了目标指示精度模型的正确性,搞清了影响目标指示精度的各种因素,为反舰导弹目标指示方式的选择提供了有益的参考。
The target indication precision model of the air-to-surface missile is built up on condition that the terminal guidance radar search model is given.The idea of error analysis is introduced.Through considering the change of the terminal guidance radar effective search region caused by the auto-control termination error,the target indication precision model is modified.The target indication precision model of the super-sonic speed anti-ship missile is simulated at working different distance and different searching angle of the terminal guidance radar by means of an analytic algorithm.The simulation results show that the model is correct.The influence factor of the requirement of the target indication precision is analyzed.The study is helpful in choosing of the target indication method.
出处
《舰船电子工程》
2011年第4期53-56,共4页
Ship Electronic Engineering
基金
航空科学基金项目(编号:20085584010)资助
关键词
空舰导弹
目标指示
末制导雷达
搜索扇面角
air-to-surface missile
target indication
terminal guidance radar
searching sector angle
