摘要
针对舰载导弹发射时的环境条件,对导弹自控飞行终点散布的影响进行了分析,通过对载舰及导弹在轨上的运动、大气温度及常值风等环境条件的研究,得到它们对导弹自控飞行终点散布影响的一般规律。对舰载导弹发射时,导弹随载舰一起运动的各种情况对导弹自控飞行终点散布的影响建立了数学模型,并对仿真结果进行了定量分析,为提高导弹的命中精度提供了依据。
The automata end-point distribution of a shipborne missile under different circumstances is andyzed. On the basis of the research on warship movement, movement of missile flying on the track, ambient temperature, wind speed and direction, the principle of the automata end-point distribution of missile is established and the model based on the principle is given. Finally the simulation data is analyzed quantitatively and the results indicate that it is helpful to improve the impact accuracy of missile.
出处
《系统工程与电子技术》
EI
CSCD
北大核心
2006年第5期750-752,共3页
Systems Engineering and Electronics
关键词
环境因素
自控飞行
终点散布
surrounding
automata flying
end-point distribution
