摘要
以某中远距空空导弹为背景,提出了高抛弹道的设计思路以增加有效射程,根据不同制导段飞行性能指标要求研究分析了相应的制导参数,提出了高抛弹道复合导引律。建立了导弹和目标的弹道模型,仿真分析了高抛弹道的特点,并在不同距离条件下与平直弹道情况相比,仿真表明高抛弹道对中远距离目标具有良好的攻击效果。
The parabolic trajectory is proposed for a medium long range air to air missile to increase the effective range. The guidance parameters are analyzed according to the different requirements of each guidance phase. The combined guidance law for the parabolic trajectory is proposed. The ballistic model is built to analyze the characteristics of the parabolic trajectory. Compared to the flat trajectory, the para- bolic trajectory has better attack capacity for medium/long range target
出处
《现代防御技术》
北大核心
2014年第1期46-50,共5页
Modern Defence Technology
关键词
空空导弹
高抛弹道
复合制导
air to air missile
parabolic trajectory
combined guidance
