摘要
对亚声速飞航导弹指定入射倾角的两种导引方法进行了研究,提出了实现工程化的思路.通过数学仿真,对两种方法进行了验证和比较,分析了它们各自的优缺点.
Two kinds of prescribed impact angle guidance for subsonic aerodynamic missile are studied.Engineering method is presented.Two kinds of guidance are validated and compared by mathematical simulation.Finally,their merit and disadvantage are analyzed respectively.
出处
《战术导弹技术》
北大核心
2008年第3期48-52,共5页
Tactical Missile Technology
关键词
入射角
俯仰角
弹道倾角
impact angle
pitch angle
flight path angle
