摘要
简要分析了高速大俯冲目标的特点以及防空导弹采用传统比例导引拦截此类目标的缺点,提出了对大俯冲机动目标进行实时预测的措施,着重介绍了一种准逆轨拦截的导引方法,并通过仿真实例验证了此方法的有效性。
This paper makes analysis of the characteristics of high speed maneuvering target with large diving angle and the disadvantages of interception of this kind of targets by the missile using traditional proportional guidance.It suggests a real-time prediction measure for this kind of targets and introduces a guidance method of quasi-counter trajectory interception.Simulation tests have also been carried out to verify the effectiveness of this method.
作者
束川良
朱迪
钟永建
孟万里
郝莲英
SHU Chuanliang;ZHU Di;ZHONG Yongjian;MENG Wanli;HAO Lianying(Shanghai Electro-mechanical Engineering Institute,Shanghai 201109,China)
出处
《空天防御》
2019年第1期29-32,共4页
Air & Space Defense
关键词
机动目标
防空导弹
导引律
中制导律
maneuvering target
air defence missile
guidance law
midcourse guidance law
作者简介
束川良(1966— ):男,研究员,研究方向为弹道与制导律设计。
