先进近距格斗空空导弹实现越肩发射设计分析  

The Design and Analysis on Over The Shoulder Advanced Short-range Air-to-air Missile

作　　者：李舜[1] 李佩佩[2] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009 [2]河南科技大学电子信息工程学院,河南洛阳471003

出　　处：《弹箭与制导学报》2012年第6期37-40,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：研究格斗型空空导弹实现前向越肩发射的导弹设计问题。导弹具备快速转弯飞行能力是实现越肩弹道的基础。针对前向越肩发射方式技术特点,文中从飞行平台要求、推力曲线设计、启控时间优化以及转弯控制方式等方面进行分析,通过数学建模与仿真,提出了简单实用的转弯控制方法,得到了实现越肩弹道飞行能力导弹的需用过载和转弯角速率等关键总体指标。研究结果对先进格斗导弹系统设计具有参考价值。The overall design of forward-firing over the shoulder short-range air-to-air missile was discussed.In order to accomplish the over the shoulder launch,the missle flight capability of quickly turning must be designed elaborately.On the basis of the features of forward-firing over the shoulder,some significant aspects of missle overall design were proposed and analyzed,including the design of aircraft platform,the optimization of rocket engine thrust curve,the choice of flight control moment,the control method of turning and so on.By performing typical digital simulations based on the model of missile,the effective control approach of improving the turning back capability of the missile was given,and the essential overall design parameter was estimated,including the rational turn angular rate and the required overload.The results are helpful in the overall design for advanced short-range air-to-air missiles.

关 键 词：格斗导弹 越肩发射 离轴发射 推力曲线 过载 

分 类 号：TJ760.13[兵器科学与技术—武器系统与运用工程] TJ762.23