摘要
提出了研究空射巡航导弹(ALCM)末端机动突防策略的必要性,给出了一种易于工程实现的末端机动突防策略及其有效性评估标准,建立了基于伴随技术的由目标机动引起的拦截导弹脱靶量仿真计算模型,并对脱靶量和 ALCM 的末端突防概率进行了大量的仿真计算,结果表明,该策略对提高 ALCM 的末端突防概率是有效可行的。最后,深入分析了脱靶量随各影响因素的变化规律,研究成果对 ALCM 的作战使用和末端机动突防策略的制定具有重要的理论指导意义。
This paper puts forward the necessity of research on terminal maneuvering penetration tactics of ALCM. Presents a terminal maneuvering penetration tactic easy to realize on engineering and its evaluation standard. establishes the simulation model based on adjoint technique for calculating intercepting-missile's miss distance caused by target's maneuvering,also it makes a great deal of simulations for miss distance of intercepting-missile and penetration probability of ALCM.The results prove that this tactic is effective and feasible for improving terminal penetration probability.Finally,it makes adeep study on the miss distance trendline for each impacting factors,and this research has an important directive meaning in theory for using ALCM in combat and making decisions on terminal maneuvering penetration tactics.
出处
《弹箭与制导学报》
CSCD
北大核心
2004年第S3期145-149,共5页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
空射巡航导弹
机动突防
伴随系统
仿真
air-launched cruise missile(ALCM)
maneuvering penetration
adjoint system
simulation