摘要
提出了一种掠飞制导系统设计方法。解决了反坦克导弹在直攻模式下难以有效摧毁坦克的问题。该设计方法是在直接攻击模式制导系统的基础上,通过添加弹目距离计算模块和附加角速率计算模块实现的。该制导系统控制导弹飞行到目标正上方引爆向下开口自锻成型战斗部,垂直攻击坦克的顶装甲。通过模拟试验与仿真分析验证了该制导方法的可行性和数学模型的正确性。
In order to solve the problem of antitank missile unable to damage fatally in direct impact mode, a method of flying over guidance system was brought forth. The range calculus module and the additional angular speed module were added in, based on direct impact mode guidance system. Explosively formed warhead with down open was ignited when the missile controlled by the guidance system was flying over the tank to attack its top armor vertically. The feasibility of the guidance method and the correctness of the math model were validated by the simulation test and analysis.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2009年第6期829-833,共5页
Acta Armamentarii
关键词
飞行器控制、导航技术
捷联电视导引
反坦克导弹
掠飞制导系统
control and navigation technology of aerocraft
TV guidance
antitank missile
flying overguidance system