摘要
NCADE导弹是美国雷锡恩公司研制的空射反导导弹,为了准确地获得NCADE导弹的弹道特性,根据NCADE导弹的特点,建立了导弹数学模型并设计了合理的制导控制算法,对其作战弹道进行了数字仿真研究。仿真结果表明,NCADE导弹能够以直接碰撞的方式命中目标的关键是采用了轨控方式的直接力控制系统,采用该系统是对高速弹道导弹实现动能拦截的必要手段。
The NCADE is an airborne antimissile missile developed by Raytheon company in the US. In order to obtain the exact trajectory character of NCADE, a mathematical model is established and a reasonable guidance and control algorism is designed based on the charac- ter of the missile, the digital simulation of the NCADE missile is carried out subsequently. Simulation result shows that the key factor of NCADE missile ＇ s ability to hit the target directly is achieved by its adoption of an orbit control mode reaction-jet control system which is essential to accomplish kinetic energy interception against high speed ballistic missiles.
出处
《弹箭与制导学报》
CSCD
北大核心
2013年第6期6-8,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
中航工业集团创新基金(2012C01428)资助
