摘要
探索了先进中距复合制导空空导弹末制导截获概率模型,分析了影响末制导角截获概率的因素。从要求的目标角截获概率出发,研究了先进中距空空导弹在采用惯性中制导、不加指令修正情况下的最大发射后不管攻击距离。给出了蒙特卡罗法仿真结果。
The acquisition probabilities model of the medium range air-to-air missiles is investigated. Factors winch affect the angle acquisition probabilities of the terminal guidance are analyzed. The medium range air-to-air missiles' maximum launch range based on the angle acquisition probabilities without radio instructions in inertial guidance is studied. The results of simulation with the method of Monte Carlo are given.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第2期11-13,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
