摘要
为了保证导弹对目标大角度攻击的效果,设计了一种带有过重力补偿项的比例导引制导律。在二维平面内建立弹-目相对运动数学模型,在传统的比例导引律基础上,增加了过重力补偿项并将其作为补偿指令引入制导回路,从而建立了仿真模型,分析了投放条件和过重力补偿系数对制导系统的影响。仿真结果表明,此制导律可实现近似-90°的末端落角,达到期望的性能要求,证明该方法的正确性和有效性。
A kind of proportional navigation guidance law with over-gravity Compensation is designed to ensure impact angle of missile. Two-dimensional motion model for missile and target is established, the over-gravity compensation is introduced to the guidance loop, as an additional command. The model of guidance law with the over-gravity compensation is established. The effect of initial conditions and over-gravity compensation are analyzed. Finally ,the simulation results indicate that this guidance law can get nearly negative ninety degree impact angle and show the validity of the proposed method.
出处
《火力与指挥控制》
CSCD
北大核心
2014年第2期46-48,51,共4页
Fire Control & Command Control
基金
国家航空科学基金资助项目(20110142003)
关键词
比例导引律
过重力补偿
落角
proportional navigation guidance law, over-gravity compensation, impact angle