摘要
从系统动力学出发,基于制导与控制原理,建立了防空导弹拦截末端机动的TBM微分对策模型,并根据极大极小原理,得到了微分对策的最优策略,确定了防空导弹的测向推力矢的最佳方向。
According to the theory of systemic dynamics,based on the principle of control and guide,the differential games model of air-defence missile intercepting TBM is built.And based upon maxi-mini theory,the optimal strategies is concluded,and the optimal orientation of side jet force vector is confirmed.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第S8期715-716,723,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
863计划课题(2004AA780101-1)
关键词
微分对策
战术弹道导弹
极大极小原理
侧向推力矢
differential games
tactical ballistic trajectory missile
maxima and minium theory
side jet force vector
