摘要
根据弹道导弹末制导子导弹用于封锁机场跑道的总体方案,探讨了子导弹经抛撒、导引飞行后,形成沿跑道方向均匀散布的控制制导律,建立了数学模型,并经全弹道仿真,计算出了子导弹沿跑道散布的结果。
According to the overall systerr, alternative, a guidance law for the terminal guided submissiles of strategic missiles is presented. The system mathematical model is established. Finally, dispersion of the submissiles along the runway is given through digital simulation.
出处
《战术导弹技术》
1998年第2期25-31,8,共8页
Tactical Missile Technology
关键词
弹道导弹
末制导子导弹
机场跑道
制导律
Strategic missile Terminal guided submissiles Runway Guidance law
