摘要
大气层内拦截弹采用空气动力与燃气动力的复合控制方式是当今世界防空导弹的发展方向之一。复合控制技术的分析研究是当前急需解决的重要问题。在考虑目标机动加速度大小、目标机动时刻以及目标角闪烁的条件下 ,确定了拦截弹的控制方式由空气动力切换到复合控制时的切换时间。
One of the developing trends of the world air defence missile is that endoatmospheric interceptor uses compound control which is composed of aerodynamic control and gas-thrust-vector control.It is important to analyze and research compound control technology.Taking the target′s maneuvering acceleration,target′s maneuvering time and target′s glint noise into account,the switching time from aerodynamic control to compound control is decided.
出处
《现代防御技术》
2002年第5期30-35,共6页
Modern Defence Technology