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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。
Atmospheric interceptors using aerodynamic and gas dynamic composite control is one of the development directions of the world’s anti-aircraft missiles. Analysis of complex control technology is an urgent problem to be solved. Under the condition of the target maneuvering acceleration, the target maneuvering moment and the flickering of the target angle, the switching time of intercepting bomb control mode from aerodynamics to compound control is determined.