根据冲量原理和小偏差理论给出了后效冲量误差引起导弹命中误差的一种计算方法和模型，提出了一种用关机分离方程控制射程的方法。
On the basis of impulse fundamentals and short offset theory, a calculation method and its model of missile hit error generated by after-working impulse are given.
提出了一种基于空中发射点的在线诸元计算方法，该方法具有计算量小、制导方法误差小的特点，可用于陆基机动弹道导弹或潜射弹道导弹的快速发射。
The method has minor computer load and small guidance method error; therefore it can be used in rapid launching of land-based maneuver ballistic missiles or.
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