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统计出了实际大气状态参数与标准大气状态参数的最大偏差值。以等高程和等过载引信两种弹头引信方式建立了大气参数偏差对弹道式导弹弹头引爆点射程影响的数学模型；从理论上分析了大气参数偏差对弹道式导弹弹头引爆点对应射程产生影响的物理实质；进而以一种洲际弹道导弹为例，计算出了大气参数偏差引起弹头命中点射程偏差的具体数值。
The maximum deviation between the actual atmospheric state parameter and the standard atmospheric state parameter is calculated. The mathematical model of the influence of atmospheric parameter deviation on the range of the detonating point of the ballistic missile was set up by means of two types of warhead fuze such as equal elevation and equal overload fuze. The influence of atmospheric parameter deviation on the corresponding range of ballistic missile detonation point was analyzed theoretically Then, taking an intercontinental ballistic missile as an example, we calculate the specific numerical value of the range deviation of the warhead hit point caused by the atmospheric parameter deviation.