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通过对影响某固体弹道式导弹射程的各种干扰因素的研究和分析，确定了各随机干扰因素的统计概型，并利用蒙特卡洛方法，进行计算机数字仿真、统计分析，评定出导弹飞行的最大射程．
Through the study and analysis of various interference factors that affect the range of a solid ballistic missile, the statistical models of each random disturbance factor are determined. The Monte Carlo method is used to carry out computer numerical simulation and statistical analysis to evaluate the missile flight Maximum range.