在此基础上应用蒙特卡罗方法对算例进行仿真计算，并分析了影响弹射筒可靠性的因素。
An example is calculated on the basis of the model by Monte Carlo method. Finally, the influencing factors of reliability for ejection cylinder of solid missile have been analyzed.
最后，采用所提出的方法对两种类型的电源系统进行仿真分析，并与单纯蒙特卡罗方法仿真分析结果进行比较，验证了该方法的可行性和有效性。
The reliability results of two aircraft electrical power systems with the proposed method and the Monte Carlo method are compared, and the result shows the method is feasible and effective.
最后利用蒙特卡罗仿真对所提导航算法进行了验证，并对影响导航精度的各相关因素进行了分析。
Finally, the autonomous optical navigation algorithm is validated and the factors influencing navigation precision is analyzed using Monte Carlo simulations.
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