本文结合无人飞行器和飞航导弹的实践,扼要地介绍了均匀设计法在计算飞行力学研究中的应用,其中特别讨论了导弹的发射动力学、碰地概率和击水概率,以及导弹的数字统计打靶等在型号研制中具有重要意义的计算飞行力学课题。 Combining the practice of unmanned aerial vehicle and missile, this paper briefly introduces the application of uniform design method in the research of computational flight mechanics. In particular, it discusses the missile launch dynamics, the probability of collision and the probability of impact, as well as the missile’s digital statistics Shooting and other models in the development of the significance of computational flight mechanics issues.