摘要
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．
in this paper,several disturbance factors affecting the range of a solid ballistic missile are discussed and analyzed.And the statistical models of all the random factors are studied. Through the mathematical simulation and statistical analysis of a computer,the maximum range of a solid ballistic missile is evaluted by means of Monte Carlo's method.
出处
《弹道学报》
CSCD
1994年第4期46-50,共5页
Journal of Ballistics
关键词
导弹
弹道
蒙特卡洛法
仿真
missiles trajectory,ballistic missiles,monte carlo's method,trajectory simulation
