Monte Carlo ballistic Simulation Applied to Dispersion Analysis of Starting Control Points for Antitank Missile
This paper provides an overview of the Antitank Missile Monte Carlo starting control points dispersion analysis conducted with the ballistic simulation. First,The disturbances that affect the flight of a missile are analyzed. Then a method of how to handle with the disturbances is presented to establish a ballistic simulation model with Monte carlo method, the steps of simulating the disturbances based on Matlab are also given. Taken account of the initial angular rates disturbance, rocket engine thrust misalignment, wind disturbance, the equation that described the dynamics of the missile mass center movement should be adjusted accordingly. In this paper, a common model is established to simulate the effect of disturbances. Results indicate that missile trajectory disturbances could be substantially reduced by lowering rocket engine thrust misalignment
antitank missile starting control points ballistic simulation Monte-Carlo method Dispersion
Yang Liu Kun Li Xiaodong Song Xiaoxian Yao
School of Aerospace Science Beijing Institute of Technology Beijing, China
国际会议
哈尔滨
英文
2829-2832
2011-08-12（万方平台首次上网日期，不代表论文的发表时间）