基于Matlab Simulink的弹道仿真方法

Trajectory Simulation Method Based on Matlab Simulink

弹道仿真软件有助于飞航导弹武器飞行试验结果的分析与评定。为此,设计了基于Matlab Simulink的弹道仿真计算方法,建立了六自由度空间弹道数学模型,利用导弹相关的气动数据和控制参数测试了算法,实现了软件,仿真结果证明了该模型的准确性和可信度。

The trajectory simulation software can help to analyze and evaluate the flight experimental results of the winged missile weapon system. The trajectory simulation method was designed based on Matlab Simulink, the mathematical model of missile trajectory with six degrees of freedom was established, and the software was programmed and tested using the aerodynamic data and control parameters of the missile. The simulation results is proved the model＇s accuracy and reliabil-ity.