文章摘要
黄成,于鹏,赵锡旺.基于Matlab Simulink的弹道仿真方法[J].,2015,30(2):169-173
基于Matlab Simulink的弹道仿真方法
Trajectory Simulation Method Based on Matlab Simulink
  
DOI:10.7682/j.issn.1673-1522.2015.02.016
中文关键词: 弹道仿真  数学模型  仿真方法
英文关键词: trajectory simulation  mathematical model  simulation method
基金项目:
作者单位
黄成 91550部队,辽宁大连 116023 
于鹏 海军装备部,北京 100083 
赵锡旺 92270部队,山东威海 264309 
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中文摘要:
      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。
英文摘要:
      The trajectory simulation software can help to analyze and evaluate the flight experimental results of the wingedmissile weapon system. The trajectory simulation method was designed based on Matlab Simulink, the mathematical modelof missile trajectory with six degrees of freedom was established, and the software was programmed and tested using theaerodynamic data and control parameters of the missile. The simulation results is proved the model's accuracy and reliabil.ity.
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