摘要
中远程舰空导弹的弹道模拟仿真是中远程舰空导弹战术使用研究的基础,以某型中远程垂直发射舰空导弹为研究背景建立垂直发射舰空导弹模拟理论弹道数学模型,并采用M atlab语言对所建立的模拟理论弹道模型进行了三维数据仿真验证,验证结果证明弹道特征基本符合实际弹道形状,符合进一步的战术使用研究要求,并可为舰空导弹作战仿真提供一定的参考。
The trajectory simulation of the intermediate-long range vertical launching surface to air missile is the foundation of the research of tactic employ of the missile. Based on a certain intermediate long range vertical launching missile as research background, the author set up a mathematics model on theory trajectory level, and it is also just a simulation. The author validated the model in a three- dimensional simulation using Matlab language. The result is accord with the actual trajectory, and it can be used in further research in tactics and operation simulation.
出处
《火力与指挥控制》
CSCD
北大核心
2008年第5期156-159,共4页
Fire Control & Command Control
关键词
垂直发射舰空导弹
模拟理论弹道模型
比例导引法
MATLAB
vertical launching surface to air missile, simulation on theory trajectory, proportion guide method ,matlab