| 基于Matlab的导弹飞行动力学仿真模型库设计 |
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| 引用本文： | 吴媛媛,吴进华,唐静.基于Matlab的导弹飞行动力学仿真模型库设计[J].海军航空工程学院学报,2005,20(2):257-260. |
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| 作者姓名： | 吴媛媛 吴进华 唐静 |
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| 作者单位： | 海军航空工程学院研究生管理大队，海军航空工程学院控制工程系，海军航空工程学院研究生管理大队 烟台，264001 |
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| 摘 要： | 介绍了仿真的技术及导弹飞行力学的相关理论、Matlab软件及其部分工具箱(RTW、 Simulink等)的使用方法,通过Euler角、四元数等方法说明了导弹飞行力学各方程中变量的关系及其意义,结合具体要求设计了基于Matlab的某型导弹飞行动力学仿真模型库。
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| 关 键 词： | 飞行动力学 仿真模型库 Euler角 四元数 |
| 修稿时间： | 2004年9月27日 |
Design of Simulation Model Library Of Missile Flight Dynamics Base on Matlab |
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| WU Yuan-yuan,WUJin-hua,TANG Jing Graduate Students' Brigade of NAEI.Design of Simulation Model Library Of Missile Flight Dynamics Base on Matlab[J].Journal of Naval Aeronautical Engineering Institute,2005,20(2):257-260. |
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| Authors: | WU Yuan-yuan WUJin-hua TANG Jing Graduate Students' Brigade of NAEI |
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| Institution: | WU Yuan-yuan,WUJin-hua,TANG Jing Graduate Students' Brigade of NAEI, Department of Control Engineering,NAEI,Yantai,264001 |
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| Abstract: | The paper introduces the conception and principle of simulation and principle of flight mechanics of missile. Meanwhile, this paper also explains the operation method of Matlab and its toolbox (RTW, Simulink, etc), and introduces the relationship and meanings of the guided missile flight mechanics through the Euler Angles, Quaternion etc. At last the paper designs the model library of missile flight dynamics simulation based on Matlab. |
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| Keywords: | flight mechanics simulation model library Euler angles quaternion |
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