| 垂直热发射舰空导弹初始弹道仿真研究 |
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| 引用本文： | 房勇,孙胜春,刘方. 垂直热发射舰空导弹初始弹道仿真研究[J]. 舰船电子工程, 2010, 30(11): 110-113 |
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| 作者姓名： | 房勇 孙胜春 刘方 |
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| 作者单位： | 海军工程大学兵器工程系,武汉430033 |
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| 摘 要： | 在对垂直热发射舰空导弹弹道进行分析的基础上,将导弹初始弹道分为垂直上升飞行段和程序转弯段,并运用四元数法建立初始弹道的数学模型。利用MATLAB软件对初始弹道数学模型进行仿真,以检验模型的正确性,分析热发射导弹初始弹道的特点。
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| 关 键 词： | 垂直发射 MATLAB建模 EMC 四元数 |
Research on Trajectory Simulation of Thermal Vertical Launching Ship-to-air Missile |
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| Fang Yong,Sun Shengchun,Liu Fang. Research on Trajectory Simulation of Thermal Vertical Launching Ship-to-air Missile[J]. Ship Electronic Engineering, 2010, 30(11): 110-113 |
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| Authors: | Fang Yong Sun Shengchun Liu Fang |
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| Affiliation: | Fang Yong Sun Shengchun Liu Fang(Dept.of Weaponry Engineering,Naval University of Engineering,Wuhan 430033) |
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| Abstract: | Based on the characteristics of trajectory of thermal vertical launching ship-to-air missile,the incipient trajectory is devided into perpendicular ascension flight phase and procedure turn phase,also make use of error quaternion methodses establishment the incipient trajectory mathematics model.Taking use of MATLAB language to carry out the incipient trajectory mathematics model simulation test and program performance,so as to verify the correctness of the trajectory simulation model,analyze the characteristics of the incipient trajectory. |
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| Keywords: | vertical launching MATLAB EMC quaternion |
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