| 垂直发射防空导弹弹道仿真模型研究 |
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| 引用本文： | 鲁华杰,糜玉林,孙媛,高志华.垂直发射防空导弹弹道仿真模型研究[J].计算机与数字工程,2012,40(11):89-91. |
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| 作者姓名： | 鲁华杰 糜玉林 孙媛 高志华 |
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| 作者单位： | 海军航空工程学院 烟台 264001 |
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| 摘 要： | 弹道仿真是导弹模拟训练系统中的关键部分。为构建准确性较好、实时性较高的弹道仿真模型,在对垂直发射导弹飞行过程进行分析的基础上,将弹道分为垂直段、转弯段、制导段三部分,并根据各部分弹道的特点,分别建立其差分方程描述模型,最后通过仿真验证了模型的准确性和适用性。
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| 关 键 词： | 防空导弹 垂直发射 弹道仿真 模型 |
Research of the Model of Vertical Launching Missile Trajectory |
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| LU Huajie
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MI Yulin
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SUN Yuan
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GAO Zhihua.Research of the Model of Vertical Launching Missile Trajectory[J].Computer and Digital Engineering,2012,40(11):89-91. |
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| Authors: | LU Huajie MI Yulin SUN Yuan GAO Zhihua |
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| Affiliation: | (Naval Aeronautical and Astronautical University,Yantai 264001) |
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| Abstract: | Trajectory simulation is a key part of the missile simulation training system.To build accuracy and good real-time trajectory model,the trajectory was divided into vertical segment,turning segment and guidance segment on the basis of analyzing the process of vertical launch missile,and the difference equations of each part of the trajectory were established.Finally,the accuracy and applicability of the model was verified by simulation. |
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| Keywords: | anti-aircraft missile vertical launching trajectory simulation model |
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