| 导弹机动飞行的弹道参数估算 |
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| 引用本文： | 邓龙洲,李太玉.导弹机动飞行的弹道参数估算[J].上海航天,2006,23(6):27-32. |
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| 作者姓名： | 邓龙洲 李太玉 |
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| 作者单位： | 国防科学技术大学,航天与材料工程学院,湖南,长沙,410073 |
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| 摘 要： | 为简化计算,根据导弹的质心运动方程,通过近似处理导出了导弹机动飞行中助推段、跨越段和机动段弹道参数的估算公式。仿真计算表明,该估算公式的计算结果与理论公式的偏差较小,且方法简便,可用于导弹机动飞行的弹道设计。
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| 关 键 词： | 弹道导弹 机动飞行 弹道参数 助推段 跨越段 机动段 |
| 文章编号： | 1006-1630（2006）06-0027-06 |
| 收稿时间： | 2005-11-17 |
| 修稿时间： | 2006-03-22 |
The Trajectory Parameter Estimate of Maneuvering Ballistic Missile |
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| DENG Long-zhou,LI Tai-yu.The Trajectory Parameter Estimate of Maneuvering Ballistic Missile[J].Aerospace Shanghai,2006,23(6):27-32. |
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| Authors: | DENG Long-zhou LI Tai-yu |
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| Affiliation: | College of Aerospace and Material Engineering, NUDT, Changsha Hunan 410073, China |
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| Abstract: | To simplify the computation,the estimate equations of trajectory parameter of boost phase,crossover phase and maneuvering phase in ballistic missile's flying were brought out by approximate treatment according to the motion equation of mass center for missile in this paper.The simulation showed that the computation result of the estimate equation was similar with the one of theoretical equation.The calculation was simple,which would be applied to the trajectory design for jump ballistic missile. |
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| Keywords: | Ballistic missile Maneuvering flying Trajectory parameter Boost phase Crossover phase Maneuvering phase |
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