| 打击复杂地形目标的导弹再入机动弹道设计 |
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| 引用本文： | 陈永军,张毅.打击复杂地形目标的导弹再入机动弹道设计[J].飞行力学,2004,22(3):53-56. |
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| 作者姓名： | 陈永军 张毅 |
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| 作者单位： | 第二炮兵工程学院,603教研室,陕西,西安,710025 |
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| 摘 要： | 建立了再入机动弹道数学模型，给出了气动力系数为速度、迎角、高度的函数拟合式，进行了最佳再入机动弹道设计和仿真计算。结果表明，数学模型正确，计算方法可行，利用再入机动弹道技术可有效地打击复杂地形目标、提高导弹的作战效能和突防能力。
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| 关 键 词： | 战术弹道导弹 再入机动 弹道设计 |
| 文章编号： | 1002-0853(2004)03-0053-04 |
| 修稿时间： | 2003年7月13日 |
Reentry Maneuvering Trajectory Design of TBM on Attacking Natural Defence Target |
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| CHEN Yong-jun,ZHANG Yi.Reentry Maneuvering Trajectory Design of TBM on Attacking Natural Defence Target[J].Flight Dynamics,2004,22(3):53-56. |
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| Authors: | CHEN Yong-jun ZHANG Yi |
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| Abstract: | The mathematical model of reentry maneuvering trajectory is established. The fitting expression of aerodynamic coefficient function on velocity, attack of angle and altitude is presented. The results show that the mathematical model is correct, the method of calculation is feasible. The natural defence target can be effectively attacked, the attacking efficiency and penetrating capability of TBM can be improved by utilization of the reentry maneuvering trajectory technic. |
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| Keywords: | tactical ballistic missile(TBM) reentry maneuver trajectory design |
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