| 带鸭舵滑翔增程炮弹飞行弹道研究 |
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| 引用本文： | 易文俊,王中原,李岩,周卫平. 带鸭舵滑翔增程炮弹飞行弹道研究[J]. 弹箭与制导学报, 2007, 27(1): 150-153 |
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| 作者姓名： | 易文俊 王中原 李岩 周卫平 |
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| 作者单位： | 1. 南京理工大学弹道国防科技重点实验室,南京,210094
2. 92232部队,北京,100073 |
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| 基金项目： | 弹道国防科技重点实验室基金项目资助. |
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| 摘 要： | 文中针对鸭式布局的滑翔增程炮弹的飞行弹道特性,通过动力学分析,建立了滑翔增程炮弹的各飞行弹道段的弹道模型和控制模型,数值分析给出了滑翔增程弹飞行速度变化规律、最大射程角以及滑翔增程炮弹的滚转控制段与滑翔控制段的弹道特性,研究结果为鸭式布局滑翔增程炮弹的弹道设计提供了理论基础。
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| 关 键 词： | 滑翔增程炮弹 飞行弹道 滚转控制 滑翔控制 |
| 收稿时间： | 2006-05-17 |
| 修稿时间： | 2006-05-172006-07-14 |
Research on Ballistic Trajectory of Glide Extended-range Projectile with Canard Configuration in Flight |
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| YI Wen-jun,WANG Zhong-yuan,LI Yan,ZHOU Wei-ping. Research on Ballistic Trajectory of Glide Extended-range Projectile with Canard Configuration in Flight[J]. Journal of Projectiles Rockets Missiles and Guidance, 2007, 27(1): 150-153 |
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| Authors: | YI Wen-jun WANG Zhong-yuan LI Yan ZHOU Wei-ping |
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| Affiliation: | 1.National Key Laboratory of Trajectory of NUST, Nanjing 210094, China; 2.No. 92232 Unit, Beijing 100073,China |
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| Abstract: | Based on dynamics analysis about ballistic characteristics of a glide extended-range projectile with canard configuration in flight. The paper establishes ballistic trajectory model and control model of the glide extended-range projectile in every flight stage, numerical simulates and analyzes the speed variety law in flight, maxim departure angle, ballistic characteristics in rotation control and slide control about the glide extended-range projectile. The result offers academic basement for ballistic trajectory design of the glide extended-range projectile with canard configuration. |
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| Keywords: | glide extended-range projectile ballistic trajectory in flight rotation control glide control |
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