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| 导弹改进、改型中的飞行力学问题 | |
| 引用本文： | 关世义,马洪忠,宋福志. 导弹改进、改型中的飞行力学问题[J]. 战术导弹技术, 2005, 0(3): 1-4 |
| 作者姓名： | 关世义 马洪忠 宋福志 |
| 作者单位： | 中国航天科工集团公司第三研究院,北京100074 |
| 摘 要： | 讨论了导弹飞行性能与作战效能的关系; 介绍了国内外导弹改装、改进、改型中可能遇到的10个方面的飞行力学问题, 即发射动力学问题, 弹道问题, 增加射程(增程)问题, 末端攻击问题, 子弹头抛撒问题, 航迹规划问题, 改变飞行高度(变高)问题, 改变飞行速度(变速)问题, 改变导弹外形(变形)问题, 协同作战问题, 并进行了简短的讨论. |
| 关 键 词： | 导弹 飞行力学 飞行性能 作战效能 改进 |
| 文章编号： | 1009-1300(2005)03-0001-04 |
| 修稿时间： | 2005-02-27 |
Some Problems of Flight Mechanics in the Improvements of Guided Missile |
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| Guan Shiyi,Ma Hongzhong,Song Fuzhi. Some Problems of Flight Mechanics in the Improvements of Guided Missile[J]. Tactical Missile Technology, 2005, 0(3): 1-4 | |
| Authors: | Guan Shiyi Ma Hongzhong Song Fuzhi |
| Abstract: | The relationship between the flight performances and fire effectiveness of guided missile is discussed; ten problems of flight mechanics likely faced in the improvements of guided missile, namely launching dynamics, trajectory, enlarged range, end-games, sub-munition spreading, path planning, altitude-variation, speed-variation, shape-variation(morphing) and cooperative engagement, are introduced and briefly discussed. |
| Keywords: | guided missile flight mechanics flight performance fire effectiveness improvement |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |