| 末段修正子弹药风力修正模型研究 |
| |
| 引用本文： | 寇保华,杨涛,张晓今,张青斌.末段修正子弹药风力修正模型研究[J].战术导弹技术,2006(4):16-19. |
| |
| 作者姓名： | 寇保华 杨涛 张晓今 张青斌 |
| |
| 作者单位： | 国防科技大学,长沙410073 |
| |
| 摘 要： | 根据末段修正子弹药的工作原理，提出了克服横向风降低子弹命中精度的风力修正模型，并利用该模型对子弹末修段弹道进行了仿真．仿真结果表明，对末修子弹进行风修能有效提高子弹对跑道的射击精度，是提高末修子母弹射击效能的重要手段。
|
| 关 键 词： | 末段修正子弹药 风力修正 命中精度 |
| 文章编号： | 1009-1300(2006)04-0016-04 |
| 修稿时间： | 2005年8月1日 |
Study of the Model of Wind Correction for Terminal Correction Submunition |
| |
| Kou Baohua,Yang Tao,Zhang Xiaojin,Zhang Qingbin.Study of the Model of Wind Correction for Terminal Correction Submunition[J].Tactical Missile Technology,2006(4):16-19. |
| |
| Authors: | Kou Baohua Yang Tao Zhang Xiaojin Zhang Qingbin |
| |
| Abstract: | According to the flying characters of submunition, the mathematical model of wind correction for terminal correction submunition is provided.This model can improve the hitting precision of submunition to runway in the case of wind.The wind correction model is used to simulate the trajectory in terminal correction phase.The computational results show that it is an important measure to improve the shooting effectiveness of terminal correction submunition,and it is an important reference value and guidance to design submunition system. |
| |
| Keywords: | terminal correction submunition wind correction hitting precision |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
