| 制导炸弹发射区研究 |
| |
| 引用本文： | 陈芳,何矞,南英,黄国强.制导炸弹发射区研究[J].飞行力学,2008,26(6). |
| |
| 作者姓名： | 陈芳 何矞 南英 黄国强 |
| |
| 作者单位： | 1. 南昌航空大学,自动化学院,江西,南昌,330063
2. 南昌航空大学,航空与机械工程学院,江西,南昌,330063 |
| |
| 摘 要： | 基于小型制导炸弹(炸弹+制导)气动特性、动力学方程、制导律、目标运动模型及发射区计算等飞行数值仿真模型与算法,在炸弹发射状态一定的情况下,通过不同的炸弹轨迹倾角、偏航角和目标运动的组合,仿真计算了大量的发射区.利用仿真软件C++与Matlab,能够较为直观地比较目标在运动状态不同情况下制导炸弹的发射区和6-DOF飞行轨迹.所得结论可为制导炸弹精确打击目标提供依据,提高了制导炸弹的作战性能.
|
| 关 键 词： | 制导炸弹 发射区 6-DOF 飞行轨迹 |
Study into Launch Zone of the Guided Bomb |
| |
| CHEN Fang,HE Yu,NAN Ying,HUANG Guo-qiang.Study into Launch Zone of the Guided Bomb[J].Flight Dynamics,2008,26(6). |
| |
| Authors: | CHEN Fang HE Yu NAN Ying HUANG Guo-qiang |
| |
| Institution: | 1.College of Automation;Nanchang University of Aeronautics;Nanchang 330063;China;2.College of Aeronautics and Mechanical Engineering;China |
| |
| Abstract: | According to differential dynamic equations and guidance law,6-DOF flight trajectory and launch zone of the air-surface guided bomb,and target track,flight simulation models of a minor guided no-power bomb are calculated largely and compared with by simulation software such as C++ and Matlab considering different conditions of target movement under certain launching conditions.The paper provides a set of methods for an air-surface guided bomb to exactly get targets,and improves its tactical performance. |
| |
| Keywords: | guided bomb launch zone 6-DOF flight trajectory |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
