| 一种基于空空导弹允许发射包线的导弹平均飞行速度的近似解算 |
| |
| 引用本文： | 陈晓风. 一种基于空空导弹允许发射包线的导弹平均飞行速度的近似解算[J]. 电光与控制, 2009, 16(6) |
| |
| 作者姓名： | 陈晓风 |
| |
| 作者单位： | 火力控制技术国防科技重点实验室,河南,洛阳,471009;中航工业洛阳电光设备研究所,河南,洛阳,471009 |
| |
| 摘 要： | 以空空导弹动力允许发射包线为基础,根据导弹飞行动力学原理,利用导弹发射包线正尾后和正迎头二点的弹道值,给出了一种空空导弹平均飞行速度近似解算的方法.结果表明该方法可行、有效.
|
| 关 键 词： | 空空导弹 导弹平均飞行速度 近似解算 允许发射区 |
An Approximate Approach of Missile Average Velocity Based on Air-to-Air Missile Launch Acceptability Region |
| |
| CHEN Xiaofeng. An Approximate Approach of Missile Average Velocity Based on Air-to-Air Missile Launch Acceptability Region[J]. Electronics Optics & Control, 2009, 16(6) |
| |
| Authors: | CHEN Xiaofeng |
| |
| Affiliation: | 1.Key Laboratory of National Defense Science and Technology on Fire Control Technology;Luoyang471009;China;2.Luoyang Institute of Electro-Optical Equipment;AVIC;China |
| |
| Abstract: | Based on air-to-air missile launch acceptability region and the missile flight dynamics theory,an approximate approach of missile average velocity is offered using the ballistic trajectory values at the right head-on and the right rear.The results show that the approximate approach is effective and feasible. |
| |
| Keywords: | air-to-air missile average velocity of missile approximate approach launch acceptability region |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
