| 导弹发射条件对初段飞行性能的影响分析 |
| |
| 引用本文： | 薛翠利,关成启,查旭,王长青.导弹发射条件对初段飞行性能的影响分析[J].战术导弹技术,2006(2):9-13. |
| |
| 作者姓名： | 薛翠利 关成启 查旭 王长青 |
| |
| 作者单位： | 中国航天科工集团公司第三研究院,北京 100074 |
| |
| 摘 要： | 以导弹箱式发射方式为例,推导出了四段运动方程式,求出了对应于不同情况下导弹运动参数的变化规律，研究了导弹从助推器点火到导弹加速到给定飞行速度这一过程的飞行特性，分析了导弹出箱初始条件的变化和对导弹飞行性能的影响。仿真结果表明，该理论模型和发射条件对初段飞行性能影响的分析是合理的。
|
| 关 键 词： | 发射条件 飞行性能 影响分析 |
| 文章编号： | 1009-1300(2006)02-0009-05 |
| 修稿时间： | 2005年9月29日 |
Analysis of Initial Flight Performance Based on Launching Condition |
| |
| Xue Cuili,Guan Chengqi,Zha Xu,Wang Changqing.Analysis of Initial Flight Performance Based on Launching Condition[J].Tactical Missile Technology,2006(2):9-13. |
| |
| Authors: | Xue Cuili Guan Chengqi Zha Xu Wang Changqing |
| |
| Abstract: | Coffin-type launching missile systems are studied.The dynamics of launching systems is established in four stages.Moving parameters of missile under various launching condition are obtained.Flight characteristic from booster ignition to definite velocity is researched.The varieties of initial parameters and the influence of initial parameters on flight performance are analyzed.Through calculation simulation,the validity of analysis on initial flight performance under launching condition and the theoretical discussions are verified by the results. |
| |
| Keywords: | launching condition flight performance influence analysis |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
