|
|||||
|
|
| 一种适用于小推力轨控发动机“二次变轨”机动突防方案 | |
| 引用本文： | 李红霞,李新其,强洪夫,黄海平.一种适用于小推力轨控发动机“二次变轨”机动突防方案[J].固体火箭技术,2011,34(5):537-542. |
| 作者姓名： | 李红霞 李新其 强洪夫 黄海平 |
| 作者单位： | 1. 第二炮兵工程学院,西安,710025 2. 第二炮兵工程学院,西安710025;96301部队,怀化418008 3. 96301部队,怀化,418008 |
| 摘 要： | 针对突防发动机轨控推力较小,难以产生在拦截器末制导段内成功突防所需的机动过载的实际情况,提出避开拦截器机动性能最强的末制导段,而选择在拦截器自由飞行段和末制导结束后实施“二次机动变轨”的突防方案,旨在解决弹道中段机动突防方案的有效性问题.建立了推力方向、推力持续时间等轨控发动机主要控制参数的优化规划模型,提供了基于遗传... |
| 关 键 词： | 弹道中段 二次变轨 突防规划 遗传算法 |
A scheme of secondary orbit varying maneuver penetration applied to small thrust orbit controlling motor |
|
| LI Hong-xia,LI Xin-qi,QIANG Hong-fu,HUANG Hai-ping.A scheme of secondary orbit varying maneuver penetration applied to small thrust orbit controlling motor[J].Journal of Solid Rocket Technology,2011,34(5):537-542. | |
| Authors: | LI Hong-xia LI Xin-qi QIANG Hong-fu HUANG Hai-ping |
| Institution: | LI Hong-xia1,LI Xin-qi1,2,QIANG Hong-fu1,HUANG Hai-ping2(1.The Second Artillery Engineering Institute,Xi'an 710025,China,2.Armaments Department,Troops No.96301,Huaihua 418008,China) |
| Abstract: | Aiming at the fact that the trajectory-control thrust of penetration motor is too small to bring the required maneuvering overload of successful penetration in the terminal guidance phase,the penetration program of secondary maneuver change trajectory was proposed in the freedom sliding phase and the ending guidance phase,instead of the terminal guidance phase of the most strong maneuver ability,for solving the validity of the midcourse maneuver penetration program.The optimal program model was buit,includi... |
| Keywords: | midcourse of trajectory secondary orbit varying penetration program inherited algorithm |
| 本文献已被 CNKI 万方数据 等数据库收录！ | |