| 引用本文: | 贾沛然,汤国建.提高再入点精度的末助推级制导方法.[J].国防科技大学学报,1989,11(1):66-72.[点击复制] |
| Jia Peiran,Tang Guojian.A Guidance Method of the Last Booster to Improve the Precision at the Reentry Point[J].Journal of National University of Defense Technology,1989,11(1):66-72[点击复制] |
|
| |
|
|
| 本文已被：浏览 5292次 下载 5096次 |
| 提高再入点精度的末助推级制导方法 |
| 贾沛然, 汤国建 |
|
(自动控制系)
|
| 摘要: |
| 本文将需要速度运用于导弹末助推级以提高导弹的再入点精度，为再入机动及末制导提供较好的初始条件。文中还考虑到为调整推力方向进行姿态控制的工程可实现性。 |
| 关键词: 弹道,制导，姿态控制 |
| DOI： |
| 投稿日期：1988-04-02 |
| 基金项目: |
|
| A Guidance Method of the Last Booster to Improve the Precision at the Reentry Point |
| Jia Peiran, Tang Guojian |
|
(Department of Automatic Control)
|
| Abstract: |
| This paper applies required velocity to the missi1e's last booster to improve its precision at the reentry point，and to provide the better initial conditions for the reentry maneuver and the terminal guidance. The engineering realizability of attitude control to adjust thrust direction is a1so taken into account in it. |
| Keywords: trajectory,guidance,attitude control |
|
|
|
|
|
