| 基于特征点分段的导弹姿态全程滑态变结构控制研究 |
| |
| 引用本文： | 张云鹏,缪栋,刘云峰.基于特征点分段的导弹姿态全程滑态变结构控制研究[J].战术导弹技术,2005(2):48-51. |
| |
| 作者姓名： | 张云鹏 缪栋 刘云峰 |
| |
| 作者单位： | 西安第二炮兵工程学院,西安710025 |
| |
| 摘 要： | 将工程中常用的"分段定常"方法与全程滑态变结构控制理论相结合, 提出了独特的时变全程滑态变结构控制方法, 并结合导弹姿态控制系统特点, 提出了导弹姿态调节器设计方法和导弹姿态调节器控制算法, 为实际应用提供了一定的理论基础与依据.
|
| 关 键 词： | 全程滑态变结构控制 姿态控制系统 分段定常 姿态调节器 时变性 |
| 文章编号： | 1009-1300(2005)02-0048-04 |
| 修稿时间： | 2004年12月8日 |
Study on Global Variable Structure Control of Missile Attitude Based on Characteristic Points Subsection |
| |
| Zhang Yunpeng,Miao Dong,Liu Yunfeng.Study on Global Variable Structure Control of Missile Attitude Based on Characteristic Points Subsection[J].Tactical Missile Technology,2005(2):48-51. |
| |
| Authors: | Zhang Yunpeng Miao Dong Liu Yunfeng |
| |
| Abstract: | The usual means of subsection constant in engineering and the global variable structure control theory are combined,and a unique time-variant global variable structure control method is put forward. Considering the character of missile attitude control system, a design method and a control algorithm of missile attitude adjuster are proposed,and theoretical basis for actual application is provided. |
| |
| Keywords: | global variable structure control attitude control system subsection constant attitude adjuster time variation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
