| 最优控制与姿控喷流在导弹姿态控制中的应用 |
| |
| 引用本文： | 林枫,刘国刚.最优控制与姿控喷流在导弹姿态控制中的应用[J].航天控制,2004,22(3):20-22. |
| |
| 作者姓名： | 林枫 刘国刚 |
| |
| 作者单位： | 上海机电工程研究所,上海,200233 |
| |
| 摘 要： | 针对稀薄大气层内导弹姿态控制问题 ,提出了一种采用侧向喷流的姿态控制方案 ,并根据最优控制理论设计了控制律。仿真结果表明 ,该方案可以在最短的时间内使导弹的姿态跟踪给定的指令输入 ,并且具有较小的稳态误差
|
| 关 键 词： | 最优控制 BangBang控制 姿控喷流 偏航角 开关线 |
| 文章编号： | 1006-3242(2004)03-20-03 |
| 修稿时间： | 2004年1月15日 |
Application of Optimal Control Using Direct Side Force in Missile Attitude Control System |
| |
| Lin Feng Liu Guogang Shanghai Electro-Mechanical Engineering Institute,Shanghai.Application of Optimal Control Using Direct Side Force in Missile Attitude Control System[J].Aerospace Control,2004,22(3):20-22. |
| |
| Authors: | Lin Feng Liu Guogang Shanghai Electro-Mechanical Engineering Institute Shanghai |
| |
| Institution: | Lin Feng Liu Guogang Shanghai Electro-Mechanical Engineering Institute,Shanghai 200233 |
| |
| Abstract: | In this paper, attitude control system ap pl ying direct side force nozzle is presented as a measure to realize missile attit ude control in attenuate aerosphere, and a control law is designed. Simulation r esult indicates that missile attitude response could track command in the least time, and had small steady state error. < |
| |
| Keywords: | Optimal control Bang-Bang control Direct Side Force Yawing angle Switch cur ve |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
