| 导弹舵机自适应离散滑膜控制器设计 |
| |
| 引用本文： | 谷文圆,吴玉斌,荣竹. 导弹舵机自适应离散滑膜控制器设计[J]. 沈阳理工大学学报, 2011, 0(5): 54-57 |
| |
| 作者姓名： | 谷文圆 吴玉斌 荣竹 |
| |
| 作者单位： | 沈阳理工大学装备工程学院; |
| |
| 摘 要： | 针对所建立的导弹电动舵机的简化模型,设计了自适应离散滑膜变结构控制器,并对系统进行仿真,仿真及实验结果表明:该系统有良好的动态品质、稳定性和鲁棒性.
|
| 关 键 词： | 导弹 电动舵机 自适应 离散滑膜 变结构控制 |
Missile Actuator Controller Based on Adaptive Discrete Sliding Mode |
| |
| GU Wenyuan,WU Yubin,RONG Zhu. Missile Actuator Controller Based on Adaptive Discrete Sliding Mode[J]. Transactions of Shenyang Ligong University, 2011, 0(5): 54-57 |
| |
| Authors: | GU Wenyuan WU Yubin RONG Zhu |
| |
| Affiliation: | GU Wenyuan,WU Yubin,RONG Zhu(Shenyang Ligong University,Shenyang 110159,China) |
| |
| Abstract: | According to the established missile electric steering gear,the simplified model of adaptive discrete variable structure controller is designed,and in the system simulation experimental results show that the system has a good dynamic quality,stability and robustness. |
| |
| Keywords: | missile electromechanical actuator adaptive discrete sliding mode variable structure control |
| 本文献已被 CNKI 维普 等数据库收录！ |
|
