火力与指挥控制Issue(9):139-141,3.
火箭炮位置伺服系统的鲁棒性多内模控制
Robust Multiple Internal Model Control of Rocket Launcher Position Servo System
摘要
Abstract
In order to realize high precision position tracking control in rocket launcher position servo system,through the introduction of compensation module,a robust multiple internal model controller is designed in the paper,it is a controller which suitable for parameter variation. The theory analysis and simulation results show that the proposed method has the advantages of simple design, convenient parameter adjustment,the system can also have good target tracking performance, disturbance rejection and robustness.关键词
火箭炮/伺服系统/内模控制/参数时变/参数调整/鲁棒性Key words
rocket launcher/servo system/internal model control/parameter variation/parameter tuning/robustness分类
信息技术与安全科学引用本文复制引用
陈高华,贾彦斌,李荧兴..火箭炮位置伺服系统的鲁棒性多内模控制[J].火力与指挥控制,2014,(9):139-141,3.基金项目
山西省青年科技研究基金资助项目 ()