多管火箭炮伺服随动系统设计及仿真  

Design and Simulation of Servo System for Multiple Rocket Launchers

作　　者：周超[1] 张龙[1] 

机构地区：[1]南京理工大学机械工程学院,江苏南京210094

出　　处：《机械制造与自动化》2012年第3期91-92,96,共3页Machine Building & Automation

摘　　要：以某多管火箭炮伺服随动系统为背景,建立了系统的数学模型。为满足系统高速高精度的位置控制,设计了复合模糊PID控制器。仿真结果表明该方法可以有效地提高火箭炮的自适应能力和鲁棒性,保证了目标跟踪精度。This paper takes the servo sysytem fo multi-barrel rocket launchers as the background and builds its mathematical model. To meet the high-speed and high-precision position control of this system, it also designs the composite fuzzy PID controller. The simulation results show that the method is used to effectively improve the rocket＇ s adaptive ability and robustness and ensure the accuracy of target tracking.

关 键 词：多管火箭炮 模糊PID 仿真 

分 类 号：TH12[机械工程—机械设计及理论] TP391.9[自动化与计算机技术—计算机应用技术]