多管火箭炮伺服随动系统设计及仿真

摘要

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.%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.