防空多管火箭炮交流位置伺服系统的控制策略  

Control Strategy of Alternating Current Position Servo System for Air Defense Multiple Launch Rockets

作　　者：朱玉川[1] 马大为[1] 李志刚[1] 许寿彭[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：《兵工自动化》2006年第4期5-6,10,共3页Ordnance Industry Automation

摘　　要：采用永磁同步伺服电动机,构成多管火箭炮交流位置伺服系统。以交流永磁同步伺服电动机为执行元件,系统速度环和位置环控制采用数字控制,位置反馈取自负载端形成全闭环控制。该系统控制策略包括:模型参考自适应、滑模变结构、模糊控制、单神经元等控制。The permanent magnetism synchronous servomotor was adopted to construct the AC position servo system of multiple launch rockets. The AC permanent magnetism synchronous servomotor was used as executive component; the digital control was adopted by system speed circle and position circle control; the position feedback was gathered from self-load end to realize the whole closed loop control. The control strategies of system include： model reference self-adaptive control, slipform variable structure control, fuzzy control, single neuron control and so on.

关 键 词：多管火箭炮 永磁同步伺服电动机 滑模变结构控制 模糊控制 单神经元控制 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]