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

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.