| 防空多管火箭炮交流位置伺服系统的控制策略 |
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| 引用本文： | 朱玉川,马大为,李志刚,许寿彭. 防空多管火箭炮交流位置伺服系统的控制策略[J]. 兵工自动化, 2006, 25(4): 5-6,10 |
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| 作者姓名： | 朱玉川 马大为 李志刚 许寿彭 |
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| 作者单位： | 南京理工大学,机械工程学院,江苏,南京,210094;南京理工大学,机械工程学院,江苏,南京,210094;防空兵指挥学院,河南,郑州,450052 |
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| 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.
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| 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 |
| 文章编号： | 1006-1576（2006）04-0005-02 |
| 收稿时间： | 2005-09-26 |
| 修稿时间： | 2005-09-262005-11-25 |
Control Strategy of Alternating Current Position Servo System for Air Defense Multiple Launch Rockets |
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| ZHU Yu-chuan,MA Da-wei,LI Zhi-gang,XU Shou-peng. Control Strategy of Alternating Current Position Servo System for Air Defense Multiple Launch Rockets[J]. Ordnance Industry Automation, 2006, 25(4): 5-6,10 |
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| Authors: | ZHU Yu-chuan MA Da-wei LI Zhi-gang XU Shou-peng |
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| Abstract: | 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. |
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| Keywords: | Multiple launch rockets Permanent magnetism synchronous servomotor Slipform variable structure control Fuzzy control Single neuron control |
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