| 飞机拦阻系统电液比例控制研究 |
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| 引用本文： | 宋锦春,王艳,张志伟,张福波.飞机拦阻系统电液比例控制研究[J].航空学报,2005,26(4):520-523. |
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| 作者姓名： | 宋锦春 王艳 张志伟 张福波 |
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| 作者单位： | 1. 东北大学 机械工程与自动化学院, 辽宁 沈阳 110004;2. 东北大学 轧制技术及连轧自动化国家重点实验室, 辽宁 沈阳 110004 |
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| 摘 要： | 在分析某纯机液飞机拦阻系统不足的基础上,设计了一种新型电液比例控制的飞机拦阻系统,提高了飞机拦阻系统对不同机型、拦停距离及撞网状况的适应能力。推导出系统的输出压力-飞机拦停位移曲线,在此基础上设计了极点配置自校正PID控制器。仿真研究表明,该飞机拦阻系统过渡时间仅为0.05s,响应速度较快,取得了满意的控制效果。
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| 关 键 词： | 飞机拦阻 电液比例控制 自校正PID控制 极点配置 |
| 文章编号： | 1000-6893(2005)04-0520-04 |
| 收稿时间： | 2004-04-29 |
| 修稿时间： | 2004年4月29日 |
Study on the Electro-Hydraulic Proportional Controlled Aircraft Arresting System |
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| SONG Jin-chun,WANG Yan,ZHANG Zhi-wei,ZHANG Fu-bo.Study on the Electro-Hydraulic Proportional Controlled Aircraft Arresting System[J].Acta Aeronautica et Astronautica Sinica,2005,26(4):520-523. |
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| Authors: | SONG Jin-chun WANG Yan ZHANG Zhi-wei ZHANG Fu-bo |
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| Institution: | 1. Institute of Mechanical Engineering and Automation, Northeastern University, Shenyang 110004, China;2. The State Key Laboratory of Rolling and Automation, Northeastern University, Shenyang 110004, China |
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| Abstract: | On the basis of analyzing certain aircraft arresting system which is a pure mechanical and hydraulic system, an new type electro-hydraulic proportional controlled aircraft arresting system is designed. And the pressure-displacement curve is also deduced. This paper designs the pole configuration self-tuning PID controller. Simulation results indicate that the PID controller designed is able to satisfy the need of the aircraft arresting system, the dynamic and static characteristics of the system can be improved to a certain extent. |
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| Keywords: | aircraft arrestment electro-hydraulic proportional control self-tuning PID control pole configuration |
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