| 新型飞机除冰车加热系统温度控制器研究 |
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| 引用本文： | 王玉松,黄静静,孙毅刚.新型飞机除冰车加热系统温度控制器研究[J].中国民航学院学报,2006,24(3):16-19. |
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| 作者姓名： | 王玉松 黄静静 孙毅刚 |
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| 作者单位： | 中国民用航空学院研究生部,天津300300 |
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| 基金项目： | 中国民用航空总局科研项目 |
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| 摘 要： | 以新型飞机除冰车加热系统为研究对象，通过分析实验数据，首次提出了除冰液流量全量程范围内的加热系统数学模型，并综合应用模糊理论设计Fuzzy自整定PID参数的Smith预估控制器。MATLAB仿真结果表明，应用这种方法设计出的控制策略能较好地适应飞机除冰车模型参数的大幅度变化，并具有良好的稳态精度和自适应能力。
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| 关 键 词： | 模糊PID 参数自整定 Smith预估 飞机除冰车 温度控制 |
| 文章编号： | 1001-5000(2006)03-0016-04 |
| 收稿时间： | 2005-12-30 |
| 修稿时间： | 2006-05-25 |
Research on Temperature Control of New Type Aircraft Deicing Vehicle Heating System |
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| WANG Yu-song,HUANG Jing-jing,SUN Yi-gang.Research on Temperature Control of New Type Aircraft Deicing Vehicle Heating System[J].Journal of Civil Aviation University of China,2006,24(3):16-19. |
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| Authors: | WANG Yu-song HUANG Jing-jing SUN Yi-gang |
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| Institution: | Graduate School, CA UC, Tianjin 300300, China |
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| Abstract: | This paper presents our research on the heating system in a new aircraft deicing vehicle, Through analyzing the data of experiments, a new idea of building a full range-flow mathematical model of heating system is put forward for the first time. By making comprehensive use of fuzzy theory,a fuzzy self-tuning PID Smith controller is also designed, The result of simulation on computer with MATLAB shows that the control strategy designed this way can better adapt the large range of changing in the aircraft deicing vehicle model and has good stability precision and self-adaptive property. |
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| Keywords: | fuzzy PID parameter self-tuning Smith predict aircraft deicing vehicle temperature control |
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