| 线性插值方法在某型航空发动机模型控制器设计中的应用 |
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| 引用本文： | 强文辉,孟庆明,郑铁军. 线性插值方法在某型航空发动机模型控制器设计中的应用[J]. 航空发动机, 2005, 31(4): 43-45 |
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| 作者姓名： | 强文辉 孟庆明 郑铁军 |
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| 作者单位： | 北京航空航天大学,北京,100083 |
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| 摘 要： | 采用线性插值算法,根据已知点的精确模型求取包线内任1点的发动机模型；应用Z-N整定经验公式,对插值点进行了PID控制器设计；使用simulink进行了建模仿真。仿真结果表明,所设计的控制器控制效果良好。
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| 关 键 词： | 线性插值 航空发动机 建模 仿真 |
| 修稿时间： | 2004-11-15 |
Application of Linear Interpolation Method in Aeroengine Model Controller Design |
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| Qiang Wenhui,Meng Qingming,Zheng Tiejun. Application of Linear Interpolation Method in Aeroengine Model Controller Design[J]. Aeroengine, 2005, 31(4): 43-45 |
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| Authors: | Qiang Wenhui Meng Qingming Zheng Tiejun |
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| Abstract: | A method of establishing aeroengine model in the envelope by linear interpolation algorithm with the known precision models is presented. PID controllers for interpolation points are designed by Z - N setting empirical formula. Moreover, the controller modeling is simulated with Simulink. Simulation result shows that the obtained controller is excellent. |
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| Keywords: | linear interpolation aeroengine modeling simulation |
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