| 航空发动机非理想解耦自适应控制 |
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| 引用本文： | 樊丁,梁春燕.航空发动机非理想解耦自适应控制[J].航空动力学报,2000,15(3):328-330. |
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| 作者姓名： | 樊丁 梁春燕 |
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| 作者单位： | 1. 西北工业大学709教研室,陕西,西安,710072
2. 上海交通大学自动化研究所,上海,20030 |
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| 摘 要： | 本文对航空发动机的双变量控制方法进行了研究,提出了一种非理想解耦自适应控制方法,各子系统之间部分残余的相互耦合和非线性影响就通过自适应律本身的鲁棒性来解决.仿真结果表明该控制系统实现了解耦控制,对发动机模型参数在大范围内的变化均有良好的控制效果.
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| 关 键 词： | 航空发动机 解耦 自适应控制 |
| 收稿时间： | 1999/8/16 0:00:00 |
| 修稿时间： | 1999-08-16 |
Incompletely Decoupled Adaptive Control in Aeroengine System |
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| Fan Ding and Liang Chunyan.Incompletely Decoupled Adaptive Control in Aeroengine System[J].Journal of Aerospace Power,2000,15(3):328-330. |
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| Authors: | Fan Ding and Liang Chunyan |
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| Institution: | 7th Dept.Northwest Polytechnic University,Xi'an 710072,China;Shanghai Jiaotong University,Shanghai 200030,China |
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| Abstract: | An incompletely decoupled model reference adaptive control method is proposed for aeroengine binary control system.A new adaptive control method is applied to every incompletely decoupled subsystem,then remains of coupling and nonlinear influence can be resolved by adaptive principle robustness.This binary decoupled adaptive controller can diminish the coupling gradually and has excellent robustness to model uncertainty and external disturbances.Simulation results demonstrate the effectiveness of the incompletely decoupled adaptive controller. |
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| Keywords: | aeroengine coupling adaptive control |
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