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论文:2015,Vol:33,Issue(5):775-780 |
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引用本文： |
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许行之, 高亚奎, 章卫国, 王峰, 许奇武. 二元机翼非线性气动弹性自适应控制[J]. 西北工业大学学报 |
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Xu Xingzhi, Gao Yakui, Zhang Weiguo, Wang Feng, Xu Qiwu. Adaptive Control of Nonlinear Aeroelastic Response of a Two-Dimensional Airfoil[J]. Northwestern polytechnical university |
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| 二元机翼非线性气动弹性自适应控制 |
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| 许行之1, 高亚奎1, 章卫国1, 王峰1, 许奇武2 |
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1. 西北工业大学 自动化学院, 陕西 西安 710072;
2. 北京万源工业有限公司, 北京 100176 |
| 摘要: |
| 研究了带有前后缘控制面的二元机翼气动弹性颤振主动控制问题。采用多项式非线性模型建立气动弹性动态方程,然后考虑俯仰方向阻尼和刚度存在参数不确定性的情况下,利用Lyapunov稳定性理论设计了具有全局稳定的反馈线性化自适应和结构化模型参考自适应(SMRAC)控制律。仿真结果显示,在控制面偏转存在限制时,所设计的控制律可以有效地实现颤振的抑制,考虑阻尼不确定性对于颤振抑制具有减小收敛时间的作用,但对于系统响应特性占据主导作用的是刚度不确定性。 |
| 关键词:
自适应控制系统
非线性气动弹性
二元机翼
参数不确定性
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| Adaptive Control of Nonlinear Aeroelastic Response of a Two-Dimensional Airfoil |
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| Xu Xingzhi1, Gao Yakui1, Zhang Weiguo1, Wang Feng1, Xu Qiwu2 |
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1. Department of Automatic Control, Northwestern Polytechnic University, Xi'an 710072, China;
2. Beijing Wanyuan Industrial Co., Ltd, Beijing 100176, China |
| Abstract: |
| The question of active flutter control of an aeroelastic airfoil with leading- and trailing-edge control surfaces is investigated. The dynamical equations of a two-dimensional airfoil with polynomial nonlinearity in pitch are established. Then suppose that there are parametric uncertainties in both pitch stiffness and damping; Lyapunov function is used to design an adaptive control law of feedback linearization and a structured model reference adaptive control law. The simulation results and their analysis show preliminarily that: (1) the nonlinear controllers are effective for flutter suppression even if the control surface deflection is limited; (2) considering damping uncertainty has positive effect on reducing the convergence time but stiffness uncertainty plays the leading role for flutter control. |
| Key words:
adaptive control system
flutter
nonlinear aeroelasticity
airfoil
parametric uncertainty
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| 收稿日期: 2015-04-12
修回日期:
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| DOI: |
| 基金项目: 陕西省自然科学基金(2013JQ8026)资助 |
| 通讯作者:
Email： |
| 作者简介: 许行之(1976—),西北工业大学博士研究生,主要从事非线性气动弹性力学与控制的研究。
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