...
首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Novel linear parameter-varying modeling and flutter suppression control of a smart airfoil
【24h】

Novel linear parameter-varying modeling and flutter suppression control of a smart airfoil

机译:智能翼型的新型线性参数变化建模和颤振抑制控制

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

In this article, two novel linear parameter-varying modeling and control techniques are proposed for active flutter suppression of a smart airfoil model. The smart airfoil model is instrumented with a moving mass that can be used to actively control the airfoil pitching and plunging motions. The first linear parameter-varying modeling approach makes use of the moving mass position as a scheduling parameter, and the hard constraint at the boundaries is imposed by proper selection of the parameter-varying function. The second modeling technique utilizes nonlinear springs and dampers, which are added to both ends of the airfoil groove to confine the motion of the moving mass. A state-feedback-based linear parameter-varying gain-scheduling controller with the guaranteed H infinity performance is proposed by utilizing the dynamics of the moving mass. In this study, both the position of the moving mass and the free-stream airspeed are considered as the scheduling parameters. The numerical simulations demonstrate the effectiveness of the proposed linear parameter-varying control architectures by significantly improving the performance, while increasing the flutter speed and reducing the control effort.
机译:在本文中,提出了两种新颖的线性参数变化建模和控制技术,用于智能翼型模型的主动颤振抑制。智能翼型模型装有可移动的质量,可用于主动控制翼型的俯仰和俯冲运动。第一种线性参数变化建模方法将移动质量位置用作调度参数,并且通过适当选择参数变化函数来施加边界处的硬约束。第二种建模技术利用非线性弹簧和阻尼器,它们被添加到翼型凹槽的两端以限制运动质量的运动。通过利用运动质量的动力学,提出了一种具有保证H无限性的基于状态反馈的线性参数变化增益调度控制器。在这项研究中,移动质量的位置和自由流空速都被视为调度参数。数值仿真通过显着提高性能,同时提高颤振速度并减少控制工作量,证明了所提出的线性参数变化控制架构的有效性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号