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The impact of model uncertainty on spatial compensation in active structural acoustic control.

机译:主动结构声学控制中模型不确定性对空间补偿的影响。

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摘要

Control strategies aimed at the reduction of turbulent boundary layer noise transmission into the fuselage of an aircraft have been topics of academic and industrial research for years. There has been a great deal of knowledge culled from these research projects that has added to the understanding of the fundamental and application physics involved. However, there have been few practical realizations of these strategies due to potential limitations in application settings. This work focuses on an approach that will attempt to address one of the potential application issues, that of uncertainties in boundary conditions.; A method for optimizing a structural acoustic control system with regard to potential variations in plate boundary conditions is provided. The assumed modes method is used to build a plate model with varying levels of rotational boundary stiffness to simulate a plate with uncertain edge conditions. A transducer placement scoring process, involving Hankel singular values (HSVs), is combined with a genetic optimization routine to find locations robust to boundary condition variation. Predicted frequency response characteristics are examined, and theoretically optimized results are discussed in relation to boundary condition variations. Control system design is also impacted by uncertainty in boundary conditions, specifically in terms of the compensator required to achieve the desired control. Impact of uncertain boundary conditions on the selection of actuator and sensor locations for structural acoustic control is considered.; Results indicate it is possible to minimize the impact of uncertain boundary conditions in active structural acoustic control by optimizing the placement of transducers with respect to those uncertainties. Additionally, results indicate that optimizing with respect to a group of randomly generated boundary conditions results in a patch pair capable of performing well over the complete group of conditions. Test results were also obtained that demonstrate the importance of enforcing model coupling roll-off beyond the primary bandwidth of interest. Finally, results indicate that failure to consider possible boundary condition variations can inhibit the ability to enforce control in the presence of such variations.
机译:多年来,旨在减少湍流边界层噪声传递到飞机机身的控制策略一直是学术和工业研究的主题。这些研究项目积累了很多知识,这些知识增加了对所涉及的基础和应用物理的理解。但是,由于应用程序设置的潜在限制,这些策略的实际实现很少。这项工作侧重于试图解决潜在应用问题之一的方法,即边界条件的不确定性。提供了一种关于板边界条件中的潜在变化来优化结构声学控制系统的方法。假定模式方法用于构建具有不同水平的旋转边界刚度的板模型,以模拟具有不确定边缘条件的板。涉及汉高奇异值(HSV)的换能器放置计分过程与遗传优化例程结合在一起,以找到对边界条件变化具有鲁棒性的位置。检查了预测的频率响应特性,并讨论了与边界条件变化有关的理论上最优化的结果。控制系统的设计还受到边界条件不确定性的影响,特别是在实现所需控制所需的补偿器方面。考虑了不确定边界条件对用于结构声学控制的致动器和传感器位置选择的影响。结果表明,通过针对这些不确定性优化换能器的放置,可以在主动结构声学控制中最小化不确定边界条件的影响。另外,结果表明,针对一组随机生成的边界条件进行优化会导致补丁对能够在完整的一组条件下表现良好。还获得了测试结果,这些结果表明了加强模型耦合滚降超出所关注的主要带宽的重要性。最后,结果表明,不考虑可能的边界条件变化会抑制存在这种变化的情况下强制执行控制的能力。

著录项

  • 作者

    Sprofera, Joseph Daniel.;

  • 作者单位

    Duke University.;

  • 授予单位 Duke University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2005
  • 页码 170 p.
  • 总页数 170
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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