2DOF NATA 模型的 LMI 可行性分析

Q3 Engineering

Pollack Periodica Pub Date : 2024-02-19 DOI:10.1556/606.2024.00888

A. Wéber, M. Kuczmann

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引用次数: 0

摘要

本文介绍了不同类型的基于张量乘积模型的线性矩阵不等式控制器设计以及双自由度气动弹性翼段模型的可行性分析。张量乘积模型基于减少或消除系统的非线性行为和加权函数。基于线性矩阵不等式的方法可得到全局渐近稳定的系统。本文的目的是研究变换空间的选择和变化对基于线性矩阵不等式控制器可行性的影响。论文对不同张量乘积模型的控制器性能进行了比较。如果变换空间选择得当，线性矩阵不等式将为控制器设计提供可行的解决方案。

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LMI feasibility analysis of 2DOF NATA model

Present paper shows the different types of tensor product model based linear matrix inequality controller design and feasibility analysis of two degrees of freedom aeroelastic wing section model. The tensor product models are based on reducing or removing the nonlinear behavior of the system and weighting functions. The linear matrix inequality based method results globally asymptotically stable system. The goal of the paper is to examine that selecting and varying the transformation space influences the feasibility of the linear matrix inequality based controller. The paper gives a comparison between the different tensor product models in terms of controller performance. The linear matrix inequality gives feasible solution for the controller design if the transformation space is selected adequately.

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来源期刊

Pollack Periodica Engineering-Civil and Structural Engineering

CiteScore

1.50

自引率

0.00%

发文量

期刊介绍： Pollack Periodica is an interdisciplinary, peer-reviewed journal that provides an international forum for the presentation, discussion and dissemination of the latest advances and developments in engineering and informatics. Pollack Periodica invites papers reporting new research and applications from a wide range of discipline, including civil, mechanical, electrical, environmental, earthquake, material and information engineering. The journal aims at reaching a wider audience, not only researchers, but also those likely to be most affected by research results, for example designers, fabricators, specialists, developers, computer scientists managers in academic, governmental and industrial communities.