文章基本信息

标题：Active flutter suppression: non-structured and structured H ∞ design *
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作者：Sérgio Waitman ; Andrés Marcos
期刊名称：IFAC PapersOnLine
印刷版ISSN：2405-8963
出版年度：2019
卷号：52
期号：12
页码：146-151
DOI：10.1016/j.ifacol.2019.11.184
语种：English
出版社：Elsevier
摘要：AbstractIn this article a comparison of two controllers for the active suppression of flutter of a flexible remotely-piloted aerial vehicle is presented. TheH∞technique is used for both, but the first relies on the standard (non-structured) approach and the second on the structured synthesis. High-fidelity models derived from finite element modeling are used to verify the performance of the obtained controllers. Reduced-order models are used for the control synthesis, which are obtained from applying a combination of balanced and modal reduction techniques on the high-fidelity models. The results show that both controllers are similar in performance and robustness, and both are capable of suppressing flutter and extending the flight envelope well beyond the open-loop flutter speed.
关键词：KeywordsAerospaceaircraft controlH∞controlrobust control