主动颤振检测与控制研究

Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093) Pub Date : 2000-10-10 DOI:10.1109/NAECON.2000.894907

T. Norlander, B. Nilsson, D. Ring, U. Johansson

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引用次数: 3

摘要

介绍了沃尔沃航空公司和萨博航空公司联合开展的颤振主动抑制研究项目的结果。在风洞模型上设计了LQG控制器和参数LQ控制器，并对其进行了评价。可以看出，采用主动控制可以避免颤振;此外，参数化LQ控制设计技术适用于(实际)高性能低阶控制器的设计。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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A study on active flutter detection and control

Results from a joint Volvo Aero and Saab Aerospace research project on active flutter suppression is presented. An LQG controller and a parametric LQ controller have been designed and evaluated on a wind tunnel model. It is seen that flutter can be avoided using active control; furthermore it is shown that parametric LQ control design techniques are well suited for design of (practical) high performance low order controllers.

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Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093)

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