Active vibration control of complex structures in modal space

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Tezin Türü: Yüksek Lisans

Tezin Yürütüldüğü Kurum: Orta Doğu Teknik Üniversitesi, Fen Bilimleri Enstitüsü, Türkiye

Tezin Onay Tarihi: 2014

Tezin Dili: İngilizce

Öğrenci: KEMAL MERSİN

Asıl Danışman (Eş Danışmanlı Tezler İçin): Yiğit Yazıcıoğlu

Eş Danışman: Melin Şahin

Özet:

Aerospace structures are designed to be light-weight to obtain high performance. Reduction in weight makes the structure flexible and lower frequency modes can be easily excited. Moreover those modes have low damping and vibrations do not attenuate immediately. Passive systems are effective to control the vibrations but they can be heavy and most of the time they do not respond to changing environment conditions. An active system is necessary for low-weight adaptive vibration reduction system. Modal Space Control is used for large flexible aerospace structures due to the advantage of reducing the complexity of control system. In this study a generalized formulation of modal space control is proposed for three dimensions where each node is modeled with six degrees of freedom.