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Smart structures and their applications on active vibration control: Studies in the Department of Aerospace Engineering, METU

机译:智能结构及其在主动振动控制中的应用:METU航空航天工程系的研究

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This work presents the theoretical and experimental studies conducted in Aerospace Engineering Department of Middle East Technical University on smart structures with particular attention given to the structural modelling characteristics and active suppression of in-vacuo vibrations. The smart structures considered in these analyses are finite and flat aluminium cantilever beam-like (called as smart beam) and plate-like (called as smart fin) structures with surface bonded lead–zirconate–titanate patches. Finite element models of smart beam and smart fin are obtained. Then the experimental studies regarding open loop behaviour of the structures are performed by using strain gauges and laser displacement sensor to determine the system models. Further studies are carried out to obtain H ∞ and μ-synthesis controllers which are intended to be used in the suppression of free and forced vibrations of the smart structures. It is observed that satisfactory attenuation levels are achieved and robust performance of the systems in the presence of uncertainties is ensured. In that respect a comparative study involving H ∞ and sliding mode controls is also conducted. Recently, the studies involving aerodynamic loading are also gathering pace.
机译:这项工作介绍了在中东技术大学的航空工程系中对智能结构进行的理论和实验研究,并特别关注了结构建模特性和主动抑制真空中的振动。在这些分析中考虑的智能结构是有限的,扁平的铝悬臂梁状结构(称为智能梁)和板状结构(称为智能翅片),表面具有铅酸锆钛酸盐斑块。获得了智能梁和智能鳍的有限元模型。然后,通过使用应变仪和激光位移传感器确定系统模型,进行有关结构开环性能的实验研究。为了获得H∞和μ综合控制器,需要进行进一步的研究,以用于抑制智能结构的自由振动和强制振动。可以观察到,达到了令人满意的衰减水平,并且在存在不确定性的情况下确保了系统的稳健性能。在这方面,还进行了涉及H∞和滑模控制的比较研究。最近,涉及空气动力学载荷的研究也在加快步伐。

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