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围绕航天柔性结构的振动控制，从结构及材料的数学模型、材料及器件、基本理论与方法和一体化振动控制几个方面对一些研究的最新进展进行了介绍．主动控制和被动控制的一体化技术研究是当今航天柔性结构振动控制研究的重点，两种控制方法的结合不仅优点互补，而且提高了控制系统的性能．控制用材料和器件的研究在工程应用的推动下，也取得了较快的发展，并促进了振动控制技术的实用化
Focusing on the vibration control of aerospace flexible structure, some recent research progresses are introduced from the aspects of mathematical model of structure and materials, materials and devices, basic theory and method and integrated vibration control. Active control and passive control of integrated technology research is today’s space flexible structure vibration control research focus, the combination of two control methods not only have the advantages of each other, but also improve the control system performance. The research on control materials and devices has also achieved rapid development driven by engineering application and promoted the practical application of vibration control technology