The method can be extended to study the whole nonlinear satellite structure.
本文的方法可以推广到整星的非线性结构的研究中去。
The principle and characteristics of the force limited in satellite structure vibration testing were introduced in this paper.
介绍了卫星结构振动试验中力控技术的原理、特点,以及国外力控技术的研究和应用。
In the paper the phenomena in test for nonlinear dynamic behavior of aluminum honeycomb sandwich plate in satellite structure are analysed.
本文针对卫星主要结构材料铝质蜂窝板的非线性动力特性现象进行了振动试验及分析。
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