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Complex dynamics of a nonlinear aerospace structure: Experimental identification and modal interactions

机译:非线性航空航天结构的复杂动力学:实验识别和模态相互作用

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摘要

Nonlinear system identification is a challenging task in view of the complexity and wide variety of nonlinear phenomena. The present paper addresses the identification of a real-life aerospace structure possessing a strongly nonlinear component with multiple mechanical stops. The complete identification procedure, from nonlinearity detection and characterization to parameter estimation, is carried out based upon experimental data. The combined use of various analysis techniques, such as the wavelet transform and the restoring force surface method, brings different perspectives to the dynamics. Specifically, the structure is shown to exhibit particularly interesting nonlinear behaviors, including jumps, modal interactions, force relaxation and chattering during impacts on the mechanical stops.
机译:鉴于非线性现象的复杂性和多样性,非线性系统识别是一项艰巨的任务。本文提出了一种具有多个机械止挡的,具有强烈非线性成分的现实生活中的航空航天结构的识别方法。根据实验数据执行从非线性检测和表征到参数估计的完整识别过程。小波变换和恢复力面法等各种分析技术的结合使用,为动力学带来了不同的见解。具体而言,该结构显示出特别有趣的非线性行为,包括跳跃,模态相互作用,力松弛和在机械止动件碰撞过程中的颤动。

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