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Non-linear identification of multi-degree of freedom systems using the restoring force surface method

机译:使用恢复力表面法的非线性识别多程度的自由度系统

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In order to facilitate the non-linear identification of aircraft structures using the multi-degree of freedom restoring force surface method, a research study has been conducted to investigate the results accuracy of non-linear identification of multi-degree of freedom systems. This paper reviews the theoretical background of the restoring force method and explains its advantages and disadvantages together with practical consideration for its application. Focus is put on some practical aspects of the realization of nonlinear identification, e.g. the type of excitation force signals, the required sampling rates, signal processing issues, etc. The validation of the approach is pursued by processing simulated response data of multi-degree of freedom system with known non-linearity.
机译:为了便于使用多度自由度恢复力表面方法的飞机结构的非线性识别,已经进行了研究,以研究非线性自由度系统的非线性识别结果准确性。 本文审查了恢复力方法的理论背景,并与其应用的实际考虑说明了其优缺点。 重点是实现非线性识别的一些实际方面,例如, 激发力信号的类型,所需的采样率,信号处理问题等。通过处理具有已知非线性的多度自由度系统的模拟响应数据来验证方法的验证。

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