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A novel approach to determine upper tolerance limit of non-stationary vibrations during rocket launch

机译:一种新的方法来确定火箭发射期间非静止振动的高容差限制

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摘要

This paper firstly introduces a locally stationary model to analyze non-stationary environmental vibrations during a rocket launch.Then based on this model, a novel method is proposed to estimate the upper tolerance limit of expected non-stationary environmental vibrations, which can be used to evaluate whether equipments on rocket can experience environmental vibrations in safe.Compared with available method, the proposed method can characterize non-stationary vibration better.
机译:本文首先介绍了局部静止模型,用于分析火箭发射期间的非静止环境振动。该基于该模型,提出了一种新的方法来估计预期的非平稳环境振动的上部公差限制,可用于评估火箭的设备是否可以在安全的方法上体验环境振动,所提出的方法可以更好地表征非平稳振动。

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