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Progress in Operational Analysis of Launch Vehicles in Nonstationary Flight

机译:非平稳飞行中运载火箭的作战分析进展

摘要

This paper presents recent results in an ongoing effort to understand and develop techniques to process launch vehicle data, which is extremely challenging for modal parameter identification. The primary source of difficulty is due to the nonstationary nature of the situation. The system is changing, the environment is not steady, and there is an active control system operating. Hence, the primary tool for producing clean operational results (significant data lengths and data averaging) is not available to the user. This work reported herein uses a correlation-based two step operational modal analysis approach to process the relevant data sets for understanding and development of processes. A significant drawback for such processing of short time histories is a series of beating phenomena due to the inability to average out random modal excitations. A recursive correlation process coupled to a new convergence metric (designed to mitigate the beating phenomena) is the object of this study. It has been found in limited studies that this process creates clean modal frequency estimates but numerically alters the damping.
机译:本文介绍了正在进行的努力,以了解和开发用于处理运载火箭数据的技术的最新成果,这对于模态参数识别极为困难。困难的主要根源是由于局势的不稳定。系统正在变化,环境不稳定,并且正在运行一个主动控制系统。因此,用户无法获得用于产生干净的操作结果(大量数据长度和数据平均)的主要工具。本文报道的这项工作使用基于相关性的两步操作模式分析方法来处理相关数据集,以了解和开发流程。这种对短时间历史的处理的显着缺点是由于无法均衡随机模态激励而导致的一系列跳动现象。本研究的目标是将递归相关过程与新的收敛度量(旨在缓解跳动现象的方法)相结合。在有限的研究中已经发现,该过程可以创建干净的模态频率估计值,但是会在数值上改变阻尼。

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