首页> 外文会议>Cranfield Conference on Dynamica and Control of Systems and Structures in Space; 2004; Liguria; IT >Columbus Design, Analysis and Verification Control Approach versus the Micro-gravity Requirement
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Columbus Design, Analysis and Verification Control Approach versus the Micro-gravity Requirement

机译:哥伦布设计,分析和验证控制方法与微重力要求的比较

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摘要

The European project manned module Columbus, as part of the International Space Station, has been conceived to allow scientific experiments on micro-gravity environment. In order to face against this challenging design goal, Alenia Spazio developed a dedicated control approach, based on budget allocation of the mechanical power, covering the Design, the Analysis and the Verification aspects from system level down to the equipment one. This control method covers both the evaluations by analysis and/or by testing of the Columbus Structural and Vibro-Acoustic transmission paths and the characterisation of the disturbers (as Environment Control Life System fans, Thermal Control System pumps and valves, etc.) in terms of force at the equipment interfaces and SPL in the surrounding volume. A dedicated methodology on how to derive the induced disturber's interface forcing functions has been developed in the frame of this project.
机译:作为国际空间站的一部分,欧洲项目载人舱哥伦布被构想为可以在微重力环境中进行科学实验。为了面对这个具有挑战性的设计目标,Alenia Spazio根据机械动力的预算分配,开发了一种专用的控制方法,涵盖了从系统级到设备级的设计,分析和验证方面。该控制方法涵盖了通过分析和/或测试哥伦布结构和振动声传递路径进行的评估以及干扰源(如环境控制生命系统风扇,热控制系统泵和阀等)的特性评估。设备接口处的力和周围体积中的SPL。在该项目的框架内,已经开发了一种专门的方法,用于推导诱发的干扰源的界面强迫功能。

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