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首页> 外文会议>Instrumentation and Measurement Technology Conference, 1999. IMTC/99. Proceedings of the 16th IEEE >Space Acceleration Measurement System-II: microgravity instrumentation for the International Space Station research community
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Space Acceleration Measurement System-II: microgravity instrumentation for the International Space Station research community

机译：空间加速度测量系统-II：国际空间站研究界的微重力仪器

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The International Space Station opens for business in the year 2000, and with the opening, science investigations will take advantage of the unique conditions it provides as an on-orbit laboratory for research. With initiation of scientific studies comes a need to understand the environment present during research. The Space Acceleration Measurement System-II provides researchers with a consistent means to understand the vibratory conditions present during experimentation on the International Space Station. The Space Acceleration Measurement System-II, or SAMS-II, detects vibrations present while the space station is operating. SAMS-II on-orbit hardware is comprised of two basic building block elements: a centralized control unit and multiple remote triaxial sensors deployed to measure the acceleration environment at the point of scientific research, generally within a research rack. Ground operations equipment is deployed to complete the command, control and data telemetry elements of the SAMS-II implementation. Initially, operations consist of user requirements development, measurement sensor deployment and use, and data recovery on the ground. Future system enhancements will provide additional user functionality and support more simultaneous users.
机译：国际空间站于2000年开始营业，随着该空间站的开放，科学研究将充分利用其作为在轨实验室进行研究的独特条件。随着科学研究的开展，需要了解研究过程中存在的环境。空间加速度测量系统II为研究人员提供了一种一致的方法，以了解在国际空间站进行的实验过程中存在的振动条件。空间加速度测量系统II（即SAMS-II）可检测空间站运行时出现的振动。 SAMS-II在轨硬件由两个基本构建块元素组成：集中控制单元和多个远程三轴传感器，这些传感器通常用于在科研点（通常在研究机架中）测量加速度环境。部署地面操作设备以完成SAMS-II实施的命令，控制和数据遥测元素。最初，操作包括用户需求开发，测量传感器的部署和使用以及地面数据恢复。未来的系统增强功能将提供附加的用户功能，并支持更多同时用户。

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