| 航天器动力学环境试验综合测试系统的设计 |
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| 引用本文： | 崔俊峰,冯咬齐,于丹,周建军. 航天器动力学环境试验综合测试系统的设计[J]. 计算机测量与控制, 2006, 14(3): 363-364,385 |
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| 作者姓名： | 崔俊峰 冯咬齐 于丹 周建军 |
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| 作者单位： | 1. 中国空间技术研究院总装与环境工程部,北京,100094
2. 北京航天测控公司,北京,100037 |
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| 摘 要： | 航天器在发射之前必须经过严格的地面条件验证;其中，航天器的动力学地面环境模拟试验对其顺利完成任务具有非常重要的意义;在航天器的动力学环境试验中，数据采集设备起着非常重要的作用，介绍了航天器动力学环境试验综合测试系统研制的目的、系统工作的原理、构成、硬件结构的研制以及解决的关键问题;最后的结果表明，这套系统完全可以满足航天器动力学地面试验的任务要求。
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| 关 键 词： | 航天器 动力学环境模拟试验 高速数据采集 |
| 文章编号： | 1671-4598（2006）03-0363-02 |
| 收稿时间： | 2005-07-19 |
| 修稿时间： | 2005-07-192005-08-27 |
Design of Integrated Measurement System for Spacecraft Dynamic Environment Testing |
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| Cui Junfeng,Feng Yaoqi,Yu Dan,Zhou Jianjun. Design of Integrated Measurement System for Spacecraft Dynamic Environment Testing[J]. Computer Measurement & Control, 2006, 14(3): 363-364,385 |
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| Authors: | Cui Junfeng Feng Yaoqi Yu Dan Zhou Jianjun |
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| Abstract: | Spacecraft Dynamic environment testing plays a very important role when a spacecraft is on mission. The developing purpose of integrated measurement system for spacecraft dynamic environment testing were described, principle, consitution, hardware platform and involved key techniques of this system were also introduced. Results of the simulation showed that the system was very practical. |
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| Keywords: | spacecraft dynamic environment testing high speed date acquisition |
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