| 航天器动力学环境试验综合测试系统的设计思路 |
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| 引用本文： | 冯咬齐,崔俊峰.航天器动力学环境试验综合测试系统的设计思路[J].航天器环境工程,2003,20(4):34-39. |
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| 作者姓名： | 冯咬齐 崔俊峰 |
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| 作者单位： | 北京卫星环境工程研究所,北京,100029 |
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| 摘 要： | 文章简要介绍了动力学环境模拟试验综合测试系统的原理、构成及关键技术,给出了大中型动力学综合测试系统硬件平台及应用软件系统的设计思路。
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| 关 键 词： | 航天器 动力学环境模拟试验 数据采集与处理 综合测试系统 |
| 文章编号： | (2003)04-0034-06 |
| 收稿时间： | 2003/7/15 0:00:00 |
| 修稿时间： | 2003年7月15日 |
THE DESIGN OF INTEGRATED MEASUREMENT SYSTEM FOR SPACECRAFT DYNAMIC ENVIRONMENT TESTING |
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| FENG Yao-qi,CUI Jun-feng.THE DESIGN OF INTEGRATED MEASUREMENT SYSTEM FOR SPACECRAFT DYNAMIC ENVIRONMENT TESTING[J].Spacecraft Environment Engineering,2003,20(4):34-39. |
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| Authors: | FENG Yao-qi CUI Jun-feng |
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| Abstract: | This paper describes briefly the principle,the constitution and the involved techniques of integrated measurement system for dynamic environment testing.The design ideas of hardware platform and application software for large-scale dynamic measurement system are presented in the paper. |
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| Keywords: | spacecraft dynamic environment testing large-scale date acquisition and processing computer dynamic measurement integrated dynamic measurement system |
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