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| 航天器微振动环境分析与测量技术发展 | |
| 引用本文： | 航天器微振动环境分析与测量技术发展[J]. 航天器环境工程, 2006, 23(4): 210-214. |
| 作者姓名： | 赵 伟 |
| 作者单位： | 1.兰州空间技术物理研究所，兰州730000 |
| 摘 要： | 文章分析了航天器在轨运行时出现的准稳态加速度、瞬变加速度、振动加速度的来源及对航天器产生的影响。介绍了美国、欧空局及我国的航天器微振动测试技术现状。并就Olympus卫星、Oicets卫星和我国“神舟”号飞船的情况，深入讨论了微振动测试的方法与结果。 |
| 关 键 词： | 微振动 测试技术；航天器 |
| 文章编号： | 1673-1379(2006)-04-0210-05 |
| 收稿时间： | 2006-06-06 |
| 修稿时间： | 2006-06-06 |
Analysis on Micro-vibration Environment of Spacecraft and Measurement Technology |
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| Analysis on Micro-vibration Environment of Spacecraft and Measurement Technology[J]. Spacecraft Environment Engineering, 2006, 23(4): 210-214. | |
| Authors: | ZHAO Wei |
| Affiliation: | 1. Lanzhou Institute of Physics, Lanzhou 730000, China |
| Abstract: | The micro-accelerations of orbiting spacecraft, such as quasi-steady acceleration, transient acceleration and vibratory acceleration, are described, and its disturbance sources and effects on spacecraft are analyzed. In addition, the micro-vibration measurement technologies are illustrated, together with the measurement methods and the results of the micro-vibration. |
| Keywords: | micro-vibration measurement technology spacecraft |
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