| 航天器微振动环境分析与测量技术发展 |
| |
| 引用本文： | 赵,伟.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： | 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： | 6/6/2006 12:00:00 AM |
| 修稿时间： | 2006年6月6日 |
Analysis on Micro-vibration Environment of Spacecraft and Measurement Technology |
| |
| ZHAO Wei.Analysis on Micro-vibration Environment of Spacecraft and Measurement Technology[J].Spacecraft Environment Engineering,2006,23(4):210-214. |
| |
| Authors: | ZHAO Wei |
| |
| Institution: | 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 |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《航天器环境工程》浏览原始摘要信息 |
| 点击此处可从《航天器环境工程》下载免费的PDF全文 |
