| 微纳卫星释放分离参数的测试方法 |
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| 引用本文： | 陈有梅,付碧红,余成锋,吉彦超. 微纳卫星释放分离参数的测试方法[J]. 宇航计测技术, 2019, 39(4): 58-61. DOI: 10.12060/j.issn.1000-7202.2019.04.12 |
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| 作者姓名： | 陈有梅 付碧红 余成锋 吉彦超 |
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| 作者单位： | 1、上海微小卫星工程中心，上海 201120 |
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| 摘 要： | 采用自由落体的试验方法,在地面模拟卫星在轨释放过程,测试某微纳卫星在轨释放速度、姿态以及对卫星星上设备的冲击,卫星的释放速度通过高速摄影的测量方法,卫星的释放姿态和星上设备的冲击响应通过集成在试验卫星上的测试系统测量。该试验方法可以一次测量出卫星的释放姿态、释放速度以及释放分离对卫星星上设备的冲击响应。
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| 关 键 词： | 微纳卫星 释放分离 释放姿态 冲击响应 |
The Testing Method of Releasing Parameter for Microsatellite |
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| CHEN You-mei,FU Bi-hong,YU Cheng-feng,JI Yan-chao. The Testing Method of Releasing Parameter for Microsatellite[J]. Journal of Astronautic Metrology and Measurement, 2019, 39(4): 58-61. DOI: 10.12060/j.issn.1000-7202.2019.04.12 |
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| Authors: | CHEN You-mei FU Bi-hong YU Cheng-feng JI Yan-chao |
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| Affiliation: | 1、Shanghai Engineering Center of Microsatellite, Shanghai 201120，China |
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| Abstract: | The releasing progress of microsatellite on orbit is simulated by the free-fall method. The releasing speed is tested by high-speed photography，realeasing attitude and shock response are tested by the testing system assembled in the satellite . By this testing method can test the releasing speed、the releasing attitude and the releasing shock response simultaneously. |
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| Keywords: | Microsatellite Releasing Releasing attitude Shock response |
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