航天器电源母线纹波测试系统设计
Design of the spacecraft power bus ripple measurement system
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摘要: 航天器电源母线纹波可以反映系统的稳定性。文章设计了一种基于PXI构架的电源母线纹波测试系统,实现对航天器电源母线安全、不间断的测试,有效地反映航天器测试过程中母线的动态特性,为型号改进设计及试验分析提供参考。该系统解决了以往型号对母线纹波测试只能依靠示波器或示波表,安全系数低、数据信息量小的问题,将在航天器电测中发挥重要作用。Abstract: The power bus ripple of spacecraft reflects the spacecraft's health condition and can be used to predict its future trend. This paper provides a design of a power bus ripple measuring system based on the PXI frame, and a certain spacecraft is tested in an uninterrupted test for the power bus safety to give the dynamic characteristics of the power bus. The methodology can be used in the model design and test analysis. This system solves the problems, such as the low security and the small data capacity in the past years based merely on oscilloscope or scope meter to test the ripple, and it might play a key role in the electrical test of spacecraft.
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Keywords:
- spacecraft /
- electrical test /
- power bus ripple /
- PXI frame
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[1] 万成安, 于磊, 刘建强. 航天器直流电源系统稳定性分析方法研究[J]. 航天器工程, 2009, 18(2): 14-19 [2] Wan Cheng'an, Yu Lei, Liu Jianqiang. Research on the stability analysis strategy for spacecraft DC power system[J]. Spacecraft Engineering, 2009, 18(2): 14-19
[3] Shi Feng, Zhao Jingwei, Shu Le, et al. Experimental study on output ripple of high voltage power supply[J]. Nuclear Electronics & Detection Technology, 2006, 26(1): 54-59
[4] 石峰, 赵京伟, 舒乐, 等. 直流高压电源纹波的实验研究[J]. 核电子学与探测技术, 2006, 26(1): 54-59 [5] Wang Yongqian, Hu Qizheng, Han Guojing. Dynamics analysis of the satellite power system[J]. Chinese Space Science and Technology, 2000(4): 22-26
[6] 王庆成. 航天器电测技术[M]. 北京: 中国科学技术出版社, 2007: 20 [7] Han Dapeng, Shui Haitao, Zeng Guoqiang, et al. Analysis on dynamic behavior of spacecraft power system[J]. Spacecraft Engineering, 2012, 21(5): 76-80
[8] 王永谦, 胡其正, 韩国经. 卫星电源系统的母线性能分析[J]. 中国空间科学技术, 2000(4): 22-26 [9] Sun Yi, Song Shimin, Liu Min. Analysis of test methods spacecraft power bus quality[J]. Journal of Astronautic Metrology and Measurement, 2013, 33(2): 54-59
[10] 韩大鹏, 税海涛, 曾国强, 等. 航天器电源系统的动态特性研究[J]. 航天器工程, 2012, 21(5): 76-80 [11] 孙毅, 宋世民, 刘民. 航天器电源母线品质地面测试方法浅析[J]. 宇航计测技术, 2013, 33(2): 54-59 -
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