| 卫星长寿命高性能动调陀螺仪研制 |
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| 引用本文： | 夏永江,袁荣钢.卫星长寿命高性能动调陀螺仪研制[J].上海航天,2005,22(3):52-56. |
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| 作者姓名： | 夏永江 袁荣钢 |
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| 作者单位： | 上海航天控制工程研究所,上海,200233 |
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| 摘 要： | 在分析有关影响因素的基础上，研制了用于某卫星的长寿命高性能动力调谐陀螺。研究了轴承、力矩器和驱动系统动平衡结构，以及装调工艺，同时介绍了双轴连轴承 储油环系统的设计和试验情况。试验结果表明，所设计的长寿命陀螺的性能较好，寿命试验稳定性高。
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| 关 键 词： | 卫星 长寿命 动力调谐陀螺仪 轴连轴承 稳定性 |
| 文章编号： | 1006-1630(2005)03-0052-05 |
| 修稿时间： | 2004年5月19日 |
Research of High Performance and Long Life Dynamically Tuned Gyro for Satellite Application |
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| XIA Yong-jiang,YUAN Rong-gang.Research of High Performance and Long Life Dynamically Tuned Gyro for Satellite Application[J].Aerospace Shanghai,2005,22(3):52-56. |
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| Authors: | XIA Yong-jiang YUAN Rong-gang |
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| Abstract: | The high performance and long life dynamically tuned gyro for some satellite was development based on the analysis of effect factors in this paper. The bear, structure of driving system for torquer and dynamic balance and installation technique were studied. The design and test of double inner integral ball bearing and storage ring of lubricant oil were presented. The test results showed that the gyro designed provided good performance, which was stable in the life experiment. |
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| Keywords: | Satellite Long lifetime Dynamically tuned gyro Inner integral ball bearing Stability |
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