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| 某陀螺仪二次项测试方法研究 | |
| 引用本文： | 郑云霞,唐文林,沙立.某陀螺仪二次项测试方法研究[J].导航与控制,2011(4):31-37. |
| 作者姓名： | 郑云霞 唐文林 沙立 |
| 作者单位： | 北京航天控制仪器研究所;北京航天控制仪器研究所;北京航天控制仪器研究所 |
| 摘 要： | 本文通过对某陀螺仪二次项DSO产生原理的分析,发现陀螺仪二次项DSO与过载a0有关.通过对陀螺仪进行低过载测试试验和高过载测试试验,测试出了二次项DSO与过载a0的趋势性关系.即低过载下,陀螺仪二次项DSO与过载近似无关；高过载下,陀螺仪二次项DSO与过载之间成一定函数关系. |
| 关 键 词： | 陀螺仪 二次项 过载 测试方法 |
Testing Method for the Acceleration-square-sensitive Drift Coefficient of the Single Freedom Hydro-static Bearing Floated Gyroscope |
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| ZHENG Yun-xi,TANG Wen-lin and SHA Li.Testing Method for the Acceleration-square-sensitive Drift Coefficient of the Single Freedom Hydro-static Bearing Floated Gyroscope[J].Navigation and Control,2011(4):31-37. | |
| Authors: | ZHENG Yun-xi TANG Wen-lin and SHA Li |
| Institution: | Beijing Institute of Aerospace Control Device;Beijing Institute of Aerospace Control Device;Beijing Institute of Aerospace Control Device |
| Abstract: | |
| Keywords: | hydro-static bearing floated gyroscope acceleration-square-sensitive drift coefficient over loading test method |
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