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基于单轴旋转的光纤捷联惯导系统误差特性与实验分析 被引量:21

Error Characteristic and Experiment Analysis of FOG SINS Based on Signal-axis Rotation
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摘要 针对惯性器件偏差是影响惯导系统导航精度的主要因素,同时考虑到多种误差源对调制型捷联系统的影响,提出了一种利用惯性测量单元(IMU)四位置转停的误差调制方法。分析了调制型捷联系统的误差特性并建立了四位置转位方案模型。利用实验室自行研制的光纤捷联惯导系统分别进行IMU静止和四位置转位运动下的长时间导航实验,实验结果表明了该方法的有效性。 According to the inertial device bias is the leader factor which decrease the navigation accuracy,and considering the rotary strapdown inertial navigation system is effected by the multi-errors.The error modulation method which utilize the IMU four-position indexing is proposed in this paper.The error characters of rotary SINS are analyzed and the model of four-position indexing scheme is established.The navigation experiment with a long time on the condition of IMU static and four-position indexing are operated by the FOG SINS which is made in our lab.The experiment results show the proposed method is valid.
作者 孙枫 孙伟
出处 《宇航学报》 EI CAS CSCD 北大核心 2010年第4期1070-1077,共8页 Journal of Astronautics
基金 国家自然科学基金(60834005 60775001)
关键词 捷联惯导系统 单轴旋转 误差特性 光纤陀螺 定位误差 Strapdown inertial navigation system Signal-axis rotation Error characters FOG Position error
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参考文献14

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