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基于差分布局的MEMS陀螺温漂补偿的研究
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作者 刘书平 李擎 《北京信息科技大学学报(自然科学版)》 2016年第5期78-81,共4页
微小型导航定位系统的关键核心器件MEMS陀螺受温度影响较大,其零偏误差呈现较强的非线性且变化范围较大,常规补偿方法较为复杂。针对上述问题,通过分析MEMS陀螺敏感环境温度的统计特性,提出了一种基于陀螺差分布局的温漂误差补偿的新方... 微小型导航定位系统的关键核心器件MEMS陀螺受温度影响较大,其零偏误差呈现较强的非线性且变化范围较大,常规补偿方法较为复杂。针对上述问题,通过分析MEMS陀螺敏感环境温度的统计特性,提出了一种基于陀螺差分布局的温漂误差补偿的新方法。实验表明:在-40^+60℃的温度范围内,采用新方法补偿后MEMS陀螺的漂移差值均有显著改善,削弱了温度的影响,可有效抑制MEMS陀螺温漂。该方法结构简单,易于物理实现,具有很好的工程实用价值。 展开更多
关键词 微机电系统陀螺 温度漂移 误差补偿 差分布局 微小型导航定位系统
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柱状机体/星体与天线间的电磁兼容性 被引量:3
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作者 王东方 苏东林 《现代雷达》 CSCD 北大核心 2001年第5期80-82,共3页
针对常规飞机、卫星等的几何形状 ,用时域有限差分法 (FDTD)分析了圆柱形良导体外形 (用以模拟飞机卫星等的机体 )对机载 /星载天线 (文中采用了线天线 )辐射特性的影响。通过改变柱形的直径和长度 ,对天线辐射方向图的变化进行了大量... 针对常规飞机、卫星等的几何形状 ,用时域有限差分法 (FDTD)分析了圆柱形良导体外形 (用以模拟飞机卫星等的机体 )对机载 /星载天线 (文中采用了线天线 )辐射特性的影响。通过改变柱形的直径和长度 ,对天线辐射方向图的变化进行了大量的研究 ,并得出了一些规律性的结果。 展开更多
关键词 时域有限差分 电磁兼容 天线布局 机载天线
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Global characteristics of the second-order ionospheric delay error using inversion of electron density profiles from COSMIC occultation data 被引量:4
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作者 WANG Hu WANG Cheng +3 位作者 WANG JieXian DANG YaMing BAI GuiXia WANG QianXin 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2014年第2期365-374,共10页
It is a well known fact that ionospheric delay error is a predominant factor which influences the positioning accuarcy of GNSS.Although the main part of the first-order ionospheric delay error can be removed by the fr... It is a well known fact that ionospheric delay error is a predominant factor which influences the positioning accuarcy of GNSS.Although the main part of the first-order ionospheric delay error can be removed by the frequency-dependent behaviors of the ionosphere,the second-order ionospheric delay error must be eliminated to achieve millimetre-scale positioning accuracy.Due to COSMIC occultation providing electron density profiles on the global scale,the paper presents the first-order and the second-order ionospheric delay error analysis on the global scale using the inversion of electron density profiles from COSMIC occultation data during 2009–2011.Firstly,because of the special geographical location of three ISR(incoherent scatter radar),the first-order and the second-order ionospheric delay errors are calculated and discussed;the paper also shows and analyzes the diurnal,seasonal,semi-annual variation of ionospheric delay error with respect to signal direction.Results show that for the L1 signal path,the first-order ionospheric delay error is the largest near the equator,which is circa 7 m;the maximum second-order ionospheric delay error are circa 0.6 cm,0.8 cm and 0.6 cm respectively for L1 signals coming from the zenith,the north and the south at 10 degree elevation angles.The second-order ionospheric delay error on the L1 signal path from zenith are the symmetry between 15°and 15°with respect to magnetic equator,and are nearly zero at the magnetic equator.For the first time,the second-order ionospheric delay error on the global scale is presented,so this research will greatly contribute to analysing the higher-order ionospheric delay error characteristics on the global scale. 展开更多
关键词 IONOSPHERE GPS COSMIC ISR IGRF
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