期刊文献+

惯导系统误差自补偿技术发展综述 被引量:4

Overview for Development of Inertial Navigation System Error Self- compensation Technology
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摘要 提高精度与降低成本是惯性技术发展永恒的主题,误差自补偿技术是符合该主题的重要研究方向之一。惯导系统可通过其特有的旋转机构及其周期性运动,实现惯性仪表误差的自动补偿,从而达到提高系统精度和降低系统成本的目的。论文在综合分析国内外大量相关资料的基础上,重点对国外惯导误差自补偿技术的起源、发展和应用情况进行了研究分析,同时对国内数家单位的研究工作也进行了总结,供该领域研究工作者参考。 To improve the precision and reduce the cost is the eternal theme of inertial technology development, error self - compensation technology is one of the important research directions consistent with the theme. Inertial navigation system can realize error self - compensation for system or inertial device through unique structure ( mainly rotating mechanism) and periodic motion, so as to improve the precision of the system and reduce the system cost. Based on comprehensive analysis of a large number of domestic and international references, the origin, development and application of foreign error compen- sation technology are focused on and analyzed, including Europe and the United States in the early studies, roulette Trojan technology, rotating modulation technology. At the end several domestic research work are summarized. Through summary and comparison of the domestic and international related research work, the paper hopes to provide some ideas and refer- ence value for some related researcher.
出处 《导航定位与授时》 2014年第1期8-12,共5页 Navigation Positioning and Timing
基金 国家自然科学基金(61104184)
关键词 惯导 误差 自动补偿技术 旋转调制 Inertial navigation Error Self - compensation technology Rotation modulation
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  • 1袁保伦,饶谷音.光学陀螺旋转惯导系统原理探讨[J].国防科技大学学报,2006,28(6):76-80. 被引量:68
  • 2管桦,魏瑞轩.一种用于传感器故障检测的改进残差检验法[J].空军工程大学学报(自然科学版),2005,6(3):26-28. 被引量:5
  • 3严恭敏,秦永元.车载激光陀螺SINS/DR组合导航系统研究[J].弹箭与制导学报,2005,25(4):20-23. 被引量:11
  • 4袁保伦,饶谷音.一种新的激光陀螺惯性测量组合标定方法[J].中国惯性技术学报,2007,15(1):31-34. 被引量:26
  • 5YUAN WQ,WU Z H,SUI Y X. Six degrees of freedom vi-bration transmissibility measurement of flexural opto-me-chanical structures with 3-axis acceleration sensors [ J ]. Pre-cision Engineering ,2014,38 (3 ) :561-568.
  • 6CHANG H L,ZHOU P W,XIE ZH J,et al. Theoreticalmodeling for a six-DOF vortex inertial sensor and experi-mental verification [ J ]. Journal of MicroelectromechanicalSystems,2013,22(5) : 1100-1108.
  • 7PAN J Y,ZHANG CH X, CAI Q ZH. An accurate calibra-tion method for accelerometer nonlinear scale factor on alow-cost three-axis turntable [ J ]. Measurement Scienceand Technology,2014,25(2) :1-7.
  • 8LV H Y, QIN L, LIU J. Principle research on a singlemass six-degree-of-freedom accelerometer with six groupsof piezoelectric sensing elements[ J] . IEEE Sensors Jour-nal,2015 ,15 (6) :3301-3310.
  • 9LIU W, ZHANG Y J, YANG X F. Pedestrian navigationusing inertial sensors and altitude error correction [ J ] .Sensor Review,2015 ,35( 1 ) :68-75.
  • 10XIA Y H,LI CH G, YOU J J,et al. Influences analysis ofconfigurations on the performance of parallel type six-axisaccelerometers [ J ]. Transactions of FAMENA, 2013,37(2) :67-86.

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