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单轴旋转式惯导系统误差抑制机理分析
引用本文:高贤志,王丹.单轴旋转式惯导系统误差抑制机理分析[J].舰船科学技术,2012,34(8):67-72.
作者姓名:高贤志  王丹
作者单位:1. 海军驻天津707所军事代表室,天津,300134
2. 中国舰船研究院,北京,100192
摘    要:提高惯导系统对于惯性器件误差负面影响的抑制能力,对于改善系统的导航精度具有重要意义.本文对惯导系统误差方程进行分析,重点讨论对称位置上惯性器件误差的积累效果,系统地研究了单轴旋转调制对捷联惯性导航系统惯性器件误差的自动补偿机理,详细分析了单轴旋转对惯性器件常值误差、标度因数误差的抑制情况.对单轴旋转调制方案进行仿真,验证了理论分析的正确性.

关 键 词:捷联惯性导系统  误差抑制  单轴旋转

The analysis of error control mechanism for single-axis rotation inertial navigation system
GAO Xian-zhi , WANG Dan.The analysis of error control mechanism for single-axis rotation inertial navigation system[J].Ship Science and Technology,2012,34(8):67-72.
Authors:GAO Xian-zhi  WANG Dan
Institution:1.Military Representative Office of 707 Research Institute in Tianjin,Tianjin 300134,China;2.China Ship Research and Development Academy,Beijing 100192,China)
Abstract:It is significantly important to improve the performance of inertial navigation system navigation by controlling the negative effects on inertial navigation system for inertial measurement units.This paper analyses the error equations of the inertial navigation system,makes a focus on the inertial components accumulation effect on symmetrical position error,analyses the automatic constant error compensation mechanism of the inertial navigation system,and then discusses the error depressing of inertial components constant error,the scale factor error cased by rotating.Finally,the simulation for single-axis rotation mechanism validates the theory analysis.
Keywords:strapdown inertial navigation system  error depressing  single-axis rotation
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