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捷联惯导系统大方位失准角下的非线性对准
引用本文:魏春岭,张洪钺,郝曙光.捷联惯导系统大方位失准角下的非线性对准[J].航天控制,2003,21(4):25-35.
作者姓名:魏春岭  张洪钺  郝曙光
作者单位:北京航空航天大学自动化学院,北京,100083
摘    要:采用欧拉角描述平台坐标系与导航坐标系间的失准角,推导了适用于捷联惯导系统的非线性误差方程,证明了该方法仅适用于方位误差角为大角度,而水平误差角为小量的情况。数学仿真表明:在方位误差角为大角度情况下,采用所推导的误差方程和非线性滤波技术能获得更高的估计精度。

关 键 词:惯性导航  非线性滤波  初始对准
修稿时间:2003年5月8日

SINS Nonlinear Alignment with Large Azimuth Misalignment Angles
Wei Chunling,Zhan Hongyue,Hao Shuguang Beijing University of Aeronautics and Astronautics,Beijing.SINS Nonlinear Alignment with Large Azimuth Misalignment Angles[J].Aerospace Control,2003,21(4):25-35.
Authors:Wei Chunling  Zhan Hongyue  Hao Shuguang Beijing University of Aeronautics and Astronautics  Beijing
Institution:Wei Chunling,Zhan Hongyue,Hao Shuguang Beijing University of Aeronautics and Astronautics,Beijing 100083
Abstract:Luler angles are adopted to describe the misalignment of platform to navi- gation frame. It was pointed out that the derived error medels are only valid when the head- ing uncertainty is large and the level misalignment angles are small. The simulation results show that, under large azimuth misalignment, good alignment accuracy can be obtained us- ing the derived nonlinear error models and nanlinear filtering techniques.
Keywords:Inertial navigation  Error model  Initial alignment  Nonlinear filtering
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