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Unscented卡尔曼滤波在SINS静基座大方位失准角初始对准中的应用研究
引用本文:丁杨斌,王新龙,王缜,申功勋.Unscented卡尔曼滤波在SINS静基座大方位失准角初始对准中的应用研究[J].宇航学报,2006,27(6):1201-1204.
作者姓名:丁杨斌  王新龙  王缜  申功勋
作者单位:北京航空航天大学宇航学院,北京,100083
摘    要:静基座大方位失准角的捷联惯导系统误差方程是非线性的,如何对静基座大方位失准角的捷联惯导系统进行初始对准是需要解决的问题。本文提出了基于Unscented转换的Unsented卡尔曼滤波进行捷联惯导系统对准的方法。分别通过扩展卡尔曼滤波和Unsented卡尔曼滤波进行仿真计算,结果验证了Unscented卡尔曼滤波的有效性与优越性。

关 键 词:Unscented卡尔曼滤波  捷联惯导系统  大方位失准角  初始对准
文章编号:1000-1328(2006)06-1201-04
收稿时间:11 10 2005 12:00AM
修稿时间:2005-11-102006-06-19

Study on Unscented Kalman Filter Applied in Initial Alignment of Large Azimuth Misalignment On Static Base of SINS
DING Yang-bin,WANG Xin-long,WANG Zhen,SHEN Gong-xun.Study on Unscented Kalman Filter Applied in Initial Alignment of Large Azimuth Misalignment On Static Base of SINS[J].Journal of Astronautics,2006,27(6):1201-1204.
Authors:DING Yang-bin  WANG Xin-long  WANG Zhen  SHEN Gong-xun
Institution:BeiHang University, School of Astronautics, Beijing 100083, China
Abstract:The error function is nonlinear when the azimuth misalignment angle of SINS on static base is large,and it's a problem that how to align such SINS whose azimuth misalignment angle is large.An approach of unscented kalman filter based on unscented transformation is presented.The initial alignment of large azimuth misalignment is simulated by extended kalman filter and Unscented kalman filter respectively,and the results show that using the Unscented kalman filter is more effective and superior than using extended kalman filter.
Keywords:Unscented kalman filter  SINS  Large azimuth angle  Initial alignment
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