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一种快速精确的捷联惯导系统初始对准方法研究
引用本文:王新龙,申功勋. 一种快速精确的捷联惯导系统初始对准方法研究[J]. 中国惯性技术学报, 2003, 11(5): 19-23
作者姓名:王新龙  申功勋
作者单位:北京航空航天大学宇航学院,北京,100083
摘    要:由于传统的多位置对准方法在用卡尔曼滤波器对其状态变量进行估计时,方位失准角收敛很慢,因此提出了一种快速多位置对准估计方位失准角的方法,直接利用两水平失准角快速收敛的估计结果对传统多位置对准中方位失准角的估计,从而大大提高了捷联惯导系统静基座对准的精度和速度。计算机仿真结果验证了该方法的有效性。

关 键 词:捷联惯导系统 初始对准 卡尔曼滤波器 惯性导航系统 可观测性 计算机仿真 方位失准角
文章编号:1005-6734(2003)05-0019-05
修稿时间:2003-07-13

A Fast and Precision Initial Alignment Method for Strapdown Inertial Navigation System
WANG Xin-long,SHEN Gong-xun. A Fast and Precision Initial Alignment Method for Strapdown Inertial Navigation System[J]. Journal of Chinese Inertial Technology, 2003, 11(5): 19-23
Authors:WANG Xin-long  SHEN Gong-xun
Abstract:Although the tradition muliposition alignment technique made the strapdown inertial navigation system (SINS) having high alignment accuracy, the poor observability of SINS on stationary base, the estimation of the azimuth error will converge very slowly in initial alignment by means of Kalman filter. In this paper, a fast and accuracy estimation method of the multiposition alignment azimuth error is creatively proposed for the initial alignment of SINS on stationary base. On the basis of the fast converge of the leveling error, the azimuth error can be directly calculated. By means of this fast and accuracy initial alignment method, not only the precision of initial alignment is increased, but also the speed of initial alignment is greatly improved. The computer simulation results illustrate the efficiency of this method.
Keywords:SINS  initial alignment  Kalman filter  observability  
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