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基于方位大失准角捷联惯性导航系统初始对准问题的研究

李宏成

科技广场Issue(8):6-13,8.
科技广场Issue(8):6-13,8.

基于方位大失准角捷联惯性导航系统初始对准问题的研究

Study on Initial Alignment of Strapdown Inertial Navigation System Based on Azimuth and Large Misalignment Angle

李宏成1

作者信息

  • 1. 江西理工大学,江西 赣州 341000
  • 折叠

摘要

Abstract

For the problem of Strapdown Inertial Navigation System on stationary base under the initial align-ment, the paper proposes a new nonlinear filtering method which combines the Cubature Kalman Filter and Ex-tended Kalman Filter. Therefore, under the situation of large azimuth misalignment angle, the paper establishes a mathematical model based on stationary base. Simulation results show that: For the horizontal misalignment angle, the filtering effect of EKF is equal to E-CKF; but in large azimuth misalignment angle, the azimuth misalignment angle estimation error of E-CKF is reduced than the estimated error of about EKF 2.5'.

关键词

初始对准/容积卡尔曼滤波器/失准角/捷联惯性导航系统

Key words

Initial Alignment/Kalman Filter/Misalignment Angle/SINS

分类

交通工程

引用本文复制引用

李宏成..基于方位大失准角捷联惯性导航系统初始对准问题的研究[J].科技广场,2015,(8):6-13,8.

科技广场

1671-4792

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