| 注册
首页|期刊导航|航空兵器|基于 DGPS 的弹载捷联惯导系统性能评估技术研究

基于 DGPS 的弹载捷联惯导系统性能评估技术研究

程海彬 江云 鲁浩 徐剑芸

航空兵器Issue(3):23-26,4.
航空兵器Issue(3):23-26,4.

基于 DGPS 的弹载捷联惯导系统性能评估技术研究

Research on Performance Evaluation Technology for Missile-Borne SINS Based on DGPS

程海彬 1江云 1鲁浩 1徐剑芸1

作者信息

  • 1. 中国空空导弹研究院,河南洛阳 471009
  • 折叠

摘要

Abstract

According to the requirements of the performance evaluation of weapons systems for mis-sile-borne SINS, the accuracy analysis method of SINS transfers alignment and navigation are researched. The advantages and disadvantages of the fixed point and fixed interval smoothers algorithm are compared. A new algorithm using the navigation segment data Kalman filtering for assessment of SINS transfer align-ment and navigation error is designed;software simulation of the new algorithm is adopted, the simulation results prove that this evaluation algorithm for the fixed point and fixed interval smoothers algorithm is more practical and has more engineering value.

关键词

性能评估/捷联惯导/算法仿真/卡尔曼滤波

Key words

performance evaluation/SINS/algorithm simulation/Kalman filter

分类

军事科技

引用本文复制引用

程海彬,江云,鲁浩,徐剑芸..基于 DGPS 的弹载捷联惯导系统性能评估技术研究[J].航空兵器,2015,(3):23-26,4.

基金项目

中航导弹院科技创新基金项目 ()

航空兵器

OACSTPCD

1673-5048

访问量2
|
下载量0
段落导航相关论文