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基于WMM2010地磁模型的微卫星姿态确定

李忠亮 边少锋 李忠美

海洋测绘2012,Vol.32Issue(5):11-14,4.
海洋测绘2012,Vol.32Issue(5):11-14,4.DOI:10.3969/j.issn.1671-3044.2012.05.004

基于WMM2010地磁模型的微卫星姿态确定

Micro-satellite Attitude Determination Based on WMM2010

李忠亮 1边少锋 2李忠美1

作者信息

  • 1. 海军工程大学导航工程系,湖北武汉430033
  • 2. 91960部队,广东汕头515000
  • 折叠

摘要

Abstract

A brief description of the specificity and utility of micro-satellites, and a short introduction of the principle of three-axis attitude determination by single magnetometer are given. Based on the model named WMM2010, this paper presents the statistical method of the satellites' attitude,mainly analyzes the difference between the value of various geomagnetic truncation models and the real value, at last indicates that when the required precision is not extraordinary exact, low order models can be used as the real value stored in the satellite memory to improve the real-time attitude determination for the micro-satellites in middle or low orbits.

关键词

微卫星/地磁模型/WMM2010/卡尔曼滤波

Key words

micro-satellite/ geomagnetic field /WMM2010/ Kalman filtering

分类

天文与地球科学

引用本文复制引用

李忠亮,边少锋,李忠美..基于WMM2010地磁模型的微卫星姿态确定[J].海洋测绘,2012,32(5):11-14,4.

基金项目

国家自然科学基金(40774002,40644020) (40774002,40644020)

海岛(礁)测绘技术国家测绘局重点实验室项目(2010B04). (礁)

海洋测绘

OACSTPCD

1671-3044

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