| 注册
首页|期刊导航|航天器工程|微小卫星三轴磁强计测量误差校正方法

微小卫星三轴磁强计测量误差校正方法

刘燎 孙华苗 何波 薛力军 张迎春

航天器工程2018,Vol.27Issue(1):89-95,7.
航天器工程2018,Vol.27Issue(1):89-95,7.DOI:10.3969/j.issn.1673-8748.2018.01.012

微小卫星三轴磁强计测量误差校正方法

Error Calibration Method of Three-axis Magnetometer Measurement for Micro-satellite

刘燎 1孙华苗 2何波 1薛力军 2张迎春1

作者信息

  • 1. 深圳航天东方红海特卫星有限公司,广东深圳 518064
  • 2. 微小卫星控制系统仿真与测试工程实验室,广东深圳 518064
  • 折叠

摘要

Abstract

Measurement of the magnetic field intensity is required for micro-satellite to damp and attitude control.The measurement errors because of change of the temperature would reduce the measurement precision of the three-axis magnetometer,so the measurement errors need to be calibrated.In this paper,an error calibration method of three-axis magnetometer measurement is proposed,and the error calibration model is established based on measurement error analysis. According to the magnetic field intensity and temperature of the magnetic simulator and the out-put voltage of the three-axis magnetometer,the temperature model of three-axis magnetometer is set up.The calibration coefficient is achieved by pseudo-inverse method,and the relationship be-tween calibration coefficient and temperature,the relationship between zero-point voltage are fit-ted with linear method,then the measurement precision of the three-axis magnetometer could be compensated by temperature.The three-axis magnetometer is calibrated and tested in a magnetic simulator in which the temperature can change.The results verify the correctness and effective-ness of the calibration method proposed in the paper.

关键词

微小卫星/三轴磁强计/温度模型/标定系数/线性拟合

Key words

micro-satellite/three-axis magnetometer/temperature model/calibration coefficient/linear fitting

分类

航空航天

引用本文复制引用

刘燎,孙华苗,何波,薛力军,张迎春..微小卫星三轴磁强计测量误差校正方法[J].航天器工程,2018,27(1):89-95,7.

基金项目

国家自然科学基金(61473297),深圳市技术攻关项目(JSGG20160429165838848) (61473297)

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

访问量0
|
下载量0
段落导航相关论文