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三轴磁强计测量误差修正方法

郝 东, 绳 涛, 陈小前

郝 东, 绳 涛, 陈小前. 三轴磁强计测量误差修正方法[J]. 航天器环境工程, 2011, 28(5): 463-466
引用本文: 郝 东, 绳 涛, 陈小前. 三轴磁强计测量误差修正方法[J]. 航天器环境工程, 2011, 28(5): 463-466
Hao Dong, Sheng Tao, Chen Xiaoqian. The error correction of three-axis magnetometer measurement[J]. Spacecraft Environment Engineering, 2011, 28(5): 463-466.
Citation: Hao Dong, Sheng Tao, Chen Xiaoqian. The error correction of three-axis magnetometer measurement[J]. Spacecraft Environment Engineering, 2011, 28(5): 463-466.

三轴磁强计测量误差修正方法

基金项目: 

国家自然科学基金(项目编号:50975280);教育部新世纪优秀人才支持计划(项目编号:NCET-08-0149)

The error correction of three-axis magnetometer measurement

  • 摘要: 三轴磁强计测量误差修正对卫星姿态确定和控制具有重要意义。文章针对三轴磁强计测量误差的来源进行理论分析,引入磁场输入引起的常值漂移,建立了三轴磁强计测量误差修正模型,并基于该模型在磁环境模拟器中对Honeywell公司的三轴磁强计(HMR2300R)进行标定。实验结果表明改进模型可以将测量误差控制在50 nT以内,满足低成本敏感器在微小卫星姿态确定中的应用要求。
    Abstract: The error correction of three-axis magnetometer measurement is of great importance to satellite attitude determination and control. In this paper, the error sources of three-axis magnetometer measurement are theoretically analyzed. Considering the case of constant shift caused by the magnetic input, an error correction model is proposed, with which the three-axis magnetometer HMR2300R made by Honeywell is calibrated and tested in a magnetic simulator. The experimental results show that the error of the three-axis magnetometer measurement can be controlled within 50 nT with the proposed method, which can meet the application requirements for low cost sensors in attitude determination and control of micro-satellites.
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出版历程
  • 收稿日期:  2011-02-24
  • 修回日期:  2011-04-13

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