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Development of examination and correction system for satellite-borne fluxgate magnetometer

Research Project

Project/Area Number 02640327
Research Category

Grant-in-Aid for General Scientific Research (C)

Allocation TypeSingle-year Grants
Research Field Space and upper atmospheric physics
Research InstitutionTokai University

Principal Investigator

TOHYAMA Fumio  Tokai Univ. Faculty of Engineering, Professor, 工学部, 教授 (40056156)

Project Period (FY) 1990 – 1991
Project Status Completed (Fiscal Year 1991)
Budget Amount *help
¥1,700,000 (Direct Cost: ¥1,700,000)
Fiscal Year 1991: ¥300,000 (Direct Cost: ¥300,000)
Fiscal Year 1990: ¥1,400,000 (Direct Cost: ¥1,400,000)
KeywordsFluxgate magnetometer / Magnetometry / Calibration of magnetometer / Magnetic offset / Helmholtz coil / Geomagnetic field / ヘルムホルツ・コイル / 回転磁場制御
Research Abstract

For the geomagnetic field measurement by use of rocket or satellite-borne fluxgate magnetometer, correction of flight data and calibration on the ground are very impotant. I have developed an examination and correction system for magnetometer that was composed of a tri-axial Helmholtz coil, control computer, multiple power suplies, data recorder and analysis programs. A test magnetometer is fixed in the center of the Helmholtz coil. If institution value of satellite motion are given to the computer, the magnetometer data shows simulant changes correspondence to the satellite motion which are spin frequency, precessional angle and period. The computer gives commands to multiple power supplies and AC current is controled an amplitude, phase and frequency in the tri-axial coil. As a result of. the examinaction, good simulant output data is obtained for a test magnetometer. The output data is acquired by data recorder and is transmitted to the host computer. By the analysis programs, the correction parameters are determined. The parameters are precise angles between non-rectanglar sensor axes, sensor sensitivity for magnetic intensity and magnetic offset field from satellite body or instruments. The programs are composed of the least square method and coordinate transformation between the non-rectanglar and rectanglar system. The correction was estimated by use of the "AKEBONO" scientific satellite data. The tri-axial fluxgate magnetometer sensors boarded on the 5m-extension mast and 32Hz-sampled data of geomagnetic field vector were obtained. By use of the correction system, itwas able to determine that each sensor angle were 89.902-89.962 degrees and magnetic offset were 22-189 nT. In consequence, it is confirmed that the examination coil equipment and the analysis programs are very effective for satellite-borne magnetometer correction.

Report

(3 results)
  • 1991 Annual Research Report   Final Research Report Summary
  • 1990 Annual Research Report
  • Research Products

    (6 results)

All Other

All Publications (6 results)

  • [Publications] 遠山 文雄: "科学衛星「あけぼの」搭載用磁力計デ-タの高精度解析法" 東海大学工学部紀要.

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1991 Final Research Report Summary
  • [Publications] 遠山 文雄: "衛星搭載用フラックスゲ-ト磁力計検定装置の開発" 東海大学工学部紀要.

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1991 Final Research Report Summary
  • [Publications] F. Tohyama: "High Precision Analysis for Geomagnetic Field Data of the "AkEBONO" Satellite." Proceedings of the Faculty of Engineering of Tokai Univ.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1991 Final Research Report Summary
  • [Publications] F. Tohyama: "Development of Examination System for Satellite-borne Fluxgate Magnetometer." Proceedings of the Faculty of Engineering of Tokai Univ.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1991 Final Research Report Summary
  • [Publications] 遠山 文雄: "科学衛星「あけぼの」搭載用磁力計デ-タの高精度解析法" 東海大学 工学部紀要.

    • Related Report
      1991 Annual Research Report
  • [Publications] 遠山 文雄: "衛星搭載用フラックスゲ-ト磁力計検定装置の開発" 東海大学 工学部紀要.

    • Related Report
      1991 Annual Research Report

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Published: 1990-04-01   Modified: 2016-04-21  

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