• DocumentCode
    782462
  • Title

    A Magnetic Field Instrunent for the OGO-E Spacecraft

  • Author

    Snare, R.C. ; Benjamin, C.R.

  • Author_Institution
    University of California at Los Angeles Los Angeles, California
  • Volume
    13
  • Issue
    6
  • fYear
    1966
  • Firstpage
    333
  • Lastpage
    340
  • Abstract
    A three-axis, fluxgate magnetometer was selected for flight on the fifth Orbiting Geophysical Observatory. This instrument, along with an electron telescope, will provide data for the study of magnetohydrodynamic waves and other magnetic field structures in space. The magnetometer has sufficient dynamic range to measure magnetic field values from the surface of the earth to apogee. In addition to this wide dynamic range, the instrument provides for a resolution at all field values of 1/16 gamma. This resolution and dynamic range are accomplished by employing a tightly fed-back, closedloop magnetometer and a digital offset field generator in each of the three mutually perpendicular axes. The analog output of each axis is filtered by active filters to prevent frequency aliasing of the signals. The cutoff frequency of these filters is automatically switched to the proper frequency as the spacecraft telemetry data sampling rate is changed. In-flight calibration circuitry provides front-to-back calibration of each magnetometer channel during the flight. Packaging and construction techniques used in this instrument are also discussed.
  • Keywords
    Active filters; Calibration; Cutoff frequency; Dynamic range; Instruments; Magnetic field measurement; Magnetic fields; Magnetic separation; Magnetometers; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/TNS.1996.4324380
  • Filename
    4324380