• DocumentCode
    1124619
  • Title

    ATS-6 UCLA Fluxgate Magnetometer

  • Author

    Mcpherron, R.L. ; Coleman, P.J., Jr. ; Snare, R.C.

  • Author_Institution
    Institute of Geophysics and Planetary Physics, University of California, Los Angeles, Calif. 90024
  • Issue
    6
  • fYear
    1975
  • Firstpage
    1110
  • Lastpage
    1117
  • Abstract
    A summary of the design of the University of California at Los Angeles´ fluxgate magnetometer is presented. Instrument noise in the bandwidth 0.001 to 1.0 Hz is of order 85 my. The DC field of the spacecraft transverse to the Earth-pointing axis is Sx = 1.0 ±2.1¿, SY = -2.4 ± 1.3¿. The spacecraft field parallel to this axis is less than 5¿. The small spacecraft field has made possible studies of the macroscopic field not previously possible at synchronous orbit. At the 96° west longitude of Applications Technology Satellite-6 (ATS-6), the Earth´s field is typically inclined 300 to the dipole axis at local noon. Most perturbations of the field are due to substorms. These consist of a rotation in the meridian to a more radial field followed by a subsequent rotation back. The rotation back is normally accompanied by transient variations in the azimuthal field. The exact timing of these perturbations is a function of satellite location and the details of substorm development.
  • Keywords
    Geophysics; Instruments; Magnetic properties; Magnetic sensors; Magnetometers; Magnetosphere; Monitoring; Satellites; Sensor arrays; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1975.308162
  • Filename
    4101537