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
Link To Document :
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