4.5 Article

Space magnetometer based on an anisotropic magnetoresistive hybrid sensor

Journal

REVIEW OF SCIENTIFIC INSTRUMENTS
Volume 85, Issue 12, Pages -

Publisher

AMER INST PHYSICS
DOI: 10.1063/1.4904702

Keywords

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Funding

  1. UK Science Technology and Facilities Council (STFC) [ST/K001051/1]
  2. ESA under the General Support Technology Programme [4000106430]
  3. Permanent Open Call for Technology Demonstrators [IC-1109-001]
  4. STFC Grant [ST/I505713/1]
  5. STFC [ST/I505713/1, ST/G00725X/1, ST/K001051/1, ST/H002383/1] Funding Source: UKRI
  6. Science and Technology Facilities Council [ST/I505713/1, ST/K001051/1, ST/G00725X/1, ST/H002383/1] Funding Source: researchfish

Ask authors/readers for more resources

We report on the design and development of a low resource, dual sensor vector magnetometer for space science applications on very small spacecraft. It is based on a hybrid device combining an orthogonal triad of commercial anisotropic magnetoresistive (AMR) sensors with a totem pole H-Bridge drive on a ceramic substrate. The drive enables AMR operation in the more sensitive flipped mode and this is achieved without the need for current spike transmission down a sensor harness. The magnetometer has sensitivity of better than 3 nT in a 0-10 Hz band and a total mass of 104 g. Three instruments have been launched as part of the TRIO-CINEMA space weather mission, intercalibration against the International Geomagnetic Reference Field model makes it possible to extract physical signals such as field-aligned current deflections of 20-60 nT within an approximately 45 000 nT ambient field. (C) 2014 AIP Publishing LLC.

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