| Literature DB >> 25554336 |
P Brown1, B J Whiteside1, T J Beek1, P Fox1, T S Horbury1, T M Oddy1, M O Archer1, J P Eastwood1, D Sanz-Hernández2, J G Sample3, E Cupido1, H O'Brien1, C M Carr1.
Abstract
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, inter-calibration 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.Entities:
Year: 2014 PMID: 25554336 DOI: 10.1063/1.4904702
Source DB: PubMed Journal: Rev Sci Instrum ISSN: 0034-6748 Impact factor: 1.523