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Minimization of nanosatellite low frequency magnetic fields
KTH, School of Engineering Sciences (SCI), Mechanics, Structural Mechanics.
2016 (English)In: Review of Scientific Instruments, ISSN 0034-6748, E-ISSN 1089-7623, Vol. 87, no 3, 034705Article in journal (Refereed) PublishedText
Abstract [en]

Small weight and dimensions of the micro- and nanosatellites constrain researchers to place electromagnetic sensors on short booms or on the satellite body. Therefore the electromagnetic cleanliness of such satellites becomes a central question. This paper describes the theoretical base and practical techniques for determining the parameters of DC and very low frequency magnetic interference sources. One of such sources is satellite magnetization, the reduction of which improves the accuracy and stability of the attitude control system. We present design solutions for magnetically clean spacecraft, testing equipment, and technology for magnetic moment measurements, which are more convenient, efficient, and accurate than the conventional ones. (C) 2016 AIP Publishing LLC.

Place, publisher, year, edition, pages
2016. Vol. 87, no 3, 034705
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:kth:diva-186014DOI: 10.1063/1.4943667ISI: 000373713300051PubMedID: 27036801ScopusID: 2-s2.0-84962290773OAI: oai:DiVA.org:kth-186014DiVA: diva2:926239
Note

QC 20160504

Available from: 2016-05-04 Created: 2016-04-29 Last updated: 2016-05-04Bibliographically approved

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Belyayev, S. M.
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