Design and Optimization of a Magnetically Levitated Inductive Reaction Sphere for Spacecraft Attitud...
Design and Optimization of a Magnetically Levitated Inductive Reaction Sphere for Spacecraft Attitude Control
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Basel: MDPI AG
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Language
English
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Basel: MDPI AG
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Contents
The inductive reaction sphere (RS) brings the benefit of simple, economical, and miniaturized design, and it is capable of multi-DOF torque generation. Thus, it is a suitable choice for the angular momentum exchange actuator in attitude control of micro-spacecrafts. To synthesize symmetric distribution of eddy currents and improve the speed and sta...
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Full title
Design and Optimization of a Magnetically Levitated Inductive Reaction Sphere for Spacecraft Attitude Control
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TN_cdi_doaj_primary_oai_doaj_org_article_32446deb22af4258a95eaa8cd8b0cb6a
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_32446deb22af4258a95eaa8cd8b0cb6a
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ISSN
1996-1073
E-ISSN
1996-1073
DOI
10.3390/en12081553
