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Magnetic Torquers Only Attitude Control of a 3U Cube Satellite

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dc.contributor.authorErturk, Mehmet Fatih
dc.contributor.authorHajiyev, Chingiz
dc.date.accessioned2026-01-24T11:37:13Z
dc.date.issued2022-06-24
dc.description.abstractIn this paper, attitude control of a 3U CubeSat is discussed using magnetic torquers only. As the capabilities of attitude control systems increase, the use of magnetic torques in the CubeSat is becoming more popular. Attitude control using only magnetic torquers has been researched for years and is still a current problem to study. This paper presents the use of an LQR controller for a 3U CubeSat without full gravity gradient stability of the model in a deterministic approach.
dc.description.urihttps://doi.org/10.37394/232014.2022.18.18
dc.identifier.doi10.37394/232014.2022.18.18
dc.identifier.eissn2224-3488
dc.identifier.endpage133
dc.identifier.issn1790-5052
dc.identifier.openairedoi_________::8f7d01b6c1875ee8941ebe6482a96a2d
dc.identifier.startpage128
dc.identifier.urihttps://hdl.handle.net/11527/30911
dc.identifier.volume18
dc.language.isoeng
dc.publisherWorld Scientific and Engineering Academy and Society (WSEAS)
dc.relation.ispartofWSEAS TRANSACTIONS ON SIGNAL PROCESSING
dc.rightsOPEN
dc.titleMagnetic Torquers Only Attitude Control of a 3U Cube Satellite
dc.typeArticle
dspace.entity.typePublication

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