Characterization and verification of the optimal feedback gain of a satellite magnetorquer-based attitude control system

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dc.contributor.authorThanayuth Panyalert
dc.contributor.authorShariff Manuthasna
dc.contributor.authorJormpon Chaisakulsurin
dc.contributor.authorTanawish Masri
dc.contributor.authorKritsada Palee
dc.contributor.authorPakawat Prasit
dc.contributor.authorPeerapong Torteeka
dc.contributor.authorPoom Konghuayrob
dc.date.accessioned2026-05-08T19:24:09Z
dc.date.issued2024-8-24
dc.identifier.doi10.1016/j.asr.2024.08.047
dc.identifier.urihttps://dspace.kmitl.ac.th/handle/123456789/19428
dc.publisherAdvances in Space Research
dc.subjectInertial Sensor and Navigation
dc.subjectSpace Satellite Systems and Control
dc.subjectSpacecraft Design and Technology
dc.titleCharacterization and verification of the optimal feedback gain of a satellite magnetorquer-based attitude control system
dc.typeArticle

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