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Satellite Magnetic Attitude Control in Sun-Safe Mode Using Control Lyapunov Function

dc.rights.licenseopenen_US
dc.contributor.authorYANG, Sen
dc.contributor.authorWANG, Zhenhua
dc.contributor.authorPAN, Xiaodong
dc.contributor.authorLI, Deting
hal.structure.identifierLaboratoire de l'intégration, du matériau au système [IMS]
dc.contributor.authorZOLGHADRI, Ali
dc.date.accessioned2025-11-17T10:49:03Z
dc.date.available2025-11-17T10:49:03Z
dc.date.issued2025-04
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/207940
dc.description.abstractEnThe sun-safe mode is employed to restore the satellite to normal operating conditions in the event of a serious attitude control malfunction. In this article, a fully magnetic attitude controller based on control Lyapunov function (CLF) is proposed. This approach allows the satellite to maintain sun-pointing on the target axis while slowly rotating around this axis, thereby ensuring the satellite's stability and providing a reliable energy supply. First, an affine nonlinear system is constructed based on sun vector dynamics and attitude dynamics, and an appropriate magnetic control law is developed using a CLF to solve the stability problem of this system. Then, the magnetic control law is proven to achieve asymptotic stability without restrictive assumptions on the satellite inertia matrix. Compared with state-of-the-art magnetic control methods for sun-safe mode, the proposed method has a wider application scope and better control performance, as demonstrated by the simulation results. Finally, hardware-in-the-loop experimental results substantiate that the proposed method is both applicable and effective.
dc.language.isoENen_US
dc.subject.enControl Lyapunov function (CLF)
dc.subject.enMagnetic control
dc.subject.enSun-pointing
dc.subject.enSun-safe mode
dc.title.enSatellite Magnetic Attitude Control in Sun-Safe Mode Using Control Lyapunov Function
dc.typeArticle de revueen_US
dc.identifier.doi10.1109/taes.2024.3509386en_US
dc.subject.halSciences de l'ingénieur [physics]en_US
bordeaux.journalIEEE Transactions on Aerospace and Electronic Systemsen_US
bordeaux.page4658-4668en_US
bordeaux.volume61en_US
bordeaux.hal.laboratoriesIMS : Laboratoire de l'Intégration du Matériau au Système - UMR 5218en_US
bordeaux.issue2en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionBordeaux INPen_US
bordeaux.institutionCNRSen_US
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
bordeaux.import.sourcecrossref
hal.popularnonen_US
hal.audienceInternationaleen_US
hal.update-error.statusnewSubmission
hal.exporttrue
workflow.import.sourcecrossref
dc.rights.ccPas de Licence CCen_US
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