Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/87641
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dc.contributor.authorWang, Zhenhuaen
dc.contributor.authorShen, Yien
dc.contributor.authorZhang, Xiaoleien
dc.contributor.authorWang, Danweien
dc.date.accessioned2018-12-03T06:59:12Zen
dc.date.accessioned2019-12-06T16:46:15Z-
dc.date.available2018-12-03T06:59:12Zen
dc.date.available2019-12-06T16:46:15Z-
dc.date.issued2014en
dc.identifier.citationWang, Z., Shen, Y., Zhang, X., & Wang, D. (2014). Fault Diagnosis for Satellite Attitude Control Systems With Four Flywheels. Journal of Dynamic Systems, Measurement, and Control, 136(4), 041016-. doi:10.1115/1.4026515en
dc.identifier.issn0022-0434en
dc.identifier.urihttps://hdl.handle.net/10356/87641-
dc.description.abstractThis paper proposes a novel fault diagnosis approach for the satellite attitude control system with flywheel faults. The key contributions include fault estimation by sparse approximation algorithm and diagnosis of multiple faults. In this paper, a Taylor series expansion is used to derive a fault estimation representation. Based on the sparse property of the faults, fault estimation is formulated as a sparse approximation problem and solved using the orthogonal matching pursuit (OMP) algorithm. Simulation results demonstrate the effectiveness of the proposed method.en
dc.language.isoenen
dc.relation.ispartofseriesJournal of Dynamic Systems, Measurement, and Controlen
dc.rights© 2014 American Society of Mechanical Engineers (ASME).en
dc.subjectAttitude Control Systemen
dc.subjectFault Diagnosisen
dc.subjectDRNTU::Engineering::Electrical and electronic engineeringen
dc.titleFault diagnosis for satellite attitude control systems with four flywheelsen
dc.typeJournal Articleen
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen
dc.identifier.doi10.1115/1.4026515en
item.grantfulltextnone-
item.fulltextNo Fulltext-
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