dc.contributor.authorShen, Qiang
dc.contributor.authorWang, Danwei
dc.contributor.authorZhu, Senqiang
dc.contributor.authorPoh, Eng Kee
dc.date.accessioned2015-09-04T03:40:40Z
dc.date.available2015-09-04T03:40:40Z
dc.date.copyright2015en_US
dc.date.issued2015
dc.identifier.citationQiang, S., Wang, D., Zhu, S., & Poh, E. K. (2015). Integral-type sliding mode fault-tolerant control for attitude stabilization of spacecraft. IEEE Transactions on Control Systems Technology, 23(3), 1131-1138.en_US
dc.identifier.issn1063-6536en_US
dc.identifier.urihttp://hdl.handle.net/10220/38578
dc.description.abstractTwo fault-tolerant control (FTC) schemes for spacecraft attitude stabilization with external disturbances are proposed in this brief. The approach is based on integral-type sliding mode control strategy to compensate for actuator faults without controller reconfiguration. First, a basic integral-type sliding mode FTC scheme is designed so that sliding manifold can be maintained from the very beginning. Once the system enters the sliding mode, the dynamics of the closed-loop system with actuator fault is identical to that of the nominal healthy system. Second, the integral-type sliding mode fault-tolerant controller is incorporated with adaptive technique to accommodate actuator faults so that the required boundary information can be relaxed. The effectiveness of the proposed schemes against actuator faults is demonstrated in simulation.en_US
dc.language.isoenen_US
dc.relation.ispartofseriesIEEE transactions on control systems technologyen_US
dc.rights© 2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. The published version is available at: [http://dx.doi.org/10.1109/TCST.2014.2354260].en_US
dc.titleIntegral-type sliding mode fault-tolerant control for attitude stabilization of spacecraften_US
dc.typeJournal Article
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen_US
dc.identifier.doihttp://dx.doi.org/10.1109/TCST.2014.2354260
dc.description.versionAccepted versionen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record