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dc.contributor.authorSchlanbusch, Rune
dc.contributor.authorKristiansen, Raymond
dc.date.accessioned2022-06-29T08:38:18Z
dc.date.available2022-06-29T08:38:18Z
dc.date.issued2013
dc.description.abstractWe address the problem of state feedback translational motion control of a spacecraft formation through a modified sliding surface controller using variable gains and I^2 action for disturbance rejection. The exponential varying gains ensure faster convergence of the state trajectories during attitude maneuver while keeping the gains small (and the system less stiff) for station keeping. Integral action is introduced for rejection of disturbances with a constant nonzero mean such as aerodynamic drag. A direct consequence is a drop in energy consumption when affected by sensor noise and a decrease in size of the error states residual when operating close to the equilibrium point. A large number of simulation results are presented to show the control performance.en_US
dc.identifier.citationSchlanbusch R, Kristiansen R. Control of Spacecraft Formation with Disturbance Rejection and Exponential Gains. Modeling, Identification and Control. 2013;34(1):11-18en_US
dc.identifier.cristinIDFRIDAID 1040011
dc.identifier.doi10.4173/mic.2013.1.2
dc.identifier.issn0332-7353
dc.identifier.issn1890-1328
dc.identifier.urihttps://hdl.handle.net/10037/25647
dc.language.isoengen_US
dc.publisherNorwegian Society of Automatic Controlen_US
dc.relation.journalModeling, Identification and Control
dc.rights.accessRightsopenAccessen_US
dc.rights.holderCopyright 2013 Norwegian Society of Automatic Controlen_US
dc.titleControl of Spacecraft Formation with Disturbance Rejection and Exponential Gainsen_US
dc.type.versionpublishedVersionen_US
dc.typeJournal articleen_US
dc.typeTidsskriftartikkelen_US
dc.typePeer revieweden_US


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