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dc.creatorKoumboulis, F. N.en
dc.creatorSkarpetis, M. G.en
dc.date.accessioned2015-11-23T10:36:12Z
dc.date.available2015-11-23T10:36:12Z
dc.date.issued2001
dc.identifier10.1080/00207720010017599
dc.identifier.issn0020-7721
dc.identifier.urihttp://hdl.handle.net/11615/29816
dc.description.abstractFor the case of a linear time invariant system with nonlinear uncertain structure the problem of robust triangular decoupling with simultaneous robust disturbance rejection (RTDRDR) is studied. The necessary and sufficient conditions for the solution of the RTDRDR problem are established. The general expressions for the feedback matrices solving the problem are derived in analytic form. The resulting closed-loop system, being triangularly decoupled and having no influence from the disturbances to the output, is analytically determined. For the solution of the RTDRDR problem with simultaneous robust stability, sufficient conditions are established. The present results are successfully applied to control a vertical take-off and landing aircraft in hover.en
dc.source.uri<Go to ISI>://WOS:000171018400005
dc.subject4WS CARSen
dc.subjectSYSTEMSen
dc.subjectAutomation & Control Systemsen
dc.subjectComputer Science, Theory & Methodsen
dc.subjectOperations Research & Management Scienceen
dc.titleRobust triangular decoupling with simultaneous robust disturbance rejectionen
dc.typejournalArticleen


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