Show simple item record

dc.contributor.authorKhan, Said
dc.contributor.authorBendoukha, Samir
dc.contributor.authorNaeem, Wasif
dc.contributor.authorIqbal, Jamshed
dc.date.accessioned2019-10-15T06:45:45Z
dc.date.available2019-10-15T06:45:45Z
dc.date.issued2019
dc.identifier.citationAdvances in electrical and electronic engineering. 2019, vol. 17, no. 3, p. 275-284 : ill.cs
dc.identifier.issn1336-1376
dc.identifier.issn1804-3119
dc.identifier.urihttp://hdl.handle.net/10084/138844
dc.description.abstractIn this paper, an enhanced Integral Sliding Mode-based Linear Quadratic Gaussian (ISM-LQG) controller has been proposed and verified in real-time on a Twin Rotor multi-input-multi-output MIMO System (TRMS). A TRMS serves as a suitable laboratory-based platform to evaluate the performance of control algorithms for complex Unmanned Aerial Vehicle (UAV) systems such as rotocraft. In the proposed scheme, an ISM enhancement to an LQG has been introduced, which attempts to overcome modelling inaccuracies and uncertainties. The novelty of the proposed control law lies in hybridizing a robust control approach with an optimal control law to achieve improved performance. Experimental results on the TRMS demonstrate that the ISM-LQG strategy significantly improves the tracking performance of the TRMS pitch and hence confirm the applicability and efficiency of the proposed scheme.cs
dc.language.isoencs
dc.publisherVysoká škola báňská - Technická univerzita Ostravacs
dc.relation.ispartofseriesAdvances in electrical and electronic engineeringcs
dc.relation.urihttp://dx.doi.org/10.15598/aeee.v17i3.3031cs
dc.rights© Vysoká škola báňská - Technická univerzita Ostrava
dc.rightsAttribution-NoDerivatives 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nd/4.0/*
dc.subjectexperimental set-upcs
dc.subjectIntegral Sliding Mode controlcs
dc.subjectLinear Quadrature Gaussiancs
dc.subjectoptimal dynamic controlcs
dc.subjectTwin rotor MIMO systemcs
dc.titleExperimental Validation of an Integral Sliding Mode-Based LQG for the Pitch Control of a UAV-mimicking Platformcs
dc.typearticlecs
dc.identifier.doi10.15598/aeee.v17i3.3031
dc.rights.accessopenAccesscs
dc.type.versionpublishedVersioncs
dc.type.statusPeer-reviewedcs


Files in this item

This item appears in the following Collection(s)

Show simple item record

© Vysoká škola báňská - Technická univerzita Ostrava
Except where otherwise noted, this item's license is described as © Vysoká škola báňská - Technická univerzita Ostrava