Please use this identifier to cite or link to this item: https://doi.org/10.1016/j.mechatronics.2013.07.004
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dc.titleA bumpless hybrid supervisory control algorithm for the formation of unmanned helicopters
dc.contributor.authorKarimoddini, A.
dc.contributor.authorLin, H.
dc.contributor.authorChen, B.M.
dc.contributor.authorLee, T.H.
dc.date.accessioned2014-04-24T07:18:52Z
dc.date.available2014-04-24T07:18:52Z
dc.date.issued2013-09
dc.identifier.citationKarimoddini, A., Lin, H., Chen, B.M., Lee, T.H. (2013-09). A bumpless hybrid supervisory control algorithm for the formation of unmanned helicopters. Mechatronics 23 (6) : 677-688. ScholarBank@NUS Repository. https://doi.org/10.1016/j.mechatronics.2013.07.004
dc.identifier.issn09574158
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/50837
dc.description.abstractThis paper presents a bumpless hybrid supervisory control scheme for the formation of unmanned helicopters. The approach is based on the polar partitioning of the space, from which a finite bisimilar quotient transition system of the original continuous variable control system is obtained. Then, to implement the designed hybrid supervisory control algorithm, a hierarchical control structure is introduced with a discrete supervisor on the top layer that is connected to the regulation layer via an interface layer. Transiting over the partitioned space may cause jumps on the generated control signal which is harmful for a real flight system. Hence, a smooth control mechanism is introduced that has no jump when the system's trajectory transits from one region to its adjacent region while preserving the bisimulation relation between the abstract model and the original partitioned system. Several actual flight tests have been conducted to verify the algorithm and the control performance. © 2013 Elsevier Ltd. All rights reserved.
dc.description.urihttp://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.1016/j.mechatronics.2013.07.004
dc.sourceScopus
dc.subjectFormation control
dc.subjectHybrid supervisory control
dc.subjectImplementation issues
dc.subjectUnmanned aerial vehicles (UAVs)
dc.typeArticle
dc.contributor.departmentELECTRICAL & COMPUTER ENGINEERING
dc.description.doi10.1016/j.mechatronics.2013.07.004
dc.description.sourcetitleMechatronics
dc.description.volume23
dc.description.issue6
dc.description.page677-688
dc.description.codenMECHE
dc.identifier.isiut000324719800014
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