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Kernel-based predictive control allocation for a class of thrust vectoring systems with singular points

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dc.contributor.authorNguyen, Tam W.-
dc.contributor.authorHan, Kyoungseok-
dc.contributor.authorHirata, Kenji-
dc.date.accessioned2025-12-22T05:00:30Z-
dc.date.available2025-12-22T05:00:30Z-
dc.date.issued2025-07-
dc.identifier.issn0005-1098-
dc.identifier.issn1873-2836-
dc.identifier.urihttps://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/209970-
dc.description.abstractThis paper considers a class of thrust vectoring systems, which are nonlinear, overactuated, and time-invariant. We assume that the system is composed of two subsystems and there exist singular points around which the linearized system is uncontrollable. Furthermore, we assume that the system is stabilizable through a two-level control allocation. In this particular setting, we cannot do much with the linearized system, and a direct nonlinear control approach must be used to analyze the system stability. Under adequate assumptions and a suitable nonlinear continuous control-allocation law, we can prove uniform asymptotic convergence of the points of equilibrium using Lyapunov input-to-state stability and the small gain theorem. This control allocation, however, requires the design of an allocated mapping and introduces two exogenous inputs. In particular, the closed-loop system is cascaded, and the output of one subsystem is the disturbance of the other, and vice versa. In general, it is difficult to find a closed-form solution for the allocated mapping; it needs to satisfy restrictive conditions, among which Lipschitz continuity to ensure that the disturbances eventually vanish. Additionally, this mapping is in general nontrivial and non-unique. In this paper, we propose a new kernel-based predictive control allocation to substitute the need for designing an analytic mapping, and assess if it can produce a meaningful mapping “on-the-fly” by solving online an optimization problem. The simulations include two examples, which are the manipulation of an object through an unmanned aerial vehicle in three dimensions, and the control of a surface vessel actuated by two azimuthal thrusters.-
dc.format.extent7-
dc.language영어-
dc.language.isoENG-
dc.publisherPergamon Press Ltd.-
dc.titleKernel-based predictive control allocation for a class of thrust vectoring systems with singular points-
dc.typeArticle-
dc.publisher.location영국-
dc.identifier.doi10.1016/j.automatica.2025.112270-
dc.identifier.scopusid2-s2.0-105002122340-
dc.identifier.wosid001480743300001-
dc.identifier.bibliographicCitationAutomatica, v.177, pp 1 - 7-
dc.citation.titleAutomatica-
dc.citation.volume177-
dc.citation.startPage1-
dc.citation.endPage7-
dc.type.docTypeArticle-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.relation.journalResearchAreaAutomation & Control Systems-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryAutomation & Control Systems-
dc.relation.journalWebOfScienceCategoryEngineering, Electrical & Electronic-
dc.subject.keywordPlusUAV-
dc.subject.keywordPlusQUADROTOR-
dc.subject.keywordAuthorControl allocation-
dc.subject.keywordAuthorModel predictive control-
dc.subject.keywordAuthorApplication of nonlinear analysis and design-
dc.identifier.urlhttps://www.sciencedirect.com/science/article/pii/S0005109825001621?via%3Dihub-
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