Sliding mode control with system constraints for aircraft engines

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dc.contributor.authorYang, Shu-Bo
dc.contributor.authorWang, Xi
dc.contributor.authorWang, Hao-Nan
dc.contributor.authorLi, Yi-Guang
dc.date.accessioned2020-07-28T15:15:12Z
dc.date.available2020-07-28T15:15:12Z
dc.date.issued2019-09-19
dc.description.abstractThis paper proposes a constraint-tolerant design with sliding mode strategy to improve the stability of aircraft engine control. To handle the difficulties associated with the high-frequency switching laws, merely attenuating the chattering is far from satisfactory. System constraints on input, output, and input rate should be addressed in the design process. For a sort of uncertain nonlinear systems subjected to the constraints, sliding mode regulators are designed using Lyapunov analysis. A turbofan engine is adopted for simulation, which shows that the methodology developed in this paper can handle the speed tracking and limit protection problem in a stable fashion, despite the negative influence posed by the system constraints.en_UK
dc.identifier.citationYang S-B, Wang X, Wang H-N, et al., (2020) Sliding mode control with system constraints for aircraft engines. ISA Transactions, Volume 98, March 2020, pp. 1-10en_UK
dc.identifier.issn0019-0578
dc.identifier.urihttps://doi.org/10.1016/j.isatra.2019.08.020
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/15604
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectTurbofan engineen_UK
dc.subjectSystem uncertaintiesen_UK
dc.subjectSystem constraintsen_UK
dc.subjectSliding mode controlen_UK
dc.subjectLimit protectionen_UK
dc.subjectSpeed trackingen_UK
dc.subjectAircraft engine controlen_UK
dc.titleSliding mode control with system constraints for aircraft enginesen_UK
dc.typeArticleen_UK

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