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dc.contributor.authorStewart, P
dc.contributor.authorGladwin, D
dc.contributor.authorParr, M
dc.contributor.authorStewart, J
dc.date.accessioned2019-02-08T14:22:57Z
dc.date.available2019-02-08T14:22:57Z
dc.date.issued2009-11-05
dc.identifier.citationStewart, P., Gladwin, D., Parr, M. and Stewart, J., (2010). 'Multi-objective evolutionary—fuzzy augmented flight control for an F16 aircraft'. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 224(3), pp.293-309. DOI: 10.1243/09544100JAERO610en_US
dc.identifier.issn0954-4100
dc.identifier.issn2041-3025
dc.identifier.doi10.1243/09544100JAERO610
dc.identifier.urihttp://hdl.handle.net/10545/623488
dc.description.abstractIn this article, the multi-objective design of a fuzzy logic augmented flight controller for a high performance fighter jet (the Lockheed-Martin F16) is described. A fuzzy logic controller is designed and its membership functions tuned by genetic algorithms in order to design a roll, pitch, and yaw flight controller with enhanced manoeuverability which still retains safety critical operation when combined with a standard inner-loop stabilizing controller. The controller is assessed in terms of pilot effort and thus reduction of pilot fatigue. The controller is incorporated into a six degree of freedom motion base real-time flight simulator, and flight tested by a qualified pilot instructor.en_US
dc.description.sponsorshipUnited States Air Force European Office of Aeronautical Research and Developmenten_US
dc.language.isoenen_US
dc.relation.urlhttp://journals.sagepub.com/doi/10.1243/09544100JAERO610en_US
dc.relation.urlhttp://eprints.lincoln.ac.uk/2226/en
dc.rightsAttribution-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nd/3.0/us/*
dc.subjectFuzzy Control systems, Genetic Algorithms, F16 fighter, aircraft flight control compensationen_US
dc.titleMulti-objective evolutionary—fuzzy augmented flight control for an F16 aircraften_US
dc.typeArticleen_US
dc.contributor.departmentUniversity of Sheffielden_US
dc.source.journaltitleProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
dc.source.volume224
dc.source.issue3
dc.source.beginpage293
dc.source.endpage309


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Except where otherwise noted, this item's license is described as Attribution-NoDerivs 3.0 United States