Flight evaluation of a sliding mode online control allocation scheme for fault tolerant control

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dc.contributor.authorChen, Lejun
dc.contributor.authorEdwards, Christopher
dc.contributor.authorAlwi, Halim
dc.contributor.authorSato, Masayuki
dc.date.accessioned2021-02-03T12:02:01Z
dc.date.available2021-02-03T12:02:01Z
dc.date.issued2020-01-21
dc.description.abstractThis paper develops a sliding mode fault tolerant control scheme based on a Linear Parameter Varying (LPV) system representation of the plant. The scheme includes a control allocation component, which is capable of utilizing the available healthy actuators in the face of actuator faults/failures, in an effort to retain close to nominal fault free performance. The proposed scheme is validated using the Japan Aerospace Exploration Agency’s Multi-Purpose Aviation Laboratory (MuPAL-α" role="presentation">) research aircraft. The flight test results demonstrate good lateral-directional state tracking performance with no visible performance degradation in the presence of rudder and aileron faults.en_UK
dc.identifier.citationChen L, Edwards C, Alwi H, Sato M. (2020) Flight evaluation of a sliding mode online control allocation scheme for fault tolerant control. Automatica, Volume 114, April 2020, Article No. 108829.en_UK
dc.identifier.issn0005-1098
dc.identifier.urihttps://doi.org/10.1016/j.automatica.2020.108829
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/16293
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectFlight testen_UK
dc.subjectFault tolerant controlen_UK
dc.subjectControl allocationen_UK
dc.subjectSliding mode controlen_UK
dc.titleFlight evaluation of a sliding mode online control allocation scheme for fault tolerant controlen_UK
dc.typeArticleen_UK

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