Gust rejection properties of VTOL multirotor aircraft

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dc.contributor.authorWhidborne, James F.
dc.contributor.authorCooke, Alastair K.
dc.date.accessioned2018-01-29T14:41:20Z
dc.date.available2018-01-29T14:41:20Z
dc.date.issued2018-01-11
dc.description.abstractThe effect of rotor aerodynamics on the stability and control of multi-rotor aircraft is explored by analysis of a conceptual planar birotor aircraft. In particular, the effect of rotor tilt on the stability and zero-location is investigated. Furthermore, it is shown that designing the vehicle with outwards rotor tilt potentially results in dramatic improvement in the gust rejection properties of the vehicle.en_UK
dc.identifier.citationWhidborne JF, Cooke AK, Gust rejection properties of VTOL multirotor aircraft, IFAC-PapersOnLine, Volume 50, Issue 2, December 2017, 175-180. Control Conference Africa CCA, 7-8 December 2017, Johannesburg, South Africaen_UK
dc.identifier.issn2405-8963
dc.identifier.urihttp://dx.doi.org/10.1016/j.ifacol.2017.12.032
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/12935
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.subjectUAV controlen_UK
dc.subjectQuadrotorsen_UK
dc.subjectGust rejectionen_UK
dc.subjectStabilityen_UK
dc.subjectNon-minimum phase systemsen_UK
dc.titleGust rejection properties of VTOL multirotor aircraften_UK
dc.typeArticleen_UK

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