Method to assess lateral handling qualities of aircraft with wingtip morphing

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dc.contributor.authorDussart, GaƩtan X.
dc.contributor.authorYusuf, Sezsy Y.
dc.contributor.authorPortapas, Vilius
dc.contributor.authorLopez Matos, Guillermo E.
dc.contributor.authorLone, Mohammad M.
dc.date.accessioned2018-02-01T19:47:39Z
dc.date.available2018-02-01T19:47:39Z
dc.date.issued2018-01-13
dc.description.abstractThe impact of in- ight folding wingtip on roll characteristics of aircraft has been studied in the past. In this study, a handling qualities assessment carried out to de-risk further development of such a device. A specialised ight simulation campaign is prepared to evaluate the roll dynamics in di erent morphing con gurations. Various manoeuvres, including the O set Landing Manoeuvre and herein presented Slalom and Alignment Tracking task are used. Cooper Harper Rating scales and ight data analysis are used to collect pilot opinion and validate pilot-in-the-loop simulation results. This example is used to demonstrate the use of the slalom and Alignment Tracking manoeuvre for lateral dynamic assessment.en_UK
dc.identifier.citationGaƩtan X. Dussart, Sezsy Y. Yusuf, Vilius Portapas, et. al., Method to assess lateral handling qualities of aircraft with wingtip morphing. 2018 AIAA Atmospheric Flight Mechanics Conference, 8-12 January 2018, Kissimmee, FL, USA. Paper number AIAA 2018-1015en_UK
dc.identifier.isbn9781624105258
dc.identifier.urihttp://dx.doi.org/10.2514/6.2018-1015
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/12948
dc.language.isoenen_UK
dc.rightsAttribution-NonCommercial 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/*
dc.titleMethod to assess lateral handling qualities of aircraft with wingtip morphingen_UK
dc.typeArticleen_UK

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