Control for novel 3-DOF flight testing in a wind tunnel

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dc.contributor.authorIshola, Ademayowa A.
dc.contributor.authorWhidborne, James F.
dc.contributor.authorKasula, Pavithra
dc.date.accessioned2024-06-05T09:58:27Z
dc.date.available2024-06-05T09:58:27Z
dc.date.issued2024-05-22
dc.description.abstractA long standing ambition in the aerospace industry is to flight test aircraft in wind tunnels. We propose a robotic manipulator system that can be operated with an aircraft wind tunnel model that replicates the longitudinal dynamics of the aircraft in free flight. A nonlinear aircraft-manipulator dynamics model developed with the Euler-Lagrange method is combined with the inverse kinematics to produce the relative joint angles for the robot manipulator to reproduce free flight trajectories in the wind tunnel working section. Simple PI control is used for the manipulator joint control to replicate the translational degrees of freedom, whilst the aircraft pitch is controlled via the aircraft elevator. The proposed scheme is tested in simulation and the results demonstrate the effectiveness of the proposed scheme.en_UK
dc.identifier.citationIshola AA, Whidborne JF, Kasula P. (2024) Control for novel 3-DOF flight testing in a wind tunnel. In: 2024 UKACC, 14th International Conference on Control (CONTROL), 10-12 April 2024, pp. 321-322en_UK
dc.identifier.eisbn979-8-3503-7426-1
dc.identifier.eissn2766-6522
dc.identifier.urihttps://doi.org/10.1109/CONTROL60310.2024.10531845
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/21950
dc.language.isoen_UKen_UK
dc.publisherIEEEen_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectWind tunnelsen_UK
dc.subjectAtmospheric modelingen_UK
dc.subjectAerodynamicsen_UK
dc.subjectNonlinear dynamical systemsen_UK
dc.subjectTrajectoryen_UK
dc.subjectAircraften_UK
dc.subjectSurgesen_UK
dc.titleControl for novel 3-DOF flight testing in a wind tunnelen_UK
dc.typeConference paperen_UK

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