Dynamic inflow and ground effect in multirotor UAV attitude dynamics

dc.contributor.authorRiccardi, F.
dc.contributor.authorLovera, M.
dc.date.accessioned2020-11-19T15:40:44Z
dc.date.available2020-11-19T15:40:44Z
dc.date.issued2017
dc.description.abstractThis paper deals with the problem of modelling the attitude dynamics of a quadrotor in ground effect. More precisely, dynamic ground effect on the quadrotor pitch attitude dynamics is modeled taking into account the dynamic inflow of the rotors and the simulation results are compared to the experimental ones obtained in previous studies.
dc.identifier.other582_ERF2017
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3823
dc.language.isoen
dc.titleDynamic inflow and ground effect in multirotor UAV attitude dynamics

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