Trimming a high-fidelity multibody helicopter model for performance and control analysis

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dc.contributor.authorTrainelli, L.
dc.contributor.authorCroce, A.
dc.contributor.authorRiboldi, C.E.
dc.contributor.authorPossamai, R.
dc.date.accessioned2018-05-31T09:10:37Z
dc.date.available2018-05-31T09:10:37Z
dc.date.issued2015
dc.description.abstractThis paper brings forward the study of the dynamic behaviour of a novel lightweight helicopter featuring an innovative gimballed two-bladed main rotor. First, previous results for the isolated main rotor are extended for the case of free-coning under cyclic pitch perturbations and longitudinal gusts. Subsequently, the complete helicopter is modelled and a simple control system is derived and applied to steer the helicopter to steady hover and straight flight conditions, showing good characteristics also under gust perturbations.
dc.identifier.otherERF2015_0120_paper
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3624
dc.language.isoen
dc.subject.otherFlight Mechanics
dc.titleTrimming a high-fidelity multibody helicopter model for performance and control analysis

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