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

dc.contributor.author	Trainelli, L.
dc.contributor.author	Croce, A.
dc.contributor.author	Riboldi, C.E.
dc.contributor.author	Possamai, R.
dc.date.accessioned	2018-05-31T09:10:37Z
dc.date.available	2018-05-31T09:10:37Z
dc.date.issued	2015
dc.description.abstract	This 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.other	ERF2015_0120_paper
dc.identifier.uri	http://hdl.handle.net/20.500.11881/3624
dc.language.iso	en
dc.subject.other	Flight Mechanics
dc.title	Trimming a high-fidelity multibody helicopter model for performance and control analysis

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