Rotor state feedback in rotorcraft attitude control

dc.contributor.author	Panza, S.
dc.contributor.author	Lovera, M.
dc.contributor.author	Bergamasco, M.
dc.contributor.author	Viganò, L.
dc.date.accessioned	2018-05-31T09:10:34Z
dc.date.available	2018-05-31T09:10:34Z
dc.date.issued	2015
dc.description.abstract	An approach to rotor state feedback attitude control aimed at nominal stability, closed-loop performance, uncertainty robustness and tolerance to rotor state feedback faults is proposed. Structured ??? control based on a reduced linearized FlightLab model, an uncertainty description (changes in mass, altitude, center of mass position, speed) and requirements on the sensitivity functions is used to optimize tunings for given controller structures
dc.identifier.other	ERF2015_0066_paper
dc.identifier.uri	http://hdl.handle.net/20.500.11881/3578
dc.language.iso	en
dc.subject.other	Flight Mechanics
dc.title	Rotor state feedback in rotorcraft attitude control

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