Rotor state feedback in rotorcraft attitude control

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dc.contributor.authorPanza, S.
dc.contributor.authorLovera, M.
dc.contributor.authorBergamasco, M.
dc.contributor.authorViganò, L.
dc.date.accessioned2018-05-31T09:10:34Z
dc.date.available2018-05-31T09:10:34Z
dc.date.issued2015
dc.description.abstractAn 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.otherERF2015_0066_paper
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3578
dc.language.isoen
dc.subject.otherFlight Mechanics
dc.titleRotor state feedback in rotorcraft attitude control

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