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dc.contributor.authorCapone, Pierluigi-
dc.contributor.authorMantegazza, Paolo-
dc.date.accessioned2018-08-17T09:14:13Z-
dc.date.available2018-08-17T09:14:13Z-
dc.date.issued1995-
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/9130-
dc.description.abstractThe paper develops an indirect adaptive control for a multi-input multi-output active flutter suppression system adopting an identifier based either on an extended Kalman filter, with adaptive adjustment of the metastate covariance, or on a recursive moving block least squares technique. The related control law is designed by using an eigenstructure assignment method. The controller thus obtained is verified through extensive numerical simulations on a time varying aeroservoelastic model excited by widely varying levels of turbulence. The control system is required to adapt both to slow variations of the system operational parameters, e.g. fuel consumption, slow acceleration manoeuvres; and to fast changes, e.g. store release, violent accelerations. The capability to maintain system stability after an actuator malfunction is also verified. The results demonstrate that the extended Kalman filter is superior to the least squares method in identifying the system. However the overall performances of the adaptive controller are quite insensitive to the identification results, so that the lower computational resources and cost required for the implementation of the least squares identifier makes it a better candidate for a practical realisation.de_CH
dc.language.isoende_CH
dc.publisherNational Aerospace Laboratoryde_CH
dc.rightsLicence according to publishing contractde_CH
dc.subjectFlutterde_CH
dc.subjectEstimationde_CH
dc.subjectAdaptivede_CH
dc.subjectControlde_CH
dc.subject.ddc620: Ingenieurwesende_CH
dc.titleAdaptive control of a multi-input multi-output flutter suppression systemde_CH
dc.typeKonferenz: Paperde_CH
dcterms.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitZentrum für Aviatik (ZAV)de_CH
zhaw.publisher.placeAmsterdamde_CH
zhaw.conference.detailsNineteenth European Rotorcraft Forum, Cernobbio, Italy, 14-16 September 1993de_CH
zhaw.funding.euNode_CH
zhaw.originated.zhawNode_CH
zhaw.publication.statuspublishedVersionde_CH
zhaw.publication.reviewEditorial reviewde_CH
zhaw.title.proceedingsNineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993de_CH
zhaw.webfeedFlight Mechanics and Flight Control Systemsde_CH
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Capone, P., & Mantegazza, P. (1995). Adaptive control of a multi-input multi-output flutter suppression system. Nineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993.
Capone, P. and Mantegazza, P. (1995) ‘Adaptive control of a multi-input multi-output flutter suppression system’, in Nineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993. Amsterdam: National Aerospace Laboratory.
P. Capone and P. Mantegazza, “Adaptive control of a multi-input multi-output flutter suppression system,” in Nineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993, 1995.
CAPONE, Pierluigi und Paolo MANTEGAZZA, 1995. Adaptive control of a multi-input multi-output flutter suppression system. In: Nineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993. Conference paper. Amsterdam: National Aerospace Laboratory. 1995
Capone, Pierluigi, and Paolo Mantegazza. 1995. “Adaptive Control of a Multi-Input Multi-Output Flutter Suppression System.” Conference paper. In Nineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993. Amsterdam: National Aerospace Laboratory.
Capone, Pierluigi, and Paolo Mantegazza. “Adaptive Control of a Multi-Input Multi-Output Flutter Suppression System.” Nineteenth European Rotorcraft Forum : Cernobbio (Como), September 14-16, 1993, National Aerospace Laboratory, 1995.


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