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Non Linear Dynamic Inversion Technique

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dc.contributor.authorAranda Almansa, Joaquín
dc.date.accessioned2024-05-20T18:49:28Z
dc.date.available2024-05-20T18:49:28Z
dc.date.issued2007-11-12
dc.description.abstractOver the last two decades or so, control researchers have begun to apply alternative methodologies to flight control design. One alternative is variously called non-linear dynamic inversion or feedback linearization. The purpose of dynamic inversion is to develop a feedback control law that linearizes the plant response to commands. Simple controllers can then be designed. With dynamic inversion, a non-linear control law is designed which globally reduces the dynamics of selected controlled variables to integrators. A closed loop system is then designed to make the controlled variables exhibit specified command responses while satisfying the usual disturbances response and robustness requirements for the overall system and the various physical limitations of the aircraft’s control effectors.es
dc.description.versionversión publicada
dc.identifier.urihttps://hdl.handle.net/20.500.14468/15622
dc.language.isoen
dc.publisherGROUP FOR AERONAUTICAL RESEARCH AND TECHNOLOGY IN EUROPE
dc.relation.centerE.T.S. de Ingeniería Informática
dc.relation.departmentInformática y Automática
dc.rightsAtribución-NoComercial-SinDerivadas 4.0 Internacional
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0
dc.subject.keywordsROBUST
dc.subject.keywordsCONTROL
dc.subject.keywordsTECHNIQUES
dc.subject.keywordsNon Linear
dc.subject.keywordsDynamic
dc.subject.keywordsInversion
dc.subject.keywordsTechnique
dc.titleNon Linear Dynamic Inversion Techniquees
dc.typecapítulo de libroes
dc.typebook parten
dspace.entity.typePublication
relation.isAuthorOfPublication3c2f82d3-b350-435d-9954-9321ab17ea9b
relation.isAuthorOfPublication.latestForDiscovery3c2f82d3-b350-435d-9954-9321ab17ea9b
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