MIMO Input-Output Linearization with Applications for Longitudinal Flight Dynamics

dc.contributor.authorDelgado, Jhon Manuel Portella
dc.contributor.authorGoel, Ankit
dc.date.accessioned2022-06-24T17:38:53Z
dc.date.available2022-06-24T17:38:53Z
dc.date.issued2022-05-12
dc.description.abstractThis paper presents an extension of the input-output linearization method for nonsquare systems with more outputs than inputs. Unlike the square systems and nonsquare systems with fewer outputs than inputs, which can be completely linearized, we consider the problem of linearizing nonsquare systems with more outputs than inputs. In particular, the system is linearized by decomposing the state using a diffeomorphism, which is chosen such that the output of the system is a linear combination of the outputs of integrator chains, and the input of the system is chosen to cancel the nonlinearities using feedback linearization. In the case of nonsquare systems with more outputs than inputs, we observe that the resulting linear system can be stabilized even though it is uncontrollable at all times. This apparent contradiction is due to the switching behavior in the control action. We apply the input-output linearization method to linearize the longitudinal aircraft dynamics and demonstrate asymptotic stability of the closed-loop system despite the switching behavior.en_US
dc.description.urihttps://arxiv.org/abs/2205.06192en_US
dc.format.extent7 pagesen_US
dc.genrejournal articlesen_US
dc.genrepreprintsen_US
dc.identifierdoi:10.13016/m2jx1a-ltwg
dc.identifier.urihttps://doi.org/10.48550/arXiv.2205.06192
dc.identifier.urihttp://hdl.handle.net/11603/25036
dc.language.isoen_USen_US
dc.relation.isAvailableAtThe University of Maryland, Baltimore County (UMBC)
dc.relation.ispartofUMBC Mechanical Engineering Department Collection
dc.relation.ispartofUMBC Faculty Collection
dc.relation.ispartofUMBC Student Collection
dc.rightsThis item is likely protected under Title 17 of the U.S. Copyright Law. Unless on a Creative Commons license, for uses protected by Copyright Law, contact the copyright holder or the author.en_US
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)*
dc.rights.urihttps://creativecommons.org/licenses/by-nc-sa/4.0/*
dc.titleMIMO Input-Output Linearization with Applications for Longitudinal Flight Dynamicsen_US
dc.typeTexten_US
dcterms.creatorhttps://orcid.org/0000-0002-4146-6275en_US

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