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dc.contributor.authorQuindlen, John Francis
dc.contributor.authorHow, Jonathan P
dc.date.accessioned2018-03-26T14:16:26Z
dc.date.available2018-03-26T14:16:26Z
dc.date.issued2015-01
dc.identifier.isbn978-1-62410-339-1
dc.identifier.urihttp://hdl.handle.net/1721.1/114289
dc.description.abstractConcurrent learning model reference adaptive control has recently been shown to guarantee simultaneous state tracking and parameter estimation error convergence to zero without requiring the restrictive persistency of excitation condition of other adaptive methods. This simultaneous convergence drastically improves the transient performance of the adaptive system since the true model is learned, but prior results were limited to systems with full state feedback. This paper presents an output feedback form of the concurrent learning controller for a novel extension to partial state feedback systems. The approach modifies a baseline LQG/LTR adaptive law with a recorded data stack of output and state estimate vectors. This maintains the guaranteed stability and boundedness of the baseline adaptive method, while improving output tracking error response. Simulations of exible aircraft dynamics demonstrate the improvement of the concurrent learning system over a baseline output feedback adaptive method.en_US
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_US
dc.relation.isversionofhttps://doi.org/10.2514/6.2015-0607en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceMIT Web Domainen_US
dc.titleOutput feedback concurrent learning model reference adaptive controlen_US
dc.typeArticleen_US
dc.identifier.citationJohn F. Quindlen et al. "Output Feedback Concurrent Learning Model Reference Adaptive Control", AIAA Guidance, Navigation, and Control Conference, 2015 January 5-9, Kissimmee, Florida, USA, American Institute of Aeronautics and Astronautics, 2015 © 2015 American Institute of Aeronautics and Astronauticsen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.mitauthorQuindlen, John Francis
dc.contributor.mitauthorHow, Jonathan P
dc.relation.journalAIAA Guidance, Navigation, and Control Conferenceen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dc.date.updated2018-03-21T18:18:26Z
dspace.orderedauthorsQuindlen, John F.; Chowdhary, Girish; How, Jonathan P.en_US
dspace.embargo.termsNen_US
dc.identifier.orcidhttps://orcid.org/0000-0002-0464-4108
dc.identifier.orcidhttps://orcid.org/0000-0001-8576-1930
mit.licenseOPEN_ACCESS_POLICYen_US


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