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dc.contributor.authorQu, Zheng
dc.contributor.authorAnnaswamy, Anuradha
dc.contributor.authorLavretsky, Eugene
dc.date.accessioned2016-03-22T18:16:31Z
dc.date.available2016-03-22T18:16:31Z
dc.date.issued2016-03-22
dc.identifier.urihttp://hdl.handle.net/1721.1/101750
dc.description.abstractA dominant presence of parametric model uncertainties motivates an adaptive approach for control of very flexible aircraft (VFA). This paper proposes an adaptive controller that includes a baseline design based on observers and parameter adaptation based on a closed-loop reference model (CRM), and is applicable for a class of multi-input multi-output (MIMO) plants where number of outputs exceeds number of inputs. In particular, the proposed controller allows the plant to have first-order actuator dynamics and parametric uncertainties in both plant and actuator dynamics. Conditions are delineated under which this controller can guarantee stability and asymptotic reference tracking, and the overall design is validated on a nonlinear VFA model.en_US
dc.description.sponsorshipBoeing Strategic University Initiative.en_US
dc.language.isoen_USen_US
dc.relation.ispartofseriesACC2016 Supplementary;1363
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectAdaptive Controlen_US
dc.subjectActuator Dynamicsen_US
dc.subjectVery Flexible Aircraften_US
dc.titleSupplementary Materials to "Adaptive Output-Feedback Control for A Class of Multi-Input-Multi-Output Plants with Applications to Very Flexible Aircraft"en_US
dc.typeArticleen_US


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