Adaptive Control of Uncertain Hamiltonian Multi-Input Multi-Output Systems: with Application to Spacecraft Control

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dc.contributor.authorYoon, H.
dc.contributor.authorAgrawal, B.N.
dc.contributor.corporateSpacecraft Research and Design Center (SRDC)
dc.contributor.departmentMechanical and Aerospace Engineering (MAE)
dc.date.accessioned2013-07-18T19:18:27Z
dc.date.available2013-07-18T19:18:27Z
dc.date.issued2008
dc.descriptionThe article of record as published may be found at http://dx.doi.org/10.1109/ACC.2008.4586947en_US
dc.description.abstractA novel adaptive tracking control law for nonlinear Hamiltonian multi-input–multi-output (MIMO) systems with uncertain parameters in the actuator modeling as well as the inertia and/or the Coriolis and centrifugal terms is developed. The physical properties of the Hamiltonian systems are effectively used in the control design and the stability analysis. The number of the parameter estimates is significantly lowered as compared to the conventional adaptive control methods which are based on the statespace form. The developed control scheme is applied for attitude control of a spacecraft with both the inertia and the actuator uncertainties, and numerical examples show that the controller successfully deals with the unknown inertia/actuator parameters.en_US
dc.identifier.citationAmerican Control Conference, Seattle, WA June 11-13, 2008.
dc.identifier.urihttps://hdl.handle.net/10945/34537
dc.rightsThis publication is a work of the U.S. Government as defined
in Title 17, United States Code, Section 101. As such, it is in the
public domain, and under the provisions of Title 17, United States
Code, Section 105, is not copyrighted in the U.S.en_US
dc.titleAdaptive Control of Uncertain Hamiltonian Multi-Input Multi-Output Systems: with Application to Spacecraft Controlen_US
dc.typeConference Paper
dspace.entity.typePublication
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