SIMULTANEOUS ATTITUDE AND MANIPULATOR CONTROL FOR DETUMBLING COUPLED SATELLITES WITH APPENDAGES

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dc.contributor.advisorAkin, David Len_US
dc.contributor.authorDillow, Barrett Edwarden_US
dc.contributor.departmentAerospace Engineeringen_US
dc.contributor.publisherDigital Repository at the University of Marylanden_US
dc.contributor.publisherUniversity of Maryland (College Park, Md.)en_US
dc.date.accessioned2020-02-01T06:31:06Z
dc.date.available2020-02-01T06:31:06Z
dc.date.issued2019en_US
dc.description.abstractSatellite servicing is of increasing interest in industry. Thousands of satellites, functional and not, are tumbling and would likely need to have their attitude stabilized for servicing or orbital change maneuvers. Further, a well-studied method for achieving capture between a servicer and a client satellite is with a robotic manipulator. This research presents a set of algorithms to achieve attitude stabilisation while reducing client appendage motion. A nonlinear quaternion feedback controller is presented; its stability proven and its utility discussed. A method of client appendage mode motion is presented. Finally a manipulator control algorithm to reduce client appendage motion is presented. These methods can be employed to increase the potential number of non-cooperative serviceable satellites.en_US
dc.identifierhttps://doi.org/10.13016/ikwt-433t
dc.identifier.urihttp://hdl.handle.net/1903/25358
dc.language.isoenen_US
dc.subject.pqcontrolledAerospace engineeringen_US
dc.subject.pquncontrollednonlinear controlen_US
dc.subject.pquncontrolledrobotic manipulatoren_US
dc.subject.pquncontrolledsatellite servicingen_US
dc.titleSIMULTANEOUS ATTITUDE AND MANIPULATOR CONTROL FOR DETUMBLING COUPLED SATELLITES WITH APPENDAGESen_US
dc.typeDissertationen_US

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