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dc.contributor.authorSchamel, George C.en_US
dc.date.accessioned2015-07-10T20:00:01Z
dc.date.available2015-07-10T20:00:01Z
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/10919/54412
dc.format.extentxii, 128 leavesen_US
dc.format.mimetypeapplication/pdfen_US
dc.language.isoen_USen_US
dc.publisherVirginia Polytechnic Institute and State Universityen_US
dc.rightsThis Item is protected by copyright and/or related rights. Some uses of this Item may be deemed fair and permitted by law even without permission from the rights holder(s), or the rights holder(s) may have licensed the work for use under certain conditions. For other uses you need to obtain permission from the rights holder(s).en_US
dc.subject.lccLD5655.V856 1989.S397en_US
dc.subject.lcshLarge space structures (Astronautics)en_US
dc.subject.lcshDamping (Mechanics)en_US
dc.titleExperimental and theoretical investigation of optimal control methods with model reductionen_US
dc.typeDissertationen_US
dc.contributor.departmentAerospace Engineeringen_US
dc.description.degreePh. D.en_US
dc.identifier.oclc20438755en_US
thesis.degree.namePh. D.en_US
thesis.degree.leveldoctoralen_US
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen_US
thesis.degree.disciplineAerospace Engineeringen_US
dc.type.dcmitypeTexten_US


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