Show simple item record

dc.contributor.advisorDavid W. Wallace.en_US
dc.contributor.authorElias, Laila Mireille, 1977-en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2013-10-24T17:29:03Z
dc.date.available2013-10-24T17:29:03Z
dc.date.copyright2001en_US
dc.date.issued2001en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/81563
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.en_US
dc.descriptionIncludes bibliographical references (leaves 113-114).en_US
dc.description.statementofresponsibilityby Laila Mireille Elias.en_US
dc.format.extent114 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleA structurally coupled disturbance analysis method using dynamic mass measurement techniques, with application to spacecraft-reaction wheel systemsen_US
dc.title.alternativeCoupled reaction wheel and spacecraft structural modeling via impedance measurement techniquesen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc49870926en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record