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dc.contributor.authorEarhart, Leroy Keith, 1942-
dc.creatorEarhart, Leroy Keith, 1942-en
dc.date.accessioned2015-04-01T13:33:43Zen
dc.date.available2015-04-01T13:33:43Zen
dc.date.issued1968en
dc.identifier.urihttp://hdl.handle.net/10150/347641en
dc.language.isoen_USen
dc.publisherThe University of Arizona.en
dc.rightsCopyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author.en
dc.subjectSpace vehicles -- Guidance systems.en
dc.subjectStability of space vehicles.en
dc.subjectSatellite launching ships.en
dc.titleAnalysis and synthesis of flight control systems for large launch vehiclesen
dc.typetexten
dc.typeThesis-Reproduction (electronic)en
dc.identifier.oclc29970114en
thesis.degree.grantorUniversity of Arizonaen
thesis.degree.levelmastersen
thesis.degree.disciplineGraduate Collegeen
thesis.degree.nameM.S.en
dc.description.noteThis item was digitized from a paper original. If you need higher-resolution images for any content in this item, please contact us at repository@u.library.arizona.edu.en
dc.identifier.bibrecord.b31397670en
dc.identifier.callnumberE9791 1968 350en
dc.description.admin-noteOriginal file replaced with corrected file March 2023.
refterms.dateFOA2018-06-17T05:00:36Z


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