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dc.contributor.authorCottrell, Ronald Gelnn, 1942-
dc.creatorCottrell, Ronald Gelnn, 1942-en_US
dc.date.accessioned2014-06-03T14:49:26Z
dc.date.available2014-06-03T14:49:26Z
dc.date.issued1970en_US
dc.identifier.urihttp://hdl.handle.net/10150/318092
dc.language.isoen_USen_US
dc.publisherThe University of Arizona.en_US
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_US
dc.subjectGuided missiles -- Guidance systems.en_US
dc.subjectProportional navigation.en_US
dc.titleOptimal and suboptimal corrections for proportional navigationen_US
dc.typetexten_US
dc.typeThesis-Reproduction (electronic)en_US
dc.identifier.oclc27203334en_US
thesis.degree.grantorUniversity of Arizonaen_US
thesis.degree.levelmastersen_US
thesis.degree.disciplineAerospace and Mechanical Engineeringen_US
thesis.degree.disciplineGraduate Collegeen_US
thesis.degree.nameM.S.en_US
dc.identifier.bibrecord.b30423909en_US
dc.identifier.callnumberE9791 1970 282en_US
refterms.dateFOA2018-07-01T13:46:17Z


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