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dc.contributor.authorIshihara, Teruo, 1927-*
dc.creatorIshihara, Teruo, 1927-en_US
dc.date.accessioned2013-05-02T09:43:30Z
dc.date.available2013-05-02T09:43:30Z
dc.date.issued1969en_US
dc.identifier.urihttp://hdl.handle.net/10150/287949
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.subjectSpace trajectories.en_US
dc.subjectFeedback control systems -- Mathematical models.en_US
dc.titleGENERATION OF SUBOPTIMAL, CLOSED LOOP GUIDANCE FOR MINIMUM TIME AIRCRAFT TRAJECTORIESen_US
dc.typetexten_US
dc.typeDissertation-Reproduction (electronic)en_US
dc.identifier.oclc28096440en_US
thesis.degree.grantorUniversity of Arizonaen_US
thesis.degree.leveldoctoralen_US
dc.identifier.proquest6918336en_US
thesis.degree.disciplineGraduate Collegeen_US
thesis.degree.disciplineAerospace and Mechanical Engineeringen_US
thesis.degree.namePh.D.en_US
dc.identifier.bibrecord.b28061251en_US
refterms.dateFOA2018-06-06T05:18:33Z


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