Generalized Targeting Parameters for the Guidance of Aerospace Vehicles

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dc.contributor.authorMcCraney, Richard Marvin
dc.contributor.otherUniversity of Alabama Tuscaloosa
dc.date.accessioned2021-07-20T15:01:49Z
dc.date.available2021-07-20T15:01:49Z
dc.date.issued1968
dc.descriptionElectronic Thesis or Dissertationen_US
dc.description.abstractThis thesis presents the development of the equations necessary to compute the targeting parameters for the iterative guidance mode for all types of space missions. A brief introduction to the iterative guidance mode is presented as well as the derivation and explanation of the necessary equations to compute the targeting parameters. Experimental verification of the equations is also included.en_US
dc.format.extent62 p.
dc.format.mediumelectronic
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://ir.ua.edu/handle/123456789/7980
dc.languageEnglish
dc.language.isoen_US
dc.publisherUniversity of Alabama Libraries
dc.relation.ispartofThe University of Alabama Electronic Theses and Dissertations
dc.rightsAll rights reserved by the author unless otherwise indicated.en_US
dc.titleGeneralized Targeting Parameters for the Guidance of Aerospace Vehiclesen_US
dc.typethesis
dc.typetext
etdms.degree.departmentUniversity of Alabama. Department of Aerospace Engineering and Mechanics
etdms.degree.disciplineAerospace Engineering
etdms.degree.grantorThe University of Alabama
etdms.degree.levelmaster's
etdms.degree.nameM.S.

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