Near-optimum guidance schemes for abort landing flight in a windshear

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dc.contributor.advisorMiele, Angelo
dc.creatorWang, Jyhshing Jack
dc.date.accessioned2009-06-04T00:04:14Z
dc.date.available2009-06-04T00:04:14Z
dc.date.issued1988
dc.description.abstractIn this thesis, near-optimum guidance schemes for abort landing trajectories in a windshear are investigated. These near-optimum guidance schemes are based on the properties of the optimum trajectories. The survival capability in a severe windshear is studied. The optimal trajectories are used as ideal benchmarks against which the goodness of any guidance scheme can be measured.
dc.format.extent77 p.en_US
dc.format.mimetypeapplication/pdf
dc.identifier.callnoThesis Aero-Astro. 1988 Wang
dc.identifier.citationWang, Jyhshing Jack. "Near-optimum guidance schemes for abort landing flight in a windshear." (1988) Master’s Thesis, Rice University. <a href="https://hdl.handle.net/1911/13326">https://hdl.handle.net/1911/13326</a>.
dc.identifier.urihttps://hdl.handle.net/1911/13326
dc.language.isoeng
dc.rightsCopyright is held by the author, unless otherwise indicated. Permission to reuse, publish, or reproduce the work beyond the bounds of fair use or other exemptions to copyright law must be obtained from the copyright holder.
dc.subjectAerospace engineering
dc.subjectMechanical engineering
dc.titleNear-optimum guidance schemes for abort landing flight in a windshear
dc.typeThesis
dc.type.materialText
thesis.degree.departmentAero-Astronautics
thesis.degree.disciplineEngineering
thesis.degree.grantorRice University
thesis.degree.levelMasters
thesis.degree.nameMaster of Science
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