Closed form guidance laws for intercepting moving targets

dc.contributor.advisorO'Malley, Marcia K.en_US
dc.creatorBartley, Christopher S.en_US
dc.date.accessioned2009-06-04T06:51:42Zen_US
dc.date.available2009-06-04T06:51:42Zen_US
dc.date.issued2004en_US
dc.description.abstractA family of air-to-surface guidance laws designed to intercept moving targets has been developed. They include the effect of gravity, as well as constraints on the terminal flight path and heading angle, and are designed for tracking moving targets. These guidance laws yield equations for the commanded accelerations. They are based firmly on optimal control theory and meet the first and second variation necessary conditions that originate from Pontryagin's Minimum Principle. In addition, these solutions also meet the second variation sufficient conditions for a minimum. They have been evaluated in six degree of freedom simulations. The results show that they perform as designed, even for airframes which are rather sluggish.en_US
dc.format.extent110 p.en_US
dc.format.mimetypeapplication/pdfen_US
dc.identifier.callnoTHESIS M.E. 2004 BARTLEYen_US
dc.identifier.citationBartley, Christopher S.. "Closed form guidance laws for intercepting moving targets." (2004) Master’s Thesis, Rice University. <a href="https://hdl.handle.net/1911/17654">https://hdl.handle.net/1911/17654</a>.en_US
dc.identifier.urihttps://hdl.handle.net/1911/17654en_US
dc.language.isoengen_US
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.en_US
dc.subjectMechanical engineeringen_US
dc.titleClosed form guidance laws for intercepting moving targetsen_US
dc.typeThesisen_US
dc.type.materialTexten_US
thesis.degree.departmentMechanical Engineeringen_US
thesis.degree.disciplineEngineeringen_US
thesis.degree.grantorRice Universityen_US
thesis.degree.levelMastersen_US
thesis.degree.nameMaster of Scienceen_US
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