Optimal and sub-optimal, low-thrust, Earth-Moon trajectories using sequential quadratic programming

dc.contributor.author	Kluever, Craig
dc.contributor.department	Department of Aerospace Engineering
dc.date	2018-11-17T17:29:35.000
dc.date.accessioned	2020-06-30T08:05:55Z
dc.date.available	2020-06-30T08:05:55Z
dc.date.copyright	Mon Jan 01 00:00:00 UTC 1990
dc.date.issued	1990
dc.description.abstract	<p>http://www.worldcat.org/oclc/22939799</p>
dc.format.mimetype	application/pdf
dc.identifier	archive/lib.dr.iastate.edu/rtd/18186/
dc.identifier.articleid	19186
dc.identifier.contextkey	13304691
dc.identifier.s3bucket	isulib-bepress-aws-west
dc.identifier.submissionpath	rtd/18186
dc.identifier.uri	https://dr.lib.iastate.edu/handle/20.500.12876/72082
dc.language.iso	en
dc.source.bitstream	archive/lib.dr.iastate.edu/rtd/18186/Kluever_ISU_1990_K712.pdf\|\|\|Fri Jan 14 21:38:04 UTC 2022
dc.subject.disciplines	Aerospace Engineering
dc.subject.keywords	Aerospace Engineering
dc.title	Optimal and sub-optimal, low-thrust, Earth-Moon trajectories using sequential quadratic programming
dc.type	thesis
dc.type.genre	thesis
dspace.entity.type	Publication
relation.isOrgUnitOfPublication	047b23ca-7bd7-4194-b084-c4181d33d95d
thesis.degree.discipline	Aerospace Engineering
thesis.degree.level	thesis
thesis.degree.name	Master of Science

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