Optimal Mission Design to Lagrangian Points

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dc.contributor.guideR V Ramanan
dc.coverage.spatial
dc.creator.researcherRithwik N
dc.date.accessioned2024-04-29T08:40:53Z
dc.date.available2024-04-29T08:40:53Z
dc.date.awarded2024
dc.date.completed2024
dc.date.registered2016
dc.description.abstractnewline
dc.description.note
dc.format.accompanyingmaterialDVD
dc.format.dimensions30cm*22cm
dc.format.extentxviii, 157p
dc.identifier.urihttp://hdl.handle.net/10603/561492
dc.languageEnglish
dc.publisher.institutionDepartment of Aerospace Engineering
dc.publisher.placeThiruvananthapuram
dc.publisher.universityIndian Institute of Space Science and Technology
dc.relation110
dc.rightsuniversity
dc.source.universityUniversity
dc.subject.keywordEngineering and Technology
dc.subject.keywordEngineering
dc.subject.keywordEngineering Aerospace
dc.subject.keywordHalo orbit, Transfer trajectory, Elliptic restricted three body problem, Differential evolution, Optimization
dc.titleOptimal Mission Design to Lagrangian Points
dc.title.alternative
dc.type.degreePh.D.

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