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Model and control problem for space vehicles with propellant slosh

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dc.contributor.authorCihan, Melahat
dc.contributor.authorMelahat Cihan
dc.contributor.authorMetin O. Kaya
dc.contributor.orcid0000-0002-8426-9378
dc.contributor.orcid0000-0003-1589-8100
dc.date.accessioned2025-11-13T22:40:42Z
dc.date.issued2015-06-01
dc.identifier.doihttps://doi.org/10.1109/rast.2015.7208389
dc.identifier.openalexW1581803427
dc.identifier.urihttps://hdl.handle.net/11421/14947
dc.identifier.urihttps://doi.org/10.1109/rast.2015.7208389
dc.language.isoen
dc.rightsrestrictedAccess
dc.subjectSlosh dynamics
dc.subjectPropellant
dc.subjectRocket (weapon)
dc.subjectAerospace engineering
dc.subjectControl theory (sociology)
dc.subjectNonlinear system
dc.subjectEngineering
dc.subjectSpace launch
dc.subjectLiquid-propellant rocket
dc.subjectController (irrigation)
dc.subjectPhysics
dc.subjectComputer science
dc.subjectControl (management)
dc.subject.sdg7
dc.titleModel and control problem for space vehicles with propellant slosh
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5083272193

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