Merging spacecraft software development and system tests : an agile verification approach

dc.contributor.advisorEickhoff, Jens (Prof. Dr.-Ing.)
dc.contributor.authorBucher, Nico
dc.date.accessioned2021-03-03T08:52:52Z
dc.date.available2021-03-03T08:52:52Z
dc.date.issued2021de
dc.description.abstractIn this dissertation, the author describes an agile verification approach for spacecraft onboard software that allows for software development guided by system tests performed with the actual spacecraft. The approach was applied for the Flying Laptop small satellite, built and operated by the Institute of Space System (IRS) at the University of Stuttgart, Germany. This work contains examples of practical experience gathered during the system testing campaign of Flying Laptop.en
dc.identifier.other1750203030
dc.identifier.urihttp://nbn-resolving.de/urn:nbn:de:bsz:93-opus-ds-113315de
dc.identifier.urihttp://elib.uni-stuttgart.de/handle/11682/11331
dc.identifier.urihttp://dx.doi.org/10.18419/opus-11314
dc.language.isoende
dc.rightsinfo:eu-repo/semantics/openAccessde
dc.subject.ddc600de
dc.subject.ddc620de
dc.subject.ddc650de
dc.titleMerging spacecraft software development and system tests : an agile verification approachen
dc.title.alternativeEin agiler Verifikationsansatz für Raumfahrzeuge, der Softwareentwicklung und Systemtests vereintde
dc.typedoctoralThesisde
ubs.dateAccepted2020-12-03
ubs.fakultaetLuft- und Raumfahrttechnik und Geodäsiede
ubs.institutInstitut für Raumfahrtsystemede
ubs.publikation.seitenIV, 213de
ubs.publikation.typDissertationde
ubs.thesis.grantorLuft- und Raumfahrttechnik und Geodäsiede

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