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dc.contributor.authorLobo Gutiérrez, José Alberto
dc.contributor.authorNofrarías, M.
dc.contributor.authorRamos Castro, Juan José
dc.contributor.authorSanjuan, J.
dc.contributor.authorConchillo, A
dc.contributor.authorOrtega, J.A.
dc.contributor.authorXirgu, X
dc.contributor.authorAraujo, H.
dc.contributor.authorBoatella, C.
dc.contributor.authorChmeissani, M.
dc.contributor.authorGrimani, C.
dc.contributor.authorPuigdengoles, C.
dc.contributor.authorWass, P.
dc.contributor.authorGarcía-Berro Montilla, Enrique
dc.contributor.authorGarcía, S.
dc.contributor.authorMartínez, L.M.
dc.contributor.authorMontero, G.
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Física Aplicada
dc.date.accessioned2007-12-13T13:23:21Z
dc.date.available2007-12-13T13:23:21Z
dc.date.created2006-07
dc.date.issued2006-12
dc.identifier.citationLobo, a.; Nofrarias, M.; Ramos Castro, J.; Sanjuan, J.; Conchillo, A.; Ortega, J.A.; Xirgu, X.; Araujo, H.; Boatella, C.; Chmeissani, M.; Grimani, C.; Puigdengoles, C.; Wass, P.; García-Berro, E.; García S.; Martínez, L.M.; Montero, G. In-flight Diagnostics in LISA Pathfinder. A Sixth International LISA Symposium. College Park, Maryland: American Institute of Physics, 2006. vol.873, pàgs 522-528
dc.identifier.isbn978-0-7354-0372-7
dc.identifier.urihttp://hdl.handle.net/2117/1413
dc.description.abstractLISA PathFinder (LPF) will be flown with the objective to test in space key technologies for LISA. However its sensitivity goals are, for good reason, one order of magnitude less than those which LISA will have to meet, both in drag-free and optical metrology requirements, and in the observation frequency band. While the expected success of LPF will of course be of itself a major step forward to LISA, one might not forget that a further improvement by an order of magnitude in performance will still be needed. Clues for the last leap are to be derived from proper disentanglement of the various sources of noise which contribute to the total noise, as measured in flight during the PathFinder mission. This paper describes the principles, workings and requirements of one of the key tools to serve the above objective: the diagnostics subsystem. This consists in sets of temperature, magnetic field, and particle counter sensors, together with generators of controlled thermal and magnetic perturbations. At least during the commissioning phase, the latter will be used to identify feed-through coefficients between diagnostics sensor readings and associated actual noise contributions. A brief progress report of the current state of development of the diagnostics subsystem will be given as well.
dc.format.extent7 pàgs
dc.language.isoeng
dc.publisherAmerican Institute of Physics
dc.relation.ispartofSixth International LISA (Laser Interferometer Space Antenna) Symposium
dc.subjectÀrees temàtiques de la UPC::Física
dc.subject.lcshGravity waves
dc.subject.otherGravity waves
dc.subject.otherLISA
dc.subject.otherLISA Pathfinder
dc.subject.otherDiagnostics
dc.titleIn-flight Diagnostics in LISA Pathfinder
dc.typeConference report
dc.subject.lemacOnes gravitacionals
dc.contributor.groupUniversitat Politècnica de Catalunya. GAA - Grup d'Astronomia i Astrofísica
dc.date.end2006-06-23
dc.date.start2006-06-19
dc.description.peerreviewedPeer Reviewed
dc.rights.accessOpen Access
local.personalitzacitaciotrue


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