Search results for "CEC"

showing 10 items of 347 documents

Aalto-1, multi-payload CubeSat: Design, integration and launch

2021

The design, integration, testing, and launch of the first Finnish satellite Aalto-1 is briefly presented in this paper. Aalto-1, a three-unit CubeSat, launched into Sun-synchronous polar orbit at an altitude of approximately 500 km, is operational since June 2017. It carries three experimental payloads: Aalto Spectral Imager (AaSI), Radiation Monitor (RADMON), and Electrostatic Plasma Brake (EPB). AaSI is a hyperspectral imager in visible and near-infrared (NIR) wavelength bands, RADMON is an energetic particle detector and EPB is a de-orbiting technology demonstration payload. The platform was designed to accommodate multiple payloads while ensuring sufficient data, power, radio, mechanica…

Computer sciencePolar orbitFOS: Physical sciencesAerospace Engineering02 engineering and technologyDesign strategy01 natural sciences7. Clean energyPhysics - Space Physicsmittauslaitteet0203 mechanical engineering0103 physical sciencesBrakeAalto-1CubeSatGround segmentAerospace engineeringInstrumentation and Methods for Astrophysics (astro-ph.IM)010303 astronomy & astrophysicsavaruustekniikkaAalto spectral imagerRadiation monitortutkimussatelliitit020301 aerospace & aeronauticsRadiationSpacecraftbusiness.industryPayloadCubeSatElectrostatic plasma brakesäteilySpace Physics (physics.space-ph)satelliititHyperspectralSatelliteAstrophysics - Instrumentation and Methods for Astrophysicsbusinesskosminen säteily
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Optimal Starting Conditions for the Rendezvous Maneuver, Part 1: Optimal Control Approach

2008

We consider the three-dimensional rendezvous between two spacecraft: a target spacecraft on a circular orbit around the Earth and a chaser spacecraft initially on some elliptical orbit yet to be determined. The chaser spacecraft has variable mass, limited thrust, and its trajectory is governed by three controls, one determining the thrust magnitude and two determining the thrust direction. We seek the time history of the controls in such a way that the propellant mass required to execute the rendezvous maneuver is minimized. Two cases are considered: (i) time-to-rendezvous free and (ii) time-to-rendezvous given, respectively equivalent to (i) free angular travel and (ii) fixed angular trave…

Control and OptimizationElliptic orbitSpacecraftbusiness.industryApplied MathematicsThrust reversalRendezvousThrustComputer Science::Computational GeometryManagement Science and Operations ResearchComputer Science::RoboticsControl theoryPhysics::Space PhysicsAstrophysics::Earth and Planetary AstrophysicsCircular orbitOrbital maneuverbusinessSpace rendezvousMathematics
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Guidance Trajectories for Spacecraft Rendezvous

2007

In a previous paper of Miele et al. (J. Optim. Theory Appl. 132(1), 2007), we employed the single-subarc sequential gradient-restoration algorithm to optimize the three-dimensional rendezvous between a target spacecraft in a planar circular orbit and a chaser spacecraft with an initial separation distance and separation velocity. The achieved continuous solutions are characterized by two, three, or four subarcs depending on the performance index (time, fuel) and the constraints. In this paper, based on the solutions in Miele et al. (J. Optim. Theory Appl. 132(1), 2007), we employ the multiple-subarc sequential gradient-restoration algorithm to produce pieced guidance trajectories implementa…

Control and OptimizationSpacecraftbusiness.industryApplied MathematicsRendezvousManagement Science and Operations ResearchOptimal controlControl theorySearch algorithmTheory of computationOrbit (dynamics)Circular orbitCalculus of variationsbusinessMathematicsJournal of Optimization Theory and Applications
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Optimal Trajectories for Spacecraft Rendezvous

2007

The efficient execution of a rendezvous maneuver is an essential component of various types of space missions. This work describes the formulation and numerical investigation of the thrust function required to minimize the time or fuel required for the terminal phase of the rendezvous of two spacecraft. The particular rendezvous studied concerns a target spacecraft in a circular orbit and a chaser spacecraft with an initial separation distance and separation velocity in all three dimensions. First, the time-optimal rendezvous is investigated followed by the fuel-optimal rendezvous for three values of the max-thrust acceleration via the sequential gradient-restoration algorithm. Then, the ti…

Control and OptimizationSpacecraftbusiness.industryApplied MathematicsRendezvousThrustManagement Science and Operations ResearchOptimal controlSpace explorationComputer Science::Multiagent SystemsComputer Science::RoboticsAccelerationControl theoryPhysics::Space PhysicsOrbit (dynamics)Circular orbitbusinessMathematics
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Convergence for varying measures

2023

Some limit theorems of the type $\int_{\Omega}f_n dm_n -- --> \int_{\Omega}f dm$ are presented for scalar, (vector), (multi)-valued sequences of m_n-integrable functions f_n. The convergences obtained, in the vector and multivalued settings, are in the weak or in the strong sense.

Convergence in total variationSetwise convergenceConvergence in total variationUniform integrabilityAbsolute integrabilityPettis integralMultifunctionAbsolute integrabilitySetwise convergenceApplied MathematicsFunctional Analysis (math.FA)28B20 26E25 26A39 28B05 46G10 54C60 54C65Mathematics - Functional AnalysisMultifunctionSettore MAT/05 - Analisi MatematicaFOS: MathematicsPettis integralUniform integrabilityAnalysisJournal of Mathematical Analysis and Applications
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Characteristics of the diffuse astrophysical electron and Tau neutrino flux with six years of IceCube high energy cascade data

2020

We report on the first measurement of the astrophysical neutrino flux using particle showers (cascades) in IceCube data from 2010-2015. Assuming standard oscillations, the astrophysical neutrinos in this dedicated cascade sample are dominated (∼90%) by electron and tau flavors. The flux, observed in the sensitive energy range from 16 TeV to 2.6 PeV, is consistent with a single power-law model as expected from Fermi-type acceleration of high energy particles at astrophysical sources. We find the flux spectral index to be γ=2.53±0.07 and a flux normalization for each neutrino flavor of φastro=1.66-0.27+0.25 at E0=100 TeV, in agreement with IceCube's complementary muon neutrino results and wit…

Cosmology and Nongalactic Astrophysics (astro-ph.CO)Astrophysics::High Energy Astrophysical PhenomenaFOS: Physical sciencesGeneral Physics and AstronomyElectronpower spectrumflux [electron]energy [particle]01 natural sciencesIceCubeNuclear physics5/3Tau neutrinomuon0103 physical scienceslow [energy]Muon neutrinoddc:530010303 astronomy & astrophysicsastro-ph.HEHigh Energy Astrophysical Phenomena (astro-ph.HE)PhysicsSPECTRUMSpectral indexMuon010308 nuclear & particles physicsHigh Energy Physics::Phenomenologyflavor [neutrino]RAYSflux [neutrino]accelerationshowersoscillationPhysics and Astronomy13. Climate actionEnergy cascadePhysique des particules élémentairesastro-ph.COhigh [energy]cascade [energy]High Energy Physics::ExperimentNeutrinoAstrophysics - High Energy Astrophysical PhenomenaFermi Gamma-ray Space TelescopeAstrophysics - Cosmology and Nongalactic Astrophysics
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¿Un ministro para la esperanza? / 1

2004

Coyuntura política mundialPazVidal-Beneyto JoséEspañaPolíticaPedagogía ciudadanaEUROPAGobierno socialistaPublicaciones: Obra periodística: Columnas y artículos de opiniónMinistroCONSTITUCIÓNIndustria europeaDesigualdadComunidad Europea del Carbón y del AceroPedagogíaResponsabilidadEstabilidad socioeconómicaConstrucción europeaMiguel Ángel MoratinosAmbiciones europeístasBienMalAnalistaAsuntos ExterioresArmasEuropa laboralCECAGuerrasParticipación ciudadanaAutoridad europeaValores
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Enterococcus asini sp. nov. isolated from the caecum of donkeys (Equus asinus)

1998

Several Gram-positive, non-spore-forming and non-motile bacteria consisting of pairs or chains of cocci were isolated during an investigation of the bacterial flora of the caecum of donkeys. Physiological and metabolic data indicated that the strains belong to the genus Enterococcus; phenotypic traits of these organisms were not consistent with any of the currently known Enterococcus species. 16S rRNA gene sequence analysis placed these strains in the genus Enterococcus. Their closest relatives are Enterococcus avium, Enterococcus faecium and Enterococcus pseudoavium with a sequence similarity of 97.4%. This group of strains can be differentiated from the other Enterococcus spp. by their ph…

DNA BacterialEnterococcus avium[SDE] Environmental SciencesARN RIBOSOMAL[SDV]Life Sciences [q-bio]Molecular Sequence DataImmunologyved/biology.organism_classification_rank.speciesMicrobiologyMicrobiologyCaecumEnterococcus pseudoaviumRNA Ribosomal 16SAnimalsCecumGram-Positive Bacterial InfectionsPhylogenyComputingMilieux_MISCELLANEOUSBase CompositionBase SequencebiologySequence Analysis RNAved/biologyEquidaebiochemical phenomena metabolism and nutritionRibosomal RNAANE16S ribosomal RNAbiology.organism_classification[SDV] Life Sciences [q-bio]RNA BacterialEnterococcus[SDE]Environmental SciencesEnterococcusBacteriaEnterococcus faecium
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Deployment of the ATLAS high level trigger

2005

The ATLAS combined test beam in the second half of 2004 saw the first deployment of the ATLAS high-level triggers (HLT). The next steps are deployment on the pre-series farms in the experimental area during 2005, commissioning and cosmics tests in 2006 and collisions in 2007. This paper reviews the experience gained in the test beam, describes the current status and discusses the further enhancements to be made. We address issues related to the dataflow, selection algorithms, testing, software distribution, installation and improvements

DataflowComputer sciencebusiness.industrySoftware distributionCluster (spacecraft)medicine.anatomical_structureInformation engineeringComputer engineeringSoftware deploymentAtlas (anatomy)Systems engineeringmedicineSystem integrationbusinessSelection algorithm14th IEEE-NPSS Real Time Conference, 2005.
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Esperienze di maltrattamento infantile ed esiti psicopatologici in pazienti con disturbi del comportamento alimentare. Uno studio con la CECA.

2012

Introduzione: I disturbi del comportamento alimentare suscitano un forte interesse nel panorama clinico e di ricerca, data la loro diffusione e la svariate sfaccettature che tali profili psicopatologici assumono. Altrettanto forte è la spinta a ricercare possibili fattori eziopatogenetici nei contesti di accudimento primari ed in letteratura è ampiamente riconosciuto il ruolo determinante svolto dai contesti relazionali e dalle esperienze infantili nella strutturazione del Sé in età adulta (Bifulco & Moran, 1998; Fonagy et al., 2002). Lo studio, a carattere esplorativo, ha un duplice obiettivo: a) rilevare se e quali forme di abuso e maltrattamento si riscontrano in soggetti con DCA, b) rin…

Disturbi alimentari Maltrattamento infantile CECA-Childhood Experience of Care and Abuse.
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