Search results for " Aerospace"

showing 10 items of 42 documents

The THESEUS space mission concept: science case, design and expected performances

2018

THESEUS is a space mission concept aimed at exploiting Gamma-Ray Bursts for investigating the early Universe and at providing a substantial advancement of multi-messenger and time-domain astrophysics. These goals will be achieved through a unique combination of instruments allowing GRB and X-ray transient detection over a broad field of view (more than 1sr) with 0.5¿1 arcmin localization, an energy band extending from several MeV down to 0.3¿keV and high sensitivity to transient sources in the soft X-ray domain, as well as on-board prompt (few minutes) follow-up with a 0.7¿m class IR telescope with both imaging and spectroscopic capabilities. THESEUS will be perfectly suited for addressing …

IonizationAtmospheric Sciencecosmological modelCherenkov Telescope Array[ PHYS.ASTR ] Physics [physics]/Astrophysics [astro-ph]AstronomyDark ageMASSIVE SINGLE STARSStar formation rates Gamma ray01 natural sciencesCosmology: observationlocalizationlaw.inventionAstrophysicEinstein Telescopeobservational cosmologylawObservational cosmologyRe-ionizationCosmology: observations; Dark ages; First stars; Gamma-ray: bursts; Re-ionizationLIGOobservations [Cosmology]Telescope010303 astronomy & astrophysicsHigh sensitivityHigh Energy Astrophysical Phenomena (astro-ph.HE)PhysicsMulti-wavelengthenergy: highsezelegamma-ray burstsCosmology: observationsCosmology: observations; Dark ages; First stars; Gamma-ray: bursts; Re-ionization; Aerospace Engineering; Space and Planetary ScienceAstrophysics::Instrumentation and Methods for Astrophysicsimagingstar: formationburst [Gamma-ray]observatoryGeophysicsDark agesX rays Cosmology: observationAstrophysics - Instrumentation and Methods for AstrophysicsAstrophysics - High Energy Astrophysical PhenomenasignatureStarTIDAL DISRUPTIONGamma-ray: burstAstrophysics::High Energy Astrophysical PhenomenaSIMILAR-TO 6Socio-culturaleFOS: Physical sciencesAerospace EngineeringGamma-ray: burstsobservation [Cosmology]galaxy: luminosityX-ray astronomy: instrumentation7 CANDIDATE GALAXIESAstrophysics::Cosmology and Extragalactic Astrophysicsgamma ray: burst114 Physical sciencesSettore FIS/03 - Fisica della MateriaTelescopeX-raybursts [Gamma-ray]FIS/05 - ASTRONOMIA E ASTROFISICASettore FIS/05 - Astronomia e AstrofisicaFirst star0103 physical sciences[PHYS.PHYS.PHYS-INS-DET]Physics [physics]/Physics [physics]/Instrumentation and Detectors [physics.ins-det]KAGRAInstrumentation and Methods for Astrophysics (astro-ph.IM)Astrophysics::Galaxy AstrophysicsFirst starsLIGHT CURVESEinstein Telescope010308 nuclear & particles physicsGravitational wavegravitational radiationAstronomyAstronomy and Astrophysics115 Astronomy Space scienceCherenkov Telescope ArrayredshiftsensitivityRedshiftNEUTRON-STAR MERGERmessengerVIRGOelectromagneticLUMINOSITY FUNCTIONSpace and Planetary ScienceBLACK-HOLEGeneral Earth and Planetary SciencesGamma-ray burst[PHYS.ASTR]Physics [physics]/Astrophysics [astro-ph]
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Beta-forging of Ti6Al4V titanium alloy powders consolidated by HIP: Plastic flow and strain-rate relation

2014

Ti6Al4V is probably the best known and studied titanium alloy, not only for aerospace applications. Nevertheless the deformation behavior still represents a challenge if any modification in the deformation process is required or introduced. This work deals with deformation behavior description of Ti6Al4V HIPped powders during high temperature deformation tests carried on in the Beta-region. Laboratory compression and tensile tests have been coupled with relaxation tests in order to achieve robust data about strain rate sensibility m-coefficient and activation energy Q. These results have been fitted for the assessment of a more general exponential deformation law. The final result is a “Dor…

Materials scienceMechanical EngineeringMetallurgyStrain rateTitanium alloyDeformation (meteorology)Strain ratePlasticityCondensed Matter PhysicsCompression (physics)ForgingMechanics of MaterialsTitanium ForgingDeformation behavior Deformation process High temperature deformation Laboratory techniques Statistical correlation coefficient Ti-6al-4v Ti-beta-forging Ti6al4v titanium alloyUltimate tensile strengthActivation energy Aerospace applications Deformation Forging Plastic flow Powders Tensile testing Titanium alloyRelaxation (physics)General Materials ScienceSettore ING-IND/16 - Tecnologie E Sistemi Di Lavorazione
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Optimal design of an electro-hydraulic valve for heavy-duty vehicle clutch actuator with certain constraints

2016

Abstract The main objective of this paper is to investigate the sensitivity analysis and optimal design of a proportional solenoid valve (PSV) operated pressure reducing valve (PRV) for heavy-duty automatic transmission clutch actuators. The nonlinear electro-hydraulic valve model is developed based on fluid dynamics. In order to implement the sensitivity analysis and optimization for the PRV, the PSV model is validated by comparing the results with data obtained from a real test-bench. The sensitivity of the PSV pressure response with regard to the structural parameters is investigated by using Sobol׳s method. Finally, simulations and experimental investigations are performed on the optimi…

OptimizationOptimal design0209 industrial biotechnologyEngineeringAerospace Engineering02 engineering and technologyPressure regulatorClutch actuatorClutch controllaw.invention020901 industrial engineering & automationPressure reducing valve0203 mechanical engineeringlawControl theorySolenoid valveClutchSensitivity (control systems)Civil and Structural EngineeringAutomatic transmissionbusiness.industryMechanical EngineeringComputer Science Applications1707 Computer Vision and Pattern Recognition020302 automobile design & engineeringComputer Science ApplicationsAutomatic transmission; Clutch actuator; Optimization; Pressure reducing valve; Sensitivity analysis; Control and Systems Engineering; Signal Processing; Civil and Structural Engineering; Aerospace Engineering; Mechanical Engineering; Computer Science Applications1707 Computer Vision and Pattern RecognitionControl and Systems EngineeringAutomatic transmissionSignal ProcessingSensitivity analysisbusinessActuatorMechanical Systems and Signal Processing
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A self-routing protocol for distributed consensus on logical information

2010

In this paper, we address decision making problems, depending on a set of input events, with networks of dynamic agents that have partial visibility of such events. Previous work by the authors proposed so-called logical consensus approach, by which a network of agents, that can exchange binary values representing their local estimates of the events, is able to reach a unique and consistent decision. The approach therein proposed is based on the construction of an iterative map, whose computation is centralized and guaranteed under suitable conditions on the input visibility and graph connectivity. Under the same conditions, we extend the approach in this work by allowing the construction o…

Routing protocol020301 aerospace & aeronautics0209 industrial biotechnologyoptimal information flowComputer scienceDistributed computingMulti-agent systemVisibility (geometry)Graph theory02 engineering and technologyLogical consensus algorithm020901 industrial engineering & automationSettore ING-INF/04 - Automatica0203 mechanical engineeringConsensusRouting (electronic design automation)Wireless sensor networkConnectivity
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Temperature and density structure of hot and cool loops derived from the analysis of TRACE data

2002

We address the plasma structuring both across and along the magnetic field in two sets of solar coronal loops, observed with TRACE in the 17lÅ and 195Å passbands. We derive, after proper background removal, the density stratification and the thermal structure of the plasma in the fibrils forming the loops with two techniques: a) filter ratio diagnostic (195 Å/171 Å) and b) modeling intensity profiles along the fibrils with hydrostatic models. We find evidence of a hot fibril (T ∼ 5·106 K), with temperature and density stratification well-described with a typical non-isothermal hydrostatic loop model, and evidence of rather cold fibrils (T ∼ 2 · 105 K), isothermal and probably in dynamic con…

Settore FIS/05 - Astronomia E AstrofisicaHydrostatic modelTRACEAerospace EngineeringLoops filamentationHydrostatic models; Loops filamentation; TRACE; Aerospace Engineering
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Benchmarking of strength models for unidirectional composites under longitudinal tension

2018

© 2018 Elsevier Ltd Several modelling approaches are available in the literature to predict longitudinal tensile failure of fibre-reinforced polymers. However, a systematic, blind and unbiased comparison between the predictions from the different models and against experimental data has never been performed. This paper presents a benchmarking exercise performed for three different models from the literature: (i) an analytical hierarchical scaling law for composite fibre bundles, (ii) direct numerical simulations of composite fibre bundles, and (iii) a multiscale finite-element simulation method. The results show that there are significant discrepancies between the predictions of the differe…

TechnologyMaterials scienceComposite numberMaterials Science02 engineering and technologyFiber-reinforced composite0901 Aerospace EngineeringEngineering0203 mechanical engineeringFragmentationUltimate tensile strengthMicro-mechanicsCOMPUTED-TOMOGRAPHYLOAD-TRANSFERComposite material0912 Materials EngineeringMaterialsStress concentrationEPOXY COMPOSITESTRESS-CONCENTRATIONSScience & TechnologyDAMAGE ACCUMULATIONTension (physics)FIBER-REINFORCED COMPOSITESPolymer-matrix compositesExperimental dataMicromechanics021001 nanoscience & nanotechnologyFinite element methodEngineering Manufacturing020303 mechanical engineering & transportsWIDE FAILURE EXERCISEMechanics of MaterialsMaterials Science CompositesHYBRID COMPOSITES[PHYS.COND.CM-MS]Physics [physics]/Condensed Matter [cond-mat]/Materials Science [cond-mat.mtrl-sci]Ceramics and CompositesStrength0210 nano-technologyFINITE-ELEMENT0913 Mechanical Engineering
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Thermal Analysis of the Solar Orbiter PHI Electronics Unit

2020

“© 2020 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.”

TestingPolarimetryAerospace EngineeringComputingMilieux_LEGALASPECTSOFCOMPUTING02 engineering and technology7. Clean energylaw.inventionAeronáuticaOrbiter0203 mechanical engineeringRobustness (computer science)lawThermalAstrophysics::Solar and Stellar AstrophysicsElectronicsElectrical and Electronic EngineeringAerospace engineeringThermal analysis020301 aerospace & aeronauticsbusiness.industryAstrophysics::Instrumentation and Methods for AstrophysicsDesign phaseSpace instrumentationThermal modelingPhysics::Space PhysicsEnvironmental scienceIntegrated circuit thermal modelingScientific instrument electronicsSpace thermal controlAstrophysics::Earth and Planetary AstrophysicsbusinessThermal management of space electronics
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Boundary-layer Flows Past an Hemispherical Roughness Element: DNS, Global Stability and Sensitivity Analysis

2015

Abstract We investigate the full three-dimensional instability mechanism arising in the wake of an hemispherical roughness element immersed in a laminar Blasius boundary layer. The inherent three-dimensional flow pattern beyond the critical Reynolds number is characterized by coherent vortical structures called hairpin vortices. Direct numerical simulation is used to analyze the formation and the shedding of hairpin packets inside the shear layer. The first bifurcation characteristics are investigated by global stability tools. We show the spatial structure of the linear direct and adjoint global eigenmodes of the linearized Navier-Stokes operator and use structural sensitivity analysis to …

TriGlobal Linear StabilityDirect numerical simulation02 engineering and technologyWake01 natural sciencesInstability010305 fluids & plasmasPhysics::Fluid Dynamicssymbols.namesake0203 mechanical engineeringHairpin vortices0103 physical sciencesPhysics020301 aerospace & aeronauticsRoughness ElementHairpin vortices; Roughness Element; TriGlobal Linear Stability; Mechanical EngineeringMechanical EngineeringReynolds numberLaminar flowGeneral MedicineMechanicsVortexBoundary layerClassical mechanicsBlasius boundary layersymbolsProcedia IUTAM
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Time Versus Energy in the Averaged Optimal Coplanar Kepler Transfer towards Circular Orbits

2015

International audience; The aim of this note is to compare the averaged optimal coplanar transfer towards circular orbits when the costs are the transfer time transfer and the energy consumption. While the energy case leads to analyze a 2D Riemannian metric using the standard tools of Riemannian geometry (curvature computations, geodesic convexity), the time minimal case is associated to a Finsler metric which is not smooth. Nevertheless a qualitative analysis of the geodesic flow is given in this article to describe the optimal transfers. In particular we prove geodesic convexity of the elliptic domain.

[ MATH.MATH-OC ] Mathematics [math]/Optimization and Control [math.OC]ComputationGeodesic convexity02 engineering and technologyRiemannian geometryCurvature01 natural sciencesDomain (mathematical analysis)Low thrust orbit transfersymbols.namesakeAveraging0203 mechanical engineeringFOS: MathematicsTime transferGeodesic convexityCircular orbit0101 mathematicsMathematics - Optimization and ControlMathematics020301 aerospace & aeronauticsApplied Mathematics010102 general mathematicsMathematical analysisOptimal controlOptimization and Control (math.OC)Metric (mathematics)symbolsRiemann-Finsler Geometry[MATH.MATH-OC]Mathematics [math]/Optimization and Control [math.OC]Mathematics::Differential Geometry
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Minimum fuel control of the planar circular restricted three-body problem

2012

The circular restricted three-body problem is considered to model the dynamics of an artificial body submitted to the attraction of two planets. Minimization of the fuel consumption of the spacecraft during the transfer, e.g. from the Earth to the Moon, is considered. In the light of the controllability results of Caillau and Daoud (SIAM J Control Optim, 2012), existence for this optimal control problem is discussed under simplifying assumptions. Thanks to Pontryagin maximum principle, the properties of fuel minimizing controls is detailed, revealing a bang-bang structure which is typical of L1-minimization problems. Because of the resulting non-smoothness of the Hamiltonian two-point bound…

[ MATH.MATH-OC ] Mathematics [math]/Optimization and Control [math.OC]Lagrangian point02 engineering and technology01 natural sciences0203 mechanical engineeringControl theory0103 physical sciencesApplied mathematicsBoundary value problemCircular orbit010303 astronomy & astrophysicsComputingMilieux_MISCELLANEOUSMathematical PhysicsMathematics020301 aerospace & aeronauticsApplied MathematicsConjugate points[MATH.MATH-OC] Mathematics [math]/Optimization and Control [math.OC]Astronomy and AstrophysicsOptimal controlThree-body problemControllabilityComputational MathematicsSpace and Planetary ScienceModeling and Simulation[MATH.MATH-OC]Mathematics [math]/Optimization and Control [math.OC]Hamiltonian (control theory)Celestial Mechanics and Dynamical Astronomy
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