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Статті в журналах з теми "Satellites artificiels – Modèles mathématiques"
Kilani, Mondher. "Culture." Anthropen, 2019. http://dx.doi.org/10.17184/eac.anthropen.121.
Повний текст джерелаДисертації з теми "Satellites artificiels – Modèles mathématiques"
Lebedev, Nikolaï. "Terminaux multicapteurs pour communications par satellite : techniques de formation de voies en émission et capacité." Nantes, 2003. http://www.theses.fr/2003NANT2031.
Повний текст джерелаBorghol, Saja. "Modélisation mathématique de la charge de surface des satellites en orbite basse." Thesis, Lille 1, 2010. http://www.theses.fr/2010LIL10040/document.
Повний текст джерелаIn this work we are concerned with a mathematical study of the spacecraft charging phenomena of Low Earth Orbit (LEO).After recalling the physical context, we derive a two-fluid type model for the plasma around the spacecraft. Indeed in LEO, the plasma can be considered highly colisional compared with the case for example of Polar Earth Orbit (PEO). The model used here consist in the Euler equations for the conservation of mass, momentum and energy plus a Poisson equation for the electrostatic potentiel and is derived in the three dimensionnal case.For the mathematical study of the model, we concentrate our attention on the one dimensionnal case to point out the main difficulties.We first consider the stationnary Euler equations coupled to the Poisson equation. The charging dynamics is then embodied into the boundary conditions where the time derivative of the potentiel appears. We present rigourous existence and unicity results together with numerical simulations. Here we only use some Dirichlet boundary conditions for the macroscopic quantities. They can be far from the ones of physical interest wich we only know at a kinetic level.That's why we next propose a numerical solution to incorporate in the simulation of the evolutive Euler equations boundary condition that come from a microscopic modeling in the small mean free path regime. THe boundary condition relies on the analysis of boundary layers formation that accounts from the fact that the incoming kinetic flux might be far from the equilibrium
Bénazéra, Emmanuel. "Diagnostic et reconfiguration basés sur des modèles hybrides concurrents : application aux satellites autonomes." Toulouse 3, 2003. http://www.theses.fr/2003TOU30105.
Повний текст джерелаCouillard-Labonnote, Laurent. "Etude des propriétés optiques et radiatives des cirrus à l'aide de modèles microphysiques élaborés : analyse de mesures in situ (Néphélomètre) et satellitaire (POLDER)." Lille 1, 2001. https://pepite-depot.univ-lille.fr/RESTREINT/Th_Num/2001/50376-2001-147.pdf.
Повний текст джерелаMelachroinos, Stavros A. "Positionnement géodésique à haute fréquence de réseaux GNSS terrestres et marins." Observatoire de Paris (1667-....), 2007. https://hal.science/tel-02071426.
Повний текст джерелаThe surface deformations of the Earth’s crust and the sea-level variations measured by terrestrial or maritime GNSS networks are a subject that the CNES/GRGS team wanted to investigate thoroughly. In the first part, the main characteristics and differences of four global positioning systems that will constitute the future Global Navigation Satellite System of Systems are presented. In the second part, I concentrate in the definition of the basic geodetic components of GNSS used in positioning. In the third part, GINS scientific software package the basic tool used in this PhD study is presented. Updated modifications implemented for the needs of my research are overseen. Then validations tests of the modifications on the level of precise orbit determination (for GPS and GIOVE-A) and positioning are presented. In the fourth part, the main study of ocean tide loading – OTL in a complex coastal area that of Brittany, in France is presented. The implemented method aims to use a dedicated dense GPS network in order to evaluate/validate the performances of ocean tide models in the region. The impact of OTL on tropospheric parameters, the datum stability used to align the GNSS solution and the aliasing affects on the campaign stations’ time-series of unmodeled vertical displacement are analyzed. In the final and last part, the preliminary results of a GPS kinematic data set designated to cross compare and validate altimetric and oceanographic observations of the Antarctic Circumpolar Current are analyzed
Teyssedre, Hubert. "Observations satellitaires et modélisation de l'évolution à long terme de l'ozone stratosphérique et influence d'activités humaines." Toulouse 3, 1994. http://www.theses.fr/1994TOU30200.
Повний текст джерелаVadez, Vincent. "Simplification géométrique pour la simulation thermique radiative de satellites." Thesis, Université Côte d'Azur, 2022. http://www.theses.fr/2022COAZ4035.
Повний текст джерелаThe life cycle of a satellite includes the launch phase, the positioning on the desiredorbit, different maneuvers (deployment of solar panels and safety position), and finallyplacing the satellite on the junk orbit. The satellite gravitates in a hostile environment,exposed to thermal variations of very large amplitude, alternating sun exposure andeclipse phases. The survival of the satellite depends on the temperature of its components, the variation of which must be monitored within safety intervals. In this context, the thermal simulation of the satellite for its design is crucial to anticipate the reality of its operation. Radiative thermal simulation is essential for anticipating the generation of energy from solar and albedo radiation, and for regulating temperatures of on-board equipments. Ideal operation consists in providing appropriate cooling for components exposed to radiation, and conversely, heating of unexposed components. As an order of magnitude, the external temperature ranges from -150 to +150 degrees Celsius, and the internal electronic equipment has a safe range between -50 and +50, with a safety margin of 10 degrees. In the eclipse phase where the radiation is significantly lower, heating is provided by the energy accumulated during the exposed phase, combined with heat pipes for thermal regulation.In this thesis, the objective is to advance the knowledge on radiative thermal simulation calculation methods for satellites. To this end, two approaches are considered. Thefirst approach consists in establishing a reference calculation of a quantity governing radiative thermal simulation: view factors. Being subject to time constraints, this methodis based on a hierarchical data structure enabling progressive computation of view factors, in order to offer a satisfactory tradeoff between time dedicated to computationsand desired accuracy. For the sake of accuracy, a prediction step is added to guaranteea better convergence towards the reference value.The second approach, also motivated by time constraints, aims at reducing the geometric model of a mechanical part or a spacecraft while being faithful to the numericalsimulation. In order to render the decimation physics-informed, a preprocessing step relying on a sensitivity analysis is carried out. To better preserve the physical simulation,the geometric cost of a simplification operator is coupled to a factor deduced from thesimulation deviation between the reference model and the reduced model
Vidal, Alain. "Estimation de l'évapotranspiration par télédétection : application au contrôle de l'irrigation." Montpellier 2, 1989. http://www.theses.fr/1989MON20234.
Повний текст джерелаChen, Cheng. "Retrieving global sources of aerosol emissions from satellite observations." Thesis, Lille 1, 2018. http://www.theses.fr/2018LIL1R001/document.
Повний текст джерелаUnderstanding of the role that atmospheric aerosol play in the Earth-atmosphere system is limited by uncertainties in aerosol distribution, composition and sources. Thus, accurate chemical transport model simulation systems are crucial needed to analyse and predict atmospheric aerosols and their impacts on climate change and environment. Satellite observations have ability to provide an extensive spatial coverage and accurate aerosol products, however, are constrained by clear-sky condition, global coverage orbit cycle and information content. One of the most promising approaches is to reduce model uncertainty by improving the aerosol emission fields (i.e., model input) by means of inverse modeling relying on satellite observations as a constrain. In this study, we designed a method of simultaneous retrievals of desert dust, black carbon and organic carbon aerosol emission sources using aerosol data obtained from GRASP algorithm applied to POLDER/PARASOL satellite observations, and relying on the GEOS-Chem inverse modeling framework. Then, a satellite-based global aerosol emission database (2006-2011) has been developed. This aerosol emission database has been further evaluated by utilization in GEOS-Chem and GEOS-5/GOCART models. The model posterior simulation of aerosol properties employing the retrieved emissions shows a better agreement than the model prior simulation; it is true for not only fitted PARASOL products, but also for completely independent measurements from ground-based AERONET and satellites aerosol products (e.g., MODIS, MISR, OMI). The results suggest that the satellite-based aerosol emission database improves overall global aerosol modeling
Debèse, Nathalie. "Recalage de la navigation par apprentissage sur les données bathymètriques." Compiègne, 1992. http://www.theses.fr/1992COMPD538.
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