Search results for "Earth-Moon"

showing 2 items of 2 documents

Measurement of the cosmic ray antiproton/proton flux ratio at TeV energies with the ARGO-YBJ detector

2012

Cosmic ray antiprotons provide an important probe to study the cosmic ray propagation in the interstellar space and to investigate the existence of dark matter. Acting the Earth-Moon system as a magnetic spectrometer, paths of primary antiprotons are deflected in the opposite sense with respect to those of the protons in their way to the Earth. This effect allows, in principle, the search for antiparticles in the direction opposite to the observed deficit of cosmic rays due to the Moon (the so-called `Moon shadow'). The ARGO-YBJ experiment, located at the Yangbajing Cosmic Ray Laboratory (Tibet, P.R. China, 4300 m a.s.l., 606 g/cm$^2$), is particularly effective in measuring the cosmic ray …

PhysicsNuclear and High Energy PhysicsAntiparticleAstrophysics::High Energy Astrophysical PhenomenaDark matterSettore FIS/01 - Fisica SperimentaleEarth-MoonCosmic raymagnetic spectrometerCosmic rayHigh Energy Physics - ExperimentNuclear physicsEarth's magnetic fieldAntiprotonAntimatterantiprotonContent (measure theory)Antiproton-Proton ratio Cosmic rays Extended Air ShowersAstrophysics - High Energy Astrophysical PhenomenaEnergy (signal processing)
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On the optimal control of the circular restricted three body problem

2011

The context of this work is space mechanics. More precisely, we aim at computing low thrust transfers in the Earth-Moon system modeled by the circular restricted three-body problem. The goal is to calculate the optimal steering of the spacecraft engine with respect to two optimization criteria: Final time and fuel consumption. The contributions of this thesis are of two kinds. Geometric, first, as we study the controllability of the system together with the geometry of the transfers (structure of the command) by means of geometric control tools. Numerical, then, different homotopic methods being developed. A two-three body continuation is used to compute minimum time trajectories, and then …

[ MATH.MATH-OC ] Mathematics [math]/Optimization and Control [math.OC]Earth-Moon transfercontinuations discrète et différentielletrajectoires temps ou consommation minimalesminimum time or fuel consumption trajectories[MATH.MATH-OC] Mathematics [math]/Optimization and Control [math.OC]transfert Terre-Lunecircular restricted three-body problemshootingoptimal controlcontrôle optimalpoussée faibleméthode de tirproblème des trois corps circulaire restreintlow thrust[MATH.MATH-OC]Mathematics [math]/Optimization and Control [math.OC]discrete and differential continuation
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