2021
DOI: 10.3390/aerospace8050138
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Numerical Aspects of Particle-in-Cell Simulations for Plasma-Motion Modeling of Electric Thrusters

Abstract: The present work is focused on a detailed description of an in-house, particle-in-cell code developed by the authors, whose main aim is to perform highly accurate plasma simulations on an off-the-shelf computing platform in a relatively short computational time, despite the large number of macro-particles employed in the computation. A smart strategy to set up the code is proposed, and in particular, the parallel calculation in GPU is explored as a possible solution for the reduction in computing time. An appl… Show more

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Cited by 3 publications
(2 citation statements)
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“…It should be emphasized that the dominant computational cost of grid-based PIC algorithms is roughly proportional to the number of particles in physical volume and simulation time [137]. The computational performance can be enhanced using parallelization [138]. For example, the vectorization strategy implemented in the PIC code Smilei [139] takes advantage from the optimization of particle's projection, push, deposition operators and an efficient sorting of the particles [140].…”
Section: Numerical Algorithms Used In the Pic Approachmentioning
confidence: 99%
“…It should be emphasized that the dominant computational cost of grid-based PIC algorithms is roughly proportional to the number of particles in physical volume and simulation time [137]. The computational performance can be enhanced using parallelization [138]. For example, the vectorization strategy implemented in the PIC code Smilei [139] takes advantage from the optimization of particle's projection, push, deposition operators and an efficient sorting of the particles [140].…”
Section: Numerical Algorithms Used In the Pic Approachmentioning
confidence: 99%
“…Thrusters can be categorized based on diverse working principles, such as Hall thrusters showing a high thrust efficiency and high ion beam density due to a moderate magnetic field applied to the acceleration zone [47], pulsed plasma thrusters [48], electrospray thrusters working with ionic liquid propellants [49,50], etc. While Hall thrusters are most often used for satellites [51], applications requiring lower energies, such as the aforementioned CubeSats or other microsatellites, can be driven and navigated by microcathode arc or other plasma thrusters, field emission thrusters, electrospray thrusters, or different sorts of electric thrusters [52][53][54][55].…”
Section: Thrustersmentioning
confidence: 99%