2019
DOI: 10.1051/0004-6361/201834822
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The PLATO Solar-like Light-curve Simulator

Abstract: Context. ESA’s PLATO space mission, to be launched by the end of 2026, aims to detect and characterise Earth-like planets in their habitable zone using asteroseismology and the analysis of the transit events. The preparation of science objectives will require the implementation of hare-and-hound exercises relying on the massive generation of representative simulated light-curves. Aims. We developed a light-curve simulator named the PLATO Solar-like Light-curve Simulator (PSLS) in order to generate light-curves… Show more

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Cited by 23 publications
(25 citation statements)
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“…Since the design goal of PLATO is a photometric accuracy of 34 ppm (Rauer et al 2014), plage regions may affect the diameter measurements in some objects. The effects of faculae should thus be included into simulations, like those presented by Samadi et al (2019).…”
Section: Discussionmentioning
confidence: 99%
“…Since the design goal of PLATO is a photometric accuracy of 34 ppm (Rauer et al 2014), plage regions may affect the diameter measurements in some objects. The effects of faculae should thus be included into simulations, like those presented by Samadi et al (2019).…”
Section: Discussionmentioning
confidence: 99%
“…However, given the target selection aims mainly at finding nearby planetary systems characterizable through follow-up spectroscopy, PLATO detailed asteroseismic information will be available mainly for bright, nearby field F5-K7 dwarfs and subgiants. Moreover, the large pixel sizes of PLATO (projected size in sky: 15 arcsec, [194]) will hamper obtaining detailed information for stars in crowded fields, including star clusters, the Milky Way's bulge, and nearby galaxies.…”
Section: Limitations Of Present/planned Asteroseismic Missionsmentioning
confidence: 99%
“…As the individual raw images downlinked from the spacecraft cannot describe the distribution of stellar flux on the detectors with sufficient resolution, high resolution PSFs such as those in Fig. 4 will be reconstructed on the ground from micro-scanning sessions (Samadi et al 2019). This process, which will occur every three months during instrument calibration phases, basically consists of acquiring Fig.…”
Section: Point Spread Functionmentioning
confidence: 99%
“…To compensate for this effect, the proposed solution consists in tracking the targets by updating the placement of their apertures on board, as explained in Samadi et al (2019). This will involve both ground and flight segments of the mission, as the apertures will first be computed on the ground and then transmitted to the spacecraft.…”
Section: Updating the Masks On Boardmentioning
confidence: 99%