PROBA-3 is an ESA mission aimed at the demonstration of formation flying performance of two satellites that will form a giant coronagraph in space. The first spacecraft will host a telescope imaging the solar corona in visible light, while the second, the external occulter, will produce an artificial eclipse. This instrument is named ASPIICS (Association of Spacecraft for Polarimetric and Imaging Investigation of the Corona of the Sun). To accomplish the payload's scientific tasks, PROBA-3 will ensure sub-millimeter reciprocal positioning of its two satellites using closed-loop on-board metrology. Several metrology systems will be used and the Shadow Position Sensor (SPS) subsystem senses the penumbra around the instrument aperture and returns the 3-D displacement of the coronagraph satellite, with respect to its nominal position, by running a dedicated algorithm. In this paper, we describe how the SPS works and the choices made to accomplish the mission objectives.

Metrology on-board PROBA-3: The shadow position sensors subsystem / {Noce}, Vladimiro and {Loreggia}, Davide and {Capobianco}, Gerardo and {Fineschi}, Silvano and {Bemporad}, Alessandro and {Casti}, Marta and {Buckley}, Steven and {Romoli}, Marco and {Focardi}, Mauro and {Belluso}, Massimiliano and {Thizy}, C{'e}dric and {Hermans}, Aline and {Galano}, Damien and {Versluys}, Jorg. - In: ADVANCES IN SPACE RESEARCH. - ISSN 0273-1177. - ELETTRONICO. - 67:(2021), pp. 3807-3818. [10.1016/j.asr.2020.08.004]

Metrology on-board PROBA-3: The shadow position sensors subsystem

(Romoli), Marco;
2021

Abstract

PROBA-3 is an ESA mission aimed at the demonstration of formation flying performance of two satellites that will form a giant coronagraph in space. The first spacecraft will host a telescope imaging the solar corona in visible light, while the second, the external occulter, will produce an artificial eclipse. This instrument is named ASPIICS (Association of Spacecraft for Polarimetric and Imaging Investigation of the Corona of the Sun). To accomplish the payload's scientific tasks, PROBA-3 will ensure sub-millimeter reciprocal positioning of its two satellites using closed-loop on-board metrology. Several metrology systems will be used and the Shadow Position Sensor (SPS) subsystem senses the penumbra around the instrument aperture and returns the 3-D displacement of the coronagraph satellite, with respect to its nominal position, by running a dedicated algorithm. In this paper, we describe how the SPS works and the choices made to accomplish the mission objectives.
2021
67
3807
3818
{Noce}, Vladimiro and {Loreggia}, Davide and {Capobianco}, Gerardo and {Fineschi}, Silvano and {Bemporad}, Alessandro and {Casti}, Marta and {Buckley}, Steven and {Romoli}, Marco and {Focardi}, Mauro and {Belluso}, Massimiliano and {Thizy}, C{'e}dric and {Hermans}, Aline and {Galano}, Damien and {Versluys}, Jorg
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Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/1248919
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