2020
DOI: 10.1051/0004-6361/201937032
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Coordination within the remote sensing payload on the Solar Orbiter mission

Abstract: Context. To meet the scientific objectives of the mission, the Solar Orbiter spacecraft carries a suite of in-situ (IS) and remote sensing (RS) instruments designed for joint operations with inter-instrument communication capabilities. Indeed, previous missions have shown that the Sun (imaged by the RS instruments) and the heliosphere (mainly sampled by the IS instruments) should be considered as an integrated system rather than separate entities. Many of the advances expected from Solar Orbiter rely on this s… Show more

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Cited by 30 publications
(15 citation statements)
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“…-Role of magnetic field lines in channelling the coronal wind. Solar Orbiter remote sensing and in situ instruments, as well as observations obtained by simultaneous space missions dedicated to heliophysics, will complement the Metis observations and facilitate our understanding of the scientific questions being addressed, as discussed in the papers devoted to the Solar Orbiter joint science (Auchére et al 2019;Horbury et al 2019a).…”
Section: Scientific Objectivesmentioning
confidence: 99%
“…-Role of magnetic field lines in channelling the coronal wind. Solar Orbiter remote sensing and in situ instruments, as well as observations obtained by simultaneous space missions dedicated to heliophysics, will complement the Metis observations and facilitate our understanding of the scientific questions being addressed, as discussed in the papers devoted to the Solar Orbiter joint science (Auchére et al 2019;Horbury et al 2019a).…”
Section: Scientific Objectivesmentioning
confidence: 99%
“…The EUI Full Sun Imager (FSI) will be imaging alternatively in the 17.4 nm and 30.4 nm EUV pass-bands, with a 3.8 • × 3.8 • FOV, corresponding to (14.3 R ) 2 at 1 AU and still (4.0 R ) 2 at perihelion. This FOV is unprecedentedly large for a coronal EUV imager and will have a significant overlap (Auchère et al 2020) with the Solar Orbiter coronagraph Metis (Antonucci et al 2020).…”
Section: The Transition From Corona To the Heliospherementioning
confidence: 99%
“…Full operation of the remotesensing instrument package of Solar Orbiter, including EUI, will be restricted to three periods of ten days per 168 days orbit, corresponding to perihelion and to maximal solar latitude north and south. In between these three periods, EUI will take part in a program of much reduced, synoptic remote sensing observations (Auchère et al 2020).…”
Section: Concepts Of Operationsmentioning
confidence: 99%
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