Coordination within the remote sensing payload on the Solar Orbiter mission

被引：33

作者：

Auchere, F. ^{[1
]}

Andretta, V. ^{[13
]}

Antonucci, E. ^{[2
]}

Bach, N. ^{[12
]}

Battaglia, M. ^{[5
]}

Bemporad, A. ^{[2
]}

Berghmans, D. ^{[9
]}

Buchlin, E. ^{[1
]}

Caminade, S. ^{[1
]}

Carlsson, M. ^{[25
]}

Carlyle, J. ^{[6
]}

Cerullo, J. J. ^{[31
]}

Chamberlin, P. C. ^{[11
]}

Colaninno, R. C. ^{[4
]}

Davila, J. M. ^{[11
]}

De Groof, A. ^{[12
]}

Etesi, L. ^{[5
]}

Fahmy, S. ^{[6
]}

Fineschi, S. ^{[2
]}

Fludra, A. ^{[3
]}

Gilbert, H. R. ^{[11
]}

Giunta, A. ^{[3
]}

Grundy, T. ^{[3
]}

Haberreiter, M. ^{[22
]}

Harra, L. K. ^{[22
,32
]}

Hassler, D. M. ^{[10
]}

Hirzberger, J. ^{[8
]}

Howard, R. A. ^{[4
]}

Hurford, G. ^{[14
]}

Kleint, L. ^{[5
]}

Kolleck, M. ^{[8
]}

Krucker, S. ^{[5
]}

Lagg, A. ^{[8
]}

Landini, F. ^{[26
]}

Long, D. M. ^{[21
]}

Lefort, J. ^{[12
]}

Lodiot, S. ^{[23
]}

Mampaey, B. ^{[9
]}

Maloney, S. ^{[30
]}

Marliani, F. ^{[6
]}

Martinez-Pillet, V. ^{[27
]}

McMullin, D. R. ^{[17
]}

Muller, D. ^{[6
]}

Nicolini, G. ^{[2
]}

Orozco Suarez, D. ^{[18
]}

Pacros, A. ^{[6
]}

Pancrazzi, M. ^{[20
]}

Parenti, S. ^{[1
,9
]}

Peter, H. ^{[8
]}

Philippon, A. ^{[1
]}

机构：

[1] Univ Paris Saclay, CNRS, Inst Astrophys Spatiale, F-91405 Orsay, France

[2] Astrophys Observ Torino, Natl Inst Astrophys INAF, Via Osservatorio 20, I-10025 Pino Torinese, Italy

[3] STFC Rutherford Appleton Lab, RAL Space, Didcot OX11 0QX, Oxon, England

[4] Naval Res Lab, Space Sci Div, Washington, DC 20375 USA

[5] Univ Appl Sci & Arts Northwestern Switzerland, CH-5210 Windisch, Switzerland

[6] European Space Agcy, Estec, POB 299, NL-2200 Noordwijk, Netherlands

[7] Univ Liege, Ctr Spatial Liege, Ave Preaily, B-4031 Angleur, Belgium

[8] Max Planck Inst Sonnensyst Forsch, Justus von Liebig Weg 3, D-37077 Gottingen, Germany

[9] Royal Observ Belgium, Solar Terr Ctr Excellence SIDC, Ringlaan 3 Ave Circulaire, B-1180 Brussels, Belgium

[10] Southwest Res Inst, 1050 Walnut St, Boulder, CO USA

[11] NASA, Solar Phys Lab, Heliophys Sci Div, Goddard Space Flight Ctr, Greenbelt, MD USA

[12] European Space Agcy ESAC, Camino Bajo Castillo, Madrid 28692, Spain

[13] INAF Astron Observ Capodimonte, Naples, Italy

[14] Univ Calif Berkeley, SSL, 7 Gauss Way, Berkeley, CA 94720 USA

[15] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD USA

[16] INAF Catania Astrophys Observ, I-95123 Catania, Italy

[17] Space Syst Res Corp, Alexandria, VA USA

[18] CSIC, Inst Astrofis Andalucia IAA, Apdo Correos 3004, Granada 18080, Spain

[19] NASA, Goddard Spaceflight Ctr, ADNET Syst Inc, Code 671, Greenbelt, MD 20771 USA

[20] Univ Florence, Dipartimento Fis & Astron, SASS, Largo E Fermi 2, I-50125 Florence, Italy

[21] Univ Coll London, Mullard Space Sci Lab, Holmbury St Mary, Dorking RH5 6NT, Surrey, England

[22] Phys Meteorol Observ Davos, World Radiat Ctr, CH-7260 Davos, Switzerland

[23] ESA ESOC, Robert Bosch Str 5, D-64293 Darmstadt, Germany

[24] Univ Toulouse UPS, Inst Rech Astrophys & Planetol, CNRS, Toulouse, France

[25] Univ Oslo, Inst Theoret Astrophys, POB 1029, N-0315 Oslo, Norway

[26] Osserv Astrofis Arcetri, INAF, Florence, Italy

[27] Natl Solar Observ, 3665 Discovery Dr, Boulder, CO 80303 USA

[28] Moscow State Univ, Skobeltsyn Inst Nucl Phys, Moscow, Russia

[29] Kyung Hee Univ, Sch Space Res, Yongin 446701, Gyeonggi Do, South Korea

[30] Trinity Coll Dublin, Sch Phys, Dublin 2, Ireland

[31] ASRC Fed Space & Def, Washington, DC USA

[32] Swiss Fed Inst Technol, IPA, Honggerberg Campus, Zurich, Switzerland

[33] NASA HQ, Heliophys Div, Washington, DC 20546 USA

来源：

ASTRONOMY & ASTROPHYSICS | 2020年 / 642卷

基金：

英国科学技术设施理事会;

关键词：

space vehicles: instruments; Sun: general; instrumentation: polarimeters; instrumentation: spectrographs; telescopes; REPRESENTATIONS; INSTRUMENT; ALPHA;

D O I：

10.1051/0004-6361/201937032

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

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 synergistic approach between IS and RS measurements.Aims. Many aspects of hardware development, integration, testing, and operations are common to two or more RS instruments. In this paper, we describe the coordination effort initiated from the early mission phases by the Remote Sensing Working Group. We review the scientific goals and challenges, and give an overview of the technical solutions devised to successfully operate these instruments together.Methods. A major constraint for the RS instruments is the limited telemetry (TM) bandwidth of the Solar Orbiter deep-space mission compared to missions in Earth orbit. Hence, many of the strategies developed to maximise the scientific return from these instruments revolve around the optimisation of TM usage, relying for example on onboard autonomy for data processing, compression, and selection for downlink. The planning process itself has been optimised to alleviate the dynamic nature of the targets, and an inter-instrument communication scheme has been implemented which can be used to autonomously alter the observing modes. We also outline the plans for in-flight cross-calibration, which will be essential to the joint data reduction and analysis.Results. The RS instrument package on Solar Orbiter will carry out comprehensive measurements from the solar interior to the inner heliosphere. Thanks to the close coordination between the instrument teams and the European Space Agency, several challenges specific to the RS suite were identified and addressed in a timely manner.

引用

页数：12

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