GRS electronics for a space-borne gravitational wave observatory

被引：3

作者：

Mance, D. ^{[1
,20
]}

Zweifel, P. ^{[1
,20
]}

Ferraioli, L. ^{[1
,20
]}

ten Pierick, J. ^{[2
]}

Meshksar, N. ^{[1
]}

Giardini, D. ^{[1
,20
]}

Armano, M. ^{[3
]}

Audley, H. ^{[4
,5
]}

Auger, G. ^{[6
]}

Baird, J. ^{[7
]}

Bassan, M. ^{[8
,9
]}

Binetruy, P. ^{[6
]}

Born, M. ^{[4
,5
]}

Bortoluzzi, D. ^{[10
,11
]}

Brandt, N. ^{[12
]}

Caleno, M. ^{[13
]}

Cavalleri, A. ^{[14
,15
]}

Cesarini, A. ^{[14
,15
]}

Cruise, M. ^{[16
]}

Danzmann, K. ^{[4
,5
]}

de Deus Silva, M. ^{[3
]}

De Rosa, R. ^{[17
,18
]}

Di Fiore, L. ^{[18
]}

Diepholz, I. ^{[4
,5
]}

Dolesi, R. ^{[14
,15
]}

Dunbar, N. ^{[19
]}

Ferraioli, L. ^{[1
,20
]}

Ferroni, V. ^{[14
,15
]}

Fitzsimons, E. ^{[21
]}

Flatscher, R. ^{[12
]}

Freschi, M. ^{[3
]}

Marrirodriga, C. Garcia ^{[13
]}

Gerndt, R. ^{[12
]}

Gesa, L. ^{[22
]}

Gibert, F. ^{[14
,15
]}

Giardini, D. ^{[1
,20
]}

Giusteri, R. ^{[14
,15
]}

Grado, A. ^{[17
,18
]}

Grimani, C. ^{[23
]}

Grzymisch, J. ^{[13
]}

Harrison, I. ^{[24
]}

Heinzel, G. ^{[4
,5
]}

Hewitson, M. ^{[4
,5
]}

Hollington, D. ^{[7
]}

Hoyland, D. ^{[16
]}

Hueller, M. ^{[14
,15
]}

Inchauspe, H. ^{[6
]}

Jennrich, O. ^{[13
]}

Jetzer, P. ^{[25
]}

Johlander, B. ^{[13
]}

机构：

[1] Swiss Fed Inst Technol, Inst Geophys, Dept Earth Sci, Sonneggstr 5, Zurich, Switzerland

[2] Univ Zurich, Dept Phys, Winterthurerstr 190, Zurich, Switzerland

[3] European Space Agcy, European Space Astron Ctr, Madrid 28692, Spain

[4] Max Planck Inst Gravitat Phys, Albert Einstein Inst, Callinstr 38, D-30167 Hannover, Germany

[5] Leibniz Univ Hannover, Callinstr 38, D-30167 Hannover, Germany

[6] Univ Paris Diderot, APC, CNRS IN2P3, CEA Irfu,Obs Paris,Sorbonne Paris Cite, Paris, France

[7] Imperial Coll London, High Energy Phys Grp, Blackett Lab, Phys Dept, Prince Consort Rd, London SW7 2BW, England

[8] Univ Roma Tor Vergata, Dipartimento Fis, I-00133 Rome, Italy

[9] INFN, Sez Roma Tor Vergata, I-00133 Rome, Italy

[10] Univ Trento, Dept Ind Engn, Via Sommar 9, I-38123 Trento, Italy

[11] INFN, Trento Inst Fundamental Phys & Applicat, Rome, Italy

[12] Airbus Def & Space, Claude Dornier Str, D-88090 Immenstaad, Germany

[13] European Space Agcy, European Space Technol Ctr, Keplerlaan 1, NL-2200 AG Noordwijk, Netherlands

[14] Univ Trento, Dipartimento Fis, I-38123 Povo, Trento, Italy

[15] INFN, Trento Inst Fundamental Phys & Applicat, I-38123 Povo, Trento, Italy

[16] Univ Birmingham, Dept Phys & Astron, Birmingham, W Midlands, England

[17] INAF, Osservatorio Astron Capodimonte, I-80131 Naples, Italy

[18] INFN, Sez Napoli, I-80126 Naples, Italy

[19] Airbus Def & Space, Gunnels Wood Rd, Stevenage SG1 2AS, Herts, England

[20] Swiss Fed Inst Technol, Inst Geophys, Sonneggstr 5, CH-8092 Zurich, Switzerland

[21] Royal Observ, UK Astron Technol Ctr, Blackford Hill, Edinburgh EH9 3HJ, Midlothian, Scotland

[22] Inst Ciencies Espai CSIC IEEC, Campus UAB,Carrer Can Magrans S-N, Cerdanyola Del Valles 08193, Spain

[23] Univ Urbino Carlo Bo, DISPEA, INFN, Via S Chiara 27, I-61029 Urbino, Italy

[24] European Space Agcy, European Space Operat Ctr, D-64293 Darmstadt, Germany

[25] Univ Zurich, Phys Inst, Winterthurerstr 190, CH-8057 Zurich, Switzerland

[26] Univ Glasgow, Sch Phys & Astron, SUPA, Inst Gravitat Res, Glasgow G12 8QQ, Lanark, Scotland

[27] Univ Politecn Cataluna, Dept Engn Elect, ES-08034 Barcelona, Spain

[28] Co Gen Spazio, CGS SpA, Via Gallarate 150, I-20151 Milan, Italy

[29] NASA, Goddard Space Flight Ctr, Gravitat Astrophys Lab, 8800 Greenbelt Rd, Greenbelt, MD 20771 USA

[30] Univ Firenze, Dipartimento Fis & Astron, I-50019 Florence, Italy

[31] INFN, Sez Firenze, I-50019 Florence, Italy

来源：

11TH INTERNATIONAL LISA SYMPOSIUM | 2017年 / 840卷

关键词：

D O I：

10.1088/1742-6596/840/1/012040

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

The Gravitational Reference Sensor (GRS) electronics is a crucial element of the future space-borne gravitational wave observatory. Together with the optical metrology system, it provides position measurements of the sensor's reference body, a Test Mass (TM), for all axes. This is needed for precise spacecraft control. In addition, the GRS electronics can actuate the TM using electrostatic forces, which is used to keep the TM centered in its enclosure or to follow a certain guidance. The GRS electronics has been successfully tested during the LISA Pathfinder mission, launched in December 2015. The electronics has been designed in Switzerland by RUAG and HES-SO under supervision of ETH Zurich and University of Zurich. The paper describes the working principle and the adopted technical solutions for the LISA Pathfinder GRS electronics and for the LISA GRS electronics prototype. Both confirm the readiness of the technology for LISA.

引用

页数：5

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