LISA Pathfinder data analysis

被引：23

作者：

Antonucci, F. ^{[1
,2
]}

Armano, M. ^{[3
]}

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

Auger, G. ^{[6
]}

Benedetti, M. ^{[7
,8
]}

Binetruy, P. ^{[6
]}

Boatella, C. ^{[9
]}

Bogenstahl, J. ^{[4
,5
]}

Bortoluzzi, D. ^{[8
,10
]}

Bosetti, P. ^{[8
,10
]}

Caleno, M. ^{[11
]}

Cavalleri, A. ^{[1
,2
]}

Cesa, M. ^{[11
]}

Chmeissani, M. ^{[12
]}

Ciani, G. ^{[13
]}

Conchillo, A. ^{[14
]}

Congedo, G. ^{[1
,2
]}

Cristofolini, I. ^{[8
,10
]}

Cruise, M. ^{[15
]}

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

De Marchi, F. ^{[1
,2
]}

Diaz-Aguilo, M. ^{[16
]}

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

Dixon, G. ^{[15
]}

Dolesi, R. ^{[1
,2
]}

Fauste, J. ^{[3
]}

Ferraioli, L. ^{[1
,2
]}

Fertin, D. ^{[11
]}

Fichter, W. ^{[17
]}

Fitzsimons, E. ^{[18
]}

Freschi, M. ^{[3
]}

Marin, A. Garcia ^{[4
,5
]}

Marirrodriga, C. Garcia ^{[11
]}

Gesa, L. ^{[14
]}

Giardini, D.

Grimani, C. ^{[19
]}

Grynagier, A. ^{[17
]}

Guillaume, B. ^{[11
]}

Guzman, F. ^{[20
]}

Harrison, I. ^{[21
]}

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

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

Hollington, D. ^{[22
]}

Hough, J. ^{[18
]}

Hoyland, D. ^{[15
]}

Hueller, M. ^{[1
,2
]}

Huesler, J. ^{[11
]}

Jeannin, O. ^{[6
]}

Jennrich, O. ^{[11
]}

Jetzer, P. ^{[23
]}

机构：

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

[2] INFN, Grp Collegato Trento, I-38123 Povo, Trento, Italy

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

[4] Leibniz Univ Hannover, D-30167 Hannover, Germany

[5] Max Planck Inst Gravitat Phys, Albert Einstein Inst, D-30167 Hannover, Germany

[6] Univ Paris Diderot, APC UMR7164, Paris, France

[7] Univ Trento, Dipartimento Ingn Mat & Tecnol Ind, Mesiano, Trento, Italy

[8] INFN, Grp Collegato Trento, Mesiano, Trento, Italy

[9] CNES, DCT AQ EC, F-31401 Toulouse 9, France

[10] Univ Trento, Dipartimento Ingn Meccan & Strutturale, Mesiano, Trento, Italy

[11] European Space Agcy, European Space Technol Ctr, NL-2200 AG Noordwijk, Netherlands

[12] Univ Autonoma Barcelona, IFAE, E-08193 Bellaterra, Barcelona, Spain

[13] Univ Florida, Dept Phys, Gainesville, FL 32611 USA

[14] ICE CSIC IEEC, Fac Ciencies, E-08193 Bellaterra, Barcelona, Spain

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

[16] EPSC, UPC IEEC, E-08860 Barcelona, Spain

[17] Inst Flugmech & Flugregelung, D-70569 Stuttgart, Germany

[18] Univ Glasgow, Dept Phys & Astron, Glasgow, Lanark, Scotland

[19] Univ Urbino, Ist Fis, INFN, I-61029 Urbino, PU, Italy

[20] NASA, Goddard Space Flight Ctr, Greenbelt, MD 20771 USA

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

[22] Univ London Imperial Coll Sci Technol & Med, Blackett Lab, London, England

[23] Univ Zurich, Inst Theoret Phys, CH-8057 Zurich, Switzerland

[24] NTE SENER, E-08186 Barcelona, Spain

[25] Univ Politecn Cataluna, ES-08034 Barcelona, Spain

[26] Astrium Ltd, Stevenage SG1 2AS, Herts, England

来源：

CLASSICAL AND QUANTUM GRAVITY | 2011年 / 28卷 / 09期

关键词：

DIAGNOSTICS; MISSION; SYSTEM;

D O I：

10.1088/0264-9381/28/9/094006

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

As the launch of LISA Pathfinder (LPF) draws near, more and more effort is being put in to the preparation of the data analysis activities that will be carried out during the mission operations. The operations phase of the mission will be composed of a series of experiments that will be carried out on the satellite. These experiments will be directed and analysed by the data analysis team, which is part of the operations team. The operations phase will last about 90 days, during which time the data analysis team aims to fully characterize the LPF, and in particular, its core instrument the LISA Technology Package. By analysing the various couplings present in the system, the different noise sources that will disturb the system, and through the identification of the key physical parameters of the system, a detailed noise budget of the instrument will be constructed that will allow the performance of the different subsystems to be assessed and projected towards LISA. This paper describes the various aspects of the full data analysis chain that are needed to successfully characterize the LPF and build up the noise budget during mission operations.

引用

页数：17

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