A noise simulator for eLISA: Migrating LISA Pathfinder knowledge to the eLISA mission
| العنوان: | A noise simulator for eLISA: Migrating LISA Pathfinder knowledge to the eLISA mission |
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| المؤلفون: | Ferran Gibert, Daniele Vetrugno, H. Ward, Peter Wass, P. Pivato, S. Wen, Tobias Ziegler, J. Reiche, J. Gallegos, N. Korsakova, A. Cesarini, G. Russano, Gerhard Heinzel, Michele Armano, Michael Perreur-Lloyd, B. Kaune, Antoine Petiteau, S. Madden, M. Freschi, N. Brandt, Paul McNamara, Luigi Ferraioli, S. Paczkowski, Henri Inchauspe, Peter Zweifel, Nikolaos Karnesis, S. Waschke, A. Moroni, Tamara Sumner, Carlos F. Sopuerta, R. Giusteri, Ph. Jetzer, Christian J. Killow, José F. F. Mendes, U. Ragnit, J. Huesler, Daniele Bortoluzzi, L. Mendes, Ivan Lloro, Ignacio Mateos, Heather Audley, C. García Marirrodriga, P. Sarra, A. Schleicher, I. Harrison, H. B. Tu, Miquel Nofrarías, Pierre Binétruy, Rita Dolesi, Mauro Hueller, B. Johlander, Karsten Danzmann, Davor Mance, W. J. Weber, C. Trenkel, Jacob Slutsky, Valerio Ferroni, N. Dunbar, Catia Grimani, D. Texier, C. Zanoni, D. Wealthy, R. Gerndt, Martin Hewitson, Daniel Hollington, Oliver Jennrich, Ewan Fitzsimons, J. Baird, S. Vitale, Antonella Cavalleri, M. Cruise, P. Prat, A. Bursi, F. Martin-Porqueras, Lluis Gesa, G. Auger, R. Maarschalkerweerd, A. Wittchen, H. Rozemeijer, James Ira Thorpe, Domenico Giardini, J. A. Romera Perez, Eric Plagnol, V. Martín, M. Caleno, D. I. Robertson, Gudrun Wanner, Juan Ramos-Castro, M. Born, Ingo Diepholz |
| المساهمون: | AstroParticule et Cosmologie (APC (UMR_7164)), Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)-Observatoire de Paris, Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Centre National de la Recherche Scientifique (CNRS)-Université de Paris (UP), Observatoire de Paris, PSL Research University (PSL)-PSL Research University (PSL)-Université Paris Diderot - Paris 7 (UPD7)-Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)-Centre National de la Recherche Scientifique (CNRS), Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Centre National de la Recherche Scientifique (CNRS)-Université Paris Cité (UPCité), Institut National de Physique Nucléaire et de Physique des Particules du CNRS (IN2P3)-Centre National de la Recherche Scientifique (CNRS)-Commissariat à l'énergie atomique et aux énergies alternatives (CEA)-Observatoire de Paris, PSL Research University (PSL)-PSL Research University (PSL)-Université Paris Diderot - Paris 7 (UPD7) |
| المصدر: | J.Phys.Conf.Ser. Journal of Physics: Conference Series Journal of Physics: Conference Series 610 (2015), Nr. 1 Journal of Physics Conference Series 610 (2015) |
| بيانات النشر: | HAL CCSD, 2014. |
| سنة النشر: | 2014 |
| مصطلحات موضوعية: | History, noise, Astronomy, Residual, Astrophysics, programming, LISA Pathfinder, Education, Physics, Applied, System imperfections, Acceleration, Simulators, numerical methods, State space, ddc:530, [PHYS.PHYS.PHYS-INS-DET]Physics [physics]/Physics [physics]/Instrumentation and Detectors [physics.ins-det], MATLAB, Instrumental noise, numerical calculations, Simulation, Dewey Decimal Classification::500 | Naturwissenschaften, Konferenzschrift, computer.programming_language, Constellation, Physics, LISA, Spacecraft, business.industry, Noise (signal processing), Computer Science Applications, Pathfinder, Free fall, [PHYS.GRQC]Physics [physics]/General Relativity and Quantum Cosmology [gr-qc], On state, ddc:500, Dewey Decimal Classification::500 | Naturwissenschaften::530 | Physik, Residual acceleration, business, computer, Space probes, performance |
| الوصف: | We present a new technical simulator for the eLISA mission, based on state space modeling techniques and developed in MATLAB. This simulator computes the coordinate and velocity over time of each body involved in the constellation, i.e. the spacecraft and its test masses, taking into account the different disturbances and actuations. This allows studying the contribution of instrumental noises and system imperfections on the residual acceleration applied on the TMs, the latter reflecting the performance of the achieved free-fall along the sensitive axis. A preliminary version of the results is presented. Sorbonne Paris Cite/UnivEarthS Labex French Space Agency (CNES) |
| وصف الملف: | application/pdf |
| اللغة: | English |
| تدمد: | 1742-6588 |
| DOI: | 10.1088/1742-6596/610/1/012036⟩ |
| URL الوصول: | https://explore.openaire.eu/search/publication?articleId=doi_dedup___::31df4e84b1ebaea22dcf44329c48dd7b https://hal.archives-ouvertes.fr/hal-01554220 |
| Rights: | OPEN |
| رقم الانضمام: | edsair.doi.dedup.....31df4e84b1ebaea22dcf44329c48dd7b |
| قاعدة البيانات: | OpenAIRE |
| تدمد: | 17426588 |
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| DOI: | 10.1088/1742-6596/610/1/012036⟩ |