Search

Your search keyword '"R. Gerndt"' showing total 8 results
Start Over Author "R. Gerndt" Topic computer science applications
8 results on '"R. Gerndt"'

1. LISA Pathfinder closed-loop analysis: a model breakdown of the in-loop observables

Author

Ph. Jetzer, W. J. Weber, Lluis Gesa, Karsten Danzmann, Alexander Schleicher, F. Rivas, R. Maarschalkerweerd, A. Wittchen, J. Grzymisch, Antoine Petiteau, Paul McNamara, D. Wealthy, Gudrun Wanner, Juan Ramos-Castro, H. Rozemeijer, D. Shaul, H. Ward, Eric Plagnol, Catia Grimani, Ian Harrison, Henri Inchauspe, Ignacio Mateos, Carlos F. Sopuerta, Domenico Giardini, A. Zambotti, Michael Troebs, C. Zanoni, P. Prat, R. De Rosa, Michele Armano, B. Kaune, A. Lobo, S. Madden, Antonella Cavalleri, M. Freschi, C. Garcia Marrirodriga, N. Dunbar, M. de Deus Silva, R. Gerndt, J. Baird, M. Bassan, J. Martino, L. Mendel, Daniele Vetrugno, L. Wissel, Pierre Binétruy, L. Di Fiore, J. P. López-Zaragoza, J. Reiche, Martin Hewitson, E. D. Fitzsimons, Oliver Jennrich, Daniel Hollington, Víctor S. Martín, Daniele Bortoluzzi, A. Cesarini, Michael Perreur-Lloyd, G. Russano, Ferran Gibert, Tobias Ziegler, P. Pivato, Gerard Auger, R. Giusteri, M. Caleno, N. Korsakova, Ingo Diepholz, Miquel Nofrarías, Ivan Lloro, M. Cruise, D. I. Robertson, Peter Zweifel, M. Hueller, Luigi Ferraioli, Ruggero Stanga, Tamara Sumner, R. Flatscher, Aniello Grado, Heather Audley, U. Ragnit, N. Karnesis, Rita Dolesi, José F. F. Mendes, Davor Mance, B. Johlander, D. Texier, Jacob Slutsky, Valerio Ferroni, M. Born, D. Hoyland, Peter Wass, James Ira Thorpe, L. Martin-Polo, F. Martin-Porqueras, C. Trenke, S. Paczkowski, P. Sarra, S. Vitale, N. Brandt, L. Liu, Christian J. Killow, Gerhard Heinzel, and LISA Pathfinder Collaboration

Subjects
Physics, History, Science & Technology, 02 Physical Sciences, Observable, Astronomy & Astrophysics, 01 natural sciences, 09 Engineering, Computer Science Applications, Education, Loop (topology), Pathfinder, Control theory, 0103 physical sciences, Physical Sciences, 010306 general physics, Closed loop analysis
Abstract

This paper describes a methodology to analyze, in the frequency domain, the steady-state control performances of the LISA Pathfinder mission. In particular, it provides a technical framework to give a comprehensive understanding of the spectra of all the degrees of freedom by breaking them down into their various physical origins, hence bringing out the major contributions of the control residuals. A reconstruction of the measured in-loop output, extracted from a model of the closed-loop system, is shown as an instance to illustrate the potential of such a model breakdown of the data.

Published
2017

2. LISA Pathfinder: First steps to observing gravitational waves from space

Author

N. Karnesis, C. Garca Marrirodriga, Michele Armano, Ian Harrison, Jacob Slutsky, Valerio Ferroni, D. Hoyland, M. Freschi, Henri Inchauspe, M. Cruise, Daniele Vetrugno, Michael Perreur-Lloyd, Gerhard Heinzel, F. Rivas, Lluis Gesa, Ignacio Mateos, P. Pivato, Ph. Jetzer, Gudrun Wanner, Juan Ramos-Castro, R. Maarschalkerweerd, A. Wittchen, R. Gerndt, Peter Wass, Karsten Danzmann, Antoine Petiteau, Paul McNamara, S. Paczkowski, L. Liu, Carlos F. Sopuerta, R. Giusteri, P. Prat, N. Dunbar, Antonella Cavalleri, S. Vitale, L. Martin-Polo, J. Baird, U. Ragnit, Christian J. Killow, Domenico Giardini, M. de Deus Silva, Rita Dolesi, P. Sarra, H. Rozemeijer, Tobias Ziegler, R. De Rosa, J. Reiche, A. Zambotti, W. J. Weber, D. Shaul, A. Cesarini, G. Russano, M. Bassan, M. Hueller, J. Martino, E. D. Fitzsimons, Alexander Schleicher, R. Flatscher, Catia Grimani, F. Martin-Porqueras, Michael Troebs, Peter Zweifel, J. Grzymisch, M. Born, N. Korsakova, Aniello Grado, Heather Audley, H. Ward, Pierre Binétruy, James Ira Thorpe, L. Wissel, Daniele Bortoluzzi, L. Mendes, B. Johlander, Miquel Nofrarías, C. Zanoni, Eric Plagnol, Ruggero Stanga, Ingo Diepholz, A. Lobo, Martin Hewitson, Daniel Hollington, L. Di Fiore, Oliver Jennrich, M. Caleno, D. Wealthy, D. I. Robertson, C. Trenkel, Luigi Ferraioli, Tamara Sumner, Davor Mance, D. Texier, B. Kaune, S. Madden, Ivan Lloro, José F. F. Mendes, Víctor S. Martín, N. Brandt, J. P. López-Zaragoza, Ferran Gibert, Gerard Auger, and LISA Pathfinder Collaboration

Subjects
Physics, History, Science & Technology, 02 Physical Sciences, Gravitational wave, Settore FIS/01 - Fisica Sperimentale, Astronomy, Astronomy & Astrophysics, Space (mathematics), 09 Engineering, Computer Science Applications, Education, Pathfinder, Physical Sciences
Abstract

LISA Pathfinder, the European Space Agency's technology demonstrator mission for future spaceborne gravitational wave observatories, was launched on 3 December 2015, from the European space port of Kourou, French Guiana. After a short duration transfer to the final science orbit, the mission has been gathering science data since. This data has allowed the science community to validate the critical technologies and measurement principle for low frequency gravitational wave detection and thereby confirming the readiness to start the next generation gravitational wave observatories, such as LISA. This paper will briefly describe the mission, followed by a description of the science operations highlighting the performance achieved. Details of the various experiments performed during the nominal science operations phase can be found in accompanying papers in this volume.

Published
2017

3. Free-flight experiments in LISA Pathfinder

Author

C. Trenkel, F. Martin-Porqueras, J. Baird, Nikolaos Karnesis, Lluis Gesa, R. Gerndt, Paul McNamara, A. Bursi, A. Moroni, G. Auger, Curt Cutler, Karsten Danzmann, James Ira Thorpe, Valerio Ferroni, Gerhard Heinzel, C. Zanoni, Ian Harrison, R. Maarschalkerweerd, B. Johlander, Carlos F. Sopuerta, Michael Perreur-Lloyd, Rita Dolesi, R. Giusteri, M. Born, A. Schleicher, Daniele Vetrugno, N. Dunbar, P. Sarra, Luis Mendes, Peter Wass, Daniel Hollington, T. J. Sumner, Eric Plagnol, C. García Marirrodriga, B. Kaune, A. Wittchen, H. Rozemeijer, U. Ragnit, N. Brandt, H. Ward, S. Madden, D. Wealthy, Ingo Diepholz, P. Prat, P. Pivato, Mauro Hueller, H. B. Tu, Víctor S. Martín, Ewan Fitzsimons, Antonella Cavalleri, S. Paczkowski, Jacob Slutsky, M. Cruise, Michele Armano, Pierre Binetruy, J. A. Romera Perez, Davor Mance, José F. F. Mendes, Gudrun Wanner, Stefano Vitale, Juan Ramos-Castro, Philippe Jetzer, W. J. Weber, M. Freschi, Ivan Lloro, D. Texier, Domenico Giardini, S. Waschke, Antoine Petiteau, J. Huesler, J. Reiche, Oliver Jennrich, A. Cesarini, G. Russano, Tobias Ziegler, N. Korsakova, Peter Zweifel, H. Inchauspe, Catia Grimani, P. Maghami, Heather Audley, S. Wen, M. Caleno, D. I. Robertson, Christian J. Killow, Martin Hewitson, Luigi Ferraioli, Ignacio Mateos, Daniele Bortoluzzi, Miquel Nofrarías, J. Gallegos, and Ferran Gibert

Subjects
History, Inertial frame of reference, Testing, Orbits, General Relativity and Quantum Cosmology, LISA Pathfinder, Gravitational wave detectors, Primary (astronomy), Free flight, Spacecraft, Dewey Decimal Classification::500 | Naturwissenschaften, Physics, Noise source, Astrophysics::Instrumentation and Methods for Astrophysics, Flight experiments, Computer Science Applications, Drag, Tracking (position), Physics::Space Physics, Astrophysics::Earth and Planetary Astrophysics, ddc:500, Astrophysics - Instrumentation and Methods for Astrophysics, Space probes, realizations, Gravitation, spaced data, On-orbit performance, spectral-analysis, FOS: Physical sciences, General Relativity and Quantum Cosmology (gr-qc), Gravity waves, Education, Acceleration, Space-based, Mission requirements, ddc:530, Aerospace engineering, Instrumentation and Methods for Astrophysics (astro-ph.IM), Konferenzschrift, algorithm, business.industry, Gravitational wave, Noise, Pathfinder, Potential sources, Dewey Decimal Classification::500 | Naturwissenschaften::530 | Physik, business
Abstract

The LISA Pathfinder mission will demonstrate the technology of drag-free test masses for use as inertial references in future space-based gravitational wave detectors. To accomplish this, the Pathfinder spacecraft will perform drag-free flight about a test mass while measuring the acceleration of this primary test mass relative to a second reference test mass. Because the reference test mass is contained within the same spacecraft, it is necessary to apply forces on it to maintain its position and attitude relative to the spacecraft. These forces are a potential source of acceleration noise in the LISA Pathfinder system that are not present in the full LISA configuration. While LISA Pathfinder has been designed to meet it's primary mission requirements in the presence of this noise, recent estimates suggest that the on-orbit performance may be limited by this `suspension noise'. The drift-mode or free-flight experiments provide an opportunity to mitigate this noise source and further characterize the underlying disturbances that are of interest to the designers of LISA-like instruments. This article provides a high-level overview of these experiments and the methods under development to analyze the resulting data., 13 pages, 5 figures. Accepted to Journal Of Physics, Conference Series. Presented at 10th International LISA Symposium, May 2014, Gainesville, FL, USA

Published
2015
Full Text
View/download PDF

4. In-flight thermal experiments for LISA Pathfinder: Simulating temperature noise at the Inertial Sensors

Author

Ivan Lloro, Antoine Petiteau, Paul McNamara, J. Huesler, C. Zanoni, M. Cruise, Stefano Vitale, Martin Hewitson, Carlos F. Sopuerta, Gerhard Heinzel, Daniel Hollington, S. Paczkowski, N. Brandt, Nikolaos Karnesis, Daniele Bortoluzzi, Daniele Vetrugno, L. Mendes, Ignacio Mateos, H. B. Tu, H. Ward, G. Auger, Miquel Nofrarías, P. Pivato, S. Wen, Tobias Ziegler, P. Sarra, A. Schleicher, A. Bursi, Antonella Cavalleri, S. Waschke, Michele Armano, F. Martin-Porqueras, Oliver Jennrich, Christian J. Killow, R. Maarschalkerweerd, D. Wealthy, A. Wittchen, M. Freschi, J. A. Perez Romera, P. Prat, C. García Marirrodriga, Heather Audley, H. Rozemeijer, Michael Perreur-Lloyd, Ewan Fitzsimons, Ingo Diepholz, Mauro Hueller, Peter Wass, Pierre Binétruy, M. Born, C. Trenkel, M. Caleno, B. Johlander, James Ira Thorpe, A. Moroni, D. I. Robertson, Gudrun Wanner, Juan Ramos-Castro, José F. F. Mendes, Eric Plagnol, V. Martín, Domenico Giardini, N. Dunbar, Catia Grimani, P. Maghami, R. Giusteri, R. Gerndt, Rita Dolesi, Ph. Jetzer, Karsten Danzmann, B. Kaune, S. Madden, Henri Inchauspe, I. Harrison, Davor Mance, D. Texier, J. Gallegos, Ferran Gibert, Luigi Ferraioli, Tamara Sumner, L. l. Gesa, J. Reiche, A. Cesarini, G. Russano, Jacob Slutsky, Valerio Ferroni, Peter Zweifel, U. Ragnit, W. J. Weber, J. Baird, and N. Korsakova

Subjects
History, Astronomy & Astrophysics, Noise (electronics), Education, Physics, Applied, Inertial measurement unit, ddc:530, Aerospace engineering, Konferenzschrift, Dewey Decimal Classification::500 | Naturwissenschaften, Physics, Spacecraft, Gravitational wave, business.industry, Detector, Electrical engineering, Computer Science Applications, Pathfinder, Physics::Space Physics, Measuring instrument, Brownian noise, ddc:500, Dewey Decimal Classification::500 | Naturwissenschaften::530 | Physik, business
Abstract

Thermal Diagnostics experiments to be carried out on board LISA Pathfinder (LPF) will yield a detailed characterisation of how temperature fluctuations affect the LTP (LISA Technology Package) instrument performance, a crucial information for future space based gravitational wave detectors as the proposed eLISA. Amongst them, the study of temperature gradient fluctuations around the test masses of the Inertial Sensors will provide as well information regarding the contribution of the Brownian noise, which is expected to limit the LTP sensitivity at frequencies close to 1mHz during some LTP experiments. In this paper we report on how these kind of Thermal Diagnostics experiments were simulated in the last LPF Simulation Campaign (November, 2013) involving all the LPF Data Analysis team and using an end-to-end simulator of the whole spacecraft. Such simulation campaign was conducted under the framework of the preparation for LPF operations. Spanish Ministry of Science and Innovation (MICINN)/AYA2010-15709

Published
2015
Full Text
View/download PDF

5. Disentangling the magnetic force noise contribution in LISA Pathfinder

Author

M Armano, H Audley, G Auger, J Baird, P Binetruy, M Born, D Bortoluzzi, N Brandt, A Bursi, M Caleno, A Cavalleri, A Cesarini, M Cruise, K Danzmann, I Diepholz, R Dolesi, N Dunbar, L Ferraioli, V Ferroni, E Fitzsimons, M Freschi, J Gallegos, C García Marirrodriga, R Gerndt, LI Gesa, F Gibert, D Giardini, R Giusteri, C Grimani, I Harrison, G Heinzel, M Hewitson, D Hollington, M Hueller, J Huesler, H Inchauspé, O Jennrich, P Jetzer, B Johlander, N Karnesis, B Kaune, N Korsakova, C Killow, I Lloro, R Maarschalkerweerd, S Madden, D Mance, V Martín, F Martin-Porqueras, I Mateos, P McNamara, J Mendes, L Mendes, A Moroni, M Nofrarias, S Paczkowski, M Perreur-Lloyd, A Petiteau, P Pivato, E Plagnol, P Prat, U Ragnit, J Ramos-Castro, J Reiche, J A Romera Perez, D Robertson, H Rozemeijer, G Russano, P Sarra, A Schleicher, J Slutsky, C F Sopuerta, T Sumner, D Texier, J Thorpe, C Trenkel, H B Tu, D Vetrugno, S Vitale, G Wanner, H Ward, S Waschke, P Wass, D Wealthy, S Wen, W Weber, A Wittchen, C Zanoni, T Ziegler, and P Zweifel

Subjects
History, Magnetometer, Astronomy, Astrophysics, 01 natural sciences, LISA Pathfinder, Displacement (vector), Physics, Applied, Education, law.invention, Magnetization, law, 0103 physical sciences, ddc:530, 010303 astronomy & astrophysics, Konferenzschrift, Dewey Decimal Classification::500 | Naturwissenschaften, Physics, 010308 nuclear & particles physics, business.industry, Electrical engineering, Computer Science Applications, Computational physics, Magnetic field, Coupling (physics), Pathfinder, ddc:500, Dewey Decimal Classification::500 | Naturwissenschaften::530 | Physik, business, Excitation, Noise (radio)
Abstract

Magnetically-induced forces on the inertial masses on-board LISA Pathfinder are expected to be one of the dominant contributions to the mission noise budget, accounting for up to 40%. The origin of this disturbance is the coupling of the residual magnetization and susceptibility of the test masses with the environmental magnetic field. In order to fully understand this important part of the noise model, a set of coils and magnetometers are integrated as a part of the diagnostics subsystem. During operations a sequence of magnetic excitations will be applied to precisely determine the coupling of the magnetic environment to the test mass displacement using the on-board magnetometers. Since no direct measurement of the magnetic field in the test mass position will be available, an extrapolation of the magnetic measurements to the test mass position will be carried out as a part of the data analysis activities. In this paper we show the first results on the magnetic experiments during an end-to-end LISA Pathfinder simulation, and we describe the methods under development to map the magnetic field on-board. A post-publication change was made to this article on 26 Jun 2020 to add an author.

Published
2015

6. A noise simulator for eLISA: Migrating LISA Pathfinder knowledge to the eLISA mission

Author

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, 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, and PSL Research University (PSL)-PSL Research University (PSL)-Université Paris Diderot - Paris 7 (UPD7)

Subjects
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
Abstract

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)

Published
2014

7. Bayesian statistics for the calibration of the LISA Pathfinder experiment

Author

M Armano, H Audley, G Auger, P Binetruy, M Born, D Bortoluzzi, N Brandt, A Bursi, M Caleno, A Cavalleri, A Cesarini, M Cruise, K Danzmann, I Diepholz, R Dolesi, N Dunbar, L Ferraioli, V Ferroni, E Fitzsimons, M Freschi, C García Marirrodriga, R Gerndt, L Gesa, F Gibert, D Giardini, R Giusteri, C Grimani, I Harrison, G Heinzel, M Hewitson, D Hollington, M Hueller, J Huesler, H Inchauspé, O Jennrich, P Jetzer, B Johlander, N Karnesis, B Kaune, N Korsakova, C Killow, I Lloro, R Maarschalkerweerd, S Madden, D Mance, V Martin, F Martin-Porqueras, I Mateos, P McNamara, J Mendes, E Mitchell, A Moroni, M Nofrarias, S Paczkowski, M Perreur-Lloyd, P Pivato, E Plagnol, P Prat, U Ragnit, J Ramos-Castro, J Reiche, J A Romera Perez, D Robertson, H Rozemeijer, G Russano, P Sarra, A Schleicher, J Slutsky, C F Sopuerta, T Sumner, D Texier, J Thorpe, C Trenkel, H B Tu, D Vetrugno, S Vitale, G Wanner, H Ward, S Waschke, P Wass, D Wealthy, S Wen, W Weber, A Wittchen, C Zanoni, T Ziegler, P Zweifel, AstroParticule et Cosmologie (APC (UMR_7164)), 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), 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), 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), and Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Centre National de la Recherche Scientifique (CNRS)-Université Paris Cité (UPCité)

Subjects
History, MATLAB, detector: satellite, Calibration (statistics), Astronomy, Bayesian probability, Lisa technology packages, Gravity waves, computer.software_genre, Astrophysics, Bayesian statistics, 01 natural sciences, Degrees of freedom (mechanics), LISA Pathfinder, Education, Physics, Applied, Gravitational wave detectors, Theoretical physics, Matlab toolboxes, Operational simulations, 0103 physical sciences, numerical methods, ddc:530, [PHYS.PHYS.PHYS-INS-DET]Physics [physics]/Physics [physics]/Instrumentation and Detectors [physics.ins-det], noise: acceleration, 010306 general physics, Dewey Decimal Classification::500 | Naturwissenschaften, Konferenzschrift, Mathematics, Data processing, 010308 nuclear & particles physics, Design of experiments, System identification, statistical analysis: Bayesian, Analysis strategies, gravitational radiation detector, Computer Science Applications, Pathfinder, LISA: calibration, gravitational radiation: emission, [PHYS.GRQC]Physics [physics]/General Relativity and Quantum Cosmology [gr-qc], Bayesian Analysis, Noise (video), Data mining, ddc:500, Dewey Decimal Classification::500 | Naturwissenschaften::530 | Physik, computer, Space probes
Abstract

The main goal of LISA Pathfinder (LPF) mission is to estimate the acceleration noise models of the overall LISA Technology Package (LTP) experiment on-board. This will be of crucial importance for the future space-based Gravitational-Wave (GW) detectors, like eLISA. Here, we present the Bayesian analysis framework to process the planned system identification experiments designed for that purpose. In particular, we focus on the analysis strategies to predict the accuracy of the parameters that describe the system in all degrees of freedom. The data sets were generated during the latest operational simulations organised by the data analysis team and this work is part of the LTPDA Matlab toolbox. A post-publication change was made to this article on 26 Jun 2020 to add an author.

Published
2014

8. LTP – LISA technology package: Development challenges of a spaceborne fundamental physics experiment

Author

R Gerndt and the entire LTP Team

Subjects
History, Attitude control system, Engineering, Spacecraft, business.industry, Payload, Electrical engineering, Computer Science Applications, Education, Pathfinder, Software, Fundamental physics, Systems engineering, business
Abstract

The LISA Technology Package (LTP) is the main payload onboard the LISA Pathfinder Spacecraft. The LTP Instrument together with the Drag-Free Attitude Control System (DFACS) and the respective LTP and DFACS operational software forms the LTP Experiment. It is completed by the FEEPs of the LPF spacecraft that are controlled by DFACS in order to control the spacecraft's attitude along with the experiment's needs. This article concentrates on aspects of the Industrial development of the LTP Instrument items and on essential performance issues of LTP. Examples of investigations on specific issue will highlight the kind of special problems to be solved for LTP in close cooperation with the Scientific Community.

Published
2009

Catalog

Books, media, physical & digital resources
See catalog results