Nano-Newton electrostatic force actuators for femto-Newton-sensitive measurements: System performance test in the LISA Pathfinder mission
Creators
- 1. European Space Astronomy Centre, European Space Agency, Villanueva de la Cañada, 28692 Madrid, Spain
- 2. Albert-Einstein-Institut, Max-Planck-Institut für Gravitationsphysik und Leibniz Universität Hannover, Callinstraße 38, 30167 Hannover, Germany
- 3. Université Paris Cité, CNRS, Astroparticule et Cosmologie, F-75013 Paris, France
- 4. Dipartimento di Fisica, Università di Roma "Tor Vergata" / INFN-Sezione Roma Tor Vergata, I-00133 Roma, Italy
- 5. IRFU, CEA, Université Paris-Saclay, F-91191 Gif-sur-Yvette, France
- 6. Department of Industrial Engineering, Università di Trento and Trento Institute for Fundamental Physics and Application / INFN, I-38123 Povo, Trento, Italy
- 7. Gravitational Astrophysics Lab, NASA Goddard Space Flight Center, 8800 Greenbelt Road, Greenbelt, Maryland 20771, USA
- 8. Dipartimento di Fisica, Università di Trento and Trento Institute for Fundamental Physics and Application / INFN, I-38123 Povo, Trento, Italy
- 9. Istituto di Fotonica e Nanotecnologie, CNR-Fondazione Bruno Kessler, I-38123 Povo, Trento, Italy
Description
Electrostatic force actuation is a key component of the system of geodesic reference test masses (TM) for the LISA orbiting gravitational wave observatory and in particular for performance at low frequencies, below 1 mHz, where the observatory sensitivity is limited by stray force noise. The system needs to apply forces of order while limiting fluctuations in the measurement band to levels approaching . We present here the LISA actuation system design, based on audio-frequency voltage carrier signals, and results of its in-flight performance test with the LISA Pathfinder test mission. In LISA, TM force actuation is used to align the otherwise free-falling TM to the spacecraft-mounted optical metrology system, without any forcing along the critical gravitational wave-sensitive interferometry axes. In LISA Pathfinder, on the other hand, the actuation was used also to stabilize the TM along the critical axis joining the two TM, with the commanded actuation force entering directly into the mission's main differential acceleration science observable. The mission allowed demonstration of the full compatibility of the electrostatic actuation system with the LISA observatory requirements, including dedicated measurement campaigns to amplify, isolate, and quantify the two main force noise contributions from the actuation system, from actuator gain noise and from low frequency "in band" voltage fluctuations. These campaigns have shown actuation force noise to be a relevant, but not dominant, noise source in LISA Pathfinder and have allowed performance projections for the conditions expected in the LISA mission.
Additional details
Identifiers
- DOI
- 10.1103/PhysRevD.109.102009;
- arXiv
- arXiv:2401.00884;
- Crossref Funder ID
- 10.13039/501100004007; 10.13039/501100003981; 10.13039/100011690; 10.13039/501100000708; 10.13039/501100000853; 10.13039/501100000855; 10.13039/501100000761; 10.13039/501100000844; 10.13039/501100003006; 10.13039/100000001; 10.13039/501100002946; 10.13039/501100006360; 10.13039/100000104; 10.13039/501100004837; 10.13039/501100010198; 10.13039/501100002809; 10.13039/501100006003; 10.13039/501100002830; 10.13039/501100004794; 10.13039/100018496; 10.13039/501100005736; 10.13039/501100011072; 10.13039/501100009516;
Publishing Information
- Journal Title
- Physical Review D
- Journal Volume
- 109
- Journal Issue
- 10
- Journal Page Range
- 29 pgs.
- ISSN
- 1089-4918
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- Subject category
- S46: INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY;
- Descriptors DEI
- ACCELERATION; ACTUATORS; COMPATIBILITY; ELECTRIC POTENTIAL; FLUCTUATIONS; GRAVITATIONAL WAVES; INTERFEROMETRY; JOINING; MASS; METROLOGY; NOISE; PERFORMANCE; SENSITIVITY; SIGNALS; TIME-OF-FLIGHT METHOD; WAVE FORCES
- Descriptors DEC
- FABRICATION; VARIATIONS
Optional Information
- Copyright
- © 2024 American Physical Society
- Contract/Grant/Project number
- 2017-29-H.1-2020; ETH-05 16-2; 162449; 185051; FKZ 50OQ0501; FKZ 50OQ1601; FKZ 50OQ1801; AYA2010-15709; PID2019–106515GB-I00; ESP2013-47637-P; ESP2015-67234-P; ESP2017-90084-P; 2017-SGR-1469; CNES 1316634/CNRS 103747; ANR-10-LABX-0023; ANR-11-IDEX-0005-02
- Notes
- Contact Email: Corresponding author: vittorio.chiavegato@unitn.it; Contact Email: Corresponding author: luigi.ferraioli@erdw.ethz.ch; Contact Email: Corresponding author: williamjoseph.weber@unitn.it; Deceased.; Record automatically processed
- Funding organization
- Instituto Nazionale di Fisica Nucleare; Agenzia Spaziale Italiana; UK Space Agency; Scottish Universities Physics Alliance; University of Glasgow; University of Birmingham; Imperial College London; European Space Agency; Eidgenössische Technische Hochschule Zürich; National Science Foundation; Deutsches Zentrum für Luft- und Raumfahrt; Bundesministerium für Wirtschaft und Energie; National Aeronautics and Space Administration; Ministerio de Ciencia e Innovación; Ministerio de Asuntos Económicos y Transformación Digital, Gobierno de España; Generalitat de Catalunya; Fundación General CSIC; Centre National d'Etudes Spatiales; Centre National de la Recherche Scientifique; Observatoire de Paris, Université de Recherche Paris Sciences et Lettres; Université Paris Diderot; Labex UnivEarthS; Université Sorbonne Paris Cité; Swiss Space Office