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Analysis of the Accuracy of Actuation Electronics in the Laser Interferometer Space Antenna Pathfinder

Authors :
M. Armano
H. Audley
J. Baird
M. Born
D. Bortoluzzi
N. Cardines
E. Castelli
A. Cavalleri
A. Cesarini
A. M. Cruise
K. Danzmann
M. de Deus Silva
G. Dixon
R. Dolesi
L. Ferraioli
V. Ferroni
M. Freschi
L. Gesa
D. Giardini
F. Gibert
R. Giusteri
C. Grimani
J. Grzymisch
I. Harrison
M.-S. Hartig
G. Heinzel
M. Hewitson
D. Hollington
D. Hoyland
M. Hueller
H. Inchauspe
O. Jennrich
P. Jetzer
N. Karnesis
B. Kaune
C. J. Killow
N. Korsakova
J. P. López-Zaragoza
R. Maarschalkerweerd
D. Mance
V. Martin
L. Martin Polo
J. Martino
F. Martin Porqueras
I. Mateos
P. W. McNamara
J. Mendes
L. Mendes
N. Meshksar
M. Nofrarias
S. Paczkowski
M. Perreur Lloyd
A. Petiteau
P. Pivato
E. Plagnol
J. Ramos Castro
J. Reiche
F. Rivas
D. I. Robertson
G. Russano
J. Slutsky
C. F. Sopuerta
T. Sumner
D. Texier
J. ten Pierick
J. I. Thorpe
D. Vetrugno
S. Vitale
G. Wanner
H. Ward
P. J. Wass
W. J. Weber
L. Wissel
A. Wittchen
P. Zweifel
Source :
Review of Scientific Instruments. 91
Publication Year :
2020
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2020.

Abstract

The Laser Interferometer Space Antenna Pathfinder (LPF) main observable, labelled∆g, is the differential force per unit mass acting on the two test masses in free fall condition, after the contribution of all non-gravitational forces have been compensated. At low frequencies the differential force is compensated by an applied electrostatic actuation force,which then must be subtracted from the measured acceleration to obtain∆g. Any inaccuracy in the actuation force contaminates the residual acceleration. This study investigates the accuracy of the electrostatic actuation system and its impact on the LPF main observable. It is shown that the inaccuracy is mainly caused by the rounding errors in the waveform processing and also by the random error caused by the analog to digital converter (ADC) random noise in the control loop. Both errors are one order of magnitude smaller than the resolution of the commanded voltages. We developed a simulator based on the LPF design to compute the close-to-reality actuation voltages and consequently, the resulting actuation forces. The simulator is applied in post-processing the LPF data.

Subjects

Subjects :
Instrumentation And Photography

Details

Language :
English
ISSN :
10897623 and 00346748
Volume :
91
Database :
NASA Technical Reports
Journal :
Review of Scientific Instruments
Notes :
244904, , ETH-05 16-2, , CNES 1316634, , CNRS 103747, , ANR-10-LABX-0023, , ANR-11-IDEX-0005-02, , FKZ 50OQ0501, , FKZ 50OQ1601, , AYA2010-15709, , ESP2013-47637-P, , ESP2015-67234-P, , ESP2017-90084-P, , AGAUR 2017-SGR-1469
Publication Type :
Report
Accession number :
edsnas.20205000734
Document Type :
Report
Full Text :
https://doi.org/10.1063/1.5140406