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Modelling and simulation of the space mission MICROSCOPE

Published online by Cambridge University Press:  06 January 2010

Stefanie Bremer ,
Meike List ,
Hanns Selig  and
Claus Lämmerzahl
Stefanie Bremer
Affiliation:
ZARM, University of Bremen, Am Fallturm, 28359 Bremen, Germany email: bremer@zarm.uni-bremen.de, list@zarm.uni-bremen.de, selig@zarm.uni-bremen.de, laemmerzahl@zarm.uni-bremen.de
Meike List
Affiliation:
ZARM, University of Bremen, Am Fallturm, 28359 Bremen, Germany email: bremer@zarm.uni-bremen.de, list@zarm.uni-bremen.de, selig@zarm.uni-bremen.de, laemmerzahl@zarm.uni-bremen.de
Hanns Selig
Affiliation:
ZARM, University of Bremen, Am Fallturm, 28359 Bremen, Germany email: bremer@zarm.uni-bremen.de, list@zarm.uni-bremen.de, selig@zarm.uni-bremen.de, laemmerzahl@zarm.uni-bremen.de
Claus Lämmerzahl
Affiliation:
ZARM, University of Bremen, Am Fallturm, 28359 Bremen, Germany email: bremer@zarm.uni-bremen.de, list@zarm.uni-bremen.de, selig@zarm.uni-bremen.de, laemmerzahl@zarm.uni-bremen.de
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Abstract

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The French space mission MICROSCOPE aims at testing the weak Equivalence Principle (EP) with an accuracy of 10−15. The payload, which is developed and built by the French institute ONERA consists of two high-precision capacitive differential accelerometers. The detection of the test mass movement and their control is done via a complex electrode system. The German department ZARM is member of the MICROSCOPE performance team. In addition to drop tower tests, mission simulations and the preparation of the mission data evaluation are realized in close cooperation with the French partners CNES, ONERA and OCA. Therefore a comprehensive simulation of the real system including the science signal and all error sources is built for the development and testing of data reduction and data analysis algorithms to extract the EP violation signal. In this context the focus lays on the correct modeling of the environmental disturbances. Currently new effort to study the influence of the solar radiation and the Earth albedo to the MICROSCOPE mission scenario is underway.

Keywords

Gravitationrelativity
Type
Contributed Papers
Information
Proceedings of the International Astronomical Union , Volume 5 , Symposium S261: Relativity in Fundamental Astronomy: Dynamics, Reference Frames, and Data Analysis , April 2009 , pp. 420 - 422
Copyright
Copyright © International Astronomical Union 2010

References

Scheithauer, S. & Theil, S. 2002, Generic Drag-Free Simulator, AIAA Modeling and Simulation Conference, Monterey, CaliforniaCrossRefGoogle Scholar
Theil, S. 2002, Satellite and Test Mass Dynamics Modeling and Observation for Drag-free Satellite Control of the STEP Mission, PhD thesis, Department of Production Engineering, University of BremenGoogle Scholar
Touboul, P. & Rodrigues, M. 2001, Class. Quantum Grav., 18, 2487–98CrossRefGoogle Scholar
Chhun, R., Hudson, D., Flinoise, P., Rodrigues, M., Touboul, P., & Foulon, B. 2007, Acta Astronautica, 60, 873–879CrossRefGoogle Scholar
Cicek, M. 2005, Entwicklung und Validierung einer Methode zur Berechnung der Oberflächenkräfte auf Satelliten, Master Thesis, Hochschule ReutlingenGoogle Scholar
Guiu, É. 2007 Étalonnage de la mission spatiale MICROSCOPE: optimisation des performances, PhD Thesis, École Centrale de Nantes et l'Université de NantesGoogle Scholar
Wertz, J. R. 1978, Spacecraft Attitude Determination and Control, Kluwer Academic Publishers, Dordrecht, The NetherlandsCrossRefGoogle Scholar