Olivier Carraz

Dr. Olivier Carraz

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Research Focus & Metrics

Academic Career Length

13Years (2014-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 October 2014 in Microgravity Science and Technology
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OCOlivier Carraz
Olivier Carraz
CSChristian Siemes
Christian Siemes
LMLuca Massotti
Luca Massotti
RHRoger Haagmans
Roger Haagmans
PSPierluigi Silvestrin
Pierluigi Silvestrin

7 July 2022 in Remote Sensing
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NZNassim Zahzam
Nassim Zahzam
BCBruno Christophe
Bruno Christophe
VLVincent Lebat
Vincent Lebat
EHEmilie Hardy
Emilie Hardy
PHPhuong-Anh Huynh
Phuong-Anh Huynh
OCOlivier Carraz
Olivier Carraz
Long-term observation of Earth’s temporal gravity field with enhanced temporal and spatial resolution is a major objective for future satellite gravity missions. Improving the performance of the accelerometers present in such missions is one of the main paths to explore. In this context, we propose to study an original concept of a hybrid accelerometer associating a state-of-the-art electrostatic accelerometer (EA) and a promising quantum sensor based on cold atom interferometry. To assess the performance potential of such an instrument, numerical simulations were performed to determine its impact in terms of gravity field retrieval. Taking advantage of the long-term stability of the cold atom interferometer (CAI), it is shown that the reduced drift of the hybrid sensor could lead to improved gravity field retrieval. Nevertheless, this gain vanishes once temporal variations of the gravity field and related aliasing effects are taken into account. Improved de-aliasing models or some specific satellite constellations are then required to maximize the impact of the accelerometer performance gain. To evaluate the achievable acceleration performance in-orbit, a numerical simulator of the hybrid accelerometer was developed and preliminary results are given. The instrument simulator was in part validated by reproducing the performance achieved with a hybrid lab prototype operating on the ground. The problem of satellite rotation impact on the CAI was also investigated both with instrument performance simulations and experimental demonstrations. It is shown that the proposed configuration, where the EA’s proof-mass acts as the reference mirror for the CAI, seems a promising approach to allow the mitigation of satellite rotation. To evaluate the feasibility of such an instrument for space applications, a preliminary design is elaborated along with a preliminary error, mass, volume, and electrical power consumption budget.

13 October 2020 in Planetary and Space Science
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FMFabian Müller
Fabian Müller
OCOlivier Carraz
Olivier Carraz
PVPieter Visser
Pieter Visser
OWOlivier Witasse
Olivier Witasse

24 June 2022 in Remote Sensing
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MPMichael Plumaris
Michael Plumaris
DDDominic Dirkx
Dominic Dirkx
CSChristian Siemes
Christian Siemes
OCOlivier Carraz
Olivier Carraz
Interplanetary missions have typically relied on Radio Science (RS) to recover gravity fields by detecting their signatures on the spacecraft trajectory. The weak gravitational fields of small bodies, coupled with the prominent influence of confounding accelerations, hinder the efficacy of this method. Meanwhile, quantum sensors based on Cold Atom Interferometry (CAI) have demonstrated absolute measurements with inherent stability and repeatability, reaching the utmost accuracy in microgravity. This work addresses the potential of CAI-based Gradiometry (CG) as a means to strengthen the RS gravity experiment for small-body missions. Phobos represents an ideal science case as astronomic observations and recent flybys have conferred enough information to define a robust orbiting strategy, whilst promoting studies linking its geodetic observables to its origin. A covariance analysis was adopted to evaluate the contribution of RS and CG in the gravity field solution, for a coupled Phobos-spacecraft state estimation incorporating one week of data. The favourable observational geometry and the small characteristic period of the gravity signal add to the competitiveness of Doppler observables. Provided that empirical accelerations can be modelled below the nm/s2 level, RS is able to infer the 6 × 6 spherical harmonic spectrum to an accuracy of 0.1–1% with respect to the homogeneous interior values. If this correlates to a density anomaly beneath the Stickney crater, RS would suffice to constrain Phobos’ origin. Yet, in event of a rubble pile or icy moon interior (or a combination thereof) CG remains imperative, enabling an accuracy below 0.1% for most of the 10 × 10 spectrum. Nevertheless, technological advancements will be needed to alleviate the current logistical challenges associated with CG operation. This work also reflects on the sensitivity of the candidate orbits with regard to dynamical model uncertainties, which are common in small-body environments. This brings confidence in the applicability of the identified geodetic estimation strategy for missions targeting other moons, particularly those of the giant planets, which are targets for robotic exploration in the coming decades.

17 December 2025 in Advances In Space Research
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JEJoão Encarnação
João Encarnação
CSChristian Siemes
Christian Siemes
IDIlias Daras
Ilias Daras
OCOlivier Carraz
Olivier Carraz
ASAaron Strangfeld
Aaron Strangfeld
RPRoland Pail
Roland Pail

18 February 2026 in Physical Review A
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NMNoémie Marquet
Noémie Marquet
YBYannick Bidel
Yannick Bidel
MCMalo Cadoret
Malo Cadoret
ABAlexis Bonnin
Alexis Bonnin
SSSylvain Schwartz
Sylvain Schwartz
NZNassim Zahzam
Nassim Zahzam