P. BOUYER - Stanford Universityweb.stanford.edu/.../18_Bouyer_Airborne_Atom_Sensors.pdfBOUYER -...
Transcript of P. BOUYER - Stanford Universityweb.stanford.edu/.../18_Bouyer_Airborne_Atom_Sensors.pdfBOUYER -...
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AIRBORNE ATOM SENSORS : FROM GROUND TO SPACE
P. BOUYER
Laboratoire Charles Fabry de l’Institut d’Optique, Palaiseau, France
Physics Dept, Stanford University, Stanford, USA
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ATOM-BASE INERTIAL SENSORS
Atom-based Inertial Sensors are based on the
manipulat ion and the control at the
"quantum level" of atoms using light or
magnetic fields.
Atomic interferometry has demonstrated over
the past 10 years chat it can be more
sensitive than other techniques (optical
interferometry, vibrating system ...).
Starts to be many laboratory experiments in
the world (in US, France, Germany, Italy): 3
leading laboratories in France and US
( S t a n f o r d , P a l a i s e a u , P a r i s ) h a v e
d e m o n s t r a t e d t h e f e a s i b i l i t y o f a
transportable inertial base using atom
interferometry.
1.4 m
2
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We use an (optical) ruler to precisely measure the (atomic) test mass position
S i m i l a r t o f a l l i n g c o r n e r c u b e gravimeter (FG5)
FG 5 : Laser phase is read by optical interferometry
Atom sensor : Laser phase is read by atom interferometry.
An Atom Interferometer “reads” the position of an atom proof mass using “atom/laser telemetry”
ATOM-BASE ACCELEROMER : BASIC PRINCIPLE
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Interference fringes : Nat~cos(2πaT2∕λ+Φ)
Extract acceleration from interference signal
From S. Merlet, et al. arXiv:0806.0164v1
ATOM-BASE ACCELEROMER : BASIC PRINCIPLE
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Interference fringes : Nat~cos(2πaT2∕λ+Φ)
Extract acceleration from interference signal
From S. Merlet, et al. arXiv:0806.0164v1
ATOM-BASE ACCELEROMER : BASIC PRINCIPLE
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ATOM-BASE GRAVIMETER
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HOW TO COPE WITH VIBRATIONS
Sensitivity improved from 80 to 30 ng/√Hz Sensitivity improved from 80 to 20 ng/√Hz
Passive/Active
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ULTIMATE SENSITIVITY : LONG BASELINE AND SPACE
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ULTIMATE SENSITIVITY : LONG BASELINE AND SPACE
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FROM GROUND TO AIRBORNE IN 0-G FLIGHT
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DEVELOPMENT OF AIRBORNE COMPONENTS
Light Source Fiber Optics
Atomic Physics Chamber :robust and flexible
Control Real-TimeComputing
Man-machine ITF
Measurement: camera accelerometer…
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I.C.E. : 0-G TESTS
First tests in March 2007 : 500 parabolas since then.
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I.C.E. : 0-G TESTS
First tests in March 2007 : 500 parabolas since then.
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Stern et al., Eur. Phys. J. D 53, 353–357 (2009)
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ATOM INTERFEROMETRY IN MICROGRAVITY
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Env. 10 mg max = 1s interrogation
Performances : 10-10 m.s-2 .Hz-1/2
100 measures ⇒ 10-11 m.s-2
Need special isolation strategy
VIBRATIONS
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VIBRATIONS
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One frequency range needs to be cancelled (directly averaged in interference signal)
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VIBRATION ISOLATION
Need to stabilize the retroreflecting mirror.
Use of piezzo-accelerometer readout and optical delay line (developped for LISA)
OPTICAL DELAY LINE DEVELOPPEDBY CEDRAT UNDER CNES CONTRACT
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VIBRATIONS IN THE PLANE
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Accelerometer wilcoxon 728 A
Atom interferometer fringes
1 ms interrogation: 1 mg/√Hz
With better reference accelerometer : 0.1 µg/√Hz
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TOWARDS COMPACT AIRBORNE SENSOR
Integrated telecoms technology (all integrated optics).
Compact and simple sensor head (10 x 10 x 50 mm3).
Scalable sensitivity/accuracy : 10 ng demonstrated
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TRANSPORTABLE SENSORS FOR GRAVITY MONITORING
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Philippe BOUYERVincent MENORETJean-Philippe BRANTUTRémi GEIGER
Arnaud LANDRAGINFrank PEREIRAChristian BORDE Alexandre BRESSONYannick BIDELFrançois DEYSACPierre TOUBOUL
Linda MONDIN
Jean MIGNOT
http://www. IFRAF.org/ http://www.atomoptic.fr/http://www.ice-space.fr/
Thomas BOURDELMartin St-VINCENTGuillaume STERNBaptiste BATTELIER
Oualid CHAIBI
Nassim ZAHZAMOlivier CARRAZ
De gauche à droite : G. Varoquaux (IO), N. Zahzam (Onera), L. Mondin (CNES), A. Bresson (Onera), P. Bouyer (IO) et A. Landragin(SYRTE).
Equipe I.C.E.