Phase noise due to vibrations in Mach-Zehnder atom interferometers - - PowerPoint PPT Presentation

phase noise due to vibrations in mach zehnder atom
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Phase noise due to vibrations in Mach-Zehnder atom interferometers - - PowerPoint PPT Presentation

Phase noise due to vibrations in Mach-Zehnder atom interferometers Universit Paul Sabatier and CNRS, Toulouse Marion Jacquey Matthias Bchner Alain Miffre Grard Trnec Jacques Vigu Funding from ANR, MENRT, CNRS, Universit P.


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SLIDE 1

Phase noise due to vibrations in Mach-Zehnder atom interferometers

Université Paul Sabatier and CNRS, Toulouse Marion Jacquey Matthias Büchner Alain Miffre Gérard Trénec Jacques Vigué

Funding from ANR, MENRT, CNRS, Université P. Sabatier, IRSAMC, Région Midi-Pyrénées, BNM/LNE

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SLIDE 2

Mach-Zehnder atom interferometers

  • perating at thermal energies

The mirrors and beam-splitters of the Mach-Zehnder optical interferometers are replaced by elastic diffraction on gratings. In the Bragg regime, diffraction of order p can be used. collimated atomic beam

exit 1 exit 2

detector 3 gratings or 3 laser standing waves

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SLIDE 3

Atom interference fringes with 7Li

diffraction order p = 1 counting time = 0.1 s/point fringe visibility V = 84.5 ± 1% mean output flux I0 = 23700 c/s

0,0 335,5 671,0 1006,5 1342,0 5k 10k 15k 20k 25k 30k 35k 40k 45k

Signal (c/s) x - position of mirror M3 (nm)

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SLIDE 4
  • 167,8

0,0 167,8 335,5 503,3 671,0 2k 4k 6k 8k 10k 12k 14k 16k

Signal (c/s) x - position of mirror (M3) (nm)

diffraction order p = 2 counting time = 0.1 s/point fringe visibility V = 54 ± 1% mean output flux I0 = 8150 c/s diffraction order p = 3 counting time = 0.1 s/point fringe visibility V = 26 ± 1% mean output flux I0 = 4870 c/s

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SLIDE 5

Interests of thermal atom interferometers

the two atomic beams are spatially separated:

  • ne can apply a perturbation on one beam only

interferometric measurements of this perturbation

A B C D

examples of such perturbations an electric field atom electric polarizability a low-pressure gas index of refraction for an atom wave

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SLIDE 6

The de Broglie wavelength λdB = h / (m v) is very small very sensitive measurements The accuracy on a phase measurement increases with the flux I0 and the fringe visibility V

∆Φmin ∝ 1 / √(I0 V2)

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SLIDE 7

Fringe visibility as a function of the diffraction order p

  • ur data points with our

lithium interferometer the data points of Siu Au Lee with a neon interferometer (PRL 75 p 2638 (1995)) Decrease of the fringe visibility:

  • either an intensity mismatch
  • or a phase averaging effect.
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SLIDE 8
  • - an intensity mismatch between the interfering beams

ρ

Visibility V as a function of the beam intensity ratio ρ for two-beam interference fringes.

  • - a phase averaging effect

a phase noise ∆φ with a Gaussian distribution

V = Vmax exp(- <∆φ2>/2)

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SLIDE 9

Inertial sensitivity of atom interferometers

applications by S. Chu (measurement of g), by M. Kasevich (gradient of g and gyrometer), by G. Tino (measurement of G) . This sensitivity is due to a phase term dependent on the grating positions

φ = p kG [x1 + x3 – 2 x2]

p is the diffraction order. x x1 x3 x2

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SLIDE 10

If the gratings are moving with respect to a Galilean frame, xi xi(ti) where ti is the time at which a given atom crosses grating Gi

φ = p kG [x1(t1) + x3 (t3) – 2 x2 (t2)]

phase noise ∆φp

with ∆φp = p ∆φ1 V = Vmax exp(- p2 <∆φ1

2>/2)

Gaussian dependence of the visibility with the diffraction order p.

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SLIDE 11

Fit of the data with V = Vmax exp(- p2 <∆φ1

2>/2)

  • ur data points

Vmax = 98 ± 1 % <∆φ12> = 0.286 ± 0.008 rad2 Siu Au Lee’s data points Vmax = 85 ± 2 % <∆φ12> = 0.650 ± 0.074 rad2

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SLIDE 12

Expansion of the inertial phase term in powers of the atom time of flight T =L/u

L intergrating distance; u atom velocity

φ = p kG [x1(t-T) + x3 (t+T) – 2 x2 (t)] φ = φbending + φSagnac + φacceleration T0 φbending = p kG [x1(t) + x3 (t) – 2 x2 (t)] Τ1 φSagnac = p kG (v3x –v1x) T T2 φacceleration = p kG (a1x + a3x) T2/2

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SLIDE 13

Estimation of the phase noise from laboratory seismic noise

Model calculation of the rail supporting the three mirrors rail treated as a beam of constant section with a neutral line X(z,t)

x z

X(z,t)

z=-L z=+L

elasticity theory ρ: density of the beam material, A: area of the beam cross-section, E: Young’s modulus of the material, Iy = ∫ x2 dx dy

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SLIDE 14

The forces and torques at the two ends ε = ± 1 of the beam are related to the derivatives of X(z,t): We assume that Myε = 0 and that the forces are the sum of an elastic term and a damping term xε(t) is the position of the support at the end ε at time t. 2 low frequency resonances (oscillation of the rail almost like a solid) a series of high frequency resonances (flexion of the rail)

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SLIDE 15

The rail of our interferometer:

  • very stiff rail with a first flexion resonance at ν =460 Hz
  • simple suspension on rubber blocks with resonances in

the 40 - 60 Hz range.

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SLIDE 16

calculated phase noise spectrum |φ(ν)|2 in rad2/Hz for diffraction order p=1

low frequency suspension resonances first flexion resonance

approximate spectrum of the seismic noise of the support |xε(ν)|2 (in 10-10 m2/Hz) calculated Sagnac only phase noise spectrum |φSagnac(ν)|2 in rad2/Hz

calculated phase noise <∆φ12> = 0.16 rad2

(measured value from visibility data <∆φ1

2> = 0.286 ± 0.008 rad2)

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SLIDE 17

Fringe visibility in Mach-Zehnder atom interferometers as a function of publication date

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SLIDE 18

Conclusion

  • the existence of an important phase noise due to vibrations in our

atom interferometer.

  • a large reduction of the fringe visibility.
  • With a very stiff rail, the dominant noise term is due to Sagnac
  • effect. Need for a better rail suspension, with low resonance

frequencies.

  • With a reduced phase noise, atom interference fringes with a high

visibility should be observed: a) with higher diffraction orders p larger separation of the atomic beams b) with slower atomic beams the time of flight T=L/u increases when the velocity u decreases (Sagnac phase term ∝ T and acceleration phase term ∝ T2).

All my thanks!

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SLIDE 19

x

pλdB/2

φ = p kG (x1 + x3- 2x2)

Main advantage: this non dispersive phase is useful to

  • bserve interference fringes

Main problem: a high stability of the grating positions is needed (for example: in our experiment, a 1 radians phase shift corresponds to a variation of x1 or x3 of 53 nm)

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SLIDE 20

Phase shift induced by the electric field

Io = 100 000 c/s V = 62 %

50 100 150 200 250 300 350 400 450 500 20k 40k 60k 80k 100k 120k 140k 160k 180k

Signal (c/s)

Applied voltage V0 = 260 Volts Applied voltage V0 = 0 Volts

I0 = 100 000 c/s V = 43 %

h l b

counting time 0.36 s per data point

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SLIDE 21

Phase shift and visibility reduction due to the electric field

40 80 120 160 200 240 280 320 360 400 440 480 3 6 9 12 15 18 21 24 27

Applied voltage (Volts)

Phas shift (rad)

40 80 120 160 200 240 280 320 360 400 440 480 0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0

V/V0 Applied voltage (Volts)

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SLIDE 22

40 80 120 160 200 240 280 320 360 400 440 0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8 0,9 1,0

V isibility V /V A pplied V

  • ltage (V
  • lts)

40 80 120 160 200 240 280 320 360 400 440 3 6 9 12 15 18 21 24 27

Applied voltage (Volts) Phase shift (rad)

40 80 120 160 200 240 280 320 360 400 440

  • 0,2
  • 0,1

0,0 0,1 0,2

S// = 8,00 ± 0,06 Φm/V0² = (1,3870 ± 0,0010) × 10-4 rad.V-2

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SLIDE 23

Lithium electric polarizability values

164.111 ± 0.002 164.2 ± 0.1 169.946 164.2 ± 1.1 163.98 ± 3.4

Result atomic units Kassimi and Thakkar, extrapolated value from MP2,MP3 et MP4 calculations (1994)* Drake et al., Hylleraas calculation (1996) # Kassimi and Thakkar, Hartree- Fock calculation (1994)*

24.33 ± 0.16

Our experiment (2005)

24.3 ± 0.5

  • B. Bederson et al. (experiment

1974) Result

10-30 m3

Experiment or calculation * Phys.Rev. A 50, 2948 (1994) # Phys.Rev. A 54, 2824 (1996)