Improved noise cold atom sensor

Abstract

The invention relates to an ultracold atom sensor (10) comprising: an atom chip (ACh) including a first and a second waveguide (CPWX1, CPWX2) adapted for the propagation of microwave waves and direct currents, at least a first conducting wire (WIz) and a second conducting wire (WId, WId1) whose respective projections intersect at a point defining a first crossing point (C1), an atom generation device (ACG), a power supply device (PSD) including at least one microwave generator (GMW) and at least one direct current generator (DCG), said power supply device being configured to apply to said first and second waveguides, for the spatial separation of the two traps, said microwave signals to initiate said spatial separation, then said CMW electric currents in place of said microwave signals to maintain said spatial separation, Figure 7

Description

Title of the invention: Improved noise cold atom sensor FIELD OF THE INVENTION

[0001] The present invention lies in the field of inertial sensors and more specifically cold atom inertial sensors integrated on an atomic chip. More particularly, the invention relates to cold atom sensors on an atomic chip using microwave fields for the spatial separation of the two states used when measuring inertial parameters (typically acceleration and rotational speed). STATE OF THE ART

[0002] A cold atom interferometer interferes two electronic states, called the first internal state la> and the second internal state lb> of an atom, such as rubidium 87, in a Ramsey-type sequence. A Ramsey-type interferometer sequence measures a phase q> accumulated during the implementation of the sequence, from a measurement of at least one population of a chosen state la> or lb> (preferably a measurement of both populations for greater precision). The populations pa and pb respectively of the two states la> and lb> at the output of the interferometer are given by:

[0003] pa=l[l-cos( <p)] (D

[0004] pfe = l[l + cOS( <p)] (2)

[0005] The phase q> is related to the energy difference between E'b and E'a, respectively equal to the energies of the states a> and lb> modified by the implementation of the interferometric sequence.

[0006] and

[0007] 9=^Tr. (3)

[0008] with w the pulsation of the local oscillator producing the two pulses æ / 2 at the beginning and at the end of the interferometric sequence and TR the Ramsey time, that is to say the time elapsed between the two pulses tt / 2.

[0009] Let: [0°101 / < = 1[ l-cos(S^ TR-„>TR) ] w [00111 +

[0012] It is assumed that before the start of the Ramsey sequence all atoms are in the state la> as well as Eb > Ea with Ea and Eb the atomic energies of the states depending on the atom and the transition considered.

[0013] To make this interferometer sensitive to accelerations and rotations, it is necessary:

[0014] In the case of accelerations, separate the two states then recombine them, that is to say move them along a straight line, from their initial positions which are identical, in two opposite directions then make them follow the same trajectory in the opposite direction until they return to the same position. This makes it possible to add to the energy difference between the two states a term linked to the potential acceleration energy.

[0015] In the case of rotations, the two states must both travel a closed trajectory including a non-zero area and this in opposite directions for la> and lb>. Thus, we add to the energy difference between the two states a term dependent on the Sagnac effect and therefore on the rotation speed.

[0016] To achieve these trajectories, a known method is to use microwave separators (waveguides in which microwave signals are applied). The microwave fields created then create a "dressing" of the states, which has the effect of creating a force allowing them to be moved. This dressing modifies the energies of the states 1a> and 1b>, from Ea to E'a and from Eb to E'b.

[0017] The structure and operating principle of a gyrometer type sensor is described in documents US 15 / 778605, US 17 / 924340, US 17 / 832615 and US 17 / 832616 and is recalled below. For example, document WO2017089489 describes an inertial sensor of the gyroscope type with ultracold atoms on a chip, using trapped matter waves describing closed trajectories including an area.

[0018] Rotation measurements on this type of device are carried out by exploiting the Sagnac effect. The phase shift 6 induced by the Sagnac effect between two counter-rotating matter waves in a frame of reference rotating at angular speed Q is given by:

[0019]

[0020] where A is the area inscribed in the atomic trajectories, m the mass of the atoms and h the reduced Planck constant.

[0021] Ultracold atoms are defined as atoms whose temperature is less than 400 nanokelvins, preferably 300 nanokelvins. The temperature of thermal ultracold atoms is, for example for Rubidium atoms, between 50 and 400 nanokelvins and preferably between 100 and 300 nanokelvins.

[0022] The principle is to create a trajectory traveled in a counterpropagative manner by two clouds of magnetically trapped atoms. The creation and movement of the magnetic trap along the trajectory are carried out by conductive wires and microwave guides according to, for example, the topology illustrated [Fig.l].

[0023] Figure 1 schematically illustrates a chip 1 with ultracold atoms 12 as well as the trajectory 16 of two atomic clouds CL1 and CL2. A part of the surface of the chip 1 forms a measurement plane 13. An axis normal to the measurement plane 13 defines the axis Z measurement, according to which a rotation measurement Qz is carried out by the gyrometer.

[0024] The chip 1 comprises means adapted to generate a first ultra-cold atom trap T1 and a second ultra-cold atom trap T2, a trap making it possible to immobilize a cloud of ultra-cold atoms 12 in an internal state different from the other trap, at a predetermined distance h from said measurement plane 13. For example, the trap T1 comprises the atoms in the electronic level or state 1a> (cloud CL1) and the trap T2 comprises atoms in the state 1b> (cloud CL2). The levels 1a> and 1b> are spaced apart by a frequency co0 / 2jr. For example, in the case of rubidium 87, these are the two hyperfine levels IF=1,mF=-1> and IF=2,mF=1>, spaced apart by approximately 6.8 GHz.

[0025] These means also make it possible to move the clouds along the trajectory 16 located in a plane parallel to the measurement plane 13, at a height h from this plane, as illustrated [Fig.l]. These means consist of waveguides and conductive wires as described below.

[0026] The means comprise a first waveguide CPW1 and a second waveguide CPW2 adapted to the propagation of microwaves at cob and coa pulses. The waveguides are arranged symmetrically with respect to a Y axis of the measurement plane, preferably parallel. The two waveguides CPW1 and CPW2 are connected to at least one microwave frequency voltage or current generator. For example, each of the waveguides is produced by depositing three parallel conductive wires to produce a coplanar waveguide. In other embodiments, other types of waveguides may be used, in particular waveguides whose manufacture is compatible with microfabrication techniques by deposition or by etching. For example, a microstrip line may be produced.

[0027] The means also comprise conductive wires integrated into the chip 1 and adapted to be crossed by direct currents. The conductive wires are distributed into a conductive wire WIz along an axis of symmetry Y perpendicular to X and included in the measurement plane 13, and into a plurality of n conductive wires Wldi, i index varying from 1 to n, parallel to each other and parallel to the axis X, n being at least equal to 2. In the example of [Fig.l] n=3, i.e. three conductive wires Wldl, WId2 and WId3. The wires are arranged so as to define n crossing points Ci (crossing between WIz and Wldi) located on the axis Y, here 3 crossing points Cl, C2, C3.

[0028] Each conductive wire is connected to one or more current and / or voltage generators, themselves connected to a processing unit comprising at least one microprocessor. The voltage and / or current generators make it possible to control both direct currents and alternating currents in the wires. In particular, direct currents are controlled in the conductive wires.

[0029] In the sensor, the atom chip 1 is placed in a vacuum chamber maintained, for example, using an ion pump and preferably comprising shielding magnetic. The sensor includes an ultracold atom generation device which includes:

[0030] - an atom emitter (dispenser in English), for example produced by a heating filament delivering a rubidium vapor;

[0031] -a primary atom trap (optical and / or magnetic), allowing pre-cooling and arranging a cloud of ultracold atoms in the vicinity of the chip, to load the magnetic traps T1 and T2 described later with atoms.

[0032] The sensor also comprises a magnetic field source, external to the chip 1. It makes it possible to impose a homogeneous and stationary magnetic field Bc over a thickness at least of the order of a height h above the measurement plane 13. Advantageously, the direction of the homogeneous magnetic field is parallel to the measurement plane.

[0033] In [Fig.l] the dotted trajectory 16 illustrates the trajectory of the ultracold atom clouds 12. This closed trajectory defines an area denoted A. A distance h separates the plane of the trajectory 16 and the measurement plane 13 of the chip. Preferably h is between 500 nm and 1 mm, and preferably between 5 pm and 500 pm.

[0034] [Fig.2] illustrates the geometry of the guides and wires of the atomic chip as well as the traps T1 and T2.

[0035] The specific arrangement of the conductive wires and the waveguides, associated with the homogeneous magnetic field source, makes it possible to easily obtain two traps T1 and T2 as illustrated in part a) of [Fig.2]. Each trap T1 and T2 has a non-zero and identical minimum value V0, and an identical curvature, a necessary condition for the sensor to operate. Indeed, as explained later, when a direct current is applied to at least two conductive wires of a crossing point, the minimum potential is located vertically above this crossing point. When then a microwave power is sent into the waveguides, the central minimum is transformed into two minima on either side of the initial minimum in the direction of the waveguides.If the initial minimum is not located strictly at an equal distance from the two waveguides, the two potential minima created will not have strictly the same value of the minimum V0 and the same curvature.

[0036] Part c) of [Fig.2] illustrates the arrangement of the conductive wires defining the initial crossing point Cl and the waveguides (top view). Part b) of [Fig.2] describes the corresponding arrangement of the conductive wires and waveguides printed on a chip in profile view, in section along the conductive wire Wldl which crosses the conductive wire WIz along the axis of symmetry Y. The waveguides CPW1 and CPW2 are coplanar waveguides located on a first level NI. The insulating layer 18 advantageously makes it possible to flatten the measurement plane. The material of the The electrical insulating layer may be, for example, silicon dioxide, silicon nitride or benzocyclobutene. A conductive material is used for the manufacture of the conductive wires, for example gold, and is deposited on a substrate 15, forming a second level N2. The substrate may be, for example, silicon, aluminum nitride or silicon carbide.

[0037] Part a) shows the symmetrical separation of ultracold atoms, specific to the internal state of said ultracold atoms, and more precisely the variations in potentials as a function of the X axis of chip 1.

[0038] Curve "a" shows a potential well corresponding to the association of the homogeneous magnetic field and the field created by two intersecting conductive wires, the wire WIz carried by the current Iz and the wire Wldl carried by the current Idl. This results in a local potential well forming an atomic trap T in three dimensions. A cloud of ultracold atoms can be trapped and cooled there.

[0039] Curve "b" schematically shows the potential created by the transmission of microwaves at the cob frequency in the waveguide CPW1. The field emitted by the passage of microwaves at the cob frequency makes it possible to modify the energy of the ultracold atoms and to move the atoms of internal states lb>. Curve "e" illustrates the potential seen by the internal states lb> due to the contributions of the potentials illustrated by curve "a" and by curve "b". Curve "e" shows a local minimum of potential making it possible to locally trap a cloud of ultracold atoms of internal states lb>.

[0040] Similarly, curve "d" schematically shows the potential created by the transmission of microwaves at frequency coa in the waveguide CPW2. The field emitted by the passage of microwaves at frequency coa makes it possible to modify the energy of the ultracold atoms and to move the atoms of internal states la>. Curve "c" illustrates the potential seen by the atoms of internal states la> due to the contributions of the potentials illustrated by curve "a" and by curve "d". Curve "c" shows a local energy minimum making it possible to locally trap a cloud of ultracold atoms of internal states la>.

[0041] The combination of a DC magnetic trap (created by the direct currents in the wires and the homogeneous field Bc) and a microwave field creates what is called a "dressed" trap. By "dressed" is meant a trap created at least in part by an oscillating microwave, radio-frequency or optical field. Changes in the microwave fields (power, frequency and guide in which they propagate) make it possible to move this dressed trap and therefore to move the atoms. The DC magnetic trap is represented in [Fig.2] by curve a. The microwave field at coa is represented in [Fig.2] by curve d and the microwave field at cob is represented in [Fig.2] by curve b. The dressed trap Tl (combination of curves a and d for the state la> is re presented by curve c and the dressed trap T2 (association of curves a and b) for state lb> is represented by curve e.

[0042] The clouds of ultracold atoms of internal states 1a> and 1b> can be separated and trapped symmetrically with respect to the axis of symmetry Y by simultaneously imposing the propagation of waves of frequency coa in CPW2 and cob in CPW1. To obtain two traps whose minima are of the same value V0 and whose curvatures are of the same value, it is important that the crossing point Cl is arranged at an equal distance from CPW1 and CPW2, on the axis of symmetry Y.

[0043] [Fig. 3] illustrates the principle of generation of trajectory 16. Part a) of [Fig. 3] schematically presents a sequence of the displacement of each of the ultracold atom clouds at characteristic times t1 to t9. Part b) illustrates in a complementary manner a sequence of the different currents applied to the conductive wires, the powers applied to the waveguides and the frequencies imposed on the waveguides, for the times corresponding to those of part a).

[0044] In the sequence presented in [Fig.3], the current Iz, not shown, flowing in WIz is stationary, at a constant value. In part b) the values ​​of the currents, powers and frequencies are arbitrary. The ordinate ô frequency corresponds to a variation in frequency expressed in arbitrary units, around an average value of the frequency. The currents flowing through the conductive wires can be between 100 pA and 10 A, and the pulses injected into the waveguides can be between 6.6 GHz and 7 GHz in the case of the use of rubidium atoms.

[0045] In a step A0, there is a phase of preparation of the atoms. A cloud of ultracold atoms 12 is generated, including phases of emission of said atoms, cooling of said atoms, initialization of said atoms in at least one internal state 1a> and trapping of a cloud of said ultracold atoms in a local minimum of potential, at a distance h from the measurement plane (trap T, curve "a" of [Fig.2] part a)). The height h is different from 0 because the homogeneous magnetic field Bc is non-zero. The trapping is carried out by passing direct currents in the wire WIz and in one of the wires Wldi, the crossing point of these two wires defining the starting point (here Cl with Wldl). At the same time, a bias magnetic field Bc parallel to the plane of the atom chip is applied which is superimposed on the magnetic field created by the two preceding wires. The cloud of atoms is then trapped vertically above Cl, the intersection of the WIz and Wldl wires.

[0046] In a step B0 the internal states are initialized by coherently superimposing said ultracold atoms between said states 1a> and 1b> by a first pulse TT / 2 . This pulse can be produced by a laser, microwave emission, or more generally by a method emitting waves at a suitable transition frequency. The currents Iz and Li are imposed respectively on the wires conductors WIz and Wldl. The two internal states la> and lb> are coherently and spatially superimposed at the crossing point Cl.

[0047] The wave function is then:

[0048]

[0049] In a step C0, a cloud of atoms of internal state 1a> in a trap T1 is spatially separated from a cloud of atoms of internal state 1b> in another trap T2 and the traps are moved in opposite directions along a closed trajectory 16 contained in a plane perpendicular to the measurement axis Z. The cloud of atoms of internal states 1a> is symbolized by a disk of light texture and the cloud of atoms of internal states 1b> is symbolized by a disk of darker texture. This step is carried out from t1 to t9.

[0050] Between t1 and t2, the microwave power injected into the waveguides CPW1 and CPW2 gradually increases from 0 to its maximum value. A cob pulse is sent into the waveguide CPW1 and a coa pulse is sent into the waveguide CPW2, which makes it possible to separate the two clouds of different internal states on either side of the axis of symmetry Y, by a distance d, up to the positions shown schematically in t2. The ultracold atom trap T described previously at time ti is then transformed into two ultracold atom traps Tl and T2, each trap making it possible to immobilize a cloud of ultracold atoms of internal states different from the other trap (in this case internal states la> in one of the traps, for example Tl, and internal states lb> in the other trap T2, as described in part a) of [Fig.2].

[0051] A crossing point Ci corresponds to the crossing of the wire WIz with the wire Wldi.

[0052] Between t2 and t3, the current Idi is gradually cut off and Id2 is gradually increased to its maximum value (the time interval separating t2 and t3 is typically of the order of 10 ms and can be between 0.1 ms and 100 ms: the two traps T1 and T2 are moved to the right to the positions shown in t3.

[0053] Between t3 and t4 the current Id2 is gradually cut off and Id3 is gradually brought to its maximum value: the two traps are moved to the right to the positions shown in t4.

[0054] Between t4 and t5, the microwave power is gradually cut: the two traps are brought back to the same location on the chip, shown schematically in t5.

[0055] At t5, the pulsations of the two microwave guides are modified: the coa pulsation is imposed in CPW1 and the cob pulsation is imposed in CPW2.

[0056] Between t5 and t6, the power in the two waveguides gradually increases from 0 to its maximum value: the traps are separated in the vertical direction as shown in figure t6.

[0057] Between t6 and t7, the current Id3 is gradually cut off and Id2 is gradually brought to its maximum value: the two traps T1 and T2 are moved to the left to the positions shown in t7.

[0058] Between t7 and t8, the current Id2 is gradually cut off and Idi is gradually brought to its maximum value: the two traps are moved to the left to the positions shown in t8. This operation can be repeated several times with other first conductive wires to increase the area included in the trajectory 16.

[0059] Between t8 and t9, the microwave power in the waveguides is progressively cut off. The two traps T1 and T2 move until they merge into a single trap located at the starting point shown diagrammatically at tb

[0060] Direct currents are thus applied to the two wires corresponding to the initial crossing point Cl, and over time these currents are successively applied to the different crossing points Ci located on the axis of symmetry, while simultaneously applying microwave power to the waveguides.

[0061] During step C0 the direct currents applied to the different wires Wldi vary continuously (increase and decrease) between 0 and a maximum value Idimax (normalized to 1 in [Fig.3]), while the magnetic field Bc and the current Iz remain constant during the sequence. Throughout the sequence A0, B0 and C0 the two traps Tl and T2 remain at altitude h.

[0062] The two traps T1 and T2 move in the direction of "ignition" of the crossing points: from the crossing point Cl to the crossing point Cn. The return is carried out by inverting the microwave frequencies and by lighting the direct currents successively in the wires corresponding to the different crossing points by traveling through them from Cn to CL.

[0063] The traps are thus made to travel the closed trajectory 16.

[0064] The closed trajectory 16 of the atoms then contains an area A, the wave function atomic is therefore:

[0065] + exp(^>

[0066] With:

[0067] (p - +

[0068] In a step D0, the internal states la> and lb> are recombined by applying a second pulse tt / 2 to the ultracold atoms, which transfers the phase difference to the populations of the two atomic levels:

[0069] - 1 1 _ cos((p - (

[0070] = 2 [ 1 + cos(^ - Wt

[0071] where w is the pulsation of the 7T / 2 pulse.

[0072] The 7ï / 2 pulses can be sent to the atoms via the microwave guides or via a separate microwave transmitter.

[0073] The sequence from the first to the second pulse æ / 2 inclusive is the Ramsey sequence (see above).

[0074] Then in a step E0 the density of atoms in at least one internal state chosen from at least 1a> and 1b> is measured. This measurement can be carried out for example by laser absorption by probing the resonance between the pulsation specific to an internal state and that of the laser. Then the Sagnac phase of the ultracold atoms is determined and the rotation speed of the sensor is calculated along the Z axis.

[0075] The measurement of at least one population of atoms in one of the states la> or lb> makes it possible to determine the Sagnac phase, for example for the internal state la> by considering equation (1), then the rotation speed Qz with equation (6).

[0076] The traps can be made to travel this trajectory N times before measuring the Sagnac phase and thus measure a phase which will potentially be N times higher.

[0077] In order to implement the method described above, the ultracold atom sensor allowing measurement of rotation speed Qz comprises:

[0078] -an atomic chip 1 as described previously, with the waveguides and the conductive wires,

[0079] -an atom generation device for generating the ultracold atom cloud near the measurement plane 13 of the atomic chip,

[0080] -a generator of the homogeneous magnetic field Bc

[0081] - at least one voltage or direct current generator suitable for controlling electric currents in the conductive wires and at least one microwave voltage or current generator connected to the waveguides,

[0082] -a detection system, typically of optical intensity, adapted to measure at least one population of ultracold atoms in an internal state, this measurement allowing the determination of the Sagnac phase and the rotation speed Qz.

[0083] The gyroscope-type sensor also comprises at least one processor which controls the operation and implementation of the sensor, such as controlling the signals applied to the wires and microwave guides according to a predetermined sequence (for example the sequence of [Fig.3] b).

[0084] An accelerometer type sensor has a “simplified” operation compared to the gyroscope, because the two clouds follow a straight back and forth trajectory, as illustrated [Fig.4], which uses the same logic and formalism as [Fig.3]. Here only one wire Wld is necessary, defining the crossing point C.

[0085] Part a) of [Fig.4] schematically presents a sequence of the displacement of each of the ultracold atom clouds at characteristic times t1 to t3. Part b) illustrates the sequence of the different currents applied to the conductive wires, the powers applied to the waveguides and the frequencies imposed on the guides wave, for the times corresponding to those of part a). In the sequence presented in [Fig.4], the current Iz, not shown, flowing in WIz is stationary, at a constant value. The current applied to Wld is also constant throughout the sequence.

[0086] Initially at ti no power is applied to the waveguides and the cloud is trapped above point C.

[0087] Between t1 and t' 1, the microwave power injected into the waveguides CPW1 and CPW2 gradually increases from 0 to its maximum value, then the value remains maximum and constant between t' 1 and t' 2 via t2. A coa pulse is sent into the waveguide CPW2 and a cob pulse is sent into the waveguide CPW1, which makes it possible to separate the two clouds of different internal states on either side of the axis of symmetry Y up to the positions shown diagrammatically in t2, these positions being maintained for the entire duration t' 2 - t' 1, which may be short.

[0088] Between t'2 and t3, the microwave power in the waveguides is progressively cut off. The two traps T1 and T2 move until they merge into a single trap located at the starting point shown diagrammatically at tb

[0089] For both types of sensor, and generally for any inertial sensor, considering formulas 3, 4 and 5 we see that the phase is sensitive to the energy difference between the two "dressed" levels E'b-E'a, which is expressed as a function of the energy difference between the two atomic levels Ea-Eb:

[0090] For state la> the energy is modified from Ea to E'a with:

[0091]

[0092] For state lb> the energy is modified from Eb to E'b with:

[0093] F< _ F (8) b ~

[0094] Where Q, (respectively is the Rabi frequency associated with the dressing of the state la> (respectively lb>). To simplify the notations all the coupling factors are stored in the Rabi frequency, a function of the square root of the microwave power applied to the waveguides (amplitude of the microwave field).

[0095] Aa (respectively &b) is the mismatch between the frequency (respectively ÙY) of the microwave field covering the state la> (respectively the state lb>) and the frequency of the transition wOa (respectively w«) considered for the covering of the state la> (respectively lb>). The frequencies ^0« and ww> are the frequencies of the atomic transitions used for the implementation of the interferometer.

[0096] We have:

[0097] ma-aîOa(9)

[0098] Aè= ^-o?o&(10)

[0099] We call ^hfs the hyperfine frequency of the transition used.

[0100] An example of a transition used is the o transition of Rubidium 87 between two hyperfine levels F=1 and F=2, as illustrated [Fig.5], each level having separate Zeeman sub-levels of the same magnitude aB, with for Rubidium 87 a = 700 kHz / G, B being the continuous magnetic field, called DC, to which the atoms are subjected. We have:

[0101] œOa = whfs-aB(U)

[0102] uOb= œhfs + aB (12)

[0103] The energy difference between la> and lb> to which the Ramsey interferometer is sensitive is then expressed: 101041 E'„- É„ =Eb- E„ + ^ + l^= E„- E„- AE (13)

[0105] With 101061 +

[0107] The term AE intervenes in the oscillations of the populations given previously (formulas 5 and 6), therefore on the phase, and is at the origin of the noise of the interferometer.

[0108] In practice, to ensure the operation of the interferometer (to guarantee symmetry) it is appropriate to choose and A« = - (see for example the publication "Symmetric micowave potentials for interferometry with thermal atoms on a chip" Ammar et al, Phys. Rev. A 91, 053623; 2015). This choice has the advantage of canceling the previous term and therefore removing its effect. However, in practice, the cancellation of this AE term is not perfect and this is where the difficulty lies. This is all the more problematic experimentally:

[0109] the powers of the two microwave fields, which are proportional to C( q2 , have noise, and the equalization of the two Rabi frequencies is never perfect;

[0110] the two detuning terms Aa and &h involve the value of the DC magnetic field trapping the atoms which also contains noise (see formulas 9 to 12): [YES] = (¾ -whfs -«B (15)

[0112] A^ = - M / ifg-l- ü B (16)

[0113] We see in the formulas above that the noise of the interferometer comes on the one hand from the DC magnetic field B, comprising the homogeneous magnetic field Bc applied to the atoms and the continuous magnetic field coming from the conductive wires (term A) and on the other hand from the microwave field (term Q).

[0114] Current solutions for reducing noise on the DC magnetic field consist of using the most stable current sources possible. Current solutions for reducing noise on the microwave field amplitude consist of making servo loops on the microwave field amplitude to stabilize it as best as possible. possible.

[0115] These two solutions are not satisfactory because although they allow the noise level to be reduced, these noises always remain present in the sensor's error budget.

[0116] An aim of the present invention is to remedy the aforementioned drawbacks by proposing an inertial sensor with ultracold atoms having an attenuated noise level. DESCRIPTION OF THE INVENTION

[0117] The present invention relates to an ultracold atom sensor comprising: • an atomic chip placed in a vacuum chamber, comprising an XY plane called the measurement plane normal to a Z axis, and comprising: • a first and a second waveguide adapted to the propagation of microwave waves and direct currents, • at least a first conductive wire and a second conductive wire whose respective projections intersect at a point defining a first crossing point, • an atom generation device configured to generate a cloud of ultracold atoms near said XY plane of said atomic chip, • a generator of a homogeneous magnetic field, • a power supply device comprising at least one microwave generator and at least one direct current generator, the power supply device being configured to: • applying microwave signals and direct electric currents called CMW currents to said first and second waveguides, • apply direct currents known as CWI currents to said conductive wires, said waveguides, said conductive wires and said power supply device being configured, during the implementation of the sensor, to spatially separate a first cloud of ultracold atoms in a first internal state from a second cloud of ultracold atoms in a second internal state, by respectively forming a first and second ultracold atom trap by modifying an energy of said ultracold atoms, and to move said traps along a linear or closed trajectory included in a plane perpendicular to Z,

[0118] said power supply device being configured to apply to said first and second waveguides, for the spatial separation of the two traps, said microwave signals to initiate said spatial separation, then said CMW electric currents in place of said microwave signals to maintain said spatial separation,

[0119] the sensor further comprising a detection system adapted to measure at least a population of so-called ultracold atonias in a so-called internal state.

[0120] According to one embodiment, the sensor is of the accelerometer type, the trajectory followed by the two traps being linear.

[0121] According to another embodiment, the sensor is of the gyroscope type comprising a plurality of second conductive wires defining a plurality of crossing points, said trajectory followed by the two traps being closed and traveled in opposite directions by the first and the second trap.

[0122] According to one embodiment, each waveguide comprises three wires, two external ground wires and an internal signal wire, the CMW current being injected into the signal wire.

[0123] According to one embodiment, the power supply device further comprises at least one polarization tee connected to said at least one microwave generator and to said at least one direct current generator, and configured to apply said microwave signals and said CMW currents to said waveguides.

[0124] According to another aspect, the invention relates to a method for measuring an inertial parameter by an ultracold atom sensor comprising an atomic chip placed in a vacuum chamber, comprising an XY plane normal to a Z axis called the measurement plane, said atomic chip comprising: • a first and a second waveguide adapted to the propagation of microwave waves and direct currents, • at least a first conductive wire (Wl) and a second conductive wire whose respective projections intersect at a point defining a first crossing point, the method comprising the steps of:

[0125] A Generating a cloud of ultracold atoms near said XY plane of said atomic chip, including phases of emitting said atoms, cooling said atoms, initializing said atoms in at least a first internal state, and trapping a cloud of said ultracold atoms in a local minimum of potential, at a controlled height of said XY plane, said trapping being carried out by passing direct currents in the first and second conductive wires,

[0126] B Initialize the first internal state and a second internal state of said ultracold atoms by coherently superimposing said ultracold atoms between said first and second internal states by a pulse ji / 2,

[0127] C Spatially separate a first cloud of ultracold atoms in the first internal state from a second cloud of ultracold atoms in the second internal state, by respectively forming a first and second ultracold atom trap by modifying energies of said ultracold atoms, and moving said traps along a linear or closed trajectory included in a plane perpendicular to Z and initialized at the first crossing point,

[0128] said step of separating and moving the ultracold atoms being carried out by applying, according to a predetermined sequence, a homogeneous magnetic field to said ultracold atoms, direct currents, called CWI currents, to said conductive wires, and microwave signals (IMW) and direct electric currents, called CMW currents, to said waveguides,

[0129] the separation step comprising an initialization sub-step comprising the application of said microwave signals to said waveguides, and a maintenance sub-step comprising the application of said CMW currents in place of said microwave signals,

[0130] D Recombine said first and second internal states by applying to said ultracold atoms a second pulse ji / 2,

[0131] E Measure at least one population of said ultracold atoms in at least one said internal state.

[0132] According to one embodiment, the separation step comprises a transitional sub-step between the initialization sub-step and the maintenance sub-step, comprising an extinction of the microwave signals and an ignition of the CMW currents.

[0133] According to a first embodiment, during the transient step, the extinction of the microwave signals and the ignition of the CMW currents are carried out simultaneously. According to one embodiment, the transient step has a duration of less than 100 ps.

[0134] According to a second embodiment, during the transient step, said extinction of the microwave signals takes place before or after said ignition of the CMW currents.

[0135] According to one embodiment, during the displacement step, a spatial recombination of the two clouds takes place by progressively extinguishing the CMW currents.

[0136] According to one embodiment, during the displacement step, a spatial recombination of the two clouds takes place by switching off the CMW currents and simultaneously switching on the microwave signals again, then by progressively switching off the microwave signals.

[0137] The following description presents several exemplary embodiments of the device of the invention: these examples are not limiting of the scope of the invention. These exemplary embodiments present both the essential characteristics of the invention as well as additional characteristics linked to the embodiments considered.

[0138] The invention will be better understood and other characteristics, aims and advantages thereof will appear during the detailed description which follows and with reference to the appended drawings given as non-limiting examples and in which:

[0139] The [Fig.l] already cited illustrates an example of the topology of an atomic chip comprising conductive wires and microwave guides allowing the movement magnetic traps along a closed trajectory.

[0140] The [Fig.2] already cited illustrates the geometry of the guides and wires of the atomic chip as well as the traps T1 and T2.

[0141] The [Fig.3] already cited illustrates in its lower part an example of application of the different signals to the wires and guides according to the state of the art, in the case of a gyroscope type sensor, to make the two traps T1 and T2 (and therefore the two clouds of trapped atoms) travel the closed trajectory, and in its upper part the position of the two clouds corresponding to chosen times.

[0142] The [Fig.4] already cited illustrates in its lower part an example of application of the different signals to the wires and guides according to the state of the art to make travel, in the case of an accelerometer type sensor, the linear trajectory to the two traps T1 and T2 (and therefore to the two clouds of trapped atoms), and in its upper part the position of the two clouds corresponding to chosen times.

[0143] The [Fig.5] already cited illustrates the transition o of Rubidium 87 between two hyperfine levels F=1 and F=2 used for a cold atom inertial sensor, as well as the different frequencies of interest.

[0144] [Fig.6] illustrates the DC magnetic potential VDc Mw created by the application of direct currents to the waveguides.

[0145] [Fig.7] illustrates an ultra-cold atom sensor 10 according to the invention.

[0146] [Fig.8] illustrates the basic diagram of an embodiment of the sensor according to the invention in which the superposition of a microwave current and a direct current in the signal wire of the waveguide is done with a polarization tee

[0147] [Fig.9] illustrates an embodiment in which an additional polarization tee TPoladd has been integrated at the output of the waveguide and before the termination TMW.

[0148] [Fig. 10] illustrates on its left part the chronograms of application of the different signals during the implementation of an accelerometer type sensor according to the first variant of spatial recombination, and on its right part the displacement of the two clouds at chosen instants.

[0149] [Fig. 11] illustrates on its left part the timing diagrams of application of the different signals during the implementation of an accelerometer type sensor according to the second variant of spatial recombination, and on its right part the displacement of the two clouds at chosen instants.

[0150] [Fig. 12] illustrates the timing diagrams for applying the different signals for the implementation of a gyroscope-type sensor, according to the first variant of spatial recombination.

[0151] [Fig. 13] illustrates the movements of the two clouds at selected times associated with the signals of [Fig. 12].

[0152] [Fig. 14] illustrates the timing diagrams for the application of the different signals for the implementation of a gyroscope-type sensor according to the second variant of spatial recombination.

[0153] [Fig. 15] illustrates the movements of the two clouds at selected times associated with the signals of [Fig. 14]. DETAILED DESCRIPTION OF THE INVENTION

[0154] The Ramsey time TR is divided into two times, a time TR°ff during which no microwave signal is applied to the waveguides, and a time TR°n during which microwave signals are applied to the guides:

[0155] Tr = T°n + TRff

[0156] The noise N accumulated on the phase of the interferometer is given by:

[0157] N = aDCTR + aMWTRn ​​(17)

[0158] with oMW the phase noise of the interferometer integrating the noise produced by the microwave signals (only during T°n) and oDC the noise due to the continuous magnetic field alone (present during the entire sequence).

[0159] The unit of oMW and oDC is Hz.

[0160] From formula 14, considering that there is an error or noise ÔB on the DC magnetic field and errors or noise ôQa and 8£lh on ila and we can rewrite the difference of the two displacements AE in the form:

[0161] AE= f + + + +

[0162] The effect of noise or errors on a'« and œb has been neglected because experimentally their effects are negligible.

[0163] The term , with:

[0164] ¢7^ = ^5^ + ^3^^55(^

[0165] then constitutes a noise on the phase of the interferometer, to which it is appropriate to add the noises on the other terms contained in the phase of the interferometer, that is to say in the energy difference Eb-Ea. To simplify, we neglect the collisional shift, the detection noise, the Dicke effect, etc., and we only keep the term corresponding to the energy difference in the presence of the DC magnetic field. The noise on this term (microwave fields switched off) only involves the noise on the DC magnetic field 8B and is of the form (see for example the publication “Magnetically trapped atoms for compact atomic docks” P. Rosenbusch, Apppl. Phys. B (2009), 95, p. 227-235):

[0166] 25(5-5^)55(19)

[0167] To give an order of magnitude to the different noises, we have, with the example of Rubidium 87:

[0168] b = 431 Hz! G2,

[0169] the DC magnetic field is close to Bm — 3.23 G.

[0170] = -&h = 200 kHz

[0171] Q. = 50 kHz and = 50 kHz

[0172] 5B = ImG

[0173] B-Bm = 100 mG [°174] ÔQJQa = (%lb / tth= W3

[0175] Which gives:

[0176] , + abBl ~4 + -4) ~ 100 Hz.

[0177] And

[0178] 2b(B-Bm)ÔB~ 100 mHz.

[0179] It is noted that the presence of the two microwave fields significantly increases the noise level. This is the predominant factor that should be reduced.

[0180] The idea of ​​the invention is to reduce the noise level by replacing the microwave fields (after separation of the two states) with DC currents in order to create two magnetic traps each containing one state.

[0181] Thus, during the entire phase where the two states 1a> and 1b> are kept separate, the two microwave fields used for the dressing are cut off. During this phase of the interferometer, the phase is no longer sensitive to noise on the DC magnetic field 5B, nor on the amplitude of the microwave fields and ôklh via the noise term but the term remains sensitive to ÔB.

[0182] Microwave signals, typically IMW microwave currents, are first applied to effect the separation of the two clouds (initialization of the spatial separation), as illustrated in Figures 3 and 4 from t1 to t2. This step of progressive ignition of the waveguides is similar to what has been described in the prior art.

[0183] Then according to the invention the IMW currents are cut off and instead direct currents Idc-mw are applied to the microwave guides CPW1 and CPW2. Before and during the change of type of current applied to the waveguide, direct currents are applied to the conductive wires.

[0184] It is important to use microwave currents for the initial separation of the two states 1a> and 1b> of the interferometer because microwave currents allow the creation of selective traps of the internal state which DC currents do not allow. It is important to create selective traps of the internal state at the beginning of the separation otherwise the two states would remain mixed after the separation.

[0185] The magnetic potential DC VDC Mw created by the application of these direct currents I dc mw^ux waveguides is illustrated [Fig.6]. This magnetic potential VDC_Mw replaces the DC magnetic potential created by the microwave fields resulting from the application of the IMW microwave currents, illustrated by curves c) and e) in Figure 2a). The magnetic potential VDC mw allows to continue to trap the cold atoms and to maintain the spatial separation of the two clouds as much as necessary during the rest of the Ramsey sequence. Curve a) taken from [Fig.2] a) illustrates the DC magnetic potential created by the application of direct currents in the two conducting wires (beginning of the sequence, before the separation of the clouds and therefore before the ignition of the microwave currents).

[0186] [Fig.7] illustrates an ultracold atom sensor 10 according to the invention. The sensor 10 comprises an atom chip ACh placed in a vacuum chamber, having an XY plane called the measurement plane normal to a Z axis. The chip Ach has a first waveguide CPW1 and a second waveguide CPWX2 adapted to the propagation of microwave waves and direct currents, and at least a first conductive wire WIz and a second conductive wire Wld whose respective projections are intersecting at a point defining a first crossing point CL. The two waveguides are arranged symmetrically to a Y axis, typically but not limited to they are parallel to each other. The sensor also comprises an atom generation device ACG configured to generate a cloud CL of ultracold atoms near said XY plane of said atom chip and a generator GB of a homogeneous magnetic field Bc.

[0187] The sensor 10 according to the invention also comprises a power supply device PSD comprising at least one microwave generator GMW and at least one direct current generator GDC. There may be one microwave generator per guide or a generator common to both guides. Similarly, there may be a single common generator GDC for all the wires and waveguides, or several generators.

[0188] The power supply device PSD is configured to apply microwave signals, typically IMW currents, and direct electric currents IDc mw called CMW currents, to the waveguides CPW1 and CPW2, and to apply direct currents IDc wi called CWI currents to the conductive wires.

[0189] The waveguides, the conductive wires and the power supply device are configured, when implementing the sensor, i) to spatially separate a first cloud of ultracold atoms CL1 in a first internal state 1a> from a second cloud of ultracold atoms CL2 in a second internal state 1b>, by respectively forming a first ultracold atom trap T1 and a second trap T2 by modifying the energy of the atoms, and ii) to move the traps (T1, T2) along a linear or closed trajectory included in a plane perpendicular to Z.

[0190] According to the invention, the PSD feed device is configured to apply to the first and second waveguides, for the spatial separation of the two traps, the IMW microwave signals to initiate spatial separation, then CMW IDc mw electric currents instead of IMW microwave signals (currents) to maintain spatial separation.

[0191] Finally, the sensor 10 according to the invention comprises an SDET detection system adapted to measure at least one population of said ultracold atoms in a said internal state.

[0192] The cold atom sensor has a structure identical to that described in the prior art, with the difference that the waveguides are capable of propagating direct currents and that the power supply device makes it possible to apply direct currents to the waveguides as claimed.

[0193] By applying direct currents to the guides instead of applying microwave (hyperfrequency) signals for a good part of the Ramsey sequence, the noise component due to these crMWTRn ​​signals (formula 17) is considerably reduced due to the decrease in T^1- This reduces the amount of noise accumulated on the phase of the interferometer. It has been shown above that this noise component is the one that limits the measurement, and any gain on this noise component translates directly into a gain in measurement sensitivity.

[0194] A first type of sensor according to the invention is an accelerometer, the trajectory followed by the two traps is linear as illustrated [Fig.4] a). Two intersecting wires in Cl IWz and Iwd are necessary to define the starting / arrival point of the trajectory, and the displacement is here confused with the spatial separation.

[0195] A second type of sensor is a gyroscope. The atomic chip then comprises a plurality of second conductive wires Wldi (Wldl, Wld2, Wld3) defining a plurality of crossing points Ci (Cl, C2, C3) as illustrated [Fig.l], and the trajectory followed by the two traps is closed and traveled in the opposite direction by the two traps, as described [Fig.3] a).

[0196] The gyroscope according to the invention is compatible with any atomic chip geometry comprising two microwave guides and conductive wires, as described in the aforementioned documents US 15 / 778605, US 17 / 924340, US 17 / 832615 and US 17 / 832616.

[0197] When implementing the sensor according to the invention, the separation of the two clouds takes place with the microwave signals and once the clouds are separated, the separation is maintained with the CMW direct currents applied to the waveguides. The cutting of the microwave fields and their replacement by two DC currents can be done in three different ways.

[0198] In a first variant, the power supply device PSD is configured so that the microwave signals are switched off simultaneously with the direct electric currents being switched on. This mode allows rapid switching off of the microwave currents. croondes, therefore to reduce (see equation (17)) and therefore to reduce the accumulation of noise due to the term ^mw.

[0199] According to a first embodiment, the time tttans during which the switching off and on takes place simultaneously is fast, which means that the rising or falling edge is fast compared to the frequencies of the magnetic trap. Typically, tttans must be less than or equal to 100 ps.

[0200] According to a second embodiment, the simultaneous switching off and on are carried out with two slow ramps (a slow RF ramp descends and at the same time a rising DC ramp), which means that the ramps must be slow compared to the frequencies of the magnetic trap. Typically, tttans must be at least 10 ms.

[0201] Between these two values ​​of ttransaccording to a third embodiment the ramps have complex shapes to make adiabatic shortcuts.

[0202] In a second variant, the power supply device PSD is configured so that the microwave signals are extinguished before the CMW electric currents are switched on. This mode allows for even faster extinction of the microwave currents than the first mode, but complicates the transfer between the traps using the IMW microwave currents and the traps using the DC currents Idcmw. The time during which nothing is applied is called tint. This time should be less than the inverse of the trap frequency cop. The trap frequency illustrates its “stiffness”. The shape of the magnetic potential creating the trap is approximated in the vicinity of the minimum by a parabola. Let r be the distance to the minimum of potential Vo, the potential can be written as:

[0203] y~ Vo + 1 nw2r2

[0204] Thus it is appropriate that:

[0205] t. t ±

[0206] In a third variant, the power supply device PSD is configured so that the extinction of the microwave signals occurs after the ignition of the CMW electric currents. This mode simplifies the transfer between the traps using the IMW microwave currents and the traps using the DC IDC mw- currents.

[0207] According to one embodiment, each waveguide comprises three wires, two external ground wires and an internal signal wire, and the direct current CMW is injected into the signal wire (coplanar guides). But the sensor 10 according to the invention can integrate any type of microwave guide compatible with the application of direct currents, such as microstrips.

[0208] According to one embodiment, the superposition of a microwave current and a direct current in the signal wire of the waveguide is done with a polarization tee. Thus, the PSD power supply device further comprises at least one polarization tee TPol rization connected to the microwave generator and the DC generator, and configured at the input of each guide to apply the microwave signal (microwave current IMW) and the CMW current (DC current IDcmw) to the waveguides, as illustrated in the schematic diagram of [Fig.8]. A polarization tee is a component with two inputs, one for a DC current, the other for an oscillating current and an output allowing to obtain the superposition of the DC current and the oscillating current. The output can also be used as an input for the superposition of the DC current and the oscillating current, the two inputs are then two outputs one giving the DC current and the other the oscillating current. In order to avoid unwanted reflections of the microwave signal having crossed the microwave guides, a TMW microwave termination is integrated at the output of the atomic chip as also illustrated [Fig.8].

[0209] Preferably, to ensure good separation between the direct currents and the microwave signals at the output of the microwave guide, an additional polarization tee TPoladd is integrated at the output of the waveguide and before the TMW termination, as illustrated in the principle diagram of [Fig.9].

[0210] According to another aspect of the invention, the invention relates to a method for measuring an inertial parameter by an ultracold atom sensor according to the invention as described previously. The method comprises a first step A consisting of generating a cloud CL of ultracold atoms near the XY plane of the atom chip, including phases of emitting the atoms, cooling the atoms, initializing the atoms in at least a first internal state, and trapping a cloud of ultracold atoms in a local minimum of potential, at a controlled height of the XY measurement plane, the trapping being carried out by passing direct currents in the first and second conductive wires. This step is similar to step AO described in the prior art.

[0211] In a step B, the first internal state 1a> and the second internal state 1b> of the ultracold atoms are initialized by coherently superimposing the ultracold atoms between the first and second internal states by a pulse ji / 2. This step is similar to step B0 described in the prior art.

[0212] In a step C, the first cloud of ultracold atoms in the first internal state is spatially separated from the second cloud of ultracold atoms in the second internal state, respectively forming a first ultracold atom trap T1 and a second ultracold atom trap T2. This separation is carried out by modifying the energies of the ultracold atoms. Then the traps (T1, T2) are moved along a linear (accelerometer) or closed (gyroscope) trajectory included in a plane perpendicular to Z and initialized at the first crossing point.

[0213] Step C of separation and displacement of ultracold atoms is carried out in ap- folding, according to a predetermined sequence: • a homogeneous magnetic field Bc with ultracold atoms, • direct currents, called CWI currents, to the conductive wires, • microwave signals, typically IMW microwave currents, and direct electric currents, called CMW currents, to the waveguides.

[0214] In the method according to the invention, the separation step comprises an initialization sub-step Cinit comprising the application of microwave signals to said waveguides, and a maintenance sub-step Cmaint comprising the application of electric currents CMW in place of said microwave signals. The originality of the method according to the invention lies in the separation and displacement step C, and particularly in the Cmaint step.

[0215] In a step D, the first and second internal states are recombined (the two clouds are then spatially merged again once the trajectory has been completed) by applying a second ji / 2 pulse to the ultracold atoms, which closes the Ramsey sequence initialized with the first ji / 2 pulse. This step is similar to step DO described in the prior art.

[0216] Finally, in a step E, at least one population of ultracold atoms is measured in at least one said internal state, from which a value of an inertial parameter (acceleration, speed and / or angle of rotation relative to a given axis) is deduced. This step is similar to step E0 described in the prior art.

[0217] In the method according to the invention, the usual sequence used to separate and recombine the two states 1a> and 1b> is modified.

[0218] The usual sequence consists of: • Gradually switch on the two microwave fields each in a waveguide (CPW1 and CPW2) of the chip, this allows the two states 1a> and 1b> to be separated; • Maintain the two microwave fields in the guides CPW 1 and CPW2 to keep the two states la> and lb> separated (this separation with the microwave fields is shown in [Fig.2] a)); • Gradually turn off the two microwave fields to spatially recombine the two states la> and lb>. This spatial recombination is different from the recombination of step D. The spatial recombination takes place once just before step D for the accelerometer (time t3 of [Fig.4] a)), and takes place twice during the closed trajectory for the gyrometer (time t5 and tç of [Fig.3] a)).

[0219] The sequence according to the invention is, for the example of a three-wire coplanar waveguide, described below. • Gradually turn on the two microwave fields, each in a guide waveform of the chip, this allows to separate the two states la> and lb>; • Once the states are separated, cut off, preferably quickly, the two microwave fields and switch on, preferably at the same time and quickly, a DC current in the two signal lines of the two microwave guides. This makes it possible to create two separate DC magnetic traps, each containing one of the two internal states la> and lb> (these two traps are shown in [Fig.6]); • Spatially recombine the two states, during the displacement step, according to two variants:

[0220] According to a first variant by progressively switching off the two DC currents flowing through the two signal lines of the two microwave guides;

[0221] According to a second variant by switching off, preferably quickly, the two DC currents flowing through the two signal lines of the two microwave guides and, preferably at the same time, by quickly switching on the two microwave fields again, then by gradually switching off the two microwave fields to recombine the two states 1a> and 1b>.

[0222] Preferably, the separation step of the method according to the invention comprises a transient sub-step Ctrans between the initialization sub-step Cinit and the maintenance sub-step Cmaint, comprising the extinction of the microwave signals and the ignition of the CMW currents.

[0223] The cutting of microwave fields and their replacement by two DC currents can be done according to the three variants described previously:

[0224] First variant: during the transient stage, the extinction of the microwave signals and the ignition of the CMW currents are carried out simultaneously. Preferably the transient stage has a duration of less than 100 ps.

[0225] Second variant: during the transient stage, the extinction of the microwave signals takes place prior to the ignition of the CMW currents.

[0226] Third variant: during the transient stage, the extinction of MW signals after the ignition of CMW currents

[0227] We will now illustrate the method according to the invention by examples of timing diagrams.

[0228] We call: • P1MW and P2mw the power of the microwave signal respectively applied to the guide CPW1 and CPW2, • coa the pulse sent into the waveguide CPW2 and cob the pulse sent into the waveguide CPW1, • Iz the intensity of the direct current applied to the first conductive wire WIz • Id, Idb Id2, Id3 the intensities of the direct currents called CWI currents applied to the second conductive wire(s), • IlDC-MwCt I2DC-mw the intensities of the direct currents called CMW applied respectively to the waveguides CPW1 and CPW2.

[0229] Figures 10 a), 11a) illustrate the timing diagrams for applying the different signals when implementing an accelerometer-type sensor respectively according to the first and second variants of spatial recombination, during the separation / displacement step C. Figures 10 b) and 11 b) illustrate the displacement of the two clouds at selected times. These figures also illustrate the first variant of the extinction / ignition sequencing, i.e. an extinction of the MW powers simultaneously with the ignition of the CMW currents.

[0230] Throughout the sequence, a coa pulse is applied to CPW2 and cob to CPW1 (same as [Fig.4] a)).

[0231] In [Fig. 10] between t1 and t2 the microwave powers are applied to the guides. At t2 the two clouds CL1 and CL2 are separated. Then between t2 and t3 the MW signal is gradually switched off and the direct currents IlDc-Mwet I2DC-mw are simultaneously switched on. Between t3 and t4 these currents are maintained for the measurement. Then between t4 and t5 the currents IlDc-Mwet I2DC_Mw are gradually reduced which spatially recombines the two clouds (first variant of spatial recombination). At t5 the two clouds are spatially recombined.

[0232] According to a first embodiment, the currents Id and Iz remain constant. According to a second embodiment illustrated [Fig. 10] a) the current Iz decreases slightly when the currents IlDc-Mwet I2dc.mw are applied, in order to increase the potential barrier between the two states ([Fig.6]). When these currents are no longer applied, Iz is slightly increased again. According to this second embodiment, Id preferably varies like Iz.

[0233] In [Fig. 11] the beginning of the sequence is identical up to time t4. Between t4 and t5', simultaneously with the extinction of the direct currents, the microwave signals are switched on again, the clouds are still separated. Between t5' and t6', spatial recombination is carried out by progressively extinguishing the MW signals (second variant of spatial recombination). At t6' the two clouds are spatially recombined.

[0234] Figures 12 and 14 illustrate the timing diagrams for the application of the different signals respectively for the implementation of a gyroscope type sensor, respectively according to the first and second variant of spatial recombination, during the separation / displacement step C. Figures 13 and 15 illustrate the displacements of the two clouds at chosen times. These figures also illustrate the first variant of the extinction / ignition sequencing, i.e. an extinction of the MW powers simultaneously with the ignition of the CMW currents.

[0235] In Figures 12 and 13, the two clouds are separated by applying MW power to the two guides (between t1 and t2). For this, direct currents Id1 and Idz are applied respectively in WIz and Wid1. Then, between t2 and t3, the MW signals are replaced by the direct currents IlDc-Mw and I2DC-Mw. Between t3 and t4, the two clouds are moved along Y from the first crossing point Cl to the second crossing point C2 by switching off the current Id1 and switching on the current Id2 in WId2. Between t4 and t5, the two clouds are moved along Y from the second crossing point C2 to the third crossing point C2 by switching off the current Id2 and switching on the current Id3 in WId3. Then between t5 and t6 we proceed to the first spatial recombination of the two clouds in C3 (finalizing the half-travel of the closed trajectory) by extinguishing the direct currents IlDc-Mwet I2DC Mw (first variant of spatial recombination).At t6 the frequencies applied to the waveguides are reversed and we start again for the second half-turn, again proceeding to separate the two clouds by applying MW fields to the guides between t6 and t7.

[0236] Here also according to an embodiment illustrated in [Fig. 12] the current Iz is slightly decreased when applying the currents IlDc-Mwet I2DC Mwet re-increase when they are switched off, and the currents Idl and Id3 follow the variations of Iz. According to another embodiment the currents Iz and Idl, Id2 and Id3 do not have two plateaus (see for example variation of ldi in [Fig.3]).

[0237] In Figures 14 and 15, the sequence is identical up to t5. Between t5 and t6', the direct currents are simultaneously switched off and the microwave signals are switched on again; the clouds are still separated. Between t6' and t7', spatial recombination is carried out by progressively switching off the MW signals (second variant of spatial recombination). The same will apply between t1 1' and t12', where the direct currents are simultaneously switched off and the microwave signals switched on, then between t12' and t13', spatial recombination is carried out by progressively switching off the MW signals.

Claims

1. Claims Ultra-cold atony sensor (10) comprising: • an atomic chip (ACh) placed in a vacuum chamber, comprising an XY plane called the measurement plane normal to a Z axis, and comprising: • a first and a second waveguide (CPWX1, CPWX2) adapted to the propagation of microwave waves and direct currents, • at least a first conductive wire (WIz) and a second conductive wire (Wld, Wldl) whose respective projections intersect at a point defining a first crossing point (Cl), • an atom generation device (ACG) configured to generate a cloud of ultracold atoms near said XY plane of said atomic chip, • a generator (GB) of a homogeneous magnetic field (Bc), • a power supply device (PSD) comprising at least one microwave generator (GMW) and at least one direct current generator (GDC), the power supply device being configured to: • applying microwave signals (IMW) and direct electric currents (IDc mw) called CMW currents to said first and second waveguides, • apply direct currents known as CWI currents to said conductive wires, • said waveguides, said conductive wires and said power supply device being configured, during the implementation of the sensor, to spatially separate a first cloud (CL1) of ultracold atoms in a first internal state from a second cloud (CL2) of ultracold atoms in a second internal state, by respectively forming a first (Tl) and second (T2) ultracold atom traps by modifying an energy of said ultracold atoms, and to move said traps (Tl, T2) along a linear or closed trajectory included in a plane perpendicular to Z, • said power supply device being configured to apply to said first and second waveguides, for the spatial separation of the two traps, said microwave signals to initiate said spatial separation, then said CMW electric currents in place of said microwave signals to maintain said spatial separation, • the sensor further comprising a detection system (SDET) adapted to measure at least one population of said ultracold atoms in a said internal state.

2. Sensor according to one of the preceding claims of accelerometer type, said trajectory followed by the two traps being linear.

3. Sensor according to one of the preceding claims of gyroscope type comprising a plurality of second conductive wires (Wldi) defining a plurality of crossing points (Ci), said trajectory followed by the two traps being closed and traveled in opposite directions by the first and the second trap.

4. Sensor according to one of the preceding claims in which each waveguide comprises three wires, two external ground wires and an internal signal wire, the CMW current being injected into the signal wire.

5. Sensor according to one of the preceding claims wherein the power supply device further comprises at least one polarization tee connected to said at least one microwave generator and to said at least one direct current generator, and configured to apply said microwave signals and said CMW currents to said waveguides.

6. Method for measuring an inertial parameter by an ultracold atom sensor comprising an atomic chip (ACh) placed in a vacuum chamber, comprising an XY plane normal to a Z axis called the measurement plane, said atomic chip comprising: • a first and a second waveguide (CPWX1, CPWX2) adapted to the propagation of microwave waves and direct currents, • at least a first conductive wire (Wl) and a second conductive wire (W2) whose respective projections are intersecting at a point defining a first crossing point (0),

7. the method comprising the steps of: A Generating a cloud of ultracold atoms near said XY plane of said atomic chip, including phases of emitting said atoms, cooling said atoms, initializing said atoms in at least a first internal state, and trapping a cloud of said ultracold atoms in a local minimum of potential, at a controlled height of said XY plane, said trapping being carried out by passing direct currents in the first and second conductive wires, B Initialize the first internal state and a second internal state of said ultracold atoms by coherently superimposing said ultracold atoms between said first and second internal states by a pulse ji / 2, C Spatially separating a first cloud of ultracold atoms in the first internal state from a second cloud of ultracold atoms in the second internal state, respectively forming a first (Tl) and second (T2) ultracold atom trap by modifying the energies of said ultracold atoms, and moving said traps (Tl, T2) along a linear or closed trajectory included in a plane perpendicular to Z and initialized at the first crossing point, said step of separating and moving the ultracold atoms being carried out by applying, according to a predetermined sequence, a homogeneous magnetic field (Bc) to said ultracold atoms, direct currents, called CWI currents, to said conductive wires, and microwave signals (IMw) and direct electric currents, called CMW currents, to said waveguides, the separation step comprising an initialization sub-step comprising the application of said microwave signals to said waveguides,and a holding sub-step comprising applying said CMW electric currents in place of said microwave signals, D Recombining said first and second internal states by applying to said ultracold atoms a second pulse ji / 2, E Measure at least one population of said ultracold atoms in at least one said internal state. Method according to the preceding claim in which the separation step comprises a transitional sub-step between the initialization sub-step and the maintenance sub-step, comprising an extinction microwave signals and ignition of CMW currents.

8. Method according to the preceding claim in which, during the transient step, the extinction of the microwave signals and the ignition of the CMW currents are carried out simultaneously.

9. Method according to the preceding claim in which the transient step has a duration of less than 100 ps.

10. A method according to claim 6 wherein, during the transient step, said extinction of the microwave signals occurs before or after said ignition of the CMW currents.

11. Method according to one of claims 6 to 10 in which during the displacement step a spatial recombination of the two clouds takes place by progressively extinguishing the CMW currents.

12. Method according to one of claims 6 to 10 in which during the displacement step, a spatial recombination of the two clouds takes place by switching off the CMW currents and simultaneously switching on the microwave signals again, then by gradually switching off the microwave signals.

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