www.nature.com/scientificreports OPEN Highly sensitive atomic based MW interferometry Dangka Shylla, Elijah Ogaro Nyakang’o & Kanhaiya Pandey We theoretically study a scheme to develop an atomic based micro-wave (MW) interferometry using Received: 10 July 2017 the Rydberg states in Rb. Unlike the traditional MW interferometry, this scheme is not based upon Accepted: 13 April 2018 the electrical circuits, hence the sensitivity of the phase and the amplitude/strength of the MW field is not limited by the Nyquist thermal noise. Further, this system has great advantage due to its much Published: xx xx xxxx higher frequency range in comparision to the electrical circuit, ranging from radio frequency (RF), MW to terahertz regime. In addition, this is two orders of magnitude more sensitive to field strength as compared to the prior demonstrations on the MW electrometry using the Rydberg atomic states. Further, previously studied atomic systems are only sensitive to the field strength but not to the phase and hence this scheme provides a great opportunity to characterize the MW completely including the propagation direction and the wavefront. The atomic based MW interferometry is based upon a six-level loopy ladder system involving the Rydberg states in which two sub-systems interfere constructively or destructively depending upon the phase between the MW electric fields closing the loop. This work opens up a new field i.e. atomic based MW interferometry replacing the conventional electrical circuit in much superior fashion. Atomic based standards such as time and length is already adopted and established due to their high reproduc- ibility, accuracy, resolution and stability . Atoms have also been successfully used for DC and AC (MW and RF) 2–5 magnetometry, reaching impressive sensitivity and spatial resolutions . Inspired by these successes recently, the 6–11 atom based MW and RF electrometry has been investigated using the Rydberg states of the atoms . The suc- cess of these experiments for high sensitive electrometry is due to property of the Rydberg states i.e. availability of closely spaced levels (in the range of MW and RF region) with very high electric polarizability. The strength 12,13 sensitivity for MW field using the traditional antenna method is only upto 10 mV/cm which is limited by the thermal noise. The sensitivity is improved upto 30 μV/cm using the optical method for the electro-magnetic fields 8,14 converted by the dipole antenna . The atomic based MW sensor improves the sensitivity further upto 8 μV/ cm which is limited by the natural decay rate of the ground and the Rydberg states, lasers linewidth, the transit time broadening, and Doppler mismatch between probe and the control lasers. The transit time broadening can 15 16 be removed completely using the cold atomic cloud, cold atomic beam , or nano cell . The Doppler mismatch between probe and the control laser can be removed using the cold atom, nano cell or collimated atomic beam. However, with very simple experimental set-up with Rb cell at room temperature, the strength sensitivity of experimentally demonstrated four level system is already three orders of magnitude better than the electrical circuit based MW sensor. Further the frequency range of the atomic based MW sensor is from radio frequency (RF), MW to terahertz regime. Next, the spatial resolution of the atomic based MW sensor is sub-wavelength (λ /650) which is difficult to achieve with traditional antenna method as the dimension of the antenna itself MW happens to be λ /2. MW e Th atomic based electrometry is based upon the phenomenon of electromagnetically induced transparency (EIT) in which the absorption property of a probe laser is altered in the presence of control lasers and MW (or RF) field in a four level system. EIT is sensitive to the field’s strength, frequency and the polarization and so the electrometry. An oscillating electro-magnetic field i.e. MW electric field is characterized by it’s strength/amplitude, fre- quency, polarization and the phase. The previously studied atomic based MW electrometry is not phase sensitive as EIT in a simple multilevel system, happens to be insensitive to the absolute phase of probe and the control fields but only it’s robustness depends upon the phase stability . Phase of the MW fields is detected using traditional MW interferometry which is based upon the electri- 19–21 cal circuit, whose performance is greatly limited by its bandwidth and the Nyquist thermal noise . Here, we Department of Physics, Indian Institute of Technology Guwahati, Guwahati, Assam, 781039, India. Correspondence and requests for materials should be addressed to K.P. (email: email@example.com) Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 1 www.nature.com/scientificreports/ Figure 1. (a) The energy level diagram for loopy ladder system. (b) Transitions shown by the red and green arrow lines are the two sub-system to close the loop. The probe laser (dotted red arrow line) and the control laser (solid blue arrow line) are part of both the sub-system. (c) The typical experimental set up for the phase dependent MW electrometry. explore a six-level loopy ladder system which replaces the traditional electrical circuits based MW interferometry by the atomic MW interferometry, as the absorption property of the probe laser has phase dependency on the MW fields. This is based upon the interference between two sub-systems driven by the MW fields forming the loop. The limitation of the atomic based MW interferometry is again same as in case of the atomic based MW 6,8 sensor studied with four-level system and is not limited by the thermal noise. But this system is two orders of 6,8 magnitude more sensitive to field strength (upto 80 nV/cm) in comparison to the previously explored system due to its loopy nature. There are loopy system which has been studied previously and has phase sensitivity but loop is completed using the weak magnetic dipole transition . In contrast to the previous system this six-level loopy system involves allowed electric dipole transition. This paper is organized as follows. In the section namely “Method”, we describe the method of realizing the six-level loopy ladder system in Rb and possible experimental set-up. In subsequent sub-section we present the semi-classical model and solution for the relevant density matrix element. Further we provide the physical inter- pretation of the obtained mathematical solution in terms of the interference between the two sub-systems and in terms of the dressed state picture. In the next section namely “Results” we present various results including the lineshape of the probe absorption, the phase dependency of it, the comparison of the amplitude/strength sensi- tivity of this system with the previously studied four-level system and the frequency range. Finally in the section namely “Discussion” we give our conclusion for this study. Method Realization of the system. The considered six-level loopy ladder system is shown in Fig. 1a. The probe laser at 780 nm is at the D line i.e. driving the 5 S → 5 P transition in the Rb. The control laser at 480 nm is 2 1/2 3/2 1 1 2 driving the 5Pn → S and the three reference MW fields are driving the transition, n Sn → P, 3/2ryd ryd ryd 2 3 3 4 1 4 1 2 3 n Pn → S and n Sn → P. The unknown MW field is driving the n Sn → P. The n , n , n and ryd ryd ryd ryd ryd ryd ryd ryd ryd n are rydberg states which are chosen according to the frequency range of the MW field. ryd e t Th ypical experimental setup for phase dependent MW electrometry is shown in Fig. 1(c) in which a probe laser at 780 nm and a control laser at 480 nm are counter-propagating inside the Rb cell. The four MW con- trol fields are generated by a single frequency synthesizer having arrangements of controlling the frequency, phase and the amplitude or the four different MW field frequencies combined using a frequency combiner (e.g. ZN4PD-02183-S+ from minicircuit company can be operated between 2–18 GHz). The output of the frequency Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 2 www.nature.com/scientificreports/ synthesizer or combiner is amplified and fed to MW horn. All four MW fields are propagating perpendicular to the probe and the control lasers with a uniform phase inside the Rb cell. it () ωφ + ij ij Semi-classical analysis. e e Th lectric field, associated with the transition |i〉 → |j〉 is , where E is Ee ij ij iφ ij amplitude, ω is the frequency and φ is the phase. We define Rabi frequency for the transition Ω = dE e / ij ij ij ij ij |i〉 → |j〉 having the dipole moment matrix element d . Please note that Ω is a complex quantity which can be ij ij iφ ij written as |Ω | e , where φ is due to the phase of the electric field associated with it. The Rabi frequencies of the ij ij ref ref ref unk probe and the control lasers are Ω and Ω respectively, whereas Ω , Ω , Ω and Ω are the Rabi frequencies 12 23 34 45 56 36 unk of the MW fields. It is important to note here that the phase of Ω is to be characterized w.r.t to the reference ref ref ref MW fields Ω , Ω and Ω . The superscript ref or unk denotes the reference and unknown MW field 34 45 56 respectively. e t Th otal Hamiltonian for this system is given as Ω ii ,1 +− it ωω it ii ,1 ++ ii ,1 He = () +| ei〉〈i +| 1 i=1 ref Ω ii ,1 +− it ωω it ii ,1 ++ ii ,1 + () ee +|ii 〉〈 +| 1 i=3 unk 6 Ω 36 it ωω −it 36 36 + () ee +|36 〉〈 |+ hc .. +| ω jj 〉〈 | ∑ j j=1 (1) If the energy of the state |i〉 is ℏω then the general quantum mechanical state of the system is −it ω |Ψ〉= ct ()|〉 ie ∑ i (2) i−1 We define δ = ω − (ω − ω ) and δ = ω − (ω − ω ) i.e. the detunings of the probe and control lasers from 12 12 2 1 23 23 3 2 their respective resonance. Similarly δ = ω − (ω − ω ), δ = ω − (ω − ω ), δ = ω − (ω − ω ) and 34 34 3 4 45 45 5 4 56 56 6 5 δ = ω − (ω − ω ) are the detunings for the MW fields for the respective transitions. In the rotating frame (i.e 36 36 6 3 it δ it () δδ + it () δδδ +− 12 12 23 12 23 34 with a unitary transformation ; ; ; ; c′= c c′= ce c′= ce c′= ce 11 22 33 44 it () δδδ +− +δ it () δδδ +− ++ δδ 12 23 34 45 12 23 34 45 56 c′= ce ; c′= ce ) and using the rotating wave approximation, (where the 55 66 i[( ωω +−ω )] ij ji terms with e is dropped out for the transition |i〉 → |j〉 if ω > ω ) we get following Hamiltonian j i H =| [0 11 〉〈 |− δδ |〉 22 〈| −+ () δ |〉 33 〈| 12 12 23 −+ () δδδ −|44 〉〈 |− () δδδ + −+| δ 55 〉〈 | 12 23 34 12 23 34 45 Ω Ω 12 23 −+ () δδδ −+ δδ +|66 〉〈 |+ |〉 12 〈| + |〉 23 〈| 12 23 34 45 56 2 2 ref ref ref Ω Ω Ω 34 45 56 + |〉 34 〈| + |〉 45 〈| + |〉 56 〈| 2 2 2 unk it () δδ −−δδ + 34 45 56 36 + eh |〉 36 〈| +. c.] (3) In general, the Hamilitonian H is time dependent except for a particular condition when δ − δ − δ + δ = 0. 34 45 56 36 e t Th ime evolution of the density matrix, ρ is given by Linblad master equation as ρρ =− [, HL ][ + ρ() t ] (4) where, L[ρ(t)] is Linblad matrix and defined as below. L[ρ(t)] = decdec decdec dec γγ γγ γ 12 13 14 15 16 Γ− ρρ −− ρρ −− ρρ 22 12 13 14 15 16 2 2 2 2 2 decdec decdec dec γγ γγ γ 12 23 24 25 26 −− ρρ Γ+ Γ− ρρ −− ρρ − ρ 21 32 21 22 33 23 24 25 26 2 2 2 2 2 decdec decdec dec γγ γγ γ 13 23 34 35 36 −− ρρ −Γ ρρρ −Γ +Γ −− ρρ − ρ 32 34 63 31 32 33 33 66 34 35 36 2 2 2 2 2 decdec decdec dec γγ γγ γ 14 24 34 45 46 −− ρρ −Γ ρρ −Γ ρρ −− ρ 34 4 41 42 43 33 44 45 46 2 2 2 2 2 decdec decdec dec γγ γγ γ 15 25 35 45 56 −− ρρ −− ρρ −Γ ρρ − 51 52 53 54 55 56 2 2 2 2 2 decdec decdec dec γγ γγ γ 16 26 36 46 56 −− ρρ −− ρρ −− ρρ Γ 61 62 63 64 65 66 2 2 2 2 2 (5) Where, Γ is the decay of the population from state |i〉 (i = 1, 2, .. to 6) to state |j〉 (j = 1, 2, .. 6) and Γ is the total ij i population decay rate of state |i〉. In the case of the weak probe, the population transfer does not take place and it is completely irrelevant to know the population dynamics between different levels. The only important parameter dec is Γ and Γ , i.e. the total decay rate of states, which governs the decoherence rate (γ ) between the two levels |i〉 i j ij Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 3 www.nature.com/scientificreports/ ref ref ref ukn Figure 2. e n Th ormalized absorption, ρ Γ /Ω vs Time for Ω =Ω =Ω =Ω =Γ , Ω =. 05Γ and 12 2 12 23 34 45 56 2 36 2 δ = δ = δ = δ = δ = δ = 0. 12 23 34 45 56 36 Figure 3. Comparison of complete numerical solution with the analytical solution for the normalized ref ref ref absorption (Im(ρ )Γ /Ω ) vs δ /Γ of the probe laser with Ω= Ω= Ω= Ω= Γ , 12 2 12 12 2 23 34 45 56 2 unk Ω= 05 .Γ , φ = 0 and δ = δ = δ = δ = δ = 0. 23 34 45 56 36 36 2 Γ+ Γ ij dec and |j〉 as γ = . In addition to the total decay rate of states, the linewidth of lasers driving the transition ij dec dec has to be also included for . For example, in this study we take the value of γ =× 23 π .05 MHz, which ij 12 includes natural radiative decay of excited state, Γ = 2π × 6 MHz and the 780 nm laser linewidth of 2π × 50 kHz. decdec decdec dec We also take γ ==== γγγγ =× 2π 100 kHz mainly dominated by the laser linewidths of 13 14 15 16 780 nm and the 480 nm as compared to the radiative decay rate (=2π × 1 kHz) of the Rydberg states |3〉, |4〉, |5〉 7 dec and |6〉 . We also take γ = 2π × 500 kHz in some cases in order to check it’s stringency. From Eqs 3, 4 and 5 we get 36 coupled differential equations with the property ρ = ρ . In order to solve these ij ji set of coupled equation we adapt similar method as in the case of previously studied multi-level systems . In the case of weak probe approximation, there will be no population transfer and hence the time evolution of the population i.e. the diagonal terms of the density matrix such as ρ , ρ , ρ , ρ , ρ , and ρ can be ignored. 11 22 33 44 55 66 Similarly the time evolution of the off-diagonal terms ρ for i = 2; j = 3, 4, 5, 6 and i = 3; j = 4, 5, 6 and i = 4; j = 5, ij 6 and i = 5; j = 6 can be also ignored. The time evolution of the relevant density matrix element is given below. Ω Ω 12 23 ρρ = ii () −+ ρρ − γρ 12 11 22 13 12 2 2 ref Ω Ω Ω 12 23 34 ρρ =−ii + ρρ + i 13 23 12 14 22 2 unk 36 −− it () δδ −+ δδ 34 45 56 36 + ie ργ − ρ 16 13 ref ref Ω Ω Ω 12 34 45 ρρ =−ii + ρρ + i − γρ 14 24 13 15 14 22 2 ref ref Ω Ω Ω 12 45 56 ρρ =−ii + ρρ + i − γρ 15 25 14 16 15 22 2 unk ref Ω Ω Ω 12 36 it () δδ −−δδ + 56 34 45 56 36 ρρ =−ii + ei ρρ + − γρ 16 26 13 15 16 (6) 22 2 dec Where, γ =+  γδ i , 12 12 12 Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 4 www.nature.com/scientificreports/ dec γγ =+ [( i δδ + )], 13 13 12 23 dec γγ =+ [( i δδδ +− )], 14 14 12 23 34 dec γγ =+ [( i δδδ +− + δ )], 15 15 12 23 34 45 dec γγ =+ [( i δδδ +− ++ δδ )], 16 16 12 23 34 45 56 Now, we apply the four-photon resonance condition for the MW fields i.e. δ − δ − δ + δ = 0. In this case 34 45 56 36 the system will reach steady state i.e. , for all the elements on the time scale of few tens of 1/Γ as shown in ρ = 0 ij Fig. 2. In the weak probe condition and in the steady state, ρ ≈ 1, ρ ≈ ρ ≈ ρ ≈ ρ ≈ ρ ≈ 0 and ρ = ρ ≈ 0 11 22 33 44 55 66 ij ji for i = 2; j = 3, 4, 5, 6 and i = 3; j = 4, 5, 6 and i = 4; j = 5, 6 and i = 5; j = 6. Finally, we get the following set of equations Ω Ω ii 12 23 ρ = + ρ 12 13 22 γγ 12 12 ⁎⁎ ref unk Ω Ω Ω ii i 23 34 36 ρ = ρ + ρ + ρ 12 14 16 22 γ γ 2 γ 13 13 13 ref ref Ω Ω ii ρ = ρ + ρ 14 13 15 22 γ γ 14 14 ref ref ii Ω Ω 45 56 ρ = ρ + ρ 15 14 16 22 γ γ 15 15 unk ref ii Ω Ω 36 56 ρ = ρ + ρ 16 13 15 22 γ γ 16 16 (7) e a Th bove equation gives solution for ρ as i Ω 2 γ ρ = 1 |Ω | 4 γγ 12 13 1 + 1E +++ ITATA1 EITATA2Int where, ref2 |Ω | 4 γγ 13 14 EITATA1 = ; ref2 1 |Ω | 4 γγ 14 15 1 + ref2 1 |Ω | 1 + 4 γγ 15 16 unk2 |Ω | 4 γγ 13 16 EITATA2 = ; ref2 1 |Ω | 4 γγ 15 16 ref2 1 |Ω | 1 + 4 γγ 14 15 ref ref ref unk 1 |Ω || Ω| |Ω || Ω| cos () φ 34 45 56 36 8 γγ γγ 13 14 15 16 Int =− ; ref2 ref2 |Ω ||Ω| 1 1 45 56 1 ++ 4 γγ 4 γγ 14 15 15 16 unk ref ref ref φφ =− φφ −− φ (8) 36 34 45 56 The refractive index, n of the probe laser is related with the density matrix element, ρ as , where λ (=780 nm) is the wavelength of the probe laser and N is atomic number n =+ 13λΓ N /(2) πρ (/Ω ) p 212 24,25 density . The imaginary part of n is related with the absorption and real part with dispersion. We define the normalized absorption [(Γ /Ω ) Im(ρ )] i.e. for the stationary atoms, the absorption of the probe laser at reso- 2 12 12 nance in the absence of all the control lasers is 1. In order to verify the approximation made above, we have checked the analytical solution of ρ given by the Eq. 8 and the complete numerical solution in the steady state for various values of control fields and detunings. It has excellent agreement between complete numerical and approximated analytical solution as shown in Fig. 3. e Th solution for ρ in Eq. 8 has the following interpretation. Interpretation. Interference between two sub-system. Equation 8 looks very complicated but it can be inter- preted in the following simple way. The closed loop system can be realized by two open loop sub-systems |3〉 → |4〉 → |5〉 → |6〉 and |3〉 → |6〉 → |5〉 → |4〉 shown with red and green arrows respectively as shown in Fig. 1b. These two sub-system shares a common |1〉 → |2〉 → |3〉 ladder system. In order to understand the absorption property of the probe laser Ω , we switch on the control fields one by one and in the sequence for the two Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 5 www.nature.com/scientificreports/ ref ref Figure 4. Normalized absorption (Im(ρ )Γ /Ω ) vs δ /Γ of the probe laser with Ω= Ω= Ω= 12 2 12 12 2 23 34 45 ref unk unk Ω= Γ , δ = δ = δ = δ = δ = 0 and (a) Ω= Γ (b) Ω= 05 .Γ . 23 34 45 56 36 56 2 36 2 36 2 sub-systems. Firstly, the control laser Ω causes transparency for the probe laser Ω and known as EIT. For path 23 12 ref shown with the red color, the control field Ω recovers the absorption against the EIT created by Ω and known 34 23 ref ref as EITA. Again the control fields Ω causes transparency against the EITA created by the Ω and Ω , and 45 23 34 ref ref ref known as EITAT. Finally the Ω causes absorption against the EITAT created by the Ω , Ω and Ω , and 56 34 45 known as EITATA and expressed by EITATA1 in Eq. 8. (In order to understand the transparency and absorption in the sequence, we strongly advice the readers to see the paper ). The other path shown with green color will also unk ref ref cause EITATA by sequence of the control fields Ω , Ω and Ω which is expressed by EITATA2. Further, these 36 56 45 two sub-system causing EITATA1 and EITATA2, interferes with each other and expressed by the Int term in the Eq. 8, which is phase(φ) dependent. In the other words, the closed loop |3〉 → |4〉 → |5〉 → |6〉 → |3〉 causes absorption against EIT created by the control laser Ω . The closed loop has two-open loop sub-systems which interfere destructively (for φ = 0) and ref ref ref unk dec constructively (for φ = π) with each other. As shown in Fig. 4a, for , Ω= Ω= Ω= Ω= Γ () γ 34 45 56 36 2 there is a complete transparency at the line center for φ = 0. This is due to perfect destructive interference between the two-subsystems as the strength is same for both, i.e. EITATA1 = EITATA2. er Th e is maxi-mum absorption at the line center for φ = π as the two sub-systems are interfering constructively. For ref ref ref unk dec Ω= Ω= Ω≠ Ω γ , there is a absorption peak at the line center for φ = 0, as shown in 34 45 56 36 Fig. 4b. This is due to unequal strength of the individual system (EITATA1 > EITATA2), hence the destructive interference between them is not perfect. Dressed state approach. At high Rabi frequencies (much greater than the absorption peaks linewidths) of the control lasers and MW fields, the linewidth of the absorption peak can be explained using dressed state picture. In this condition there is no interference between the absorption peaks as they are well separated from each other. e p Th osition of the absorption peak is determined by the eigenvalues of the Hamiltonian associated to the control fields as given below 0 00 0 ⁎ ref unk Ω ΩΩ 34 ii φφ 36 34 36 δ ee 0 22 2 ref ref Ω Ω 34 −ii φφ 45 34 45 H = 0 ee δδ − 0 c 23 34 ref ref Ω Ω 45 −ii φφ 56 45 56 00 ee δδ −+ δ 23 34 45 unk ref ΩΩ 36 −− ii φφ 56 36 56 0 ee 0 δδ −+ δδ + 23 34 45 56 2 2 (9) For general control fields detunings and Rabi frequencies, the position of the absorption peaks will be compli- cated. However, the expression becomes simpler for zero detuning of control fields and with ref ref ref unk Ω= Ω= Ω= Ω= Ω , but with arbitrary values of Ω . In this condition the positions of the 23 34 45 56 36 2 unk2 2 unk2 23 unk absorption peaks (i.e. eigenvalues of the H ) are − , 4( Ω+ |Ω |+ 2) Ω+ |Ω |+ 8Ω|Ω|cosφ 36 36 36 Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 6 www.nature.com/scientificreports/ 1 1 2 unk2 2 unk2 23 unk 2 unk2 2 unk2 23 unk − , 0, , 4( Ω+ |Ω |− 2) Ω+ |Ω |+ 8Ω|Ω|cosφ 4( Ω+ |Ω |− 2) Ω+ |Ω |+ 8Ω|Ω|cosφ 36 36 36 36 36 36 8 8 and . 2 unk2 2 unk2 23 unk 4( Ω+ |Ω |+ 2) Ω+ |Ω |+ 8Ω|Ω|cosφ 36 36 36 e eig Th envectors determines the dressed state in terms of the bare atomic states. For example the normalized eigenvector corresponding to eigenvalue 0 is unk |Ω | iφ 36 1 − e 1/2 unk2 unk − 1 |Ω | |Ω | 36 36 12 +− cosφ + 2 2 0 Ω 1( 10) unk iφ Ω e This is the central dressed state (or the central absorption peak) and is expressed as 1 − 1/2 unk unk Ω Ω 36 36 246 −+ / . The linewidth of the dressed state or the absorption peak is ] 12 +− cosφ + 2 2 Ω Ω given in terms of the bare atomic states decay rate. For example, if dressed state is written as 2 2 2 2 C |2〉 + C |3〉 + C |4〉 + C |5〉 then the linewidth of it will be |C | Γ + |C | Γ + |C | Γ + |C | Γ Hence the linewidth 2 3 4 5 2 2 3 3 4 4 5 5 unk unk unk unk Ω Ω Ω Ω 36 36 36 36 of the cenetral absorption peak is given by / 12 +− cosφΓ+ Γ+ Γ 12 +− cosφ + 2 2 24 6 2 Ω Ω Ω Ω which is phase dependent. In order to crosscheck the expression for the linewidth, we fit (shown with black solid line) the central peak of the normalized absorption obtained by Eq. 8 with Lorentzian prole fi to find the linewidth for three different phases as shown in Fig. 4. The fitted linewidths for φ = 0, φ = π/2 and φ = π are 0.13Γ , 0.47Γ and 2 2 0.64Γ respectively, while the calculated linewidths are 0.13Γ , 0.39Γ and 0.54Γ respectively. There is a small mis- 2 2 2 2 match between the fitted and the calculated linewidths by the dressed state approach for φ = π/2 and φ = π. This is because, as we see in Fig. 4, the central absorption peak is broadened for φ = π/2 and φ = π and the interference between peaks starts playing a role in the modification of the linewidth similar to three level system . Results Probe laser absorption. e Th normalized absorption (Im(ρ )Γ /Ω ) vs probe detuning (δ ) for three dif- 12 2 12 12 ferent phases, φ = 0,π/2 and π is shown in Fig. 4. For the central absorption peak i.e. at δ = 0, only the linew- idth depends upon the phase but not the position, while both the position and the linewidth depends upon the phase(φ) for the other four absorption peaks. This has been explained in the previous section. Now, we consider the effect of the temperature as lineshape of EIT is significantly changed by the thermal 27–32 averaging . The thermal averaging of ρ is done numerically for the room temperature (T = 300 K) for the counter-propagating configuration of the probe (Ω ) and the control laser (Ω ) with wave-vectors k and k 12 23 780 480 respectively by replacing δ with δ + k v and δ with δ − k v for moving atoms with velocity v, while the 12 12 780 23 23 480 Doppler shift for the MW fields are ignored. Further the ρ is weighted by the Maxwell Boltzman velocity distri- mv Thermal m − bution function and integrated over the velocity as 2k T , where k is Boltzman con- ρ = ρ () ve B dv 12 12 2πkT kT stant and m is atomic mass of Rb. The integration is done over velocity range which is three times of . The Doppler averaging changes the absorption profile significantly as shown in Fig. 5. One of the interesting modifi- cation is the phase dependency of the probe laser absorption at the zero detunings of the probe. The probe laser absorption is minimum for φ = 0 and maximum for φ = π as shown with red and blue curve respectively in Fig. 5. This modification is due to mismatch of Doppler shift for probe at 780 nm and the control at 480 nm for moving atom. Please note that without thermal averaging at zero detunings of the probe, control laser and MW fields, probe laser absorption has no significant difference between φ = π/2 and π. Phase sensitivity. Sinusoidal behavior. As seen in the previous section that the absorption prole o fi f the probe 6–11 laser depends upon the phase, φ. Please note that the previously studied (i.e. four-level) system were insensitive ref ref ref to the phase of the MW field. This is also clear from Eq. 8 in the special case with Ω= Ω= Ω= 0, which 34 45 56 reduces the six-level loopy ladder system to four-level system and will have no phase dependency. e p Th robe absorption at room temperature vs the phase φ with all the detunings to be zero is shown in Fig. 6. From the plot shown with red open circle in Fig. 6a we observe more than 15% change in the probe absorption for the change of the phase from 0 to π for the chosen combinations of the control Rabi frequencies. In particular, we unk have chosen low value of Ω= 01 .Γ and the optimized control fields Rabi frequencies i.e. |Ω | = 2Γ , 36 2 23 2 ref ref ref Ω= 15 .Γ , and Ω= Ω= 4Γ . The numerical data points (red open circle) are fitted by a function 34 2 45 56 2 A + Bsin(f φ + θ), where A, B, f and θ are kept as free parameters that yields f = 1 and the fitting is shown with unk black curve in Fig. 6a. Now, choosing a high value of and keeping the other parameters unchanged, Ω= 25 .Γ 36 2 we observe more than 80% change in the probe absorption for the change of the phase from 0 to π as shown crossed red points, but there is a deviation from sinusoidal behavior. This deviation is compared with the t fi ted ref black curve as shown in Fig. 6b. On increasing the value of Ω to 3Γ and keeping the other parameters unchanged, there is a splitting of the absorption at φ = π as shown by the solid circled points in this figure. Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 7 www.nature.com/scientificreports/ Thermal Figure 5. Normalized absorption of the probe laser with thermal averaging (Im(ρ )Γ /Ω ) vs δ /Γ with 2 12 12 2 ref ref ref unk Ω= Ω= Ω= Ω= Γ , Ω= 05 .Γ and δ = δ = δ = δ = δ = 0. 23 34 45 56 36 23 34 45 56 2 36 2 Thermal Figure 6. Absorption of the probe laser aer t ft hermal averaging in arbitrary scale obtained as (Im( ))/ Thermal unk max(Im(ρ )) vs phase φ with δ = δ = δ = δ = δ = δ = 0 and (a) Ω= 01 .Γ , |Ω | = 2Γ , 12 23 34 45 56 36 23 2 36 2 ref ref ref unk ref Ω= 15 .Γ , and Ω= Ω= 4Γ . (b) crossed points Ω= 25 .Γ , |Ω | = 3Γ , Ω= 2Γ , and 34 2 45 56 2 36 2 23 2 34 2 ref ref unk ref ref ref Ω= Ω= 4Γ , solid circled points Ω= 25 .Γ , |Ω | = 3Γ , Ω= 3Γ , and Ω= Ω= 4Γ . 45 56 2 36 2 23 2 34 2 45 56 2 unk Optimization of sensitivity. Now, we maximize the phase sensitivity for this system for given value of by ref ref ref using the parameters, Ω , Ω , Ω , and Ω . In order to do this we define a quantity called sensitivity as 34 45 56 Thermal Thermal Thermal Thermal S == Im[( ρφ 0) −= ρφ () πρ ]/Im[(φρ =+ 0) () φπ = ], which is a measure of the 12 12 12 12 unk phase/strength sensitivity of the system and is to be maximized. For given value of Ω , we maximize the S by ref ref ref minimizing 1/S or -S using matlab inbuilt function “fmincon” treating Ω , Ω , Ω , and Ω as free parame- 34 45 56 ref ref ref ters but bounded in the region from 0 to 5 Γ . Please note that the values 5Γ for Ω , , and is well Ω Ω Ω 2 2 23 34 45 56 in the experimental reach. unk We first consider the case without thermal averaging i.e. T = 0. The maximized sensitivity, S vs Ω is max unk plotted in Fig. 7(a). The S increases with Ω and starts saturating around 0.05Γ . The corresponding maxi- max 2 ref ref ref mizing values of Ω , Ω , Ω , and Ω are also plotted in Fig. 7(b). The optimum value of the Ω is as high as 23 34 45 56 23 possible which is 5Γ in this case as it is bounded by this limit. This is more clear from the Fig. 8, where S 2 max ref ref ref unk increases with Ω and then saturates around Γ for any given values of Ω , Ω , Ω , and Ω . 23 2 34 45 56 36 Next, we consider the room temperature case (T = 300 K), which makes the problem a bit more complicated, as the lineshape of the absorption gets modified significantly as described previously. The maximum sensitivity unk (S ) vs Ω is plotted in the Fig. 9(a). The S at T = 300 K is much lower than the case at T = 0 as the satura- max max unk tion point is around = 1.5 Γ as compared to 0.05Γ and hence at T = 0 the system can detect the phase of 2 2 unk lower values of Ω . Unlike the case of T = 0, in this case for S the value of Ω ≠ 5Γ but has optimum values max 23 2 as shown in Fig. 9(b). Strength sensitivity. e q Th uantity, S defined above can also be used as a measure of the strength/amplitude unk sensitivity for Ω for the six-level loopy ladder system. Now we compare the strength sensitivity of the six-level 6–11 loopy ladder system with the previously studied four-level system . The solution of ρ for the four-level system Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 8 www.nature.com/scientificreports/ unk ref ref Figure 7. (a) The maximum sensitivity S (%) vs /Γ (b) The optimum value of /Γ and /Γ for Ω Ω Ω max 2 2 2 36 34 56 ref unk S (shown by left scale), Ω /Γ and /Γ (shown by right scale) vs for δ = δ = δ = δ = δ = δ = 0 Ω Ω max 23 2 2 12 23 34 45 56 36 45 36 and T = 0. Figure 8. S (%) = Im[ρ (φ = 0) − ρ (φ = π)]/Im[ρ (φ = 0) + ρ (φ = π)] × 100 vs Ω /Γ for max 12 12 12 12 23 2 unk δ = δ = δ = δ = δ = δ = 0, Ω= 0.Γ 005 and T = 0. 12 23 34 45 56 36 36 2 unk ref ref Figure 9. (a) S (%) vs Ω /Γ (b) The optimum value of Ω /Γ , Ω /Γ , and Ω /Γ shown by left scale max 36 2 23 2 34 2 56 2 ref unk and Ω /Γ shown by right scale vs Ω /Γ for δ = δ = δ = δ = δ = δ = 0 and T = 300 K. 45 2 36 2 12 23 34 45 56 36 Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 9 www.nature.com/scientificreports/ unk Figure 10. (a) S (%) vs ΩΓ / for six-level loopy and four-level ladder system (b) ratio (R) of the sensitivity max 36 2 unk between six-level and four-level system vs ΩΓ / at T = 0 with all the detunings to be zero and for 36 2 γ = 2π × 100 kHz and γ = 2π × 500 kHz. dec dec ref ref ref can be obtained from the six-level loopy ladder system by setting Ω= Ω= Ω= 0 in Eq. 8 and is given 34 45 56 by Eq. 11. 2 γ ρ = 12(4) l 1 |Ω | 4 γγ 12 13 1 + unk2 1 |Ω | 1 + 4 γγ (11) 13 16 e s Th ubscript (4l) indicates for four-level system. Further the thermal averaging can be done in a similar fash- mv Thermal m − ion as in the case of the six-level system i.e. 2k T . We define the strength sensitiv- ρ = ρ () ve B dv 12(4) l 12(4) l 2πkT unk ity for the four-level system for unknown Ω as change in the absorption in the presence and the absence of the unk Ω normalized by the sum of the two conditions which is mathematically expressed as Thermal unk Thermal unk Thermal unk Thermal unk S = / . We maxi- [ρρ (0 |Ω |≠ )( −|Ω| = 0)] [ρρ (0 |Ω |≠ )( +|Ω| = 0)] () 36 12(4) ll 36 12(4) 36 12(4) ll 12(4) mize the sensitivity of the four-level system adapting similar method as for the six-level system but with only one optimizing parameter i.e. Ω . First, we consider T = 0 case. The maximized strength sensitivity for the six-level loopy ladder system and the four-level system is compared in Fig. 10. From this figure it is clear that the six-level system has more sensitivity as compared to the four-level system as shown in Fig. 10(a). In order to quantify this comparison, we plot the ratio of the sensitivities of the six-level to four-level system in Fig. 10(b). The ratio is more for the low values of the unk Ω . The increased sensitivity for the six-level loopy system is due to the interferometric nature of the system unk ref ref ref where the effect of small Ω is enhanced by the large values of the Ω , Ω and Ω as the int term in Eq. 8 36 34 45 56 involves multiplication of these quantities. The strength sensitivity of both the systems decreases with increased γ (from 2π × 100 kHz to 2π × 500 kHz) but the effect is more for the four-level system in comparison to the dec six-level system as shown Fig. 10b. Now, we consider the case at the room temperature. The strength sensitivity for the six-level and previously studied four-level is plotted in Fig. 11(a). Form this plot it is clear that the six-level system has much superior strength sensitivity as compared to the four-level system. Further we quantify the comparison by plotting the ratio unk (R) of the sensitivities of the six-level to the four-level for different values of Ω in Fig. 11(b). In order to check the stringency of γ on the sensitivity, we also plot S for these two systems taking γ = 2π × 500 kHz. dec max dec We also plot the R vs maximum sensitivity (S ) of the six-level system which gives the information about the max unk possibility of the detection of . This is an important plot because there is a possibility that the R might be huge but can not be detected by the six-level system as well. e Th detection of S up to 1% is very much feasible max using locking detection. At this value of sensitivity for the six-level system, the sensitivity of the four-level system will be around % as shown in Fig. 12. unk Finally one more important point is that, for the six-level loopy ladder system the MW field can be detected by just varying the phase of the reference MW fields, while in the case of the four-level system we need to insert and remove MW mechanical shield. Frequency range. e f Th requency range of the atomic based MW interferometry can be any where from the range of the few tens of MHz, GHz and THz. The rydberg states can be chosen depending upon the interest of the frequency region of MW field. For example, for frequency in the range of few tens of GHz n ’s should around ryd Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 10 www.nature.com/scientificreports/ unk Figure 11. (a) S (%) vs for six-level loopy and four-level ladder system (b) ratio (R) of the sensitivity ΩΓ / max 36 2 unk between six-level and four-level system vs at T = 300 K with all the detunings to be zero and for ΩΓ / 36 2 γ = 2π × 100 kHz and γ = 2π × 500 kHz. dec dec Figure 12. Ratio (R) of the sensitivity between six-level and four-level system vs S (%) of the six-level system max unk at T = 300 K. The variation of S (%) corresponds to range of Ω from 0.005Γ to 0.02Γ . max 2 2 7 9 54 while for tens of MHz it should be higher number and it is around 57 in case of Cs . For THz regime this should be around 20 . Discussion In conclusion we theoretically study a six-level loopy ladder system using Rydberg states for the phase sensi- tive MW or RF electrometry. This is based upon the interference between the two sub-systems of EITATA. In counter-propagating configuration of the probe and control laser there is a change of the lineshape of the probe absorption due to Doppler averaging. The limitation of the proposed system is the decoherence rate between the ground state and the Rydberg states but not the thermal Nyquist noise as in the case of the electrical circuit based MW interferometry. 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Acknowledgements K.P. would like to acknowledge the discussion with David Wilkowski at CQT NTU and Sambit Bikas Pal at CQT NUS for this work. Author Contributions K.P. conceived the idea and did all the initial calculations, D.S. crosschecked all the calculations and helped in writing the paper, E.O. also crossed checked few calculations and helped in writing the paper. All authors reviewed the manuscript. Additional Information Competing Interests: The authors declare no competing interests. Publisher's note: Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations. Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 12 www.nature.com/scientificreports/ Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Cre- ative Commons license, and indicate if changes were made. The images or other third party material in this article are included in the article’s Creative Commons license, unless indicated otherwise in a credit line to the material. If material is not included in the article’s Creative Commons license and your intended use is not per- mitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this license, visit http://creativecommons.org/licenses/by/4.0/. © The Author(s) 2018 Scientific REPO R TS | (2018) 8:8692 | DOI:10.1038/s41598-018-27011-1 13
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