PONTIFICIA UNIVERSIDAD CATÓLICA DEL PERÚ  ESCUELA DE POSGRADO      Polarimetric measurements of single‐photon geometric phases  Artículo publicable para optar el título de Magíster en Física que presenta:  Yonny Daniel Yugra Carcasi    Asesor:  Prof. Francisco de Zela  Jurado:  Prof. Eduardo Massoni   Prof. Hernán Castillo  Lima, 2015  RESUMEN  Nombre del graduando: Yonny Daniel Yugra Carcasi  Posgrado en: Física  Título del artículo publicado:  Polarimetric measurements of single‐photon geometric phases  Este artículo ha sido publicado en:  PHYSICAL REVIEW A, Volume 89, Issue 1, 2014  DOI: http://dx.doi.org/10.1103/PhysRevA.89.012124  Resumen:  Se  presenta  mediciones  polarimétricas  de  fases  geométricas  generadas  en  la  evolución  de  la  polarización  de  fotones  a  lo  largo  de  trayectorias  no‐geodésicas  en  la  esfera  de  Poincaré.El  núcleo  del  arreglo  polarimétrico  consiste  de  siete  placas  retardadoras.  Este  arreglo  permite  realizar  cualquier  transformación unitaria del  grupo  SU(2) en el espacio de  polarización. Haciendo uso de  la  invariancia gauge de  las  fases geométricas  bajo  transformaciones  locales  U(1),  es  posible  anular  la  contribución  dinámica a  la fase total, con  lo cual se  logra que esta última coincida con  la  fase  geométrica.  Como  la  fase  total  es  accesible  a  las  mediciones  experimentales,  la  fase  geométrica  se  torna  así  también  accesible  a  las  mismas. Se demuestra que nuestro dispositivo es  robusto  frente a diversas  perturbaciones  que  usualmente  afectan  arreglos  interferométricos,  ya  que  utilizamos un solo haz de fotones. Nuestro arreglo polarimétrico de muestra  ser  una  herramienta  sumamente  versátil  que  podría  ser  utilizada  para  someter a prueba la robustez de las fases geométricas frente a varias fuentes  de decoherencia.  PHYSICAL REVIEW A 89, 012124 (2014) Polarimetric measurements of single-photon geometric phases O. Ortı´z,1 Y. Yugra,1 A. Rosario,1 J. C. Sihuincha,1 J. C. Loredo,2 M. V. Andre´s,3 and F. De Zela1 1Departamento de Ciencias, Seccio´n Fı´sica, Pontificia Universidad Cato´lica del Peru´, Apartado 1761, Lima, Peru 2Centre for Engineered Quantum Systems, Centre for Quantum Computer and Communication Technology, and School of Mathematics and Physics, University of Queensland, 4072 Brisbane, Queensland, Australia 3Departamento de Fı´sica Aplicada y Electromagnetismo, Universidad de Valencia, c/Dr. Moliner 50, Burjassot, Valencia, Spain (Received 9 October 2013; published 24 January 2014) We report polarimetric measurements of geometric phases that are generated by evolving polarized photons along nongeodesic trajectories on the Poincare´ sphere. The core of our polarimetric array consists of seven wave plates that are traversed by a single-photon beam. With this array, any SU(2) transformation can be realized. By exploiting the gauge invariance of geometric phases under U(1) local transformations, we nullify the dynamical contribution to the total phase, thereby making the latter coincide with the geometric phase. We demonstrate our arrangement to be insensitive to various sources of noise entering it. This makes the single-beam, polarimetric array a promising, versatile tool for testing robustness of geometric phases against noise. DOI: 10.1103/PhysRevA.89.012124 PACS number(s): 03.65.Vf, 03.67.Lx, 42.65.Lm I. INTRODUCTION Even though experiments testing different properties of ge- ometric phases are continuously reported, theoretical develop- ments can expand at such an accelerated pace that experimental testing can be temporarily left behind. This seems to be the case with the subject of geometric phases. Since Berry’s seminal work [1], which brought to light the appearance of geometric phases in adiabatically evolving, cyclic quantum processes, there have been considerable generalizations of the subject. From Hannay angles in the classical domain [2] to geometric phases in mixed quantum states subjected to nonunitary and noncyclic evolutions [3–7], the original concept of geometric phases has been widely expanded. Experimental testing is required not only because of fundamental reasons lying at the basis of all empirical sciences, but because experimental input can help us to find the answer to open questions. Notably, the question about a proper, self-consistent definition of a geometric phase for nonunitary evolutions still remains open [8–13]. Similarly, the kind of robustness that geometric phases might have against decohering mechanisms is also an open question of utmost importance, particularly in the realm of quantum computation [14]. It is thus useful to explore as many experimental techniques as possible. One should not refrain from mirroring experiments already performed with one technique and conduct similar experiments based on another independent technique. This can provide not only new insights, but an enlarged versatility as well. Geometric phases are particularly well suited for such an approach, as they notoriously appear in the evolution of two-level systems. Such systems can be realized under manifold situations, i.e., quantal and classical ones. The drawbacks of one technique could then be replaced by some advantages of the other. For example, the physical realization of the qubit as a spin one-half particle, e.g., a neutron, has its counterpart in the realization of the qubit as a polarized photon. While as a source of the former, one needs a nuclear reactor, as a source of the latter, a diode-laser suffices. On the other hand, the versatility reached in experiments with neutrons can outperform that reached with their optical counterparts. A challenge is thereby put on the latter as to how to improve their versatility. We have addressed such a challenge in the present work. We report on experiments performed with single photons, which to some extent mirror previous experiments that were conducted with neutrons [15–18]. Our experiments put under test theoretical predictions about SU(2) evolutions along nongeodesic paths. Using neutrons, experiments along these lines have been conducted by exploiting the advantages offered by polarimetric techniques. In contrast to interfero- metric techniques [19], polarimetric ones have an intrinsic robustness because they require a single beam [20]. The challenge posed here, however, is how to manipulate two coherently superposed states that are not spatially separated. In interferometry, the (binary) path degree of freedom can be used together with an “internal” degree of freedom, e.g., the spin, that is carried along by the particle. In polarimetry, instead, there is only one path. One must then figure out how to deal with this restriction and nevertheless reach a versatility that is comparable to that of interferometry. The latter offers, for example, the possibility of spin-path entanglement. In neutron polarimetry, energy-polarization entanglement and even a tripartite energy-polarization-momentum entanglement have been achieved [21]. Although an all-optical version of the latter seems difficult to implement, there are other features that can be exploited with advantage in optical polarimetry. We show here how to exploit the invariance of geometric phases under local gauge transformations [22] in order to nullify the dynamical part of the total (Pancharatnam) phase [23], thereby making this phase coincide with the geometric phase. What is meant by gauge invariance is the invariance under the change |ψ(s)〉 → |ψ ′(s)〉 = exp [iα(s)] |ψ(s)〉 of an unitarily evolving state |ψ(s)〉. By exploiting this invariance, one can nullify the dynamical contribution to the total phase, P = arg〈ψ(s1)|ψ(s2)〉, between an initial and a final state, |ψ(s1)〉 and |ψ(s2)〉, respectively. What remains after elimination of the dynamical part is the purely geometric contribution g to the total phase, P = g + dyn. The SU(2) evolutions we have addressed are those of the type given by Un(θ,ϕ,s) = exp [−isn(θ,ϕ) · σ/2]. Here, n is a unit vector, σ is the triple of Pauli matrices, and s is the 1050-2947/2014/89(1)/012124(8) 012124-1 ©2014 American Physical Society O. ORT´IZ et al. PHYSICAL REVIEW A 89, 012124 (2014) rotation angle (on the Bloch or Poincare´ sphere). We could generalize our approach so as to deal with unit vectors that depend on s, but we have focused on cases with a fixed n. We also restricted ourselves to deal with pure single-photon states. These restrictions are justified in view of the extension already achieved by considering the production of geometric phases in systems subjected to transformations Un(θ,ϕ,s) of the above type. Previous experimental tests were restricted to particular trajectories that a system follows when subjected to some special transformations [15,17,18]. The cases we address here let us study what happens when we lift these restrictions. In such a case, a series of features shows up that is worthwhile to analyze before undertaking a systematic investigation of, say, the sensitivity of geometric phases to environmental influences. A main motivation of the present work was to analyze and explain the appearance of the aforementioned features. This opens the way for using this array as a basic component for testing the impact of decohering mechanisms. II. POLARIMETRY The standard procedure to exhibit the relative phase between two states is to make them interfere and then record the intensity of the interfering pattern by varying the relative phase. An archetypical setup for doing this is a Mach-Zehnder interferometer. Expressed in the language of quantum gates [24], such a device consists of two Hadamard gates—i.e., two beam splitters—and a phase shifter. A Hadamard gate can be represented in terms of Pauli matrices as UH = (σx + σz)/ √ 2, while the phase shifter can be represented as Uφ = exp(−iφσz/2). Hereby, we establish a one-to-one correspondence between the eigenvectors |±〉 of σz and the two paths of the interferometer. The action of the interferometer on an input state |+〉 is thus given by |+〉 → UHUφUH |+〉. The output intensity that is recorded at, say, a |+〉 detector reads I = |〈+|UHUφUH |+〉|2 = (1 + cosφ)/2. Now, instead of assigning the states |±〉 to the two possible paths of the inter- ferometer, we can make them correspond to the horizontal and vertical polarization states of a single light beam. We thereby change from interferometry to polarimetry. In the latter, the action of Uφ and UH can be realized with the help of quarter- wave (Q) and half-wave (H ) plates. Indeed, we have that Uφ = Q(π/4)H ((φ − π )/4)Q(π/4) and UH = −iH (π/8). The ar- guments in H and Q refer to the angles made by the plate’s major axis and the vertical direction. Up to a global phase, the action of the Mach-Zehnder interferometer can then be mirrored in polarization space by letting a polarized light beam traverse a gadget that consists of a couple of aligned retarders. In the present case, such an array is given by Q(π/2)H ((2π − φ)/4)Q(π/2). This last expression is obtained by us- ing Q(α)H (β) = H (β)Q(2β − α) and Q(α)H (β)H (γ ) = Q(α + π/2)H (α − β + γ − π/2). Hence, by setting a hor- izontal polarizer before a detector and recording the intensity as a function of φ, we get a pattern that looks the same as the interferogram produced with the Mach-Zehnder device. Polarimetry has the great advantage of being largely insensitive to those perturbations that in the case of interferometry lead to random phase shifts. On the other hand, the states |±〉 cannot be individually addressed, as they are no longer spatially sep- arated from one another, as occurs in interferometry. We must then find a way to extract the desired information by adequately projecting the manipulated states before detection. In the case of geometric phases, this is indeed possible, as we show next. Following a similar procedure as the one introduced by Wagh and Rakhecha [20]—thereby extending to single photons some techniques already employed with classical light [25–27]—we consider an initial, horizontally polarized state |h〉 and submit it to a π/2 rotation around the x axis. This produces a circularly polarized state (|h〉 − i |v〉) /√2. By submitting this state to the transformation exp (−iφσz/2), we get V |h〉 ≡ exp (−iφσz/2) exp (−iπσx/4) |h〉, which is the state (|h〉 − ieiφ |v〉)/√2, up to a global phase. Hence, we have generated a relative phase shift φ − π/2 between |h〉 and |v〉. If we now apply U ∈ SU(2), we then ob- tain UV |h〉 = (e−iφ/2U |h〉 − ieiφ/2U |v〉)/√2. We are inter- ested inUn(θ,ϕ,s) = exp [−isn(θ,ϕ) · σ/2] and the geometric phase that this transformation generates. We recall that the geometric phase is given by [22] g(C) = arg〈ψ(0)|ψ(s)〉 − Im ∫ s 0 〈ψ(s ′)| ˙ψ(s ′)〉ds ′, (1) for a path C joining the initial state |ψ(0)〉 with the fi- nal state |ψ(s)〉. As already said, g is invariant under local gauge transformations. We exploit this property in order to nullify the dynamical contribution to g . That is, we choose a gauge transformation |ψ(s)〉 → |ψ ′(s)〉 = exp [iα(s)] |ψ(s)〉 so that 〈ψ ′(s)| ˙ψ ′(s)〉 = 0. In other words, instead of applying Un(θ,ϕ,s), we apply exp [iα(s)]Un(θ,ϕ,s) and measure the total phase arg〈ψ(0)|ψ(s)〉. In the present case, this can be achieved by setting α(s) = s 〈+| n · σ |+〉 /2. That is, we seek to implement the transformation |h〉 → UnV |h〉 = (e−iγ /2Un |h〉 − ieiγ /2Un |v〉)/ √ 2, where γ (s) = φ − α(s). We can realize this with the help of wave plates. To begin with, Un can be implemented with a gadget proposed by Simon and Mukunda [28], which is given by Un(θ,ϕ,s) = Q ( π + ϕ 2 ) Q ( θ + ϕ 2 ) ×H (−π + θ + ϕ 2 + s 4 ) Q ( θ + ϕ 2 ) Q (ϕ 2 ) . (2) The rotation axis is here given by n = (sin θ cosϕ, sin θ sinϕ, cos θ ) and the Pauli matrices are de- fined according to the convention that is commonly employed in optics. That is, the diagonal matrix in the basis {|h〉,|v〉} of horizontally and vertically polarized states is σx . The other two Pauli matrices follow from cyclically completing the change σz → σx . With this choice, our gauge is given by α(s) = s 2 sin θ cosϕ. (3) On the other hand, V (γ ) = e−iγ σz/2e−iπσx/4 can be implemented as V (γ ) = Q(π/4)H ((γ − π )/4)H (π/4). The total transformation is thus Utot ≡ V †UnV = H ( −π 4 ) H ( γ + π 4 ) Q ( −π 4 ) ×Un(θ,ϕ,s)Q (π 4 ) H ( γ − π 4 ) H (π 4 ) . (4) 012124-2 POLARIMETRIC MEASUREMENTS OF SINGLE-PHOTON . . . PHYSICAL REVIEW A 89, 012124 (2014) Applying as before relations such as Q(α)H (β) = H (β)Q(2β − α), Q(α)H (β)H (γ ) = Q(α + π/2)H (α − β + γ − π/2), etc., we reduce the above array to one that consists of seven plates: Utot(θ,ϕ,φ,s) = Q [ π 4 − γφ(s) 2 ] Q [ −π − ϕ 2 − γφ(s) 2 ] Q [ π − θ − ϕ 2 − γφ(s) 2 ] H [−θ − ϕ 2 − s 4 − γφ(s) 2 ] ×Q [ π − θ − ϕ 2 − γφ(s) 2 ] Q [ π − ϕ 2 − γφ(s) 2 ] Q [ −π 4 − γφ(s) 2 ] , (5) where γφ(s) = φ − α(s). We use this notation to emphasize that γ depends on both φ and s. Note that by going from Eq. (4) to Eq. (5), the gauge-fixing role—originally played by the plates implementing V (γ )—turns to be shared by all seven plates of the final array. The path followed by the polarization state subjected to Utot can be represented on the Poincare´ sphere by a circular arc; see Fig. 1. This arc is fixed by n(θ,ϕ), by the initial polarization state, and by s. The latter fixes the angle by which the initial state is rotated. Once we have fixed n and the initial state, we record the geometric phase as a function of s. This is done by varying the registered intensity as a function of γφ(s), which plays a double role. First, it contains the phase shift φ that is required to implement the polarimetric version of the Mach-Zehnder interferometer, as discussed above. Second, it contains the gauge shift α(s) that is required to make the total phase coincide with the geometric phase. In order to extract this geometric phase, we project the state UnV (γ ) |h〉 onto the state V (γ ) |h〉 = e−iγ /2(|h〉 − ieiγ |v〉)/√2. The recorded intensity is thus given by I = |〈h|V †(γ )UnV (γ )|h〉|2. As we shall see, after having fixed θ , ϕ, and s, we can let γ (viz., φ) vary so as to generate an intensity pattern I (φ), whose maxima and minima determine the value of the geometric phase at (s,θ,ϕ). This value can be compared with the theoretical one, which is FIG. 1. (Color online) Path followed on the Poincare´ sphere by the Stokes vector that corresponds to an initial state |h〉 being submitted to a transformation exp(−isn · σ/2). The rotation axis n has polar angles θ = π/3,ϕ = π/4. The dynamical contribution to the total phase P is gauged-away all along the curve, so that P = g holds at each value of s. given by g = P − dyn, where P = arg〈ψ(0)|ψ(s)〉 = arg 〈h|Un(s) |h〉 = − arctan [ sin θ cosϕ tan ( s 2 )] , (6) dyn = Im ∫ s 0 〈ψ(s)| ˙ψ(s)〉ds = Im ∫ s 0 〈h|U †n(s)(−in · σ )Un(s) |h〉 ds = − s 2 〈h| n · σ |h〉 . (7) The theoretical expression for the geometric phase thus reads thg = − arctan [ sin θ cosϕ tan ( s 2 )] + s 2 sin θ cosϕ. (8) On the other hand, a straightforward calculation of the intensity I = |〈h|V †[φ − α(s)]Un(θ,ϕ,s)V [φ − α(s)]|h〉|2 gives I = cos2 ( s 2 ) + sin2 ( s 2 ) {cos θ cos[α(s) − φ] + sin θ sinϕ sin[α(s) − φ]}2. (9) We then have Imin(s) = cos2 ( s 2 ) , (10) Imax(s) = cos2 ( s 2 ) + sin2 ( s 2 ) [cos2 θ + (sin θ sinϕ)2], (11) where we have used that the maximum of f (α) = a cosα + b sinα is given by √ a2 + b2. From the above equations, we get 1 − Imax 1 − Imin = sin 2 θ cos2 ϕ, (12) 1 − Imax Imin = sin2 θ cos2 ϕ tan2 ( s 2 ) . (13) We can thus express thg in terms of the experimentally accessible quantities Imin and Imax as g(s) = √ 1 − Imax(s) 1 − Imin(s) arccos[ √ Imin(s)] − arctan [√ 1 − Imax(s) Imin(s) ] for −π < s < π, (14) 012124-3 O. ORT´IZ et al. PHYSICAL REVIEW A 89, 012124 (2014) g(s) = √ 1 − Imax(s) 1 − Imin(s) arccos[− √ Imin(s)] + arctan [√ 1 − Imax(s) Imin(s) ] ±π for π < s < 3π. (15) Note that g is undefined for s = π ; cf. Eq. (8). The ±π that appears in g(s > π ) comes from the Pancharatnam contribution, arg 〈h|Un(s) |h〉, that is contained in thg . Indeed, 〈h|Un(s) |h〉 = cos(s/2)[1 − i sin θ cosϕ tan(s/2)], so that arg 〈h|Un(s) |h〉 = arg [cos(s/2)] − arctan[sin θ cosϕ tan(s/2)]. For π < s < 3π, we have that arg [cos(s/2)] = ±π . III. EXPERIMENTAL PROCEDURE AND ANALYSIS OF RESULTS A sketch of our experimental arrangement is shown in Fig. 2. Its core is the array of seven plates that realize the transformation Utot(θ,ϕ,φ,s), as given in Eq. (5). Our single- photon source was a beta barium borate (BBO) crystal pumped by a cw diode laser (measured central wavelength 400 nm; spectral linewidth lies between 0.5 and 1 nm at operating temperatures; output power 37.5 mW). Two photon beams were produced in the BBO crystal by type-I spontaneous para- metric down-conversion, with each beam having a wavelength of 800 nm. One beam, the idler or heralding one, was directed towards an avalanche photodetector. The other, signal beam, was directed towards the array of seven plates. Coincidence SPCM FPGA PC BBO H CLF PUtot L F M P FIG. 2. Polarimetric array. The set of seven wave plates shown at the bottom can be oriented so as to realize the desired SU(2) transformation (Utot) in polarization space. Polarized photons enter this array after having been produced in a nonlinear, beta barium borate (BBO) crystal that is fed by a diode laser (L) that emits 400 nm light whose polarization is fine tuned with a λ/2 plate (H ) placed before the crystal. Polarizers (P ) set before and after the retarders project the photon’s polarization as required (see text). Signal photons are recorded in coincidence with their heralding twins in a single- photon counting module (SPCM). Other components are M: mirrors; CL: converging lenses; F: filters, FPGA: field programmable gate array; and PC: personal computer. counts (I ) of idler and signal beams made up our raw data, with coincidences being defined within a time window of 10.42 ns. Our photon-counting module was a Perkin-Elmer SPCM-AQ4C, with a dark count rate of 500 ± 10 cps. Photons were collected with the help of converging lenses that focused them into multimode fiber-optic cables having fiber-coupling connectors at both ends. The recorded coincidences were obtained according to the following procedure. For given values of θ , ϕ, and s, the seven plates were oriented as prescribed in Eq. (5), with γ = φ − s sin θ cosϕ/2. The angle φ was varied from 0◦ to 360◦ in steps of 40◦. Coincidence counts were recorded as a function of φ and then normalized to obtain the intensity I (φ). Theoretically, I (φ) is given by Eq. (9), with s, θ , and ϕ kept fixed. By repeated measurements, we sampled 30 points for each value of φ. The parameter s took values si from 40◦ to 320◦ in steps of 40◦. After averaging the recorded coincidence counts for eachφ, we obtained a series of points I (φi). A best fit I (φ) to these points was found, where I (φ) is a sinusoidal function whose parameters were fixed by the least-squares method. Figure 3 shows the so-obtained curves for θ = π/2, ϕ = π/3 and different values of s. From these curves, we determined Imax and Imin. By entering Imax and Imin in Eqs. (14) and (15), the experimental values ofg(s,θ,ϕ) can be obtained and compared with the ones predicted by Eq. (8). Figure 4 shows our experimental results together with the corresponding theoretical predictions. As can be seen, two of the three cases seem to reflect a systematic departure of our experimental findings from the theoretical predictions. We will come back to this point below. As for the single-photon production, it was checked by the standard procedure [29,30] of measuring the degree of second-order coherence, g(2), between the output fields of a beam splitter, i.e., the reflected (R) and transmitted (T) beams. Detections at gates T and R were conditioned upon detection at a third gate G. In such a case, g(2) = PGTR/(PGT PGR), where the Pa denote probabilities for simultaneous detection at gates specified by label a. In terms of photo counts Na , the degree of coherence can be expressed as [31] g(2) = NGTRNG/(NGT NGR). It has a value that is less than 1 for nonclassical light. We obtained g(2) = 0.187 ± 0.011 in our experiments. Several sources of experimental error could be identified. The main source of error came from the accuracy with which our plates could be oriented, i.e., approximately ±1◦. Another possible source of error came from our photons having a wavelength of 800 nm instead of the 808 nm that would be required for optimal performance of our wave plates. These are zero-order plates whose effective retardances at the produced wavelength made them slightly differ from being λ/2 and λ/4 plates. However, the corresponding departures (0.505λ instead of λ/2 and 0.253λ instead of λ/4) were small enough to be neglected as a sensible source of error. Accidental coincidence counts were also estimated to be too small (contribution to g(2) less than 0.19) for them to have a noticeable influence on the departures of our experimental findings from the theoretically predicted values when s > π (see Fig. 4, middle and right panels). As illustrated in Fig. 4, left panel, the agreement between the theoretical predictions and measured values was very good. However, we also observed slight departures that occasionally increased. The dashed curves in Fig. 4, middle and right panels, correspond to the targeted geometric phase 012124-4 POLARIMETRIC MEASUREMENTS OF SINGLE-PHOTON . . . PHYSICAL REVIEW A 89, 012124 (2014) 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s40° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s80° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s120° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s160° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s200° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s240° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s280° 0 Π 2 Π 3 Π 2 2 Π 0 0.5 1 Μ I s320° FIG. 3. (Color online) The geometric phase is experimentally fixed by the maxima and minima of the measured curves Iexp(φ). The plotted curves correspond to θ = π/3, ϕ = π/3. g(s,θ,ϕ). Large departures seemed to reflect a drift of the measured values with respect to the assumed theoretical curve, rather than random fluctuations around this curve. In what follows, we substantiate our claim that the ±1◦ accuracy in the orientation of our plates does explain occasional, systematic departures of experimental measurements from theoretical predictions. Depending on the measured quantity, rotation errors of this magnitude can give rise to inaccuracies of various sorts, such as those recently reported in [32]. It is important to identify error sources and their effects, especially when one’s ultimate goal is to have a good understanding of how the geometric phase behaves in a noisy environment. Let us denote by δi the departure of the ith plate’s orientation from its nominal value. For a quarter-wave plate, we must then set Q(x + δ) instead of Q(x) in Eq. (5). To first order in δ, we get dQ(x) = Q(x + δ) − Q(x) = √2iδRx , with Rx = ( sin(2x) −cos(2x) −cos(2x) −sin(2x) ) . (16) Similarly, for a half-wave plate, we obtain dH (x) = H (x + δ) − H (x) = 2iδRx . If we now replace the operators Q(x) and H (x) in Eq. (5) by Q(x) + dQ(x) and H (x) + dH (x), respectively, and then expand the result to first order in the δi , we obtain Uδtot = Utot + 7∑ i=1 Uδi , (17) whereUδi reads likeUtot [see Eq. (5)], except that its ith factor is replaced by dH (x) when i = 4 and by dQ(x) otherwise. Uδtot is then a function of all δi=1,...,7. From the amplitude 〈h|Uδtot |h〉, we can calculate the total intensity Iδ = ∣∣〈h|Uδtot |h〉∣∣2, once again to first order in the δi . With this expression, by choosing different values for the δi , we can study how much Iδ(φ) differs from the I (φ) given in Eq. (9). We have found that the departures from I can be very sensitive to a change from, say, δi ≈ +1◦ to δi ≈ −1◦, keeping fixed all the other δj =i . The values of Imax and Imin can be calculated using I (φ) and Iδ(φ) in order to assess the sensitivity of the array to changes δi ≈ ±1◦ in the setting of the plates. The values of Imax and 0 4 Π 9 8 Π 9 4 Π 3 16 Π 9 1.5 1 0.5 0 s g 2, 3 0 4 Π 9 8 Π 9 4 Π 3 16 Π 9 1.5 1 0.5 0 s g 3 4 0 4 Π 9 8 Π 9 4 Π 3 16 Π 9 1.5 1 0.5 0 s g 3 3 FIG. 4. (Color online) Geometric phase g(s,θ,ϕ) as a function of parameter s for three choices of (θ,ϕ). Curve g(s,π/2,π/3) closely matches experimental results. However, g(s,π/3,π/4) and g(s,π/3,π/3) seem to systematically deviate from the measured values. By properly identifying the actual values of (θ,ϕ), the theoretical curves do match experimental results. Dashed curves correspond tog(s,π/3,π/4) (middle panel) and tog(s,π/3,π/3) (right panel). Full curves correspond tog(s,π/3 + δθ,π/4 + δϕ) with δθ = 3◦π/180◦, δϕ = −7◦π/180◦ (middle panel) and tog(s,π/3 + δθ,π/3 + δϕ) with δθ = 5◦π/180◦, δϕ = −4◦π/180◦ (right panel). Most error bars are smaller than symbols. 012124-5 O. ORT´IZ et al. PHYSICAL REVIEW A 89, 012124 (2014) Imin that correspond to Iδ(φ) show that inaccuracies δi ≈ ±1◦ can explain the observed differences between recorded phases and theoretically predicted ones; cf. Eqs. (14) and (15). The last claim can be confirmed by the following, in- dependent approach. Inaccuracies δi ≈ ±1◦ should translate into a departure of θ and ϕ from their nominal values. Let us then assume that our array does not realize the trans- formation Un(θ,ϕ,s) = exp [−isn(θ,ϕ) · σ/2], but instead exp [−isn(θ + δθ,ϕ + δϕ) · σ/2], with δθ ≈ ±7◦ ≈ δϕ. The actual values of δθ and δϕ can be obtained by the following procedure. From Eq. (12), we see that Imax(si) and Imin(si) corresponding to targeted values θ and ϕ should satisfy y(si) ≡ 1 − Imax(si)1 − Imin(si) = sin 2 θ cos2 ϕ ≡ f (θ,ϕ). (18) The above equation can be used to determine the actual values of θ and ϕ, i.e., θ + δθ and ϕ + δϕ, by the least- squares method. To this end, we evaluate the right-hand side of Eq. (18) in the sought-after values, expand it to first order, i.e., we set f (θ + δθ,ϕ + δϕ) = f (θ,ϕ) + (sin 2θ cos2 ϕ)δθ − (sin2 θ sin 2ϕ)δϕ, and then determine δθ , δϕ as ( δθ δϕ ) = (AT WA)−1AT Wb. (19) Here, (·)−1 means the Moore-Penrose pseudoinverse, b is the column vector [y(si) − f (θ,ϕ)]T , with i = 1, . . . ,n (n is the number of recorded points), A is the n × 2 matrix whose rows are all equal to (sin 2θ cos2 ϕ,−sin2 θ sin 2ϕ), and W is the inverse of the covariance matrix, i.e., W = diag(σ−21 , . . . ,σ−2n ). The latter corresponds to statistically uncorrelated measurements having different variances σi at different values si . We have assessed these variances in two different ways: first by fitting a Gaussian to the distributions of measured points (cf. Fig. 3), which gives us σi for each value I (φj ) and hence for Imin, Imax, and g by error propagation. Second, from our raw data, which consists of 30 values for each φi – with s, θ , ϕ being kept fixed, we randomly chose 10 values for each φi and calculated g as we did when using the 30 values. By iterating this procedure several times (≈40), we got a series of values for each g(s,θ,ϕ). From each series, we obtained a mean value and its corresponding maximal and minimal departures. These departures constitute our error bars. Such an estimation is justified by the statistical independence of our measurements. Thus, randomly sampling 10 out of 30 measured values amounts to having recorded 10 values in each run of the experiment, while repeating it several times (≈40). From the two methods, we observe that our measured values σi span a range that goes from a minimum of 1.3 × 10−4 to a maximum of 0.12. The plotted error bars (cf. Fig. 4) are mostly smaller than the symbols and can barely be seen only in cases for which σi ≈ 0.1. Now, the above-mentioned application of the least-squares method holds whenever inaccuracies δsi of the si can be neglected. In our case, the nominal value of s enters in the orientations of our wave plates and the inaccuracies of these orientations are precisely the assumed main source of errors. Nevertheless, the above application of the least-squares method is justified. Indeed, we can assess the values of the δsi by using Eq. (10). That is, we set δsi ≈ |si − 2 arccos ( √ Imin(si))| as an estimator of the inaccuracies of the si . These inaccuracies turn out to be negligible in comparison to our σi—besides, if they were not, they would modify the above results only to higher order than the first in (δθ,δϕ) because our y(si) do not depend on s, as Eq. (18) shows. The least-squares method can thus be iteratively applied to find successive values of δθ and δϕ, until thg (s,θ + δθ,ϕ + δϕ) of Eq. (8) eventually matches experimental results. In the present case, however, it proved more practical to seek the right choice of θ and ϕ by hand, i.e., by trial and error when plottingthg (s,θ + δθ,ϕ + δϕ) together with its measured values. Indeed, by doing so in the cases of Fig. 4, middle and right panels, we quickly found values δθ ≈ ±7◦ ≈ δϕ for which the theoretical curves very closely approximate our experimental results. Figure 4 shows the curves obtained with δθ = 3◦, δϕ = −7◦ (middle panel) and δθ = 5◦, δϕ = −4◦ (right panel). Such a result is consistent with the assumed errors δi ≈ ±1◦, which may accumulate so as to produce inaccuracies δθ ≈ ±7◦ ≈ δϕ. Thus, departures of θ and ϕ from their targeted values do explain our experimental findings. We have thereby assessed the amount by which the theoretically predicted value thg (s,θ,ϕ) might differ from the experimentally realized one. Such a difference should be taken into account when assessing, with the help of a polarimetric array, the robustness of g against decohering mechanisms. Finally, let us point out the following feature of our array. As can be seen from Eqs. (14) and (15), the geometric phase we produce depends on θ and ϕ only through |sin θ cosϕ|. This means that we can fix the actually realized values of θ and ϕ only up to changes (θ,ϕ) → (θ ′,ϕ′) that leave |sin θ cosϕ| invariant. Instead of seing this as a weakness of our approach, such a feature can be helpful when seeking to exploit the robustness of g against decoherence. Indeed, if one is able to confine decohering effects to those regions in the plane (θ,ϕ) for which the variations in |sin θ cosϕ| are sufficiently small, then g will vary also within acceptable limits. Of course, these limits will depend on the application one has in mind and on the decohering mechanisms, which should be studied in detail. Such an endeavor goes beyond the scope of the present paper and is deferred to future work. IV. CONCLUSIONS Our polarimetric setup proved to be a versatile tool for testing geometric phases. The main part of it, an array made of one λ/2 and six λ/4 plates, allows us to realize geometric phases that are associated to nongeodesic paths on the Poincare´ sphere. Although we have limited ourselves to study circular trajectories, our approach can be extended to deal with arbitrary paths. Our experimental results fit very closely with the theoretical predictions once we have accurately identified the trajectory on the Poincare´ sphere that has been actually realized by our setting. The end product of such a setting is a geometric phase g that is nontrivially related to various parameters entering our setup. Indeed, coincidence counts must be optimized by adjusting the laser polarization, the acquisition window for photon counts must also be properly fixed, and the wave plates must be repeatedly set to their nominal orientations when recording the data from which g can be extracted. Not only because of the photon-counting statistics but mainly because of our ±1◦ accuracy in the 012124-6 POLARIMETRIC MEASUREMENTS OF SINGLE-PHOTON . . . PHYSICAL REVIEW A 89, 012124 (2014) setting of the plates, one could expect experimental results falling within some region around the theoretical curves, as reported, e.g., in [32]. If that were the case, our polarimetric array would have proven to be inappropriate for studying the robustness of geometric phases against noise. However, our array does produce geometric phases that are in accordance with theoretical expressions. Occasionally, these expressions must be evaluated a posteriori, thereby identifying the actually realized values of the parameters fixing g . Once the value of g has been fixed, our array can be used for assessing the robustness of this g against noise. To this end, the array must be complemented so as to simulate different kinds of noise. For instance, one can replace the single- crystal photon’s source and use instead polarization-entangled photons produced by parametric down-conversion in a two- crystal geometry [33,34]. This produces variable entangled polarization states. After tracing over the polarization of one of these photons, its twin photon is brought into a mixed polarization state ρ = (1 + rn · σ )/2, with r ∈ [0,1] being the degree of polarization. Such a state can be submitted to a polarimetric array similar to the one discussed in this paper. Now, ρ can be written in the form ρ = λ+|n+〉〈n+| + λ−|n−〉〈n−|, with λ± = (1 ± r)/2 and n · σ |n±〉 = ±|n±〉. Applying to |n±〉 the techniques of the present work, one can get the corresponding (pure-state) geometric phases ±g . This is all one needs [35] to obtain the geometric phase of the mixed state ρ, thereby assessing the effect of noise. Experiments along these lines have already been performed in neutron polarimetry [17,18]. The kind of noise studied in [17] translated into a Stokes vector r = rn of the restricted form r = (0,−r,0), and the explored paths on the Bloch sphere originated from unitary transformations that depended on two of the three Euler angles [17]. By appropriate choice of these two angles, one can generate purely geometric, purely dynamical, or combinations of both phases. However, once this choice is made, one cannot freely address different paths on the Bloch sphere. Nevertheless, these results represented a considerable extension of previous ones [15], which dealt with Pancharatnam’s phase only. Further progress in assessing the robustness of geometric phases was achieved by addressing adiabatic evolutions [18]. Here, the dynamical contribution to the total phase was eliminated by spin-echo techniques, which impose some restrictions on the class of paths being explored. Our all-optical setting offers some advantages compared to neutron polarimetry. It allows choosing arbitrary paths on the Poincare´ sphere, as well as different kinds of noise to be explored in conjunction with the chosen path. The aforementioned remote state preparation of mixed states is not the only choice. 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