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Ultrashort pulse characterization by spectral shearing interferometry with spatially chirped ancillae

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Abstract

We report a new version of spectral phase interferometry for direct electric field reconstruction (SPIDER), in which two spatially chirped ancilla fields are used to generate a spatially encoded SPIDER interferogram. We dub this new technique Spatially Encoded Arrangement for Chirped ARrangement for SPIDER (SEA-CAR-SPIDER). The single shot interferogram contains multiple shears, the spectral amplitude of the test pulse, and the reference phase, which is accurate for broadband pulses. The technique enables consistency checking through the simultaneous acquisition of multiple shears and offers a simple and precise calibration method. All calibration parameters — the shears, and the upconversion-frequency— can be accurately obtained from a single calibration trace.

©2009 Optical Society of America

1. Introduction

Ultrashort pulse characterization [1] is a key technology underpinning much of ultrafast science. Progress in the field continues to occur on many fronts — extending the range of measurable pulse parameters, such as duration, wavelength, and complexity, improving the sensitivity and single-shot capability, and providing spatial, in addition to temporal, resolution. Less easily quantified but equally important issues are precision, robustness, ease of use and the diagnosis, identification, and quantification of errors. Innovations on this front have included simplified geometrical setups [2, 3], theoretical analysis of the influence of various errors [4], and the exploitation of redundant data to identify misalignment or violations of the assumptions on the pulse properties [5, 6]. Spectral shearing interferometry (SSI), a popular class of techniques whose best-known example is Spectral Phase Interferometry for Direct Electric field Reconstruction (SPIDER) [7] is widely used due to its efficient acquisition and direct retrieval algorithm with computation requirements which scale linearly with the time-bandwidth product of the unknown pulse, and its natural suitability to broadband optical input. Also, its direct retrieval formula renders analysis of the influence of various errors a straightforward matter and its one dimensional data encoding makes the acquisition of multiple shots, and subsequent analysis of their shot-to-shot variations, convenient and rapid. Geometrically simplified arrangements have also been developed [3]. The common feature of all SSI techniques is the interference of two spectrally sheared replicas of the unknown pulse. This introduces two parameters, the shear and the interferometric reference phase, which must be calibrated to a precision which increases with the time-bandwidth product of the unknown pulse. Novel geometries for the convenient determination of these parameters [8, 9, 10] are therefore of interest, supplementing the well-established techniques [7]. Additionally, whilst typical raw SSI data contains some redundant information [5] enabling self-consistency checking, this can be supplemented by taking several measurements at different shears which should result in identical retrieved fields.

Most currently known SPIDER variants [7, 8, 9, 11, 12, 13] are implemented as single shear devices. Changing the shear involves moving parts which requires additional calibration and prevents single-shot multiple shear operation. A significant recent development in this context is Chirped Ancillae aRrangement- (CAR-)SPIDER [14], in which an upconverted replica of the unknown pulse with spatially varying frequency is produced through the phase-matching properties of a long crystal. This replica is split, and two-dimensional spectral interferometry is performed between itself and a laterally inverted copy, yielding an interferogram in which the shear varies with position. The zero-shear line encodes the reference phase, whilst the shear calibration can be performed by blocking each arm individually. CAR-SPIDER is therefore an attractive device in the light of the previous discussion. However, the collinear long-crystal geometry limits both the measureable bandwidth and the maximum pulse length. Also in the long-crystal arrangement the spatial carrier of the interferogram depends on frequency, requiring an additional calibration for broadband pulses.

In this paper, we present a device which we dub Spatially Encoded Arrangement for CAR-SPIDER (SEA-CAR-SPIDER), in which spatially chirped ancillae are produced by a diffraction grating and split before undergoing upconversion with the test pulse. This removes the restriction on the pulse parameters imposed by the long-crystal geometry and also renders the spatial carrier independent of frequency, so that the reference phase is truly self-calibrated. Furthermore, the arrangement permits a convenient determination of all calibration parameters in a single step with much greater precision than CAR-SPIDER, as well as a direct verification of the ancillae monochromaticity which is important for accurate measurement of long pulses.

2. SEA-CAR-SPIDER theory

We shall describe the SEA-CAR-SPIDER concept using Fig. 1. The test pulse E(ω)=I(ω)exp[(ω)] is taken to be spatially uniform and propagating along the z-axis. It undergoes sum-frequency generation with two spatially chirped ancillae A and B, one of which has been laterally inverted about the y-axis (i.e. by an odd number of reflections in the xz-plane), so that in the crystal their local frequencies are ωAup+αx and ωBup-αx, where ω up is the upconversion frequency common to both ancillae at x=0. The ancillae wavevectors also form an angle ϑ in the x-z-plane, symmetrically about the z-axis. The sum-frequency beams, labelled TP+A and TP+B in Fig. 1, are re-imaged onto the entrance slit of an imaging spectrometer, whilst all other beams are blocked. The spectrometer entrance slit lies along the x-axis, so the field incident on the slit is the coherent sum of two replicas of the test pulse, upconverted with frequencies ω A and ω B respectively. Their converging angle forms spatial interference fringes [8], which provide the carrier onto which the phase is encoded. Internally, the spectrometer wavelength-disperses the beams along the y-axis, yielding a two-dimensional interferogram S(ω,x). It is of the form

S(ω+ωup,x)=I(ω+αx)+I(ωαx)+D(ω,x)+D*(ω,x)
D(ω,x)=I(ω+αx)I(ωαx)exp[iΓ(ω,x)]
Γ(ω,x)=ϕ(ω+αx)ϕ(ωαx)+kxx+C(ω)

where D(ω,x) is the positive-spatial-frequency AC sideband, Γ(ω,x) is the interferogram phase, C(ω) is the zero-shear calibration phase, which is theoretically zero due to symmetry but may be present due to imperfect imaging, and kx=ω up ϑ=c is the spatial carrier of the fringes. Note that it is independent of the signal frequency w because the spatial tilt is applied to the ancillae, rather than the upconverted replica as in CAR-SPIDER [14]. At all x-positions x≠0, the interferogram phase contains the finite differences ϕ(ω+αx)-ϕ (ω-αx) i.e. spectral shearing interferometry data of shear Ω=2αx. This linear mapping of position to shear is the distinguishing feature of a CAR-SPIDER arrangement.

The reconstruction procedure is as follows: the positive-spatial-frequency AC sideband D(ω,x) is isolated using 2D Fourier filtering, as with SEA-SPIDER [8]. The interferogram phase Γ(ω,x) is the complex argument of the sideband. The calibration phase must then be determined. If the spectrum has no nulls, then Γ(ω,x) is well defined along x=0 and C(ω) can be obtained directly at this position and subtracted from Γ(ω,x) to obtain the finite differences [14]. The carrier kxx does not vary with frequency and hence is irrelevant to the reconstruction. Alternatively, in the case of signal dropouts along x=0, or for increased precision, the calibration phase can also be obtained by weighted averaging along the x axis. We use the fact that, except for the calibration phase, Γ(ω,x) is an odd function in x about x=0. Therefore by averaging across a symmetric interval centred at x=0 the calibration phase can be isolated. In practice this requires a method which is robust against 2π phase discontinuities. We use

C(ω)=12unwrap[Arg0D(ω,x)D(ω,x)dx]

where Arg is the principal value of the argument and unwrap denotes a one-dimensional phase unwrapping routine which removes 2π discontinuities.

 figure: Fig. 1.

Fig. 1. SEA-CAR-SPIDER concept: test pulse (TP), spatially chirped ancillae A and B with local frequencies ω A and ω B increasing along the arrows, and sum-frequency beams TP+A and TP+B. The coordinate system used in the text is shown. The entrance slit of the imaging spectrometer is parallel to the x-axis. The spatial fringes along x are used to encode the phase.

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After subtracting the calibration phase, the standard concatenation procedure can be performed at any x as desired. The spectral intensity of the unknown pulse, modulated by the phasematching efficiency and the spectrometer response, is also obtained from the x=0 signal. Therefore, all data is recorded near the upconversion frequency, enabling a specifically optimized spectrometer to be used. Even though a single SEA-CAR-SPIDER interferogram contains tens of independent datasets, online reconstruction of each of these is still possible owing to the fast algebraic reconstruction algorithm of SPIDER.

We note that as with filter-SPIDER [10] and CAR-SPIDER, our new device does not rely on temporal stretching of the ancillae to ensure quasi-monochromaticity. Thus in SEA-CAR-SPIDER, which is free from the pulse length restrictions of the long-crystal arrangement, strongly chirped pulses can be characterized without the need for correction of the reconstructed phase [15].

 figure: Fig. 2.

Fig. 2. Example SEA-CAR-SPIDER traces calculated for pulses with different order polynomial spectral phases. (a) Transform-limited pulse; (b) quadratic spectral phase; (c) cubic spectral phase; (d) quartic spectral phase. The fringes map out the phase gradient scaled by the shear.

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The spatial carrier in SEA-CAR-SPIDER enables an intuitive interpretation of the fringe pattern, because, as we now show, the fringe contours follow the phase derivative of the unknown pulse. Let x con(ω) be a fringe contour, defined by Γ= constant. Then

dΓ[ω,xcon(ω)]dω=Γ[ω,xcon(ω)]ω+Γ[ω,xcon(ω)]xxcon(ω)ω=0

In (3) we approximate the finite differences with a derivative, and write

Γ(ω,x)ϕ(ω)ω2αx+kxx.

The calibration phase is typically very small and ignored in (6). The spatial derivative is

Γ(ω,x)x=ϕ(ω)ω2α+kx.

The second term on the right hand side of (7) represents the spatial carrier and is much larger than the first term — otherwise the sidebands would not be distinct in the Fourier domain. We neglect the first term and substitute (7) into (5), yielding

xcon(ω)ω=2αxcon(ω)kx2ϕω2.

Therefore the fringe contours follow the spectral phase gradient scaled by the local shear and the inverse of the spatial carrier. This is illustrated in Fig. 2 which shows calculated traces for a transform-limited pulse and for pulses with quadratic, cubic and quartic polynomial spectral phases. Note that for a transform-limited pulse (Fig. 2 (a)) the fringe contours are flat, reflecting the frequency independence of the spatial carrier. The fringe pattern provides a simple and useful visual tool for aligning a laser qualitatively without the need for running a reconstruction algorithm.

3. Experimental Setup

Our experimental implementation of SEA-CAR-SPIDER is depicted in Fig. 3. The test pulse TP is split with beamsplitter BS1 and vertically focussed into the nonlinear crystal χ (2) with a cylindrical lens CL with focal length fcl=500mm. The delay-line DL1 is for coarse adjustment of the delay between ancillae and test pulse and only requires initial adjustment. The ancillae are prepared as follows: the reflected beam from BS1 is dispersed by a grating of pitch Λ=300mm-1 and angle of incidence γ=10°. The spherical lens L1 is positioned one focal length f 1=500mm away from the grating and the crystal is mounted f 1 further down-stream. Between the lens and the crystal the ancilla beam is split at 50/50 beamsplitter BS2 and one arm is spatially inverted. The coarse delay line DL2 is used to achieve temporal overlap between the ancillae and needs no subsequent adjustment. The χ (2) crystal (L=250µm BBO) is placed in the back Fourier plane of L1, where the spatial chirp of the ancillae is α=cos[β (ω up)]ω up 2=(2π cf 1Λ) where β (ω up) is the diffracted angle of the beam from the grating. A half-wave retarder λ/2 is introduced into the ancilla arm to ensure type-II upconversion with the ancilla polarization aligned to the e-axis and the TP polarization to the o-axis of the crystal, respectively. After spatial filtering (SF), which blocks the other beams, the sumfrequency beams are re-imaged onto a 2D imaging spectrometer by lens L2 with focal length f 2=300mm. The home-built spectrometer provides astigmatism-free imaging over a wide spectral and spatial extent [16]. The signal is recorded with a 1280×1024pixel CMOS detector with 8 bit ADC resolution. Single-shot data is recorded at a rate of 30 Hz limited by memory and data-transfer capacities. If the signal strength is insufficient, averaging is of course possible unless the shot-to-shot fluctuations are extreme.

 figure: Fig. 3.

Fig. 3. SEA-CAR-SPIDER experimental setup. For detailed explanation refer to text. The inset shows the spatio-spectral structure of the test pulse and the ancillae beams in the crystal plane. The test pulse upconverts with different ancilla frequencies from the two oppositely spatially chirped ancilla beams in each spatial position across the crystal resulting in a varying shear across x.

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As with all χ (2)-based pulse characterization methods, the phase-matching efficiency is a consideration. In SEA-CAR-SPIDER, multiple upconversion frequencies are used to achieve the different shears, and the geometry is non-collinear with the two ancillae subtending an angle J symmetrically about the test pulse. Good phase-matching must simultaneously occur for every combination of upconversion frequency and signal frequency and for both ancillae. We are assisted by the fortuitous phase-matching properties of Type II sum-frequency generation in BBO, which is very broadband for frequencies polarized along the ordinary axis, which in our case is the test pulse, whilst being more narrowband for the e-rays, which are the ancillae in SEA-CAR-SPIDER and hence require a much smaller acceptance bandwidth. It is also relatively insensitive to the non-collinear angle of the e-ray, which is necessary for simultaneously phase-matching the upconversion from both ancillae. For our 250 µm crystal, with non-collinear angle ϑ/2≈±5°, we calculated phase matching bandwidths (full-width at half-maximum efficiency) of 200 mrad/fs for the test pulse frequency and 29 mrad/fs for the ancillae. The latter figure determines the maximum shear range. This is adequate for the 60 fs pulses characterized below. For the few-cycle regime, a thinner crystal clearly must be used. However, our calculations show that the particular requirements of SEA-CAR-SPIDER — upconversion with a range of quasi-monochromatic frequencies, and a non-collinear geometry — present only a minor restriction beyond the phase-matching requirements of a single-shear, collinear SPIDER setup. For example, using a 30 µm thick BBO crystal with an otherwise identical geometry, phase matching bandwidths of 2.9 rad/fs for the test pulse and 0.2 rad/fs for the ancillae are possible, sufficient to measure few-cycle pulses.

It should be noted that SEA-CAR-SPIDER could be operated as zero additional phase (ZAP) device, an advantage for few-cycle pulses which undergo significant dispersion in transmissive optics, by using a cylindrical mirror instead of CL and reflection of the test-pulse off BS1 rather than transmission.

We also note that several issues arise if the spectral intensity of the test pulse contains null points i.e. frequencies where the spectral intensity drops to zero. First, since the ancillae are derived from the test pulse, they will also contain spectral nulls, and so upconversion cannot occur with these frequencies. This will result in certain shears being absent from the interferogram: the fringes at row x are formed by interference between replicas of the test pulse which have been mixed with frequencies ω up±αx. If a spectral null falls on either of these frequencies, the amplitude of the corresponding replica will be zero, resulting in no fringes, and hence no phase information. This limitation can be overcome by using an external pulse without spectral nulls (such as a pick-off of the laser output) to form the ancillae. We have verified this simple modification experimentally.

A second issue arising from regions of zero spectral intensity is the relative phase ambiguity of spectral shearing interferometry [18]. We have recently developed a new algorithm for resolving this ambiguity by combining the information using multiple shears [19]. SEA-CAR-SPIDER is particularly well suited for acquiring the raw data for the multiple-shear algorithm, and we are currently investigating this combination.

4. Calibration

In order to obtain a single-step calibration of the shear slope α, as well as the central up-conversion frequency ω up and the x-origin, the TP arm was blocked and the spatial filter SF temporarily removed. In this configuration, the second harmonic of the ancillae, as well as their sum-frequency signal (purple lines emerging from the crystal in Fig. 3) are obtained. Fig. 4 (a) shows the calibration data obtained from the average of 50 single-shot acquisitions. A linear fit of the slopes of the two ancillae provides α=22.93±0.06mrad=fs=mm. From the crossing point of the two ancillae the x-origin and ω up are obtained. We determine the x-origin to be pixel 762.3±0.1. The upconversion frequency is found to be ω up=2.38767±2×10-5 rad/fs. All errors are estimated using the covariances of the fit parameters.

 figure: Fig. 4.

Fig. 4. SEA-CAR-SPIDER calibration: (a) Spatially resolved spectrum of the upconversion from the two ancilla pulses yields calibration of upconversion frequency and shear. 20 dB color scale. The black dashed lines are linear fits. (b) Fitting the shear using the sum-frequency signal. Central frequencies of individual spectral slices (black dots) obtained from cross-correlation, linear fit (black line). (c) Residuals of fits of the ancilla as in (a) in red circles, residuals of fit (b) in black dots.

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The sum-frequency mixing between the ancillae appears as the vertical line at frequency ω up in Fig. 4 (a). Its position with respect to the crossing point is a useful check of the axial alignment of the crystal-to-spectrometer reimaging system. If L2 is correctly relay imaging the crystal plane to the spectrometer entrance slit, then all three lines cross at the same point.

The spectral width of the ancillae can also be obtained from the calibration data of Fig. 4 (a). This is useful in verifying that the ancillae are sufficiently monochromatic, a basic requirement of spectral shearing interferometry. In the case of SEA-CAR-SPIDER, where many shears are available, the spectral width of the ancillae determines the minimum shear from which a meaningful reconstruction can be performed. Here, we obtain a monochromaticity of 1.85mrad=fs FWHM in the second harmonic, i.e. 1.31mrad=fs in the fundamental, granting a maximal time window for test pulses of T=4.8ps. The ancillae spectral width is αs, where s is the FWHM spot size produced by lens L1. The monochromaticity can therefore be further increased by using a higher pitched grating and a tighter ancillae focus.

We note that a similar calibration procedure was performed in the original CAR-SPIDER arrangement. However, because the upconversion was performed using the asymmetric phase-matching in a long crystal it was impossible to block the test pulse and hence the shear calibration was performed using the upconverted signal pulses. As we now illustrate, the SEA-CAR-SPIDER procedure offers greater precision because the second harmonics of the ancillae are much more narrowband than the test pulse. In CAR-SPIDER, the calibration would be obtained by recording the individual signals separately and obtaining their displacement by cross-correlation, disregarding regions of low intensity. One such fit is shown in Fig. 4 (b). The residuals of the slope fits are directly compared in Fig. 4 (c). Using this method we get shear slopes of α sig=22.76±2.5mrad/fs/mm. From the signal fits we further determine the x-origin to be 760.2±2.2pixels. The upconversion frequency is not determined by this method. As expected due to the greater spectral width of the signals the errors in determining the calibration parameters are significantly larger compared to the new calibration procedure presented above. This emphasizes the precision advantage of the calibration offered by the ancilla preparation in SEA-CAR-SPIDER.

 figure: Fig. 5.

Fig. 5. Evaluation of the stability of the calibration parameters. We recorded 50 single-shot calibration traces and performed the fitting routines on each. (a) Shear slope α. (b) Position of x-origin (zero shear row) determined from the crossing point. (c) Upconversion frequency ω up.

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We investigated the sensitivity of the calibration against fluctuations of the beam-pointing and displacement. Our device preserves vertical symmetry (y-axis in our coordinate system) and relay images all beams. It turns out that beam-pointing and displacement changes in the vertical direction do not affect the device calibration. Vertical beam pointing fluctuations cause the signal to move off the spectrometer entrance slit reducing the signal intensity. Horizontal beam displacements cause a change in the spatial carrier, which does not affect the calibration or reconstruction. A beam-pointing change θx in the horizontal plane causes the two spatially chirped ancilla fields to move into opposite directions due to the lateral inversion in the ancilla preparation setup. This leads to a shift in the upconversion frequency of Δω up≈αx to first order, whilst the zero shear position is not affected. Due to the low (near normal) diffraction angle from the grating the variation of the shear slope α is negligible.

We tested these conclusions by recording 50 single-shot calibration traces and determining the calibration parameters shear slope α, zero shear row and upconversion frequency ω up as shown in Figure 5. Confirming our analysis above we find that α, and the x-origin are constant within the uncertainty of our fits. The upconversion frequency ω up varies by 0.0239 mrad/fs consistent with typical beam pointing fluctuations of our chirped pulse amplification (CPA) system.

5. Demonstration

In this section we show the characterization of pulses from a home-built CPA system. The laser delivers 60 fs pulses centered around 800 nm at a repetition rate of 2kHz.

 figure: Fig. 6.

Fig. 6. (a) Typical single-shot SEA-CAR-SPIDER interferogram for a 54 fs pulse. (b) Spatial lineout at center wavelength showing the spatial carrier fringes. (c) 2D-DFT of the interferogram (80 dB scale). The black rectangle indicates the sideband filter; the green rectangle indicates the signal-free region used to determine the noise amplitude. (d) Γ(ω,x) after filtering (2π scale). The spatial carrier has been removed for clarity.

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A typical single-shot SEA-CAR-SPIDER interferogram is shown in Fig. 6(a). The regions of low intensity are caused by dead rows in our detector and imperfections in the upconversion crystal. Confirming the calibration of the upconversion frequency, the signal is centered around λ=398nm which is equivalent to ω 0+ω up=(2.345+2.388) rad/fs or 397:98nm where ω0 is the pulse center frequency.

To aid isolating the interferometric component from the baseband term in the Fourier-filtering procedure we use a high spatial carrier of kx=2.15rad=pix (where kx=π is the Nyquist rate) resulting in fine fringes. A lineout at λ=398nm is shown in Fig. 6(b). The two-dimensional discrete Fourier transform of these data is shown in Fig. 6(c); the black rectangle indicates the filter region. The phase of the filtered sideband is shown in Fig. 6(d) with the spatial carrier removed for clarity. The symmetry of the signal about x=0 is evident. After subtracting the calibration phase and extracting the amplitude as described in section 2 we obtain the spectral phase for each spectral shear Ω present in the data. The resulting reconstructed spectral phase ϕ(ω) is displayed in Fig. 7 (a) for a subset of the shears present in the SEA-CAR-SPIDER interferogram. The reconstructions show good agreement which we quantify below. Fig. 7 (b) shows the corresponding temporal intensities.

 figure: Fig. 7.

Fig. 7. Example reconstructions for different shears Ω=12.07,13.27, and 18.08mrad=fs. (a) Spectral domain with amplitude extracted from the trace at x=0 and the 3 phases corresponding to each shear. (b) Temporal domain: intensities and phases for each shear.

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6. Robustness and precision of the pulse field reconstruction

In this section we investigate the uncertainty of our measurements, showing that SEA-CAR-SPIDER is accurate and precise. Several features of the SEA-CAR-SPIDER enable a convenient and empirical evaluation of the uncertainty. Its single-shot nature enables the random errors to be evaluated by studying the statistics of an ensemble of sequential acquisitions, whilst the presence of systematic errors caused by spatial nonuniformities is revealed by differences between the reconstructions from different shears. The magnitude of the errors resulting from various misalignments, instabilities, or miscalibrations can also be conveniently calculated due to the simple analytic reconstruction algorithm.

We first evaluate the magnitude of the random errors by examining the statistics over N=50 single-shot traces. We reconstruct each shot independently at K=12 different shears Ωk, ranging from 8.4 to 14.4 mrad/fs, yielding a set of reconstructed phases ϕk,n(ω) from which shot-to-shot statistics can be obtained. We calculate the mean square shot-to-shot spectral phase variation σ 2 k (ω)=〈[Δϕk,n(ω)]2in, where Δ denotes deviation from the mean value, and angle braces denote the mean value over an ensemble which is specified by the subscript. We find that σk(ω) is less than 0.05 rad across the full-width at 10% maximum bandwidth, but does not vary greatly between shears. It is shown for Ω=10mrad=fs by the black dash-dotted line in Fig. 8 (c). The shot-to-shot variation of the temporal RMS pulse duration was less than 0.33 fs for the different shears with smaller variations for larger shears. We also calculated the RMS field variation εk [20] for each shear, which was typically around 0.0087.

We now consider possible sources of shot-to-shot fluctuations. The phase error resulting from camera shot noise can be evaluated by the following procedure: the noise density in the Fourier domain is evaluated by examining a region with no signal, as shown by the green rectangle in Fig. 6(c). The total noise energy in the filtered signal is then estimated by multiplying this density by the area of the sideband filter. By Parseval’s theorem, this is equal to the noise energy in D(ω,x) after inverse Fourier transforming. Assuming the noise is uniformly spread over the (ω,x) domain, the noise variance η 2 D=〈[ΔD(w,x)]2〉 on the samples of D(ω,x) is then estimated. Here, we find a peak SNR of max D(ω,x)/ηD=536. By contrast, before the filtering, the peak SNR was 49. The noise on Γ is then η 2Γ(ω,x)≈η 2 D/2|D(ω,x)|2 [19], the intensity-dependence arising because in regions of low intensity the phase is less well defined. Assuming these errors are independent, the variance on the reconstructed phase resulting from the concatenation algorithm is the sum of their variances at the sampled points ωn=ω 0 +nΩ for n=0,1,…. Therefore, the variance of the reconstructed phase difference between ωm and ωn is

γ2={Δ[ϕ(ωm)ϕ(ωn)]}2=k=nm1ηΓ(ωk+Ω2,x)2.

As an indicative measure we choose ωn=2.3142 and ωm=2.3797rad/fs as the lower and upper frequencies at half the maximum spectral intensity. Here, we find γ=0.02rad, consistent with the observed shot-to-shot fluctuations.

 figure: Fig. 8.

Fig. 8. Reconstruction of a 59 fs pulse for shears from 8.4 to 14.4 mrad/fs. (a) Spectral domain: intensity (red, left axis) and mean phase (dark blue line, right axis) and ±1 standard deviation (light blue region) across the shears. (b) Temporal domain: mean intensity (red) and ±1 standard deviation interval (light red region) across the shears. (c) RMS phase variations magnified: over all shots at a single shear (black dash-dotted), over all 12 shears (blue, solid), and expected variation in the reconstructed phase resulting from fluctuations in the upconversion frequency (green dashed).

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Another source of shot-to-shot variation is the fluctuation in ω up, as described in section 4. An error Δω up in this quantity leads to a shift in the reconstructed spectrum, giving a phase error of ≈Δω up ∂ϕ (ω)/∂ω. Using the RMS value of Δω up obtained from the data in Fig. 5(c), we computed the resulting phase errors which are shown by the green dashed line in Fig. 8(c). These are consistent in magnitude with the observed phase fluctuations (black dash-dotted line).

We now examine the systematic errors. Some of these are revealed by inconsistencies between the reconstructions from different shears. We computed the mean-square variation over the different shears σ 2(ω)=〈[Δϕk(ω)]2k, where ϕk(ω)=〈ϕk,n(ω)〉n is the shot-averaged phase reconstructed using shear Ωk. We have plotted σ(ω) as blue solid line in Fig. 8(c). It is of similar magnitude to the shot-to-shot fluctuations. In SEA-CAR-SPIDER, disagreement between the reconstructions from different shears arises from spatial inhomogeneities in the beam. We verified the presence of a spatially varying spectrum by recording a 2D spectrum of the test-pulse and extracting the variation of the spectral moments across the beam x-axis. This can also be directly extracted from the data trace by comparing the extracted amplitudes at different shear positions with the expected amplitudes |E(ω+αx)‖E(ω-αx)|, which can be calculated from the spectrum |E(ω)| extracted at the x-origin. Since all temporal characterization techniques involve either spatial averaging or spatial selection, the ability to quantify the spatial variation is an advantageous feature.

The final systematic errors we considered arose from the accuracy of our calibration of α and the x-origin. An error Δα leads to a fractional shear error of ΔΩ/Ω=Δα/a which we measure as 0.3 %, indicated by the error bars in Fig. 5(a). The resulting phase error is also fractional, scaled by the same amount, and is negligible for the data presented here. The error in the x-origin is more difficult to analyze, as it affects both the shear and the calibration phase. However, performing the reconstruction algorithm on this data with a range of different values for the x-origin did not affect the reconstructed phase. We note that had we used the calibration method using the broadband signals, these errors would have become significant.

Since averaging of the statistically independent shot-to-shot fluctuations reduced the random errors to significantly below the systematic errors, the latter define the ultimate precision of our measurement. For an intuitive visualization of their magnitude, we plot the temporal profile (shown in Fig. 8 (b) on logarithmic scale) corresponding to the grand average phase 〈ϕk(ω)〉k with the variation between the shears indicated by the shaded area. We achieve a temporal intensity dynamic range of 10-4.

We also verified the accuracy of the reconstruction by measuring the spectral phase introduced by a 10 cm long piece of BK7 glass which we inserted into the beam. We measured a quadratic phase of φ 2=4440±26fs2, in close agreement with the theoretical value of 4442fs2.

7. Conclusion

We have demonstrated a novel self-referenced and easily calibrated ultrafast pulse characterization technique. A full set of data, consisting of the calibration phase, the spectral amplitude of the unknown pulse, and the spectral phase encoded with multiple shears, is recorded in a single shot. The redundant information contained in each single shot data trace provides useful material for consistency checks. A high precision shear and upconversion frequency calibration is straightforward and can be done in one single step for all shears present without the need of any manual or motorized adjustments. We envisage that this device will be beneficial for its inherent reliability through a lack of moving parts, its improved precision, and the redundant information in the trace which assists error determination.

Acknowledgments

This research was supported in part by the European Commission through the Research Training Network XTRA (contract MRTN-CT-2003-505138) and by EPSRC ER/S24015/OJ. DRA was supported by an Oxford University Clarendon Fund Scholarship. IAW acknowledges support from the Royal Society.

†Both authors contributed equally to the work presented.

References and links

1. I. A. Walmsley and C. Dorrer, “Characterization of ultrashort electromagnetic pulses,” Adv. Opt. Photon. 1, 308–437 (2009). [CrossRef]  

2. P. O’Shea, M. Kimmel, X. Gu, and R. Trebino, “Highly simplified device for ultrashort-pulse measurement,” Opt. Lett. 26, 932–934 (2001). [CrossRef]  

3. A. S. Radunsky, I. A. Walmsley, S.-P. Gorza, and P. Wasylczyk, “Compact spectral shearing interferometer for ultrashort pulse characterization,” Opt. Lett. 32, 181–183 (2007). [CrossRef]  

4. C. Dorrer, “Influence of the calibration of the detector on spectral interferometry,” J. Opt. Soc. Am. B 16, 1160–1168 (1999). [CrossRef]  

5. C. Dorrer and I. Walmsley, “Precision and consistency criteria in spectral phase interferometry for direct electric-field reconstruction,” J. Opt. Soc. Am. B 19, 1030–1038 (2002). [CrossRef]  

6. R. Trebino, Frequency-Resolved Optical Gating: The Measurement of Ultrashort Laser Pulses (Springer, 2002). [CrossRef]  

7. C. Iaconis and I. A. Walmsley, “Spectral phase interferometry for direct electric-field reconstruction of ultrashort optical pulses,” Opt. Lett. 23, 792–794(1998). [CrossRef]  

8. E. Kosik, A. Radunsky, I. Walmsley, and C. Dorrer, “Interferometric technique for measuring broadband ultrashort pulses at the sampling limit,” Opt. Lett. 30, 326–328(2005). [CrossRef]   [PubMed]  

9. J. R. Birge, R. Ell, and F. X. Kärtner, “Two-dimensional spectral shearing interferometry for few-cycle pulse characterization,” Opt. Lett. 31, 2063–2065 (2006). [CrossRef]   [PubMed]  

10. T. Witting, D. R. Austin, and I. A. Walmsley, “Improved ancilla preparation in spectral shearing interferometry for accurate ultrafast pulse characterization,” Opt. Lett. 34, 881–883 (2009). [CrossRef]   [PubMed]  

11. A. Monmayrant, M. Joffre, T. Oksenhendler, R. Herzog, D. Kaplan, and P. Tournois, “Time-domain interferometry for direct electric-field reconstruction by use of an acousto-optic programmable filter and a two-photon detector,” Opt. Lett. 28, 278–280 (2003). [CrossRef]   [PubMed]  

12. P. Baum, S. Lochbrunner, and E. Riedle, “Zero-additional-phase SPIDER: full characterization of visible and sub-20-fs ultraviolet pulses,” Opt. Lett. 29, 210–212 (2004). [CrossRef]   [PubMed]  

13. M. Lelek, F. Louradour, A. Barthelemy, and C. Froehly, “Time resolved spectral interferometry for single shot femtosecond characterization,” Opt. Commun. 261, 124–129 (2006). [CrossRef]  

14. S.-P. Gorza, P. Wasylczyk, and I. A. Walmsley, “Spectral shearing interferometry with spatially chirped replicas for measuring ultrashort pulses,” Opt. Express 15, 15168–15174 (2007). [CrossRef]   [PubMed]  

15. J. Wemans, G. Figueira, N. Lopes, and L. Cardoso, “Self-referencing spectral phase interferometry for direct electric-field reconstruction with chirped pulses,” Opt. Lett. 31, 2217–2219 (2006). [CrossRef]   [PubMed]  

16. D. R. Austin, T. Witting, and I. A. Walmsley, “Broadband astigmatism-free Czerny-Turner imaging spectrometer using spherical mirrors,” Appl. Opt. 48, 3846–3853 (2009). [CrossRef]   [PubMed]  

17. R. W. Boyd, Nonlinear optics (Academic Press, 2003).

18. D. Keusters, H.-S. Tan, P. O’Shea, E. Zeek, R. Trebino, and W. S. Warren, “Relative-phase ambiguities in measurements of ultrashort pulses with well-separated multiple frequency components,” J. Opt. Soc. Am. B 20, 2226–2237 (2003). [CrossRef]  

19. D. R. Austin, T. Witting, and I. A. Walmsley, “High precision self-referenced phase retrieval of complex pulses with multiple-shearing spectral interferometry,” J. Opt. Soc. Am. B 26, 1818–1830 (2009). [CrossRef]  

20. C. Dorrer and I. A. Walmsley, “Accuracy criterion for ultrashort pulse characterization techniques: application to spectral phase interferometry for direct electric field reconstruction,” J. Opt. Soc. Am. B 19, 1019–1029 (2002). [CrossRef]  

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Figures (8)

Fig. 1.
Fig. 1. SEA-CAR-SPIDER concept: test pulse (TP), spatially chirped ancillae A and B with local frequencies ω A and ω B increasing along the arrows, and sum-frequency beams TP+A and TP+B. The coordinate system used in the text is shown. The entrance slit of the imaging spectrometer is parallel to the x-axis. The spatial fringes along x are used to encode the phase.
Fig. 2.
Fig. 2. Example SEA-CAR-SPIDER traces calculated for pulses with different order polynomial spectral phases. (a) Transform-limited pulse; (b) quadratic spectral phase; (c) cubic spectral phase; (d) quartic spectral phase. The fringes map out the phase gradient scaled by the shear.
Fig. 3.
Fig. 3. SEA-CAR-SPIDER experimental setup. For detailed explanation refer to text. The inset shows the spatio-spectral structure of the test pulse and the ancillae beams in the crystal plane. The test pulse upconverts with different ancilla frequencies from the two oppositely spatially chirped ancilla beams in each spatial position across the crystal resulting in a varying shear across x.
Fig. 4.
Fig. 4. SEA-CAR-SPIDER calibration: (a) Spatially resolved spectrum of the upconversion from the two ancilla pulses yields calibration of upconversion frequency and shear. 20 dB color scale. The black dashed lines are linear fits. (b) Fitting the shear using the sum-frequency signal. Central frequencies of individual spectral slices (black dots) obtained from cross-correlation, linear fit (black line). (c) Residuals of fits of the ancilla as in (a) in red circles, residuals of fit (b) in black dots.
Fig. 5.
Fig. 5. Evaluation of the stability of the calibration parameters. We recorded 50 single-shot calibration traces and performed the fitting routines on each. (a) Shear slope α. (b) Position of x-origin (zero shear row) determined from the crossing point. (c) Upconversion frequency ω up.
Fig. 6.
Fig. 6. (a) Typical single-shot SEA-CAR-SPIDER interferogram for a 54 fs pulse. (b) Spatial lineout at center wavelength showing the spatial carrier fringes. (c) 2D-DFT of the interferogram (80 dB scale). The black rectangle indicates the sideband filter; the green rectangle indicates the signal-free region used to determine the noise amplitude. (d) Γ(ω,x) after filtering (2π scale). The spatial carrier has been removed for clarity.
Fig. 7.
Fig. 7. Example reconstructions for different shears Ω=12.07,13.27, and 18.08mrad=fs. (a) Spectral domain with amplitude extracted from the trace at x=0 and the 3 phases corresponding to each shear. (b) Temporal domain: intensities and phases for each shear.
Fig. 8.
Fig. 8. Reconstruction of a 59 fs pulse for shears from 8.4 to 14.4 mrad/fs. (a) Spectral domain: intensity (red, left axis) and mean phase (dark blue line, right axis) and ±1 standard deviation (light blue region) across the shears. (b) Temporal domain: mean intensity (red) and ±1 standard deviation interval (light red region) across the shears. (c) RMS phase variations magnified: over all shots at a single shear (black dash-dotted), over all 12 shears (blue, solid), and expected variation in the reconstructed phase resulting from fluctuations in the upconversion frequency (green dashed).

Equations (9)

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S (ω+ωup,x)=I(ω+αx)+I(ωαx)+D(ω,x)+D*(ω,x)
D (ω,x) = I(ω+αx)I(ωαx) exp [iΓ(ω,x)]
Γ (ω,x)=ϕ(ω+αx)ϕ(ωαx)+kxx+C(ω)
C (ω)=12unwrap[Arg0D(ω,x)D(ω,x)dx]
dΓ[ω,xcon(ω)]dω=Γ[ω,xcon(ω)]ω+Γ[ω,xcon(ω)]xxcon(ω)ω=0
Γ (ω,x)ϕ(ω)ω2αx+kxx.
Γ(ω,x)x = ϕ(ω)ω 2 α + kx .
xcon(ω)ω = 2αxcon(ω)kx 2ϕω2 .
γ2 = {Δ[ϕ(ωm)ϕ(ωn)]}2=k=nm1ηΓ(ωk+Ω2,x)2.
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