Open Access
Issue
A&A
Volume 663, July 2022
Article Number A9
Number of page(s) 28
Section Astronomical instrumentation
DOI https://doi.org/10.1051/0004-6361/202142945
Published online 01 July 2022

© H. Gan et al. 2022

Licence Creative CommonsOpen Access article, published by EDP Sciences, under the terms of the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

1 Introduction

The Epoch of Reionization (EoR) is a watershed period in the history of the Universe, where neutral hydrogen (HI) in the inter-galactic medium (IGM) became ionized by ultraviolet radiation from stars and quasars (Ciardi & Ferrara 2005; Furlanetto et al. 2006; Morales & Wyithe 2010; Pritchard & Loeb 2012). Its study is aimed at shedding light on the fundamental processes of the early Universe (Madau et al. 1997; Shaver et al. 1999; Tozzi et al. 2000).

The Thomson scattering optical depth of cosmic microwave background radiation, the Gunn-Peterson troughs of high-redshift quasar spectra, and the Ly-α emitting high-redshift galaxies (LAEs) are indirect observational probes of the EoR. Studies of these phenomena have suggested that reionization took place at redshift ɀ = 6–10 (Becker et al. 2001; Fan et al. 2006; Clément et al. 2012; Schenker et al. 2013; Mortlock 2016; Planck Collaboration XLVII 2016; Greig et al. 2019, 2016; Davies et al. 2018; Mason et al. 2019; Planck Collaboration VI 2020; Heinrich & Hu 2021). The most direct probe of the EoR, however, is through the 21 cm line of neutral hydrogen (Field 1958). The expected redshift range of the EoR corresponds to observational frequencies between about 120–200 MHz, requiring low-frequency radio telescopes. There are mainly two types of observational approaches to detecting the 21 cm signal: (1) using radio interferometry to measure the 21 cm spatial brightness-temperature fluctuations (Zaroubi et al. 2012); (2) using a single receiver to measure the globally averaged 21 cm brightness temperature as a function of frequency (Shaver et al. 1999). In this work, we focus on the first approach.

Radio interferometers such as the GMRT1 (Paciga et al. 2011, 2013), LOFAR2 (van Haarlem et al. 2013; Patil et al. 2017; Mertens et al. 2020), MWA3 (Bowman et al. 2013; Barry et al. 2019; Li et al. 2019), and PAPER4 (Ali et al. 2015; Cheng et al. 2018; Kolopanis et al. 2019), along more sensitive second-generation instruments such as HERA5 (DeBoer et al. 2017; HERA Collaboration 2021) and SKA6 (Koopmans et al. 2015) are designed to statistically measure the spatial fluctuations of the 21 cm signal. Furthermore, LEDA7 (Greenhill & Bernardi 2012), PRIZM8 (Philip et al. 2018), SARAS 3 (Singh et al. 2017; Thekkeppattu et al. 2021)9, and EDGES10 (Bowman et al. 2018) are aimed at measuring the global 21 cm signal. Cohen et al. (2018) predicted a tight correlation between features of the 21 cm power spectrum and of the global signal and, hence, the two signals potentially complement each other by providing consistency checks.

The detection of the 21 cm signal is very challenging because the observed sky at low radio frequencies is dominated by strong galactic and extra-galactic emissions, which are three to five orders of magnitudes brighter than the 21 cm signal (Shaver et al. 1999). Because it is difficult to model and remove these foregrounds from the observed data, some experiments alternatively use the “foreground avoidance” technique (Kerrigan et al. 2018), which discards certain Fourier modes that are heavily affected by the foregrounds. However, giving up Fourier modes (typically at low k values) leads to a loss in sensitivity (Chapman et al. 2016). The LOFAR-EoR Key Science Project (KSP), therefore, does not use the foreground avoidance strategy; rather, it models and removes the foregrounds. In addition, the data are contaminated by “radio frequency interference” (RFI), largely from human activities (Offringa et al. 2012). Finally, ionospheric and instrumental effects can distort the signal (Labropoulos et al. 2009; Vedantham & Koopmans 2015, 2016; Mevius et al. 2016, 2021). Therefore, to extract the 21 cm signal from the data, we need to correct for these effects accurately during calibration (Barry et al. 2016; Trott & Wayth 2016; Patil et al. 2016, 2017).

The LOFAR-EoR KSP published its first upper limit on the 21 cm signal power spectrum using only 13 hours of data, with observations centered on the north celestial pole (NCP) in the redshift range of ɀ = 7.9–10.6 (Patil et al. 2017). It was reported that the residual power exceeded the expected thermal noise level (then defined by the Stokes-V power spectrum) by a factor of 2–3, approaching an excess variance of an order of magnitude in the power spectrum. This was coined as “excess variance” (Patil et al. 2016, 2017; Mertens et al. 2020). A more recent analysis by Mertens et al. (2020) reported a considerably lower excess variance following improvements in gain calibration, showing that gain fluctuations are unlikely to be the dominant cause of the remaining excess variance. However, the excess variance in the 21 cm power spectra is still significantly larger than the thermal noise level (then defined via time differencing of visibilities) despite the application of very smooth gain solutions.

In order to analyze more nights of data and separate the 21 cm signal from a mixture of foregrounds as well as instrumental, ionospheric, and RFI effects, it is important to first identify possible causes of excess variance and quantify how much each of them contributes to its level. Mertens et al. (2020) summarized various plausible sources of excess variance: un-subtracted foreground sources that are far from the NCP: polarization leakage (Jelić et al. 2015; Asad et al. 2015, 2016); direction-dependent gain errors due to the overfitting of data and the removal of short baselines (<250λ) (Patil et al. 2017; Mevius et al. 2021); direction-independent gain errors due to the incomplete sky model that are propagated from long baselines to short baselines (Barry et al. 2016; Patil et al. 2016; Ewall-Wice et al. 2017); remaining low-level RFI after flagging (Wilensky et al. 2019; Offringa et al. 2019); and uncorrected ionospheric scintillation with very short decorrelation timescales (i.e., of seconds) (Vedantham & Koopmans 2016). Until now, however, no comprehensive study has been carried out to explore whether there is just one dominant contribution from a particular source or whether it is a combination of many factors, and, if so, which factors play a role.

In this work, we analyze a subset of the above-mentioned possible causes using 13 night observations of the NCP. After the DI and DD calibration, we perform post-calibration flagging to reduce the unfiltered RFI before the DI and DD calibration and filter out bad data. Earlier studies already have shown that early-stage RFI flagging is unlikely to cause effects exceeding the 21 cm signal (Offringa et al. 2019). The selection of nights is based on the analysis in Mertens et al. (2020). While Mertens et al. (2020) discarded nights that are highly correlated to each other or have an unusually behaving ionosphere, in this work, we include these nights in the analysis. We specifically focus on parameters that characterize the possible excess variance causes: (1) the gain variance over time or frequency that quantify gain smoothness; (2) the local sidereal time (LST), which is related to the orientation of the instrument with respect to the sky; (3) the diffractive scale, rdiff, and structure–function slope β, which give good estimates for the ionospheric condition during an observation. We discuss how these effects could contribute to the excess variance. After having chosen the characteristic parameters, we correlate them with the excess variance in the 21 cm signal power spectra to assess whether the chosen parameters contribute to the excess variance.

The paper is organized as follows: in Sect. 2, we describe the data processing steps and the resulting data products after each step. In Sect. 3, we define the excess variance in the context of 21 cm signal power spectra and discuss possible causes of the excess variance in detail. We also introduce the relevant parameters which can characterize each possible cause. The correlations between the excess variance and its possible causes are analyzed in Sect. 4. In Sect. 5, we summarize the results and discuss possible improvements in the future.

2 Observations and data processing

The data analyzed in this work were collected by the LOFAR High-Band-Antenna (HBA) system (van Haarlem et al. 2013) over 13 nights between 2012 and 2014. The duration of observation ranges from 8 to 12 hours. Detailed information for each night is summarized in Table 1. We use the same observations that were analyzed by Mertens et al. (2020). While they excluded three nights (L80850, L254871, and L203277) that are known to have highly correlated residuals or to suffer more from ionospheric effects, we do include these nights in our analysis because we are interested in the sources of the excess variance. The analysis of these three additional nights could potentially provide clues about the excess causes. The observations are centered on the north celestial pole (NCP), for several reasons: (1) the NCP is observable during the night throughout the entire year from the location of LOFAR and the beam is stable with the sky rotating inside of it; (2) due to its location, the uv-tracks for the NCP are circular (Yatawatta et al. 2013) and Earth-rotation synthesis produces a dense uv-coverage during a full track.

The acquired data are processed on the Dawn HPC cluster (Pandey et al. 2020) by the following steps as described in detail in Patil et al. (2017) and Mertens et al. (2020): (1) pre-processing including visibility flagging and averaging; (2) calibration including direction-independent (DI) and direction-dependent (DD) calibration; (3) imaging; (4) residual foreground removal; and (5) power-spectrum analysis. While the pre-processing and DI-calibration steps are similar to the ones adopted by Patil et al. (2017), the DD-calibration, foreground removal and power-spectrum analysis strategies have improved since and follow Mertens et al. (2020). Imperfections in the data processing during each step can introduce excess variance. Here, we briefly summarize each step in the processing and its resulting data products. These data products are used in the subsequent analyses.

Pre-processing. RFI-flagging is performed on the raw visibility data which are stored in Measurement Set (MS) files as a function of frequency, time, station and polarization. RFI-flagging is done using AOFLAGGER (Offringa et al. 2012) on the highest data resolution (2 s and 64 channels per subband with the four edge channels flagged due to aliasing from the poly-phase filter, resulting in 183 kHz effective width per sub-band) and on a lower resolution after averaging (2 s and 15 channels per sub-band), respectively. Known bad stations and baselines are also flagged. This flagging typically results in a loss of ~5% of the data (Offringa et al. 2012). After flagging, the data are further averaged to 2 s and 3 channels per sub-band.

DI- and DD-gain calibration. The visibilities are affected by the ionosphere, instrument, and strong foreground emission. The calibration step is aimed at correcting for the ionospheric and instrumental effects and removing the dominant bright foreground sources in our sky model with their gain solutions applied11. We describe the propagation of the radio signal from a source to a pair of antenna elements by the radio-interferometry measurement equation (RIME) (Hamaker et al. 1996; Smirnov 2011). The equation relates the observed complex visibility to the model visibility by multiplying it with a series of 2×2 gain matrices, known as Jones matrices, which describe different propagation effects including ionospheric and instrumental signal distortions and instrumental (de)polarization of the signal. The calibration is performed by the code SAGECALCO (Yatawatta 2011, 2015, 2016). The resulting gains are complex numbers and are calculated per antenna and direction. The gains have similar dimensions as the observed visibilities, namely, (frequency, time, polarization) and gains from two different antennas can be combined to obtain gain solutions for baselines.

The gain calibration process is done in two steps: direction independent (DI-) and direction dependent (DD-) calibration. The main differences between the two calibration steps are the sky models, baseline cuts, clustering of sky components during calibration and the way those gains are applied (summarized in Table 2). DI-calibration uses only a subset of the NCP sky model due to computational limitations, that is, the 1416 brightest components with an apparent-flux limit of >35 mJy, including the relatively bright source 3C61.1 (a total flux about 35 Jy at 150 MHz, Yatawatta et al. 2013). The sky components are clustered into two directions: 3C61.1 and the remainder, each with their gain solution. In DD calibration, the full NCP sky model with 28 755 components, including 18 shapelets and Cygnus A and Cassiopeia A (Cas A and Cyg A, hereafter), is used. This sky model is clustered into 122 groups of sources to handle DD gain variations due to the time-varying primary beam and the ionosphere. DI and DD calibration exclude baselines that are shorter than 50λ and 250λ, respectively. The 50λ cut is chosen to minimize effects from the Galactic diffuse emission and the 250λ cut is chosen to avoid signal loss (for details, see Patil et al. 2017; Mertens et al. 2020). In addition, gain solutions are applied differently in DI and DD calibration: DI gain solutions are directly applied to the observed visibilities, whereas DD gain solutions are applied to the sky-model visibilities and their product is subtracted from the observed visibilities.

Imaging. The residual visibilities after DI and DD calibration are gridded and imaged using WSCLEAN (Offringa et al. 2014) for each sub-band and two polarizations (Stokes I and V) to create an (l,m,v) image cube. Each image in units of Jy PSF–1 is naturally weighted and has a field of view (FoV) limited to 12° × 12° with 0.5 arcmin pixel size. Images from different subbands are combined to form an image cube. After gridding, these images are trimmed with a Tukey spatial filter of 4° × 4° FoV to focus on the primary beam and maximize the sensitivity. For the thermal-noise estimation, we additionally create alternating (i.e., “even” and “odd”) 10 s images to generate gridded and time-differenced visibilities (Mertens et al. 2020). Any effect that changes on a timescale that is much longer than 10 seconds will therefore cancel in this difference and we consider this an excellent estimator of the thermal noise, in agreement with calculations based on the SEFD.

Residual foreground removal. After DD calibration and subtraction of the gain-corrected sky-model visibilities, the residual visibilities still contain (partially polarized) emission from the diffuse foregrounds and sources that are not included in the calibration model. These residuals are also only corrected for DI gain errors. Imaging is performed with settings that limit gridding errors to a negligible error (Offringa et al. 2019). Gaussian Process Regression (GPR) (Mertens et al. 2018, 2020) is subsequently applied to remove residual foregrounds from the inner 3° × 3° of the images, restricted to well within the first null of the primary beam and used in power-spectrum estimates. GPR uses the property that the Stokes-I components of foregrounds have spectrally-smooth emission. This can be distinguished from the 21 cm signal, which is rapidly fluctuating in frequency (Iliev et al. 2006; Mellema et al. 2006).

Power-spectrum analysis. After removing the residual foregrounds, various power spectra are estimated by taking the Fourier transform of visibility cubes along the frequency axis. After the Fourier transform, the resulting delays and baseline lengths are transformed to wave numbers in units of inverse co-moving distance (Mpc) following the cosmological convention of Morales & Hewitt (2004). Finally, the power spectra P(k) are transformed into units of K2h–3cMpc3.

After processing 13 night observations from LOFAR, following the described pipeline and given the sensitivity of the instrument, we should expect that final residual power spectra are dominated by thermal noise and are relatively flat as a function of k. However, the resulting power spectra are significantly higher than the thermal noise level and we discuss possible causes in the next sections.

Table 1

Thirteen night observational details used for analysis in this paper.

Table 2

Differences between DI- and DD-gain calibrations.

3 Thermal noise and excess variance

The raw data contain various components: foreground emission, RFI, instrumental and ionospheric distortions, thermal noise, and the 21 cm signal. If DI and DD calibration and foreground removal are applied correctly, the data after the processing, including calibration and foreground removal, should only contain the 21 cm signal and thermal noise. However, the data processing, especially calibration and foreground removal, is not perfect. These imperfections in the processing could result in adding extra power (“excess variance”) to the final data products. Figure 1 shows the excess variance of the 13 nights of LOFAR-HBA NCP observations after calibration and foreground removal (i.e., sky-model and GPR subtractions). Although we do not completely rule out the scenario that this excess power is some real power from the sky, or a rapid gain variation that is not yet understood, our current analysis suggests that this excess is mostly artificial and it should be distinguishable from thermal noise. Thermal noise is incoherent and, hence, it can be reduced by adding more visibilities. On the other hand, part of the excess variance is coherent (Mertens et al. 2020). The coherent part of excess variance does not average down by increasing the number of visibilities contrary to the thermal noise (see Patil et al. 2016, 2017; Mertens et al. 2020).

Below, we discuss plausible causes for the excess variance in the LOFAR data and its power spectra and discuss its characteristics in more detail. We provide parameters that can be used to describe the correlation between the excess variance and its causes.

3.1 Thermal noise

Patil et al. (2017) used the Stokes-V power spectra as an estimator of the thermal noise contribution to the 21 cm power spectrum, based on the expected low level of circularly polarized emission from radio sources. Given the fact that thermal noise is still expected to be much higher than the 21 cm signal, ideally, the ratio between the residual Stokes I and Stokes V power spectra should approach unity from above. These ratios for the three redshift bins considered in Patil et al. (2017), however, showed an excess well beyond thermal noise, typically by a factor 2–3. Furthermore, Mertens et al. (2020) found that the Stokes-V signal is not fully dominated by thermal noise, even after improved calibration. For example, some Stokes I emission can instrumen-tally leak into Stokes V, and random errors on the gain solutions can increase the power in Stokes V above thermal noise, via such leakage.

To obtain a much more accurate thermal noise estimation and to account for any possible leakage, Mertens et al. (2020) used two additional thermal noise metrics: the time-difference visibilities δtV(u, v, ν) and the sub-band-difference visibilities δvV(u, v, ν). The time-difference visibilities are calculated by subtracting two alternating (“even” and “odd”) gridded visibility sets with 10 second time differences. These time-differenced visibility sets should produce an excellent thermal noise estimate because most of the foreground and some ionospheric errors cancel out on this timescale, even though it has been found that on very short baselines, the timescale is comparable to the decorrelation timescale of ionospheric scintillation noise (Vedantham & Koopmans 2015). The second estimator is calculated by subtracting visibility sets between 195.3-kHz sub-bands. Because the subtraction between sub-bands removes spectral structures on the sub-band or larger scale, this estimator is more sensitive to the spectrally-uncorrelated excess noise in the data.

In addition, the excess variance in residual power spectra appears to have two components (Mertens et al. 2020): (1) spectrally uncorrelated excess on short baselines (<100λ) and (2) spectrally and temporally (between a few nights) correlated excess (lex ~ 0.25–0.45 MHz) that is stronger in the foreground-dominated wedge. The latter is currently not removed by the GPR method, which separates different signal components by using distinct frequency-correlation characteristics in each component (Mertens et al. 2018). The first excess component does not have specific spectral coherence, so it is difficult to remove via GPR. On the other hand, the frequency coherence scale of the second excess component is similar to that of the 21 cm signal. This similarity makes it difficult to distinguish them only via GPR.

Thanks to huge improvements in the calibration process compared to the previous work by Patil et al. (2017), the excess variance (Mertens et al. 2020; Mevius et al. 2021) is significantly reduced and the noise level almost reaches thermal noise in the region k > 1 hc Mpc–1. However, the excess variance still remains higher than thermal noise, especially in the region of k < 1 hc Mpc–1.

thumbnail Fig. 1

Excess variance power spectra ratios (i.e., the Stokes I over Stokes V ratio) for the 13 nights of LOFAR observations after DI and DD calibration and foreground removal (sky model and GPR). The dashed lines indicate, from bottom to top, the 5° (the primary beam), 20°, and instrumental horizon delay lines. The excess variance is larger in the wedge-like region under the dashed lines. Some baselines are flagged in L205852 (k ~ 0.07 hc Mpc–1) and in L253987 (k ~ 0.05 hc Mpc–1).

3.2 Excess variance

In this subsection, we briefly review how various effects can contribute to the observed excess variance.

3.2.1 Radio frequency interference and data flagging

The frequency range of 134.1782–146.0922 MHz, included in our observations, is contaminated by RFI. Currently, AOFLAG-GER flags RFI on a ~ 12.2 kHz scale. As a result, a small number of channels and sub-bands are fully flagged after the preprocessing. Low-level RFI under the threshold can also affect the data and introduce frequency structures at high k. Additionally, Offringa et al. (2019); Wilensky et al. (2020) found that a combination of data missing due to RFI flagging and averaging data could result in “excess power” at high k. However, given the current approach to RFI flagging, these effects in our data should be significantly smaller than the predicted 21 cm signal and thermal noise (Offringa et al. 2019).

In this paper, therefore, we do not investigate residual RFI further, since there is currently no clear evidence for its contribution to the observed excess variance. Flagging data, however, can have an effect, since it can create an achromatic point spread function. This will be investigated in more detail in a future study.

3.2.2 Ionospheric phase error and scintillation

Ionospheric propagation effects can be an important source of errors at low radio frequencies. They depend on multiple factors, such as time, frequency, direction, and baseline (Aarons 1982; Thompson et al. 2001). During the calibration step, some of these ionospheric effects can be corrected for (Pearson & Readhead 1984; Smirnov 2011), but not all of them, especially, on shorter baselines where effects vary rapidly with time and direction (see Vedantham & Koopmans 2015, for an extensive discussion). The DI calibration is done at 10 second intervals and only corrects for a flux-weighted ionospheric phase variation over the entire field of view. In DD-calibration, our sky model is clustered into 122 directions and any DD ionospheric phase fluctuations on timescales that exceed the solution interval (typically 2.5–20 min) are solved for each direction. Hence, the directional and temporal dependence of the ionosphere can only be accounted for in a limited way. According to Vedantham & Koopmans (2015), under typical ionospheric conditions – at a frequency of ν = 150 MHz, height h = 300 km and ionospheric turbulence travelling along a bulk of wind at speed of v = 100–500km h–1 – the decorrelation time for short baselines (< 300 m) varies between 4 and 22 s, while the decorrelation time for long baselines (>2 km) ranges between 30 and 150s. Thus, the typical calibration time intervals are longer than the actual decorrela-tion timescales of ionospheric phase errors (about a few seconds) on short baselines. This results in gain errors and leaves rapidly varying ionospheric scintillation in the data. The remaining scintillation (known as “scintillation noise”) may appear as frequency correlated excess variance in power spectra (Koopmans 2010; Vedantham & Koopmans 2015, 2016). This type of excess variance is contained in the foreground wedge (Vedantham & Koopmans 2015). Similarly, gain errors induced by the ionosphere on intermediate and longer baselines are also applied to the sky model on short baselines and thus can lead to another indirect excess variance (see Sect. 3.2.3 for more details on the same effect due to an incomplete or incorrect sky model) that can also enter the EoR window (e.g., Ewall-Wice et al. 2017).

In addition to phase errors, the “Faraday rotation” causes any linearly polarized signal to rotate, including any linear polarization leaking to Stokes I due to instrumental polarization leakage (Jelić et al. 2010) and it is currently considered to be a second-order effect. This effect can contaminate “the EoR window,” but is expected to be far below the current excess variance seen in our LOFAR data (Asad et al. 2018).

The ionospheric phase variance per baseline to first-order follows a power law, namely, the phase structure function (van der Tol 2009; Mevius et al. 2016), where we can obtain two metrics for the ionospheric quality representation, the fitted slope β, and the diffractive scale rdiff. The exponent of the structure function β varies from 5/3 to 2, depending on the ionospheric structure. A lower power index of 5/3 comes from Kolmogorov turbulence, while the higher index 2 suggests nonturbulent structures such as traveling ionospheric disturbances (TIDs) (Velthoven, van 1990) or density ducts (Loi et al. 2015).

The diffractive scale is the length scale over which the phase variance corresponds to 1 rad2. A large diffractive scale indicates longer time coherence of the signal and smaller phase fluctuations over a given field of view. Therefore, the diffractive scale should be a good first-order representation of the ionospheric state during an observation. We correlate β and rdiff, respectively, with the excess variance to assess whether there is any correlation between the ionospheric quality and the excess variance in power spectra.

3.2.3 Gain-calibration errors

The calibration of LOFAR EoR KSP data is completed in two steps (see Sect. 2): DI- and DD-calibration. Gain solutions in the two steps are obtained with different (although motivated) choices for the sky models, baseline cuts, time, and frequency resolution. The obtained solutions are applied to our data differently. While DI gains are directly applied to the visibility data, DD gains are applied first to the model visibilities and subsequently subtracted from DI-calibrated visibility data. In this subsection, we discuss how gain errors in DI- and DD-calibration (summarized in Table 2) from different sources can contribute to the excess variance.

Sky-model incompleteness. Currently, we use a sky model consisting of 28 773 unpolarized components (28 755 delta function components and 18 shapelets (Yatawatta 2011; Mertens et al. 2020)) for DD calibration. For DI calibration, only the 1416 brightest components of the sky model are used. This subset is chosen from the NCP model with an apparent flux limit of >35 mJy to reduce the processing time but still fulfill the signal-to-noise ratio (S/N) required for the DI calibration at high time resolution (Mertens et al. 2020). The sky model is built from wide-field images with ~6 arcsec resolution by an iterative process using a program called BUILDSKY (Yatawatta et al. 2013) and all Dutch baselines. The source components in the model have individual spectral dependencies. The model, even though it is already quite extensive, has some known limitations: diffuse emission from the Milky Way is not part of the sky model (even though it is not negligible on baselines <100λ); extra-galactic sources typically have an angular size similar to the resolution of LOFAR images (~6 arcsec when using all Dutch baselines ~100 km), which limits the spatial accuracy of the model for each source.

These limitations make the construction of an accurate sky model difficult (Patil et al. 2017). The difference between the true sky and the modelled sky, however, is less than 5% on the flux scale according to Scaife & Heald (2012); Patil et al. (2017); Mertens et al. (2020)12. This flux difference is distributed over many sources and acts as a “confusion noise source,” limited to the foreground wedge of 21 cm power spectra. It does not change the absolute flux scale. However, the difference between the sky model and the true sky affects the gain solutions by absorbing this model incompleteness into the gain solutions. These gain errors, on all baselines, when applied to the data or the model lead to excess power on a wide range of spatial and frequency scales, also in the EoR window (Patil et al. 2016; Barry et al. 2016; Ewall-Wice et al. 2017, 2018). Especially, very bright sources, such as Cas A and Cyg A, enter the FoV through their undulating sidelobes and could be a source of the excess variance. These bright sources have higher power than the fainter sources that enter the FoV through the rather slowly varying primary beam (Morales et al. 2012; Mertens et al. 2020). A single bright source is added coherently to the power spectrum, whereas many fainter sources (adding to the same total flux) is added incoherently. Thus, a few bright sources can dominate excess variance. Gain errors can both suppress structures that are not included in the model and add structures when applied to the model and subtracted from the data (Mouri Sardarabadi & Koopmans 2018).

Diffuse emission. The unmodeled diffuse emission and partly polarized galactic emission can be a potential source of the excess variance as well. In our analysis, we tackle the problem in two ways: (1) applying 50λ cut on baselines to suppress the diffuse emission (the diffuse emission becomes problematic with baselines shorter than 100λ) and (2) applying GPR to remove spectrally smooth diffuse emission. The unpolarized part of the diffuse emission is spectrally smooth and can be removed well by GPR (Mertens et al. 2018). The polarization leakage of the diffuse to Stokes I, however, can introduce spectral fluctuations similar to the frequency structure of the 21 cm signal (Jelić et al. 2015; Asad et al. 2015, 2016; Mouri Sardarabadi & Koop-mans 2018). The predicted level of leakage is estimated to be much smaller (i.e., ~1%) than the observed level of excess variance (Asad et al. 2016) and hence it should not be a main source of the excess variance at the current level.

lnstrumental gain changes. Visibilities are affected by the instrument mainly due to their time-, frequency-, and direction-dependent gains variations. DD-calibration corrects for these variations by solving gains independently for 122 directions as a function of frequency and time, thus incorporating the beam model and very slow ionospheric changes (see Sect. 3.2.2).

Foreground sources that are far from the beam center and are not included in the sky model or not correctly subtracted, can leave chromatic PSF sidelobes in the central part of the beam being analyzed for the 21 cm signal, and also affect the gain solutions on longer baselines. These induced gain errors can affect the gain solutions on shorter baselines, similarly to ionospheric gain errors, which in our case are inferred from the longer baselines only (Patil et al. 2016; Ewall-Wice et al. 2017). The beam pattern changes more rapidly with increasing frequency. Therefore, the excess variance caused by the chromatic beam pattern can be indirectly investigated by their baseline and frequency dependence (Patil et al. 2016). LOFAR also has an instrumentally polarized response. If the calibration process does not take this into account, this effect can cause polarized signals to change the total intensity (i.e., the Stokes I component) (Jelić et al. 2010, 2015). This effect is known as “polarization leak-age”. The instrumentally polarized signal can introduce spectral fluctuations in power spectra, further exacerbated by Faraday rotation (see Sect. 3.2.2), and mimic or contaminate the 21 cm signal. This effect has been estimated to be very small for LOFAR-HBA and likely only contributes to ~1% of the observed excess variance (Asad et al. 2015, 2016; Jelić et al. 2015). In this work, we do not focus on analyzing the contribution of instrumental polarization.

Gain regularization. During DD-calibration, we assume that direction-independent and non-smooth responses such as the structure in the band-pass response of stations and cable reflections (Offringa et al. 2013; Beardsley et al. 2016; Kern et al. 2020; Mertens et al. 2020) are taken out in the DI-calibration step and hence gain solutions should be spectrally smooth. The smoothness of gains is enforced by using SAGECAL-CO (Yatawatta 2016) with a third-order Bernstein polynomial (Yatawatta 2015).

Currently, gain solutions are only mildly regularized in the DI-calibration step due to the uncorrected band-pass and cable reflection structures in frequency. The remaining structure in the frequency direction can introduce small chromatic gain errors. These errors could result in spectral fluctuations in the EoR window and can be a source of excess variance.

Patil et al. (2016); Barry et al. (2016); Ewall-Wice et al. (2017) showed that using small regularization constants (i.e., low regularization) can allow the gains to overfit the data. The extra frequency-dependent gain structure introduced by overfitting, when applied to the calibration model, can both leak power in the EoR window (excess variance) and lead to signal loss (bias). Previously, Patil et al. (2017) tried to tackle the latter problem by excluding the short baselines <250λ, used for 21-cm signal analyses, in DD-calibration. However, the gain-regularization parameters and the number of iterations used in Patil et al. (2017) were sub-optimal and resulted in high excess variance on the excluded baselines. Mertens et al. (2020) significantly improved the DD-calibration method by optimizing regulariza-tion values (Mevius et al. 2021). The results showed that excess variance due to overfitting in the DD-calibration step is not a major contribution with the improved calibration scheme.

3.3 Time and sky-model power dependence

If excess variance depends on how much power the instrument receives, the expectation is for it to depend on local sidereal time (LST). To investigate this further, the data was binned in LST ranges and compared to sky-model power-spectrum simulations.

3.3.1 LST dependence

The sky-related effects on the 21 cm signal power spectra can be analyzed, for example, by analyzing the LST dependence of the excess variance. The power received by LOFAR is a product of the intensity coming from the sky and an averaged beam model which depends on receiver gains. Hence, an excess variance power that correlates with LST must come from a change in the product of the two (i.e., the sky intensity and the averaged beam). For similar LST ranges, the observed sky is similar (barring strong variable sources, which is a reasonable assumption at low frequencies). Therefore, for multiple observations within similar LST ranges, the difference between nights is likely to come from a difference in the instrument, uv-coverage, flagging, ionosphere, or RFI, and so on. However, effects that are uncorrelated between nights (e.g., RFI is more likely to correlate with UT, because it is caused by human activities) or are stochastic in nature (e.g., the ionosphere) are unlikely to show a strong LST dependence in the integrated power over multiple nights.

In this work, we examine the correlation between the sky and the excess variance by looking at the variation of excess variance with LST. For this purpose, we sliced each observation into 3 hour (3h) LST ranges. The duration of the observations and the resulting 3 hour slices from each night are shown in Fig. 2. We created a power spectrum for each slice after applying GPR foreground-removal with parameters optimized using data from the entire night to avoid overfitting and assuming that the power spectrum of the sky and signal does not change in a slightly rotated NCP. We estimated the excess variance level of each slice. By comparing individual LST slices, we were able to assess how the excess variance correlates with LST and also whether there are changes between nights within the same LST range.

thumbnail Fig. 2

Duration of observations in LST for 13 nights. For analyzing the LST-dependence on excess variance, each observation yields three to four 3 h LST slices (in red) and power spectra are estimated for each 3h slice, respectively. The data which do not fully cover a 3 h LST range are discarded (in blue) and are not included in the analysis.

3.3.2 Sky-model power simulations

Besides any LST dependence, to further assess whether the excess power correlates with received power, and from which sources, we simulated visibilities based on two sky models: (1) the two brightest radio sources in the northern sky, Cas A and Cyg A, which are outside the instrument's field of view (~30º and ~50º away from the NCP, respectively); (2) the first 1416 bright sources that are used for DI-calibration and account for ~99% of total sky model power together with A-team sources (de Gasperin et al. 2020) including Cas A and Cyg A. The simulations were created by matching the same observing times, sub-bands, and the uv-coverages of all 13 observations, with and without post DD-calibration flagging. The simulated visibility sets were also sliced into 3h LST bins to create power spectra. Finally, they were compared with power spectra from the actual observations.

4 Results

In this section, we present and discuss the correlations between the excess variance of the LOFAR-EoR power spectra and the metrics discussed in the Sect. 3.2. We focus on gain calibration and sky-model and ionospheric related effects, as well as the impact of flagging.

thumbnail Fig. 3

Distance of Cluster82, Cluster84, and Cluster89 from the NCP.

4.1 Gain solutions

Before analyzing power spectra from LOFAR data, we first analyze gain solutions that are used to calibrate observed data. The gain solutions are obtained by SAGECAL-CO as described in Sect. 2. As discussed in Sect. 3, gains are solved under the physics-motivated assumption that instrumental and ionospheric effects are smooth in frequency and on short time intervals. Therefore, irregular behaviors of gains, namely, non-smooth gains, over frequency or time, can be considered as gain errors. Such gain errors can propagate to power spectra of the 21 cm signal and contribute to the excess variance.

4.1.1 Gain smoothness

We calculated and analyzed averages of gain solutions over time and frequency, respectively, to assess their smoothness level and investigate whether there are possible errors in gains. We limited ourselves to three out of the 122 directions: Cluster82, Cluster84, and Cluster89 (see Fig. 3), which are inside, around, and outside the full-width-half-maximum (FWHM) of LOFAR-HBA tiles being ~3.8º at 150 MHz (van Haarlem et al. 2013), respectively. Detailed information about the three clusters is summarized in Table 3. Figures 4 and 5 show the DD-gain average over time and frequency of 13 observations for the selected three clusters and three core stations, respectively. The three stations are selected based on their location: CS003 resides on a 320 m diameter island at the core of LOFAR, known as the “Superterp;” CS026 and CS401 reside on two opposite sides (in the east and west) of CS003 outside the Superterp within ~1 km diameter from the LOFAR core. The DD-gain solutions calibrate measured visibilities for each station, polarization, time, and frequency. To obtain the gain average over time or frequency, each polarization component (XX, XY, YX, YY) is added in quadrature to obtain the total intensity. Afterwards, gains are averaged over time or frequency for each station, respectively. At this stage, the averaged gains have two dimensions, namely, (station, time) or (station, frequency). We note that these gains are not applied to the sky-model and subtracted from the data, but those from the Bernstein-polynomial fit. The latter is sufficiently smooth not to cause the observed excess variance (Mertens et al. 2020); hence, any gain averages and variances only act as an indicator of other gain effects that might affect the power spectrum.

Gain smoothness over frequency. Time-averaged gains do not show a strong frequency dependence for the three selected source clusters (i.e., the direction). For specific observations and stations, for example, the time-averaged gains for observation L246309 in Cluster84 and CS003HBA1 (the cyan line on the left column and middle row in Fig. 4) increases as frequency increases, but this tendency only appears in a few cases. It is rather random and there is no strong correlation between gains and different clusters or nights. The time-averaged gains are in general smooth between neighboring frequency intervals and we do not see huge jumps in the gain average for a selected cluster, station and night. We notice that the time-averaged gain in Clus-ter89 (bottom row in Fig. 4) has less smooth curves compared to ones from Cluster82 and Cluster84 (first two rows in Fig. 4). A cluster located farther from the NCP have gains solutions that are less smooth over frequency compared to gains for a cluster closer to the NCP. We see that in a given cluster and a station, gains per night show a slight increase towards its two frequency ends and this increase is more obvious in outer clusters (from top to bottom in Fig. 4), where the S/N is lower (Mertens et al. 2020; Mevius et al. 2021). The different level of smoothness in gains is possibly also related to the different solution time interval in each cluster. Cluster89 has one solution in every 20 min while Clus-ter82 has 4 solutions and Cluster84 has 8 solutions per 20 min, respectively. This means that a single data point in Cluster82, Cluster84 and Cluster89 is a time-averaged gain over 5 min, 2.5 min, and 20 min, respectively. Finer time intervals are better at catching small variations in ionospheric and beam effects.

Gain smoothness over LST. Figure 5 shows frequency-averaged gains as a function of LST per night and station. The frequency-averaged gains are calculated in a way similar to how the time-averaged gain is calculated, however, this time we average over frequency in the final step, instead of time. There are gaps among data points appearing around LST15-20 in all three clusters because the starting times of some observations are later in LST and observations end earlier in LST. We note that gains are more sparsely distributed in Cluster89 compared to ones in Cluster82 and Cluster84 due to the longer solution time interval. In a fixed cluster, the station-to-station difference (between columns in Fig. 5) is rather small compared to the cluster difference (between rows in Fig. 5). For a fixed station and a night, the gain averaged over frequency per night shows a clear LST-dependence. The frequency-averaged gain typically shows a sinusoidal behavior with LST. This is because the beam shape changes over time due to the Earth's rotation. The smoothness of the sinusoidal gain curves depends largely on the cluster (i.e., the direction, between rows in Fig. 5). Cluster84 is ~3.7° away from the NCP and the FWHM of HBA tiles in core stations is ~3.8° at 150MHz (van Haarlem et al. 2013). As a result, Cluster84 (middle row in Fig. 5) is still within the FWHM of HBA tiles and the corresponding gains do not change rapidly compared to Cluster89 (bottom row in Fig. 5), which is farther away from the NCP than Cluster84. We observe that as the cluster is located farther away from the NCP, the frequency-averaged gain fluctuates more rapidly (from top to bottom row in Fig. 5) and vice versa.

Night to night correlation. The LST dependence of the gains is very strong and in a fixed cluster, the sinusoidal behavior of gains is similar between stations as well except for some specific nights appearing as outliers. We note that some specific nights keep appearing as outliers in the same station of multiple clusters. For instance, two observations L90490 and L86762 (in pink and teal, respectively) constantly deviate from other nights in station CS401HBA1 for gain averages over time and frequency for Cluster84 and Cluster89 (last column on the second and third panels in Figs. 4 and 5). Similarly, L80847 and L80850 in Clus-ter89 and CS026HBA1 appear as outliers. We suspect that the “outlier nights” come from some station-based effects, such as station orientations or broken tiles in stations that occurred for specific observations. To check this point, we compare tile flagging of core stations between observations and figure out that observations can be categorized into three groups based on their similarity of tile flagging: (1) L80847 and L80850; (2) L86762 and L90490; and (3) the rest. We note that observations in the same group were taken closely in UTC (in Table 1) and they tend to have more similar tile flagging. As we expected, the outliers exactly come from the tile flagging groups (1) and (2) which have different tile flagging compared to other observations. This supports that the night to night difference in gain average is mainly due to the tile flagging difference between observations, which leads to differences in their station beams and, hence, their DD gains.

Table 3

Information of three clusters used for DD-calibration gain analysis.

4.1.2 Correlation between gain solutions and excess variance

The instrument and the sky should have spectrally smooth gains; hence, any abrupt jump in the gain average or variance over frequency or time is an indication of excess noise13. To assess whether there is a correlation between excess variance and gain errors, we plotted excess variance against the DD-gain variance. Four polarization components in gains, solutions were added in quadrature to calculate a “total intensity” equivalent. The gains were then averaged over core stations to increase the S/N and the variance is calculated along the time axis; hence, the calculated variance is given as a function of frequency.

To estimate the excess variance in the 21 cm power spectra, we used the Stokes I and V components of the spatial power spectra. The spatial power spectra were obtained by performing Fourier transform along the spatial coordinate (u, v) on measured visibility cubes. The spatial power spectrum is given as a function of frequency and baseline (k). We averaged the spatial power spectrum over baseline for the Stokes I and V, respectively. For a given frequency, we took the ratio of the averaged Stokes I and V. Finally, the gain variance over time and the Stokes I/V ratio was mapped by matching frequency. We note that a disadvantage of this analysis is that the baseline dependence on gains and excess variance will be erased because we are averaging over baselines to calculate the Stokes I/V ratio as a function of frequency. In a forthcoming paper, we will examine excess noise in more detail as a function of baseline and delay.

Figure 6 shows excess variance as a function of DD-gain variance over time in Cluster84 per night, respectively. We immediately note that the excess variance does not strongly depend on either frequency or gain variance. Rather, the gain variance over time increases as frequency increases and this is consistent for all 13 night observations. Since the primary-beam FWHM is inversely proportional to frequency and gets narrower as frequency increases, we can expect that gains fluctuate more for higher frequencies, and the gain variance increases as well. This is indeed seen in the figure.

However, our current analysis is limited to a relatively narrow frequency range (134.1–147.1 MHz) compared to the three-fold broader frequency range (121.8–159.3 MHz) that was previously presented in Patil et al. (2017). To be able to investigate the frequency dependence of gain variance, we need to add more data with a wider frequency range. In the future, we will extend our analysis to a wider redshift range. This extended analysis can give a more clear correlation between excess variance and frequency. However, the current conclusion is that excess variance does not correlate with gain variance. If anything, it has a slight anti-correlation for some nights.

thumbnail Fig. 4

Time-averaged DD-gains as a function of frequency from 13 night LOFAR observations (in different colors) in Cluster82 (top row), Cluster84 (middle row), and Cluster89 (bottom row). The calculated time averages are separately plotted for three chosen core stations – CS003HBA1 (left column), CS026HBA1 (middle column), and CS401HBA1 (right column), respectively. The color code denotes different nights and each data point indicates a time average at a fixed frequency and a night. Time-averaged gains are smoother over frequency as the cluster is closer to the NCP (from bottom to top).

thumbnail Fig. 5

Frequency-averaged DD-gains as a function of time from 13 night LOFAR observations (in different colors) in Cluster82 (top row), Cluster84 (middle row), and Cluster89 (bottom row). The calculated time averages are separately plotted for three chosen core stations – CS003HBA1 (left column), CS026HBA1 (middle column), and CS401HBA1 (right column), respectively. The color code denotes different nights and each data point indicates a frequency average at a fixed time and a night. Frequency-averaged gains fluctuate more rapidly over LST as the cluster is farther away from the NCP (from top to bottom).

thumbnail Fig. 6

Excess variance as a function of DD-gain variance over time in Cluster84 for 13 nights. The color denotes frequency. Each data point in a fixed night is a gain variance over time at a fixed frequency with the corresponding Stokes I/V ratio. There is no strong correlation between the excess variance and gain variance over time. However, the gain variance has a frequency dependence: higher frequencies tend to have higher gain variances.

thumbnail Fig. 7

Median value over 13 nights of the ratio (i.e., Stokes I over Stokes V) of the cylindrical power spectra per LST bin. We define this as a cylindrical “excess variance” power spectrum. The dashed lines indicate the 5° (the primary beam; bottom), 20° (middle), and instrumental (top) horizon delay lines, respectively. The excess variance is especially high (>5) in the wedge region below the ~20° delay line in all LST bins. The excess variance has an LST dependence and LST 09-12 has the highest excess power in the wedge region compared to other LST bins.

4.2 Sky-related effects

In this subsection, the impact of sky-related effects on excess variance is investigated by performing jackknife tests on the observed 21 cm power spectra and the simulated power spectra. Individual observations and simulated visibility sets are divided into 3 h LST bins (see Fig. 2) and power spectra are created for each of them. By limiting observations into 3h LST bins, we expect to be able to obtain equivalent PSFs and primary beams for different observations per 3 h LST bin. This way, we can focus on investigating the impact of some bright sources which might be more prominent at a given LST.

4.2.1 LST dependence

Each night was divided into 3 h LST bins and the data that do not fully cover the full 3 h LST were discarded. Based on these 3 h LST bins, we created visibility cubes and estimate their power spectra. We note that the number of observations in each 3h LST bin is not equal for each night (Fig. 2). We also created power spectra for 1h and 6h LST bins, respectively, but find that the 3 h bins have the optimal duration. The 1 h LST bins have very limited uv-coverage and the generated power spectra end up containing much higher excess variance and residual foregrounds compared to power spectra from longer observations. The 6 h LST bins have a good uv-coverage but result in only 1 or 2 bins per night; hence, the 6 h LST bins do not provide sufficient information about LST dependence. The 3 h LST bins still have a relatively good uv-coverage and provide us with enough information about LST dependence.

Figure 7 shows the median of 13 nights of cylindrical excess variance power spectra (i.e., the residual Stokes I and V ratio) per LST bin. We see that even after the DI-, DD-calibration, and foreground removal with GPR, there is still significant excess variance in power spectra, especially in the foreground wedge region (below the ~20° delay lines). The excess variance can reach up to ~10 times the expected Stokes-V power (thermal noise) in the primary beam region, namely, the area below the ~5° delay lines in LST09-12. In LST21-00, we see a horizontal stripe (k ~ 0.3 hc Mpc–1) of lower excess variance. In this particular LST bin, we have fewer samples compared to other LST bins, namely, only two observations (L246309 and L246297). The power in Stokes V is higher in L246309 around k ~ 0.3 hc Mpc–1 and when we take the median of the Stokes I/V ratio, this higher power in Stokes V from one night stands out. This is not limited in LST21-00 of L246309 because we also see a similar stripe around k ~ 0.3 hc Mpc–1 in the full night excess variance power spectrum of L246309 in Fig. 1. It is not clear why the power of Stokes V in L246309 is higher than other nights. Adding more samples possibly removes the stripe and gives a cleaner EoR window (the region above the ~90° delay line). The excess variance in the wedge below the ~20° delay lines changes drastically, depending on LST. LST09-12 shows the highest excess variance level in the wedge region compared to other LST bins. LST03-06 and LST06-09, on the other hand, show relatively a lower excess variance level. To further quantify the LST-dependence of the excess variance, we calculate the excess variance by averaging the median ratio of the cylindrical residual Stokes I and V over k and k. The top panel in Fig. 8 shows the excess variance as a function of LST for all 13 nights. The excess variance varies with LST and it has the lowest values around LST03-06 and LST06-09. The excess variance shows a slight increase for other LST bins. This suggests that the excess variance depends on LST and is correlated with the sky. Both RFI and ionosphere are less likely to correlate with LST, that is, the PSF and primary beam. Different LST bins have different PSFs and primary beams and hence this difference is more prominent for bright sources in the sky seen by the instrument. RFI and ionosphere do not suffer from changing PSFs and primary beams. The scatter within each LST bin, however, is considerable and this is further investigated below.

4.2.2 Simulation

To verify whether the LST dependence of the excess variance is correlated with the power spectrum of the sky model, we simulated the visibilities and performed a similar test on the simulations. Our current sky model has more than 28 000 components (see Sect. 2). However, the dominant contribution comes from very bright sources such as Cas A and Cyg A, therefore, we did not use the entire sky model in the simulation but, instead, we limited the simulation to the use of (1) Cas A and Cyg A only; (2) the 1416 brightest components used for DI-calibration and Α-team sources, which contribute about 99% to the sky power spectrum. We used DPPP14 to predict visibilities including the LOFAR-HBA beam model. In this step, we used the UNFLAG option to remove all the antenna flagging from the observation, mainly from RFI flagging, as simulated data do not have RFI issues (see Appendix A for more discussion). The predicted visibilities were then sliced in LST as we sliced the observations and then they were subsequently imaged by WSCLEAN using baselines longer than 40λ and shorter than 260λ. Finally, the created image cubes were used to estimate the cylindrical power spectra in Stokes I, at this stage, we also perform post-processing flagging to filter out some uv-cells with bad uv-coverage. This extra step is needed because we are now working on relatively short observations (3 hours long) and the uv-cells with bad coverage can add extra power into the EoR window. The impact and necessity of flagging on simulated data (RFI unflagging and uv-cell flagging) are discussed in Appendix A. Figure 9 shows the cylindrical power spectra of the Stokes I from two different simulations with sky models (1) and (2) mentioned above. The left panel shows that the power from Cas A and Cyg A is concentrated under the instrumental horizon delay lines (top dashed lines) and above the primary beam (bottom dashed lines). Adding more sources to simulation, in the right panel, adds more power into the region below the horizon, especially to the primary beam region (below the bottom dashed lines).

Simulation cross-checks between nights. The k-averaged simulated Stokes I power spectra with the two models per LST and per night are shown in Fig. 8 (middle and bottom). The typical power in Stokes I increases about an order of magnitude from the Cas A and Cyg A only model to the DI-calibration model with Α-team sources. We notice that even within a fixed LST bin, the simulated power can be different from night to night. This night-to-night difference happens because our simulations are based on real observations. We follow the same observing times and beam patterns (including antenna flagging, sub-bands) of real observations. This implies that (1) antennas in stations are flagged differently for each night; (2) the 3h LST bins based on the observing time are not exact and can have up to 10-sec errors, because of the 10 s time interval in data and the difference in start and end times between observations; (3) the number of sub-bands differs from night to night. While the difference in LST bins and the number of sub-bands per night are already defined, the station flagging difference is more due to defects in the instrument at a specific time in a real observation that do not exist in a simulation. To make our simulations more realistic, we manually “unflag” antennas from RFI flagging during the simulation and then flag uv-cell with bad coverage at the stage of power spectrum estimation as discussed earlier. In this way, we do not flag extra stations in simulations. Typically, up to 5% of total visibilities are filtered out in the uv-cell flagging. The 10 s of difference in 3h LST bins should not lead to a significant difference in power because the modeled power is smooth over time and 10 seconds accounts for less than 0.1% of the 3 h observing run. Therefore, we conclude that the difference between nights mostly originates from the difference in the number of sub-bands and from the uv-cell flagging. We also notice that there might be differences in tile and antenna flagging between nights, which could also contribute to the difference between nights per 3h LST data, however, single tile or antenna flagging in simulations cannot be switched off easily at the current level; hence, we do not discuss this case in this paper.

Correlation between simulations and the excess variance. The k-averaged power spectra of the excess variance and the simulated Stokes I from two models are compared (from top to bottom in Fig. 8). We note meaningful similarities in the progression of the averaged power spectra over LST between the excess variance and the simulations. The LST-dependence we first see from the excess variance in Figs. 7 and 8 (top) also appears in the simulations in Fig. 8 (middle and bottom) and Fig. 9 with the minimum power appearing at LST06-09, especially when comparing their lower envelopes.

To verify the strength of correlations between the simulated Stokes I power and the excess variance level more accurately, we performed three different correlation tests on the data sets, including a Pearson correlation test as well as Spearman and Kendall rank correlation tests. As we discussed already, the night-to-night difference within a given 3 h LST bin can still be significant both for observations and simulations, due to the differences in the number of subbands and flagging status between nights. When the simulated Stokes I and the excess variance level are correlated, this night-to-night difference can possibly introduce outliers and the correlation test results will not reflect the actual strength of the correlation accurately. Thus, in Fig. 10, we show how we took the median value per 3h LST bin for the excess variance and the simulated Stokes I between nights and performed correlation tests on the median values. The rms of the simulated Stokes I power and the excess variance between nights per LST bin are also present on top of each data point, respectively, to show the night-to-night spread per LST bin.

We performed three types of tests because they are sensitive to different correlation characteristics. The Pearson test is sensitive to linear correlations and is susceptible to outliers. The Spearman and Kendall tests are less sensitive to outliers and are able to detect higher-order monotonie relationships. The correlation test results are summarized in Table 4. Overall, the Cas A and Cyg A simulation shows a strong correlation with the excess variance with the correlation coefficients ranging between 0.60 and 0.71, while the DI sky model and Α-team simulation shows a rather moderate correlation with the correlation coefficients ranging between 0.33 and 0.58. However, the p-values from both models are relatively high (0.11–0.21 for the Cas A and Cyg A model and 0.22–0.47 for the DI sky model and Α-team) and, hence, the correlations are not robust. This is partially due to the limited sample size after processing and the night-to-night spread in each LST bin. These limitations can be mitigated when more nights are combined. At this moment, we conclude that the excess variance correlates moderately with the bright sources in the sky, especially with very strong sources such as Cas A and Cyg A. This indicates that the excess variance might be leakage from the sky power.

thumbnail Fig. 8

LST-dependence of excess variance and two sky models. Top: excess variance averaged over k per night and per LST in orange. Middle: simulated Stokes I cylindrical power spectra averaged over k per night and LST with Cas A and Cyg A in red. Bottom: simulated Stokes I cylindrical power spectra averaged over k per night and LST with the DI-calibration model (including the 1416 brightest components that account for ~99% of the flux from our sky model) and A-team sources in green. Different markers indicate different observations. The difference between nights in simulations mainly comes from the different number of sub-bands per night (see Table 1) and flagging based on uv-cells. The excess variance from observations and the simulated Stokes I power from the two models (in middle and bottom) shows a similar LST-dependence.

thumbnail Fig. 9

Median cylindrical Stokes I power spectra of the 13 night simulations with two different sky models per LST bin based on the 13 observations including uv-cell flagging. Left: Cas A and Cyg A model. Dashed lines indicate, from bottom to top, 5° (the primary beam), 20° and instrumental horizon delay lines. Right: the DI-calibration model (including the 1416 brightest components that account for ~99% of the flux from our sky model) and Α-team sources. LST03-06 and LST06-09 in both simulations show lower power compared to other LST bins and this trend is consistent with what we have seen with the excess variance in Fig. 7 and the top panel of Fig. 8.

thumbnail Fig. 10

Correlation between the median simulated Stokes I from two sky models and the median excess variance over LST. Top: correlation between the Cas A and Cyg A model and excess variance over LST. Bottom: correlation between the DI sky model (that accounts for ~99% of the power in the sky model) and Α-team sources and excess variance over LST. Different colors indicate different LST bins. The error bars on each data point indicate the RMS of the simulated Stokes I power and the excess variance between nights per LST bin, respectively (we note that they are not observation errors), to show the night-to-night spread of the data per LST bin. The correlation between the simulated power from the two models and the excess variance show a moderate correlation but it is not strong, due to the limited sample size and night-to-night spread of the data.

4.2.3 Variance maps

We created wide-field (20° × 20°) maps of the residual Stokes I intensity standard deviation along frequency incoherently averaged over seven observations to assess whether the excess variance in the power spectra comes from specific sources or directions in the sky. These images are created after DI-, DD-calibration and GPR foreground removal from seven observations, focusing on the excess variance dominant part of the power spectra (see Fig. 7), under the instrument horizon. For each 3h LST residual Stokes I power spectrum, we create maps from specific regions in the power spectra – passing only the data under 5° delay line (first column; roughly the primary beam area), between 5° and 20° delay lines (second column), between 20° and 90° delay lines (third column), respectively. The filtered power spectra are Fourier transformed along kx, ky (k=kx2+ky2)$\left({{k_ \bot} = k_{\rm{x}}^2 + k_{\rm{y}}^2} \right)$, and k directions into image space. The created images are shown in Fig. 11.

In all wide-field maps, the residual power is stronger around the central part where the instrument has the highest sensitivity and the power spectra are estimated (on the central 4° × 4° FoV). For a fixed LST bin, the residual power from the primary beam region is mostly added to the central part of images (first column) and the residual power outside the primary beam is scattered more evenly over the entire FoV (second and third columns). From left to right, we plot the images corresponding to the different regions of the power spectra in (k, k) space, however, the power difference is marginal and we see a plateau of the residual power in the EoR window (third column). This indicates that most of the residual power still comes from foregrounds (first two columns), and some of this power is not from local sources (that they would add power as single sources as shown in the first column), but possibly from distant sources such as Cas A and Cyg A (which scatter power rather evenly over the entire FoV). Even after the calibration methods including DI-, DD-calibration, sky-model subtraction and GPR foreground removal, these foreground sources are not sufficiently removed. Therefore, further improvement of calibration methods, especially on foreground removal is still needed.

In Fig. 12, we present very wide-field images (100° × 100°) after DD-calibration to investigate how the power from Cas A and Cyg A contributes to the excess variance. The images are created from observation L254116 combining 62 sub-bands and applying the baseline cut 50–250λ used for the power spectrum estimation. The positions of Cas A and Cyg A are marked with blue circles on top. The time- and frequency-averaged beam patterns per 3h LST are also overlaid on top with different colors indicating different gains (from inside to outside: red, blue, green, magenta, and gray corresponding to –10 dB, –20 dB, –30 dB, –40 dB, and –50 dB gains, respectively).

The actual residual power we see in the power spectrum is the multiplication of the sky power in the images and the average beam. The residual power in the very wide-field sky images in Fig. 12 show that the residual power sharply decreases outside the primary beam (the LOFAR core station FWHM at 150 MHz is around 3.8º (van Haarlem et al. 2013)), but there is extra power coming from the direction of Cas A and Cyg A, the power is especially strong from the Cas A direction. The power changes over LST and becomes minimum at LST06-09. This is in line with the excess variance and the simulated Cas A and Cyg A power progression over LST in Fig. 8. The averaged beam pattern rotates over time and the –50 dB sidelobe (in gray) sweeps through Cas A and Cyg A, the overlap is maximum in LST00-03 and minimum in LST09-12. This explains the decreasing excess variance in the first three LST slices. In LST09-12, the residual power in the sky from Cas A is strong again. While the –50 dB sidelobe is almost on the opposite side of Cas A and Cyg A this time, however, the –40 dB sidelobe (in magenta) has an extended arm towards Cas A direction that allows power from Cas A to enter. The combination of these two effects possibly results in a higher excess variance in Fig. 8.

This further supports that the excess power depends on LST and that it is correlated with sky-related effects, such as gain errors from an imperfect sky model or extra power from the sky that is not part of the sky model. These effects are not corrected in the DD calibration. Using the simulated Stokes I power of Cas A and Cyg A as an example, we estimate the calibration accuracy required to avoid the excess variance from the two sources. The spherically averaged power spectrum of Cas A and Cyg A from one-night observation (L246309) is shown in Fig. 13. The simulated power from only Cas A and Cyg A observed by the LOFAR-HBA system is around 2 × 105 mK2 at k = 0.1 hc Mpc–1, while the estimated power from the 21 cm EoR signal is around 10 mK2 level at k = 0.1 hc Mpc–1. Based on these results, we estimate that the Stokes I power of Cas A and Cyg A must be reduced at least by ~99.3% to be able to distinguish the 21 cm signal from the excess variance caused by Cas A and Cyg A.

Table 4

Three correlation test results on the simulated Stokes I power from two sky models and the excess variance level.

thumbnail Fig. 11

Standard deviation of the residual Stokes I intensities along the frequency direction, after sky-model subtraction and GPR residual foreground removal at 2.5 arcmin resolution incoherently averaged over seven nights per 3 h LST from different regions of (k, k) space – passing only the data under 5° delay line (first column), between 5° and 20° delay lines (second column), between 20° and 90° delay lines (third column) in the power spectra, respectively. All images are in units of Kelvin. As we show in Fig. 7 LST03-06 and LST06-09 once again show lower residual power compared to other LST bins.

thumbnail Fig. 12

Very wide images after DD-calibration from observation L254116 combining 62 sub-bands with the position of Cas A and Cyg A and the time- and frequency-averaged beam patterns overlaid. From inside to outside, different color (red, blue, green, magenta, and gray) indicate different beam gains, corresponding to –10 dB, –20 dB, –30 dB, –40 dB, and –50 dB. The actual excess variance we see in the power spectra should be the multiplication of the residual Stokes I power and the beam effects. In the sky images, we see the extra power coming especially from the Cas A direction. This power is at its peak in LST00-03, decreasing in LST06-09 and increasing again in LST09-12. This tendency corresponds with what we observed in the LST progression of excess variance and the simulated power of Cas A and Cyg A in the top and middle panels of Fig. 8. The averaged beam rotates over time, as we can see in the images, the –50 dB sidelobe (in gray) sweeps through Cas A and Cyg A from LST00-03 to LST09-12. In the first three LST slices, the sidelobes rotate away from Cas A and Cyg A, at the same time, the power from Cas A and Cyg A decreases. As aresult, the excess variance effect from Cas A and Cyg A decreases from LST00-03 to LST06-09. In LST09-12, although the –50 dB envelope is located in the opposite direction of Cas A and Cyg A, the –40 dB sidelobe (in magenta) has an extended arm towards Cas A direction and the extra power from Cas A direction increases again. This combined effect results in increased power in LST09-12, as we see in Fig. 8.

thumbnail Fig. 13

Spherically averaged power spectrum estimated from one-night (L246309) Cas A and Cyg A only simulation. Compared the Cas A and Cyg A introduced Stokes I power to the estimated 21 cm signal at k = 0.1 hc Mpc–1, the Cas A and Cyg A power should be reduced by ~99.3% or even higher in the calibration to be able to distinguish the 21 cm signal from the Cas A and Cyg A power.

4.3 Ionospheric effects

In this subsection, we investigate potential correlations between the excess variance and ionospheric effects using the phase structure function, from which we derive the fitted slope β and the diffractive scale, rdiſſ. These metrics are used to describe ionospheric conditions during observation and are obtained from LOFAR observations by fitting the phase variance as a function of baseline length per 3h LST bin (we refer to Mevius et al. (2016), Sect. 3 and Appendix B for details). Figure B.1 shows the binned phase structure functions of 13 observations at 140 MHz for LST00-03 (top three rows) and LST03-06 (bottom three rows), with the results of the power-law phase-structure function fits superimposed with solid lines in red. We calculate the Pearson’s coefficient R2 to estimate the quality of the fit. R2 ranges between 0.87 and 0.99 for all observations and LST bins, yielding representative β and rdiff values. We list the resulting values β, rdiſſ and R2 per LST bin for 13 observations in Table B.1.

Based on the study from Mevius et al. (2016), we expected the fitted slope β from structure functions to range between 5/3 (a contribution from the pure Kolmogorov turbulence in the lower atmosphere, Velthoven, van 1990) and 2.0 (from non-turbulent structures, such as travelling ionospheric disturbances (TIDs), Rufenach 1972). From our results, about 73% of β values correspond to this range. Furthermore, Vedantham & Koopmans (2015) showed that a minimum diffractive scale of 5 km at 150 MHz is required for an EoR detection. About 87% of rdiff is above 5 km for all LST bins and 13 observations, which is encouraging.

Finally, we correlated β and rdiff with the excess variance per LST bin, respectively, to assess whether the ionosphere has a sky-dependence or correlates with the excess variance. The results are shown in Fig. 14. In addition, we performed a Pearson correlation test per LST bin to provide a PCC and a P-value as single number measures for the correlation between the ionosphere and excess variance. The results are summarized in Table B.1. The PCC values suggest no strong correlations (PCC < 0.6) between the ionosphere and excess variance over different LST bins, neither for rdiff nor β, with a possible exception for the bin LST09-12. We expect that ionospheric effects are more likely to correlate with Earth-based effects than with the sky, thus, they are more correlated with UT than with LST. If there is any correlation between the ionosphere and excess variance, this should appear consistently over all LST bins. The PCCs between LST bins vary widely in our results, ranging between –0.71 and 0.32 for rdiſſ and between 0.02 and 0.66 for β, respectively. In particular for rdiff, the PCC alternates between positive and negative correlations for different LST bins. We suspect that these slightly higher PCCs in LST09-12 (–0.71 for rdiſſ and 0.66 for β) more likely come from a random statistical error than a real correlation. In addition, our samples per LST bin are very limited (from 2 to 11 per bin, see Fig. 2), and having one or two noisy data points in a bin could heavily affect the final result of the Pearson test. In summary, we conclude that the excess variance is not strongly correlated with the ionosphere at the current level.

5 Conclusions

The LOFAR-EoR Key Science Project is aimed at detecting the 21 cm hydrogen signal originating from the Epoch of Reioniza-tion in the redshift range of ɀ ≈ 7–11. The detection of the 21 cm signal, however, requires very high precision calibration to correct corrupting effects from the strong galactic and extragalactic foregrounds, the ionosphere, RFI and instrument’s limitations, and so on. After the current best-effort in calibration, there is still extra power that is above the expected thermal noise level in the 21 cm power spectra, which is known as the “excess variance” (Patil et al. 2016, 2017; Mertens et al. 2020). There are two known types of this excess variance: (1) the spectrally-uncorrelated excess on short baselines (<100λ) and (2) the spectrally and temporally (within a few nights) correlated excess (lex ~ 0.25–0.45 MHz) that is stronger in the foreground dominated wedge (Mertens et al. 2020). In this paper, we examine the correlations between possible sources, such as errors resulting from DD-gain solutions, sky-related effects, and ionospheric effects as well as the excess variance. Our two main conclusions are as follows:

We find no correlation between either the diffractive scale or the ionospheric phase structure function fit slope and excess variance, suggesting that the ionosphere is not a dominant contributor to the excess variance at the current level of sensitivity.

On the other hand, the level of excess variance shows a trend with local sidereal time (LST), suggesting that excess variance depends on the sky as affected by the instrument (not the ionosphere). By limiting observations into equivalent 3h LST bins, the difference in the point spread functions (PSFs) and primary beams between nights is minimised within each LST bin. In this way, sky-related effects are closely related to PSFs and primary beams and, hence, they will be reflected as an LST dependence. Investigating this further, we find that the simulated Stokes I power of bright sources in the sky model shows a similar progression in LST with the excess variance.

We show that the excess variance presents a similar LST dependence in the residual Stokes I images. The images show a clear imprint of the primary beam (within 5° from the phase centre), but also a plateau for the power spectrum region in the EoR window. In our very-wide sky images, we further show that some of the power left after DD-calibration is coming from the direction of Cas A and Cyg A. These results again support the conclusion that excess variance could be leakage from the sky power, and some of this power is not the result of local sources (in the case of which, there should be no plateau), but of distant sources such as Cas A and Cyg A.

We conclude that excess variance, as seen on the NCP with the LOFAR-HBA system, is likely dominated by residuals of bright sources after sky-model subtraction due to their still-limited sky models, which is further exacerbated by flagging and gridding effects. Although it has been suspected that the ionospheric effects might significantly contribute to the residual noise in the 21 cm power spectra, we conclude that the ionosphere does not show any strong correlation with the excess variance at the current level. Rather, the excess variance is correlated with LST and the sky model. Thus our future analysis will focus on analyzing the time dependence of gain solutions, enforcing smoother solutions in time, and improving the sky model.

Based on our analysis, we suggest the following strategies for future improvements:

Improving the sky model. The correlation between the excess variance and the sky model is strong. We know that the current sky model is not perfect and this incompleteness in the model can be further propagated to gains during calibration and further contribute to the excess variance in the power spectra. Our current sky model does not include diffuse Stokes I, Q, and U emission and the inclusion of the diffuse components will improve the power spectrum results (Prasad et al. 2016; Gehlot 2019).

Applying finer time intervals for DD-gains. As we see in Sect. 4.1.1, the smoothness of DD-gains in time is not as good as the one in frequency. Depending on the cluster, we still see jumps between time-consecutive gains, as in Cluster82 in Fig. 5. We suspect that for some clusters, the current solution intervals are too long to take into account some rapidly-varying ionospheric scintillation whose decorrelation time is a few seconds (Vedantham & Koopmans 2016). Solving gains for shorter time intervals can help enforce smoother gains in this case.

Focusing on a “cleaner” time window. We see both from the observations and simulations that the excess variance and the power from foreground sources are lower in a specific time range, LST03-09. While the excess variance is possibly correlated with errors from the calibration or the incompleteness in the sky model, it is difficult to change the current sky model or the calibration process to fundamentally solve the problem. However, since we now know that the time window LST03-09 is relatively “clean” in terms of the excess variance, we can “avoid” the excess variance by focusing on this specific time range for future analyses.

Categorizing the excess variance in k-space. Based on observations and simulations, we know that most of the power in cylindrical power spectra is concentrated in the foreground wedge (the region below the 20° delay line in the power spectra). The excess variance is also higher in the wedge region. Our current approach calculates the excess variance per 3h LST bin by averaging over all k values and this does not take into account the k-dependence nature of the excess variance. In a future work, we plan to categorize the excess variance depending on k. This will better address the correlation between the excess variance and its possible causes.

Combining more data. As we discussed in Sect. 4.2, the correlations between the simulated Stokes I from sky models and excess variance are non-negligible but not yet robust, given high p-values from correlation test results. This is partially due to the limited sample size and the night-to-night variation in each LST bin. By combining a greater number of nights, the night-to-night variation in each LST bin will be reduced and the correlation will become more clear (if a correlation indeed exists).

The analysis in this paper shows that the excess variance is more likely to be correlated with the sky-related effects than other effects such as ionospheric effects. In particular, the far and bright sources such as Cas A and Cyg A dominate the effects. The correlation, however, is not yet decisive. By implementing the proposed strategies, we will be able to reduce the level of excess variance and reach deeper limits in the near future.

thumbnail Fig. 14

Excess variance (i.e., the Stokes I and V ratio) as a function of diſſractive scale rdiff (top two rows) and fitted slope β (bottom two rows) at 140 MHz per LST bin for 13 observations with the shaded area indicating the 1 – σ excess variance over 13 observations and all LST bins. The color denotes different LST bins. The ionosphere and excess variance distributions vary from night to night (different data points per LST bin) and also from LST to LST. No strong correlation between the excess variance and the diſſractive scale is found at the current level.

Acknowledgements

The authors would like to thank the anonymous referee and the editor for the comments which helped improve and clarify this manuscript. HG and LVEK would like to acknowledge support from the Centre for Data Science and Systems Complexity (DSSC) at the University of Groningen and a Marie Skłodowska-Curie COFUND grant, no. 754315. AG would like to acknowledge IUCAA, Pune for providing support through the associateship programme. BKG gratefully acknowledges the support from the National Science Foundation through award for HERA (AST-1836019). ITI was supported by the Science and Technology Facilities Council [grant numbers ST/I000976/1 and ST/T000473/1] and the Southeast Physics Network (SEP-Net).

Appendix A Impact of flagging on simulated data

The visibility simulations performed in this work are based on real observations. This implies that the simulations will have the equivalent RFI flagging (on baselines) and uv-coverage as observations. We notice that these can be a disadvantage for the power spectrum estimation of the simulated data: (1) simulations are not contaminated by RFI, hence having extra baselines flagged will lead to a data loss and this might introduce extra power in the power spectra (Offringa et al. 2019); (2) when simulations are sliced into 3h LST bins, the uv-coverage will be limited, as we have seen with the observations. Hence, it may be necessary to flag uv-cells with bad coverage even in the simulations before the power spectrum estimation to optimize the results.

To investigate the impact of RFI flagging from observations and the poor uv-coverage on the simulations, we estimate 3h LST power spectra of simulated visibilities (using the 1416 brightest and A-team sources) applying four different flagging conditions (summarized in Table. A.1): (1) uv-cells not flagged and RFI unflagged; (2) uv-cells flagged and RFI unflagged (the condition we use for the analysis); (3) uv-cells not flagged and RFI flagged; (4) uv-cells flagged and RFI flagged.

The results of power spectra with different flagging conditions are shown in Fig. A.1. The power spectra clearly show that having RFI flagging certainly introduces extra power over the EoR window (bottom left and right in Fig. A.1). Since we are simulating bright sources and their fluxes are known to be smooth in frequency, the resulting power should be constrained in the foreground wedge, especially, below the instrument horizon. Any extra structures, especially above the foreground wedge, are considered to be from effects other than foregrounds. Once the RFI flagging is removed (top left in Fig. A.1), the added power is significantly reduced. However, we see some vertical structures around k ~ 0.13 – 0.15 hcMpc–1 in LST00-03, LST06-09 and LST12-15, the added power comes from a few uv-cells with bad coverage. After the application of uv-cell flagging, we note that the vertical power from the bad uv-coverage is reduced, while the power from foregrounds remains in the foreground wedge. Therefore, we conclude that applying a uv-cell flagging and RFI unflagging (flagging condition 2) is optimal for the power spectrum estimation in this case.

Table A.1

Summary of four different flagging conditions used for testing.

thumbnail Fig. A.1

Median cylindrical Stokes I power spectra of the 13 night simulations with the DI-calibration model (including the 1416 brightest components that account for ~99% of the flux from our sky model) and Α-team sources per LST bin with 4 different flagging conditions. Top left: uv-cells not flagged and RFI unflagged. Top right: uv-cells flagged and RFI unflagged (the condition we use for the analysis). Bottom left: uv-cells not flagged and RFI flagged. Bottom right: uv-cells flagged and RFI flagged. Dashed lines indicate, from bottom to top, 5° (the primary beam), 20° and instrumental horizon delay lines. RFI flagging adds extra power to the EoR window (bottom left and right) and unflagged bad uv-cells add vertical structures in the power spectra (top left). Hence, applying uv-cell flagging and unflagging RFI (top right) is optimal for the power spectrum estimation in this case.

Appendix B Ionospheric phase structure function metrics

The spatial structure of the ionosphere can be described by its power spectrum or its Fourier inverse “phase structure function,” which is defined as follows (van der Tol 2009; Mevius et al. 2016): D(r)= (ϕ(r)ϕ(r+r))2 ,$D\left(r \right) = \left\langle {{{\left({\phi \left({r'} \right) - \phi \left({r' + r} \right)} \right)}^2}} \right\rangle ,$(B.1)

where ϕ(r) is an ionospheric phase at a position r. For Kol-mogorov turbulence, the phase structure function is reduced to: D(r)=(rrdiff)β,$D\left(r \right) = {\left({{r \over {{r_{{\rm{diff}}}}}}} \right)^\beta},$(B.2)

where rdiff is the spatial scale where the phase variance corresponds to 1 rad2, which is known as the diffractive scale (Narayan et al. 1992). For pure Kolmogorov turbulence, β corresponds to 5/3.

In particular, β and rdiff are useful single number metrics for the ionospheric quality. We construct the phase structure function for the 13 night observations and fit for parameters β and rdiff to determine the ionospheric quality per night and 3h LST bin (see Mevius et al. (2016) for details). The phase structure functions per night and 3h LST are shown in Fig. B.1 and the results are summarized in Table. B.1 with the coefficient of determination R2 for each constructed phase structure function to provide the quality of the fit.

Table B.1

Summary of structure function fitted parameters per LST bin for 13 observations.

thumbnail Fig. B.1

Binned phase structure function fits of thirteen observations at 140 MHz for 3h LST bins. The fitted results are superimposed with solid lines in blue.

References

  1. Aarons, J. 1982, Proc. IEEE, 70, 360 [CrossRef] [Google Scholar]
  2. Ali, Z. S., Parsons, A. R., Zheng, H., et al. 2015, ApJ, 809, 61 [NASA ADS] [CrossRef] [Google Scholar]
  3. Asad, K. M. B., Koopmans, L. V. E., Jelić, V., et al. 2015, MNRAS, 451, 3709 [NASA ADS] [CrossRef] [Google Scholar]
  4. Asad, K. M. B., Koopmans, L. V. E., Jelić, V., et al. 2016, MNRAS, 462, 4482 [NASA ADS] [CrossRef] [Google Scholar]
  5. Asad, K. M. B., Koopmans, L. V. E., Jelić, V., et al. 2018, MNRAS, 476, 3051 [NASA ADS] [CrossRef] [Google Scholar]
  6. Barry, N., Hazelton, B., Sullivan, I., Morales, M. F., & Pober, J. C. 2016, MNRAS, 461, 3135 [CrossRef] [Google Scholar]
  7. Barry, N., Wilensky, M., Trott, C. M., et al. 2019, ApJ, 884, 1 [Google Scholar]
  8. Beardsley, A. P., Hazelton, B. J., Sullivan, I. S., et al. 2016, ApJ, 833, 102 [NASA ADS] [CrossRef] [Google Scholar]
  9. Becker, R. H., Fan, X., White, R. L., et al. 2001, AJ, 122, 2850 [NASA ADS] [CrossRef] [Google Scholar]
  10. Bowman, J. D., Cairns, I., Kaplan, D. L., et al. 2013, PASA, 30, e031 [Google Scholar]
  11. Bowman, J. D., Rogers, A. E. E., Monsalve, R. A., Mozdzen, T. J., & Mahesh, N. 2018, Nature, 555, 67 [Google Scholar]
  12. Chapman, E., Zaroubi, S., Abdalla, F. B., et al. 2016, MNRAS, 458, 2928 [NASA ADS] [CrossRef] [Google Scholar]
  13. Cheng, C., Parsons, A. R., Kolopanis, M., et al. 2018, ApJ, 868, 26 [NASA ADS] [CrossRef] [Google Scholar]
  14. Ciardi, B., & Ferrara, A. 2005, SpaCe SCi. Rev., 116, 625 [NASA ADS] [CrossRef] [Google Scholar]
  15. Clément, B., Cuby, J. G., Courbin, F., et al. 2012, A&A, 538, A66 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  16. Cohen, A., Fialkov, A., & Barkana, R. 2018, MNRAS, 478, 2193 [CrossRef] [Google Scholar]
  17. Davies, F. B., Hennawi, J. F., Bañados, E., et al. 2018, ApJ, 864, 142 [NASA ADS] [CrossRef] [Google Scholar]
  18. DeBoer, D. R., Parsons, A. R., Aguirre, J. E., et al. 2017, PASP, 129, 045001 [NASA ADS] [CrossRef] [Google Scholar]
  19. de Gasperin, F., Vink, J., McKean, J. P., et al. 2020, A&A, 635, A150 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  20. Ewall-Wice, A., Dillon, J. S., Liu, A., & Hewitt, J. 2017, MNRAS, 470, 1849 [CrossRef] [Google Scholar]
  21. Ewall-Wice, A., Chang, T. C., Lazio, J., et al. 2018, ApJ, 868, 63 [NASA ADS] [CrossRef] [Google Scholar]
  22. Fan, X., Strauss, M. A., Richards, G. T., et al. 2006, AJ, 131, 1203 [NASA ADS] [CrossRef] [Google Scholar]
  23. Field, G. B. 1958, Proc. IRE, 46, 240 [NASA ADS] [CrossRef] [Google Scholar]
  24. Furlanetto, S. R., Peng Oh, S., & Briggs, F. H. 2006, Phys. Rep., 433, 181 [NASA ADS] [CrossRef] [Google Scholar]
  25. Gehlot, B. 2019, PhD thesis, University of Groningen [Google Scholar]
  26. Greenhill, L. J., & Bernardi, G. 2012, HI Epoch of Reionization Arrays [Google Scholar]
  27. Greig, B., Mesinger, A., Haiman, Z., & Simcoe, R. A. 2016, MNRAS, 466, 4239 [NASA ADS] [Google Scholar]
  28. Greig, B., Mesinger, A., & Bañados, E. 2019, MNRAS, 484, 5094 [NASA ADS] [CrossRef] [Google Scholar]
  29. Hamaker, J. P., Bregman, J. D., & Sault, R. J. 1996, A&AS, 117, 137 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  30. Heinrich, C., & Hu, W. 2021, Phys. Rev. D, 104, 063505 [NASA ADS] [CrossRef] [Google Scholar]
  31. HERA Collaboration (Abdurashidova, Z., et al.) 2022, ApJ, 924, 51 [NASA ADS] [CrossRef] [Google Scholar]
  32. Iliev, I. T., Mellema, G., Pen, U.-L., et al. 2006, MNRAS, 369, 1625 [NASA ADS] [CrossRef] [Google Scholar]
  33. Jelić, V., Zaroubi, S., Labropoulos, P., et al. 2010, MNRAS, 409, 1647 [CrossRef] [Google Scholar]
  34. Jelić, de Bruyn, A. G., Pandey, V. N., et al. 2015, A&A, 583, A137 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  35. Kern, N. S., Parsons, A. R., Dillon, J. S., et al. 2020, ApJ, 888, 70 [NASA ADS] [CrossRef] [Google Scholar]
  36. Kerrigan, J. R., Pober, J. C., Ali, Z. S., et al. 2018, ApJ, 864, 131 [NASA ADS] [CrossRef] [Google Scholar]
  37. Kolopanis, M., Jacobs, D. C., Cheng, C., et al. 2019, ApJ, 883, 133 [NASA ADS] [CrossRef] [Google Scholar]
  38. Koopmans, L. V. E. 2010, ApJ, 718, 963 [NASA ADS] [CrossRef] [Google Scholar]
  39. Koopmans, L. V. E., Pritchard, J., Mellema, G., et al. 2015, The Cosmic Dawn and Epoch of Reionization with the Square Kilometre Array [Google Scholar]
  40. Labropoulos, P., Koopmans, L. V. E., Jelić, V., et al. 2009, ArXiv e-prints, [arXiv:0901.3359] [Google Scholar]
  41. Li, W., Pober, J. C., Barry, N., et al. 2019, ApJ, 887, 141 [NASA ADS] [CrossRef] [Google Scholar]
  42. Loi, S. T., Trott, C. M., Murphy, T., et al. 2015, Radio Sci., 50, 574 [NASA ADS] [CrossRef] [Google Scholar]
  43. Madau, P., Meiksin, A., & Rees, M. J. 1997, ApJ, 475, 429 [NASA ADS] [CrossRef] [Google Scholar]
  44. Mason, C. A., Fontana, A., Treu, T., et al. 2019, MNRAS, 485, 3947 [NASA ADS] [CrossRef] [Google Scholar]
  45. Mellema, G., Iliev, I. T., Pen, U.-L., & Shapiro, P. R. 2006, MNRAS, 372, 679 [NASA ADS] [CrossRef] [Google Scholar]
  46. Mertens, F. G., Ghosh, A., & Koopmans, L. V. E. 2018, MNRAS, 478, 3640 [NASA ADS] [Google Scholar]
  47. Mertens, F. G., Mevius, M., Koopmans, L. V. E., et al. 2020, MNRAS, 493, 1662 [Google Scholar]
  48. Mevius, M., van der Tol, S., Pandey, V. N., et al. 2016, Radio Sci., 51, 927 [Google Scholar]
  49. Mevius, M., Mertens, F., Koopmans, L. V. E., et al. 2021, MNRAS, 509, 3693 [NASA ADS] [CrossRef] [Google Scholar]
  50. Morales, M. F., & Hewitt, J. 2004, ApJ, 615, 7 [NASA ADS] [CrossRef] [Google Scholar]
  51. Morales, M. F., & Wyithe, J. S. B. 2010, ARA&A, 48, 127 [NASA ADS] [CrossRef] [Google Scholar]
  52. Morales, M. F., Hazelton, B., Sullivan, I., & Beardsley, A. 2012, ApJ, 752, 137 [NASA ADS] [CrossRef] [Google Scholar]
  53. Mortlock, D. 2016, Quasars as Probes of Cosmological Reionization, ed. A. Mesinger (Cham: Springer International Publishing), 187 [Google Scholar]
  54. Mouri Sardarabadi, A., & Koopmans, L. V. E. 2018, MNRAS, 483, 5480 [Google Scholar]
  55. Narayan, R., Blandford, R. D., Hewish, A., Lyne, A. G., & Mestel, L. 1992, Philos. Trans. Roy. Soc. Lond. A: Phys. Eng. Sci., 341, 151 [NASA ADS] [CrossRef] [Google Scholar]
  56. Offringa, A. R., van de Gronde, J. J., & Roerdink, J. B. T. M. 2012, A&A, 539 [Google Scholar]
  57. Offringa, A. R., de Bruyn, A. G., Zaroubi, S., et al. 2013, A&A, 549, A11 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  58. Offringa, A. R., McKinley, B., Hurley-Walker, N., et al. 2014, MNRAS, 444, 606 [Google Scholar]
  59. Offringa, A. R., Mertens, F., & Koopmans, L. V. E. 2019, MNRAS, 484, 2866 [CrossRef] [Google Scholar]
  60. Offringa, A. R., Mertens, F., van der Tol, S., et al. 2019, A&A, 631, A12 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  61. Paciga, G., Chang, T.-C., Gupta, Y., et al. 2011, MNRAS, 413, 1174 [NASA ADS] [CrossRef] [Google Scholar]
  62. Paciga, G., Albert, J. G., Bandura, K., et al. 2013, MNRAS, 433, 639 [CrossRef] [Google Scholar]
  63. Pandey, V., Koopmans, L., Tiesinga, E., et al. 2020, ADASS XXIX, ASP Conference Series, 524 [Google Scholar]
  64. Patil, A. H., Yatawatta, S., Zaroubi, S., et al. 2016, MNRAS, 463, 4317 [NASA ADS] [CrossRef] [Google Scholar]
  65. Patil, A. H., Yatawatta, S., Koopmans, L. V. E., et al. 2017, ApJ, 838, 65 [NASA ADS] [CrossRef] [Google Scholar]
  66. Pearson, T. J., & Readhead, A. C. S. 1984, ARA&A, 22, 97 [Google Scholar]
  67. Philip, L., Abdurashidova, Z., Chiang, H., et al. 2018, J. Astron. Instrum., 08 [Google Scholar]
  68. Planck Collaboration XLVII. 2016, A&A, 596, A108 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  69. Planck Collaboration VI. 2020, A&A, 641, A6 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  70. Prasad, P., Huizinga, F., Kooistra, E., et al. 2016, J. Astron. Instr., 5, 1641008 [NASA ADS] [CrossRef] [Google Scholar]
  71. Pritchard, J. R., & Loeb, A. 2012, Rep. Progr. Phys., 75, 086901 [CrossRef] [Google Scholar]
  72. Rufenach, C. L. 1972, J. Geophys. Res., 77, 4761 [NASA ADS] [CrossRef] [Google Scholar]
  73. Scaife, A. M. M., & Heald, G. H. 2012, MNRAS, 423, L30 [Google Scholar]
  74. Schenker, M. A., Robertson, B. E., Ellis, R. S., et al. 2013, ApJ, 768, 196 [Google Scholar]
  75. Shaver, P. A., Windhorst, R. A., Madau, P., & de Bruyn, A. G. 1999, A&A, 345, 380 [Google Scholar]
  76. Singh, S., Subrahmanyan, R., Shankar, N. U., et al. 2017, AJ, 845, L12 [NASA ADS] [CrossRef] [Google Scholar]
  77. Smirnov, O. M., 2011, A&A, 527, A106 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  78. Thekkeppattu, J. N., Subrahmanyan, R., Somashekar, R., et al. 2021, Exp. Astron., velthoven 51, 193 [CrossRef] [Google Scholar]
  79. Thompson, A. R., Moran, J. M., & Swenson, George W. J. 2001, Interferometry Synthesis in Radio Astronomy, 2nd edn. (John Wiley & Sons, Ltd) [CrossRef] [Google Scholar]
  80. Tozzi, P., Madau, P., Meiksin, A., & Rees, M. J. 2000, ApJ, 528, 597 [NASA ADS] [CrossRef] [Google Scholar]
  81. Trott, C. M., & Wayth, R. B. 2016, PASA, 33, e019 [NASA ADS] [CrossRef] [Google Scholar]
  82. van der Tol, S. 2009, PhD thesis, Delft University of Technology [Google Scholar]
  83. van Haarlem, Wise, M. W., Gunst, A. W., et al. 2013, A&A, 556, A2 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  84. Vedantham, H. K., & Koopmans, L. V. E. 2015, MNRAS, 453, 925 [NASA ADS] [CrossRef] [Google Scholar]
  85. Vedantham, H. K., & Koopmans, L. V. E. 2016, MNRAS, 458, 3099 [NASA ADS] [CrossRef] [Google Scholar]
  86. van Velthoven, P. 1990, PhD thesis [Google Scholar]
  87. Wilensky, M. J., Morales, M. F., Hazelton, B. J., et al. 2019, PASP, 131, 114507 [NASA ADS] [CrossRef] [Google Scholar]
  88. Wilensky, M. J., Barry, N., Morales, M. F., Hazelton, B. J., & Byrne, R. 2020, MNRAS, 498, 265-75 [CrossRef] [Google Scholar]
  89. Yatawatta, S., de Bruyn, A. G., Brentjens, M. A., et al. 2013, A&A, 550, A136 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  90. Yatawatta, S. 2011, in 2011 XXXth URSI General Assembly and Scientific Symposium, 1 [Google Scholar]
  91. Yatawatta, S. 2015, MNRAS, 449, 4506 [Google Scholar]
  92. Yatawatta, S. 2016, ArXiv e-prints, [arXiv:1605.09219] [Google Scholar]
  93. Yatawatta, S., de Bruyn, A. G., Brentjens, M. A., et al. 2013, A&A, 550, A136 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]

1

Giant Metrewave Radio Telescope, http://gmrt.ncra.tifr.res.in

2

Low-Frequency Array, http://www.lofar.org

3

Murchison Widefield Array, http://www.mwatelescope.org

4

The Donald C. Backer Precision Array for Probing the Epoch of Reionization, http://eor.berkeley.edu

5

Hydrogen Epoch of Reionization Array, http://reionization.org/

6

The Square Kilometer Array, http://www.skatelescope.org

7

The Large aperture Experiment to detect the Dark Ages, http://www.tauceti.caltech.edu/leda/

8

The Probing Radio Intensity at high ɀ from Marion.

9

The Shaped Antenna measurement of the background RAdio Spectrum.

10

Experiment to Detect the Global EoR Signature.

11

The sky model currently include neither the diffuse emission nor confusion-noise source.

12

The intensity scale of the model is set by the compact source NVSS J011732+892848 (RA = 1h 17m33s, Dec = 89°28′49.4″ in J2000) with an intrinsic flux of 8.1 Jy with 5% accuracy (Mertens et al. 2020).

13

We applied the Bernstein-polynomial gain fits to the sky model, before subtracting it from the data. Mertens et al. (2020) have shown these lead to spectrally smooth model power spectra; hence, any non-smooth spectral gains must be due to effects other than the instrument, possibly numerical or, still, a reflection of an incomplete sky model partly absorbed by the gain. Therefore, non-smooth gains are not the cause of the excess noise, but an indicator that some effects are not accounted for in the data model.

All Tables

Table 1

Thirteen night observational details used for analysis in this paper.

Table 2

Differences between DI- and DD-gain calibrations.

Table 3

Information of three clusters used for DD-calibration gain analysis.

Table 4

Three correlation test results on the simulated Stokes I power from two sky models and the excess variance level.

Table A.1

Summary of four different flagging conditions used for testing.

Table B.1

Summary of structure function fitted parameters per LST bin for 13 observations.

All Figures

thumbnail Fig. 1

Excess variance power spectra ratios (i.e., the Stokes I over Stokes V ratio) for the 13 nights of LOFAR observations after DI and DD calibration and foreground removal (sky model and GPR). The dashed lines indicate, from bottom to top, the 5° (the primary beam), 20°, and instrumental horizon delay lines. The excess variance is larger in the wedge-like region under the dashed lines. Some baselines are flagged in L205852 (k ~ 0.07 hc Mpc–1) and in L253987 (k ~ 0.05 hc Mpc–1).

In the text
thumbnail Fig. 2

Duration of observations in LST for 13 nights. For analyzing the LST-dependence on excess variance, each observation yields three to four 3 h LST slices (in red) and power spectra are estimated for each 3h slice, respectively. The data which do not fully cover a 3 h LST range are discarded (in blue) and are not included in the analysis.

In the text
thumbnail Fig. 3

Distance of Cluster82, Cluster84, and Cluster89 from the NCP.

In the text
thumbnail Fig. 4

Time-averaged DD-gains as a function of frequency from 13 night LOFAR observations (in different colors) in Cluster82 (top row), Cluster84 (middle row), and Cluster89 (bottom row). The calculated time averages are separately plotted for three chosen core stations – CS003HBA1 (left column), CS026HBA1 (middle column), and CS401HBA1 (right column), respectively. The color code denotes different nights and each data point indicates a time average at a fixed frequency and a night. Time-averaged gains are smoother over frequency as the cluster is closer to the NCP (from bottom to top).

In the text
thumbnail Fig. 5

Frequency-averaged DD-gains as a function of time from 13 night LOFAR observations (in different colors) in Cluster82 (top row), Cluster84 (middle row), and Cluster89 (bottom row). The calculated time averages are separately plotted for three chosen core stations – CS003HBA1 (left column), CS026HBA1 (middle column), and CS401HBA1 (right column), respectively. The color code denotes different nights and each data point indicates a frequency average at a fixed time and a night. Frequency-averaged gains fluctuate more rapidly over LST as the cluster is farther away from the NCP (from top to bottom).

In the text
thumbnail Fig. 6

Excess variance as a function of DD-gain variance over time in Cluster84 for 13 nights. The color denotes frequency. Each data point in a fixed night is a gain variance over time at a fixed frequency with the corresponding Stokes I/V ratio. There is no strong correlation between the excess variance and gain variance over time. However, the gain variance has a frequency dependence: higher frequencies tend to have higher gain variances.

In the text
thumbnail Fig. 7

Median value over 13 nights of the ratio (i.e., Stokes I over Stokes V) of the cylindrical power spectra per LST bin. We define this as a cylindrical “excess variance” power spectrum. The dashed lines indicate the 5° (the primary beam; bottom), 20° (middle), and instrumental (top) horizon delay lines, respectively. The excess variance is especially high (>5) in the wedge region below the ~20° delay line in all LST bins. The excess variance has an LST dependence and LST 09-12 has the highest excess power in the wedge region compared to other LST bins.

In the text
thumbnail Fig. 8

LST-dependence of excess variance and two sky models. Top: excess variance averaged over k per night and per LST in orange. Middle: simulated Stokes I cylindrical power spectra averaged over k per night and LST with Cas A and Cyg A in red. Bottom: simulated Stokes I cylindrical power spectra averaged over k per night and LST with the DI-calibration model (including the 1416 brightest components that account for ~99% of the flux from our sky model) and A-team sources in green. Different markers indicate different observations. The difference between nights in simulations mainly comes from the different number of sub-bands per night (see Table 1) and flagging based on uv-cells. The excess variance from observations and the simulated Stokes I power from the two models (in middle and bottom) shows a similar LST-dependence.

In the text
thumbnail Fig. 9

Median cylindrical Stokes I power spectra of the 13 night simulations with two different sky models per LST bin based on the 13 observations including uv-cell flagging. Left: Cas A and Cyg A model. Dashed lines indicate, from bottom to top, 5° (the primary beam), 20° and instrumental horizon delay lines. Right: the DI-calibration model (including the 1416 brightest components that account for ~99% of the flux from our sky model) and Α-team sources. LST03-06 and LST06-09 in both simulations show lower power compared to other LST bins and this trend is consistent with what we have seen with the excess variance in Fig. 7 and the top panel of Fig. 8.

In the text
thumbnail Fig. 10

Correlation between the median simulated Stokes I from two sky models and the median excess variance over LST. Top: correlation between the Cas A and Cyg A model and excess variance over LST. Bottom: correlation between the DI sky model (that accounts for ~99% of the power in the sky model) and Α-team sources and excess variance over LST. Different colors indicate different LST bins. The error bars on each data point indicate the RMS of the simulated Stokes I power and the excess variance between nights per LST bin, respectively (we note that they are not observation errors), to show the night-to-night spread of the data per LST bin. The correlation between the simulated power from the two models and the excess variance show a moderate correlation but it is not strong, due to the limited sample size and night-to-night spread of the data.

In the text
thumbnail Fig. 11

Standard deviation of the residual Stokes I intensities along the frequency direction, after sky-model subtraction and GPR residual foreground removal at 2.5 arcmin resolution incoherently averaged over seven nights per 3 h LST from different regions of (k, k) space – passing only the data under 5° delay line (first column), between 5° and 20° delay lines (second column), between 20° and 90° delay lines (third column) in the power spectra, respectively. All images are in units of Kelvin. As we show in Fig. 7 LST03-06 and LST06-09 once again show lower residual power compared to other LST bins.

In the text
thumbnail Fig. 12

Very wide images after DD-calibration from observation L254116 combining 62 sub-bands with the position of Cas A and Cyg A and the time- and frequency-averaged beam patterns overlaid. From inside to outside, different color (red, blue, green, magenta, and gray) indicate different beam gains, corresponding to –10 dB, –20 dB, –30 dB, –40 dB, and –50 dB. The actual excess variance we see in the power spectra should be the multiplication of the residual Stokes I power and the beam effects. In the sky images, we see the extra power coming especially from the Cas A direction. This power is at its peak in LST00-03, decreasing in LST06-09 and increasing again in LST09-12. This tendency corresponds with what we observed in the LST progression of excess variance and the simulated power of Cas A and Cyg A in the top and middle panels of Fig. 8. The averaged beam rotates over time, as we can see in the images, the –50 dB sidelobe (in gray) sweeps through Cas A and Cyg A from LST00-03 to LST09-12. In the first three LST slices, the sidelobes rotate away from Cas A and Cyg A, at the same time, the power from Cas A and Cyg A decreases. As aresult, the excess variance effect from Cas A and Cyg A decreases from LST00-03 to LST06-09. In LST09-12, although the –50 dB envelope is located in the opposite direction of Cas A and Cyg A, the –40 dB sidelobe (in magenta) has an extended arm towards Cas A direction and the extra power from Cas A direction increases again. This combined effect results in increased power in LST09-12, as we see in Fig. 8.

In the text
thumbnail Fig. 13

Spherically averaged power spectrum estimated from one-night (L246309) Cas A and Cyg A only simulation. Compared the Cas A and Cyg A introduced Stokes I power to the estimated 21 cm signal at k = 0.1 hc Mpc–1, the Cas A and Cyg A power should be reduced by ~99.3% or even higher in the calibration to be able to distinguish the 21 cm signal from the Cas A and Cyg A power.

In the text
thumbnail Fig. 14

Excess variance (i.e., the Stokes I and V ratio) as a function of diſſractive scale rdiff (top two rows) and fitted slope β (bottom two rows) at 140 MHz per LST bin for 13 observations with the shaded area indicating the 1 – σ excess variance over 13 observations and all LST bins. The color denotes different LST bins. The ionosphere and excess variance distributions vary from night to night (different data points per LST bin) and also from LST to LST. No strong correlation between the excess variance and the diſſractive scale is found at the current level.

In the text
thumbnail Fig. A.1

Median cylindrical Stokes I power spectra of the 13 night simulations with the DI-calibration model (including the 1416 brightest components that account for ~99% of the flux from our sky model) and Α-team sources per LST bin with 4 different flagging conditions. Top left: uv-cells not flagged and RFI unflagged. Top right: uv-cells flagged and RFI unflagged (the condition we use for the analysis). Bottom left: uv-cells not flagged and RFI flagged. Bottom right: uv-cells flagged and RFI flagged. Dashed lines indicate, from bottom to top, 5° (the primary beam), 20° and instrumental horizon delay lines. RFI flagging adds extra power to the EoR window (bottom left and right) and unflagged bad uv-cells add vertical structures in the power spectra (top left). Hence, applying uv-cell flagging and unflagging RFI (top right) is optimal for the power spectrum estimation in this case.

In the text
thumbnail Fig. B.1

Binned phase structure function fits of thirteen observations at 140 MHz for 3h LST bins. The fitted results are superimposed with solid lines in blue.

In the text

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