Improved Image Quality over 10' Fields with the ʻImaka Ground-layer Adaptive Optics Experiment

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Published 2018 August 17 © 2018. The American Astronomical Society. All rights reserved.
, , Citation F. N. Abdurrahman et al 2018 AJ 156 100 DOI 10.3847/1538-3881/aad1f2

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1538-3881/156/3/100

Abstract

ʻImaka is a ground-layer adaptive optics (GLAO) demonstrator on the University of Hawaii 2.2 m telescope with a 24' × 18' field of view, nearly an order of magnitude larger than previous AO instruments. In 15 nights of observing with natural guide star asterisms ∼16' in diameter, we measure median AO-off and AO-on empirical FWHMs of 0farcs95 and 0farcs64 in R band, 0farcs81 and 0farcs48 in I band, and 0farcs76 and 0farcs44 at 1 μm. This factor of 1.5–1.7 reduction in the size of the point-spread function (PSF) results from correcting both the atmosphere and telescope tracking errors. The AO-on PSF is uniform out to field positions ∼5' off-axis, with a typical standard deviation in the FWHM of 0farcs018. Images exhibit variation in FWMM by 4.5% across the field, which has been applied as a correction to the aforementioned quantities. The AO-on PSF is also 10× more stable in time compared to the AO-off PSF. In comparing the delivered image quality to proxy measurements, we find that in both AO-off and AO-on data delivered image quality is correlated with ʻImaka's telemetry, with R-band correlation coefficients of 0.68 and 0.70, respectively. At the same wavelength, the data are correlated to DIMM and MASS seeing with coefficients of 0.45 and 0.55, respectively. Our results are an essential first step to implementing facility-class, wide-field GLAO on Maunakea telescopes, enabling new opportunities to study extended astronomical sources, such as deep galaxy fields, nearby galaxies, or star clusters, at high angular resolution.

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1. Introduction

Adaptive optics (AO) is a powerful tool for correcting distortions caused by Earth's atmosphere and delivering diffraction-limited images. Despite the advantages they present, most AO systems have a relatively small field of view (FOV), which can limit the science applications. For first-generation, "classical," single-conjugate adaptive optics (SCAO), which use a single guide star and a single deformable mirror (DM) to correct for turbulence at all heights in a single direction, the correction is limited to regions close to the guide star, resulting in diffraction-limited images spanning only a few arcseconds at optical wavelengths and tens of arcseconds in the near-infrared. Because of this, extended sources such as nearby galaxies or nearby star clusters cannot easily be observed with SCAO in their entirety.

The second generation of AO seeks to mitigate the limitations of SCAO systems in a variety of ways. Multiconjugate adaptive optics (MCAO) systems use multiple DMs to correct atmospheric turbulence in more than one dimension. Correction on fields of 1'–2' with angular resolutions of 80–150 milliarcseconds (mas) have been achieved by MCAO instruments such as GeMS on Gemini (Rigaut et al. 2014) and MAD on the Very Large Telescope (VLT; Marchetti et al. 2007). Multiobject adaptive optics (MOAO) systems that use tomographic reconstruction of several widely separated guide stars (3'–5') to correct small subfields of a few arcseconds in size have achieved image resolutions of ∼150 mas. On-sky demonstrations of MOAO include Raven (Andersen et al. 2012), Canary (Gendron et al. 2011), and the future MOSAIC instrument, which includes a multiobject spectrograph with MOAO correction (Sharples et al. 2000).

Ground-layer adaptive optics (GLAO), first proposed by Rigaut (2002) to improve wide-field imaging for large telescopes, attempts to stretch the limits of AO even further. GLAO uses several guide stars to correct the shared ground-layer turbulence of a large FOV, rather than along a single path through the atmosphere, at the expense of not correcting turbulence at higher altitudes. Previous GLAO demonstrations have shown successful image correction for fields of 1'–4' with resolutions of ∼300 mas, a factor of 2 improvement over the seeing (Baranec et al. 2009; Hart et al. 2010; Orban de Xivry et al. 2016; Arsenault et al. 2017). SAM on the SOAR telescope is a facility GLAO instrument, achieving free-atmosphere limited images in I band with a resolution of ∼500 mas over a 3' FOV (Tokovinin et al. 2016). Similarly, ARGOS on the Large Binocular Telescope (LBT) is expected to improve spatial resolution by a factor of two across a 2' FOV (Gässler et al. 2012). ESO's Adaptive Optics Facility has implemented multiple systems with GLAO correction on VLT telescopes, including GRAAL (7' × 7' in J, H, and K bands) and the wide-field mode on GALACSI-MUSE (1' × 1' in the optical regime; Kuntschner et al. 2012). The potential for even larger fields exists for instruments such as ULTIMATE-SUBARU, which expects uniform point-spread functions (PSFs) with GLAO correction across a field of 20' (Hayano et al. 2014).

ʻImaka is a GLAO demonstrator on the University of Hawaii 2.2 m telescope on Maunakea aimed at quantifying the potential of the site for GLAO. The full ʻImaka 24' × 18' field is an order of magnitude larger than its MCAO predecessors and is the largest GLAO FOV deployed to date. Simulations for ʻImaka predicted a PSF FWHM of ∼300 mas (Chun et al. 2016) in the near-infrared, which is larger than the FWHM delivered by SCAO systems that can reach ∼30 mas at similar wavelengths (Wizinowich et al. 2000). As such, GLAO should be thought of not as a replacement for high-fidelity wave-front correction, small-FOV AO systems, but as a distinct, wide-field, "super-seeing"' system with a different set of advantages and science applications.

The science cases made possible with GLAO improvements are numerous. The wide FOV of ʻImaka allows large, crowded stellar fields to be imaged at higher resolution than normally allowed by the natural seeing. The increased acuity over wider fields can improve astrometric measurements significantly, providing more candidates for reference stars. The observation of large resolved objects such as nearby galaxies with stable, highly corrected PSFs will also allow more detailed study of topics such as galaxy morphology. Besides creating sharper images, the increased encircled energies obtained by GLAO correction produce a higher signal-to-noise ratio (S/N) for an otherwise identical exposure, a significant advantage for imaging as well as spectroscopy. Furthermore, ʻImaka demonstrates the promising possibility of GLAO on a wide variety of telescopes of different sizes on Maunakea, including 10 m class telescopes such as Keck, as well as the forthcoming generation of extremely large telescopes.

Commissioning of ʻImaka began in 2016 October. Analysis of the data from the three subsequent GLAO observing runs in 2017 is presented in this paper. We first present a brief description of the instrument (Section 2). Then we describe the different data sets used and their observations (Section 3), as well as their reduction (Section 4). We then define metrics used to characterize these data, including PSF modeling (Section 5). Analyses of the GLAO performance, including an examination of wavelength dependence and field variability, are presented (Section 6) before we finally discuss the implications of our findings (Section 7).

2. Instrument Description

ʻImaka is a demonstrator of wide-field GLAO with its primary goal of providing an on-sky facility to gain experience using and optimizing the performance of GLAO systems. ʻImaka is mounted at the Cassegrain focus of the University of Hawaii 2.2 m telescope on Maunakea. The instrument is built around a modified Offner optical relay (e.g., Baranec et al. 2007) with input and output focal ratios of f/10 and f/13.25, respectively. A schematic layout of the system is shown in Figure 1. This optical relay provides a flat pupil position just before the second mirror (AOM2), where we place a curvature DM consisting of 36 elements. Note that the DM is conjugate to the telescope primary mirror (i.e., the ground). All powered optical elements in the system are spheres, which simplifies alignment and fabrication. An "exit" port near the relayed focal plane provides mounting points for the wave-front sensors and the science camera.

Figure 1.

Figure 1. Layout of main elements of the ʻImaka instrument. The light from the telescope enters from the top of the diagram. The first powered element (AOM1) creates a pupil image where the deformable mirror (DM) is placed. Following the DM are the Offner secondary (AOM2) and the final concave sphere (AOM3). A large flat (AOM4) folds the beam to a side exit port, where the wave-front sensors and science camera are mounted.

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We place the wave-front sensors and the science camera at the exit port of the instrument, where an oval field 24' × 18'  is passed through the system. We can place up to five Shack–Hartmann wave-front sensors anywhere within this field, but we generally observe fields with guide stars within the periphery of the field to avoid vignetting the science camera. Each wave-front sensor consists of its own optics and camera (Raptor Photonics Kite EMCCD cameras) configured to provide 8 × 8 subapertures with 0farcs4 pixel−1 sampling and a sampling rate of up to 180 Hz. To date, the guide stars used are brighter than R ≤ 8.5 mag, and we achieve a 0 dB rejection bandwidth of about 15 Hz.

The science focal plane is located just behind the wave-front sensors. Image quality from the optical relay was optimized within an approximately 11' × 11'  central field, and the instrument can accommodate a large 11' × 11'  CCD camera or a 7' × 7'  near-infrared H4RG-15 camera. Both of these cameras are still in development, so all images to date were taken with a Finger Lakes Instrumentation ML50100 CCD camera. The camera is mounted slightly off the center of the ʻImaka science field and can be mounted in a variety of positions in order to mosaic a larger FOV. The FLI detector consists of 8176 × 6132, 6 μm pixels with a plate scale of 40 mas pixel−1 at the ʻImaka focal plane. The FOV of a single image from the camera was limited by a bandpass filter mounted to the front of the camera to 5farcm× 4farcm1.

A summary of the instrument specifications is provided in Table 1, and further details can be found in Chun et al. (2016) and references therein.

Table 1.  'Imaka AO Specifications

Telescope University of Hawaii 2.2 m, Maunakea
Deformable mirror  
  Type 36-element, CILAS curvature mirror
  Pupil size 57.5 mm pupil
Wave-front sensors  
  Number up to five Shack–Hartmann WFSs
  Patrol field 24' × 18'
  Pupil sampling × 8 subaperture
  Pixel size 0farcs4/pixel
  Subaperture field 4farcs8/subaperture
Wave-front sensor cameras  
  Type Raptor Photonics Kite EMCCD
  Wavelengths λ = 0.4–0.7 μm
  Quantum efficiency peak 50%
  Readout time 4.2 ms
System  
  Sampling rate up to 180 Hz
  Rejection bandwidth ${f}_{0\mathrm{dB}}\sim 10\mbox{--}15$ Hz

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3. Observations

The data represented in this paper span three ʻImaka observing runs: 2017 January 10–14 UT, 2017 February 13–17 UT, and 2017 May 17–22 UT. Data from 2017 January 13 UT were omitted in the analysis owing to the MASS instrument not running that night. Our analysis combines three different types of observations, described below.6

3.1. ʻImaka Focal Plane Images

The fields' positions and guide star coordinates for each run are given in Table 2. The two fields used are shown in Figure 2. For the 2017 January and 2017 February runs, we observed the Pleiades (Field 1). This field has four guide stars, each positioned around the periphery of the science field. For the 2017 May run, we switched to a second field in the galactic plane (Field 2) in order to observe a higher density of stars. This field differed slightly in that it had its fourth guide star in the center of the field, though this star was not always used in the correction (refer to Table 3). For Field 2, three different guide star and wavefront sensor (WFS) configurations were tested: all four (4WFS) and three outer WFS 0, 1, and 2 (3WFS). For further technical details, refer to Chun et al. (2016).

Figure 2.

Figure 2. Field 1 (top; 2017 January and 2017 February) and Field 2 (bottom; 2017 May). In each field, all guide stars used are marked with wave-front sensor number and R-band brightness. In Field 1, the east Pleiades field is shown in the yellow rectangle labeled RUN 3, while the west Pleiades field is shown in blue and labeled RUN 4. Positions 1 and 2 of Field 2 are shown in yellow and blue, respectively. In both figures, north is up and east is to the left. Background images retrieved from the Two Micron All Sky Survey (Skrutskie et al. 2006).

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Table 2.  Field and Guide Star Positions

Label Name R.A. (J2000) Decl. (J2000) R mag
Field 1 (January, February)
Field center 3h48m58fs0 24°10'00farcs1
WFS 0 HD 23873 3h49m21fs7 24°22'54farcs4 6.6
WFS 1 HD 23763 3h48m29fs6 24°20'48farcs9 6.9
WFS 2 HD 23886 3h49m25fs9 24°14'51farcs7 7.9
WFS 3 HD 2377 3h48m34fs8 24°10'52farcs3 8.7
Field 2 (May)
Field center 19h33m44fs8 7°49'45farcs8
WFS 0 HD 184362 19h33m46fs5 7°55'05farcs0 7.5
WFS 1 HD 184451 19h34m11fs1 7°47'08farcs8 6.9
WFS 2 HD 184244 19h33m12fs1 7°46'22farcs0 7.7
WFS 3 HD 184336 19h33m44fs8 7°49'45farcs7 8.0

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Table 3.  Observing Runs

Date Field PA Filter Frames AO-off AO-on DIMMλ MASSλ DIMM500 MASS500 Comment
(UT)   (deg)     (mas) (mas) (mas) (mas) (mas) (mas)  
2017 Jan 10 1 119 R 20 535 ± 17 313 ± 20 426 ± 7 164 ± 2 450 ± 8 173 ± 2
2017 Jan 11 1 119 R 212 931 ± 20 645 ± 10 658 ± 13 643 ± 18 695 ± 14 680 ± 19
2017 Jan 12 1 119 R 157 906 ± 13 628 ± 7 910 ± 16 701 ± 18 962 ± 17 741 ± 19
2017 Jan 14 (a) 1 119 R 61 621 ± 15 444 ± 14 681 ± 17 560 ± 28 720 ± 18 592 ± 30
2017 Jan 14 (b) 1 29 I 84 790 ± 13 587 ± 11 710 ± 16 414 ± 12 720 ± 18 455 ± 14
2017 Feb 14 1 29 I 56 589 ± 17 433 ± 12 522 ± 12 220 ± 22 574 ± 13 242 ± 24
2017 Feb 15 1 29 I 45 634 ± 42 411 ± 24 561 ± 24 184 ± 5 618 ± 27 202 ± 6
2017 Feb 16 1 29 I 14 896 ± 28 498 ± 17 1006 ± 91 160 ± 8 1106 ± 100 176 ± 9
2017 Feb 17 1 29 1 μm 59 663 ± 52 377 ± 23 445 ± 11 297 ± 21 511 ± 12 341 ± 24
2017 Feb 18 (a) 1 29 R 13 552 ± 22 370 ± 21 220 ± 25 112 ± 6 233 ± 27 118 ± 6
2017 Feb 18 (b) 1 29 I 10 661 ± 66 321 ± 8 193 ± 30 110 ± 6 213 ± 33 121 ± 6
2017 May 17 2 76 I 28 882 ± 14 332 ± 4 368 ± 12 112 ± 3 405 ± 13 124 ± 3 4WFS
2017 May 18 2 120 I 68 587 ± 9 398 ± 2 393 ± 9 208 ± 5 433 ± 9 229 ± 5 3WFS
2017 May 19 2 120 I 109 1078 ± 25 535 ± 2 581 ± 11 399 ± 11 639 ± 12 439 ± 12 3WFS
2017 May 20 2 120 I 55 712 ± 9 4290 ± 2 676 ± 16 261 ± 6 744 ± 18 288 ± 7 3WFS
2017 May 21 2 120 I 109 644 ± 5 368 ± 1 540 ± 12 115 ± 3 595 ± 13 127 ± 4 3WFS

Note. Observation setup, conditions, and results are summarized with nightly averages. Fields and position angle (PA; measured east of north to the positive y-axis of the detector) refer to those outlined in Figure 2 and Table 2. The reported FWHM is the minor FWHM of a Moffat profile. As MASS/DIMM seeing is measured at 500 nm, we present both a converted DIMMλ and MASSλ that are scaled with Equation (8) to match the observation wavelengths, in addition to the raw data in the DIMM500 and MASS500 columns. The nights of 2017 January 14 and 2017 February 18 UT each have two entries, (a) and (b), for the two half-nights in which we observed with two different filters. In the May run, the combination of wave-front sensors changed from all four to only the outer three with different configurations; this change is indicated in the rightmost column.

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In order to quantify the gains of ʻImaka, we made observations both with GLAO correction (AO-on) and with no correction (AO-off). To capture both modes in a range of seeing conditions, we cycled through different modes while taking data (i.e., one image with no correction, one image with GLAO correction, and then back to no correction). Rather than either freezing or resetting when the mode switched from AO-on to AO-off, the DM was set to an average of the last 5–10 s at the beginning of each AO-off exposure. On average, each night produced 36 frames in each mode.

Science images were taken with exposure times of 30–60 s; these times were chosen in order to average over the seeing. We used I-band and R-band Johnson filters (centered at 806 and 658 nm, respectively) and a "long-pass" filter with an effective wavelength of approximately 1 μm. Image position and filter information are listed for each night in Table 3. In addition to our science images, we took dithered sky images throughout each night, as well as twilights at the beginning of each run for use as flat fields.

3.2. ʻImaka Telemetry

In order to evaluate ʻImaka performance, we also recorded the AO system wave-front sensor measurements and DM commands. This data set (the "telemetry") provides a means to independently estimate the uncorrected aberrations, the level of correction, and the atmospheric seeing. The telemetry data are taken concurrently with our science images; however, the total recording time for the telemetry stream is limited to ∼10 s, while the science exposures are 3–6 times longer. The WFS telemetry data are taken without a filter and have an effective wavelength similar to a V+R-band filter.

The telemetry is used to reconstruct the seeing at a range of altitudes using SloDAR techniques (Wilson 2002), although turbulence profiles are not used in this paper. Instead, the telemetry is used to simply derive the integrated, ground-layer and free-atmosphere seeing independently from MASS/DIMM. Telemetry data were acquired with no AO correction and are used to compute the slope covariance matrices and maps. These are global in the sense that the covariances are computed across different wave-front sensors (the cross-covariances), as well as with themselves (the auto-covariances). A full description of the telemetry data and its analysis is described in Lai et al. (2018). The result of the telemetry processing is the estimated seeing for the ground layer and the free atmosphere for both AO-off and AO-on images.

3.3. MASS/DIMM

In addition to our own measurements, we use the seeing reported by the Maunakea Weather Center7 (MKWC). The MKWC reports seeing measured by the Maunakea seeing monitor (MKAM) installed on a 7 m tall tower between the Canada–France–Hawaii telescope and the Gemini-north telescope. MKAM is approximately 150 m north of the UH88'' telescope. The seeing monitor consists of a Multi-aperture Scintillation Sensor (MASS) and a Differential Image Motion Monitor (DIMM; Tokovinin 2002). While the DIMM measures integrated seeing of the whole atmosphere, the MASS generates a profile of seeing at a range of altitudes (0.5, 1, 2, 4, 8, and 16 km). Note that the MKWC MASS data are processed with version v2.047 of the MASS software. However, there are improvements to the MASS data analysis (Lombardi & Sarazin 2015), and we have reprocessed the data using the most recent version of the software (Kornilov 2017). Note that the data reprocessing still uses the MKAM MASS calibrations from 2009. Throughout this work, we will refer to the MASS seeing as the integrated seeing in the entire MASS profile (e.g., from 500 m to 16 km).

Both instruments report seeing at 500 nm throughout the night. Every night of focal plane data has corresponding MASS/DIMM measurements with the exception of 2017 January 13 UT, when the MASS was not working. We exclude this night from the rest of our analysis.

It should be noted that the MASS/DIMM instruments do not necessarily observe the same atmospheric profile as ʻImaka. Ideally, the telemetry's integrated seeing should be comparable to the DIMM, while the free-atmosphere seeing should match the MASS. However, the MASS/DIMM points close to zenith, while we observe at a range of altitudes. The differing paths through the atmosphere may result in different turbulence profiles. Additionally, the instruments are located at different places on the summit of MaunaKea and therefore experience different local seeing (e.g., seeing very close to the ground at the seeing monitor and dome seeing at the UH 2.2 m telescope).

4. Image Reduction

Standard image processing was applied to the science images, including flat-fielding, sky subtraction, and bad-pixel and cosmic-ray rejection. The flat-field image was created from several twilight exposures with different integration times (2–30 s) that were normalized by dividing by the σ-clipped median of all pixels in the image and then combined using a σ-clipped median. In some cases where twilight images were not taken on a given night, the flat generated from the preceding night was used. Sky images were taken periodically through the observing run each night, usually with a total of about 20 frames. Like the flats, all sky images of a given night were combined using a σ-clipping median routine that, along with a dithering procedure, removed any stars from the final combined sky image.

In addition to individual science frames, we created stacked images. For each night, one stacked image was created using the reduced images for each position, control matrix, and filter (e.g., all AO-on images on 2017 May 17 UT taken at I band using the combination of wave-front sensors 0, 1, and 3 were combined to form one image). The frames were matched and had relative astrometric transformations applied before adding them together to create single images, without further correction (e.g., for distortion, differential refraction, etc.). Because these stacked images do not capture the effects of seeing variations or zenith distance that are changing between frames, they are used only to examine the variability in AO correction across the field due to the instrument. As such, data from stacked images are only presented in Section 6.4, on field variability.

5. Image Quality Analysis

After reducing the science images, each frame was run through our star-finding algorithm. Initial FWHM estimates were obtained by eye from the cleaned science images, typically 0farcs4 in AO-on and 1farcs0 in AO-off images. These initial guesses were used in DAOphot's DAOstarfinder (Stetson 1987), to locate stars in the images. The star finder performed two passes with this initial PSF guess, locating sources above four standard deviations of the mean pixel value of the image and updating the FWHM guess accordingly. The images of the Pleiades field yielded about 15 sources each (so few because of the sparseness of the field, the short exposure times, the rejection of saturated sources, and the high S/N needed for the subsequent fitting), while the second, much denser field of the May run had 300–500 sources each.

Once the sources were located, certain cuts were made to the sample of stars. First, stars within 20 pixels of image edges or other stars were removed. Second, saturated stars (defined as anything with a peak above 20,000 ADU) were removed. Finally, we defined a minimum flux threshold for each image. Generally, this cut saved only the brightest 80% of stars in a frame. However, for Field 1, which had few stars to begin with, no flux cut was made.

Once a clean star sample was defined, we characterized the PSF of each star in a given frame using several metrics described below. To further reduce our data, all of our statistics described below were median combined for all stars in a given image, resulting in a single measurement of a given metric for each frame. Thus, each data point in all subsequent plots represents a single frame unless otherwise stated. Note that we did not apply a correction for zenith distance of observations; our FWHM data as a function of airmass fits similarly well to both a constant FWHM and a 3/5 power law, illustrating that no or very little airmass dependence is seen in our data (see the Appendix).

5.1. Nonparametric PSF Models

Before establishing a parametric model for the image plane PSFs, we took a numerical approach to their characterization using three different metrics, described below. Each metric quantifies the PSF shape and size slightly differently; thus, the values vary for the same image and can be seen in Figure 3.

Figure 3.

Figure 3. Cumulative distribution functions illustrating different PSF metrics, including the 50% encircled energy diameter, empirical FWHM, NEA width, and Moffat FWHM. Though they all approach the PSF characterization slightly differently and thus yield different results, we expect them to be somewhat consistent in the range of values measured on a given data set. Top: AO-off. Bottom: AO-on. Note that only I-band data are shown here; the four metrics in other filters demonstrate similar differences.

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Empirical FWHM: Pixels were counted in the vicinity of a star's centroid with ADU counts above half of the maximum pixel value as a brute-force method of calculating a star's FWHM. Assuming that this area is circular, we calculated the corresponding diameter: the empirical FWHM.

Encircled Energy (EE) Diameter: To obtain a more detailed profile of the sources' PSFs, we also calculated EE diameters for our sources. To do this, we created brightness profiles of each source, counting flux contained within a series of concentric annuli centered on the source's centroid. From this profile, we measured the diameter within which 25%, 50%, and 80% of the total flux was enclosed.

Noise Equivalent Area (NEA): An additional way we measure the PSF is an "NEA." A full derivation of the NEA of an arbitrary PSF can be found in King (1983), but simply put, it is the area of a region centered on a star's centroid in which the S/N is unity. This is calculated with a similar method to the EE radius, in which concentric circular regions of increasing size around a star are isolated until reaching an S/N of 1. The NEA of a Gaussian profile, for example, is 4πσ2. For the sake of comparison to PSF measurements that are widths rather than areas, we define the "NEA width" to be the diameter corresponding to a circle with area NEA.

5.2. Parametric PSF Modeling

Though the above metrics provide a good sense of image quality, they are not a complete description of stars' PSFs. These models ignore the shape of the source, which is problematic, as our sources are not radially symmetric. This is particularly apparent in AO-off images, where stars show significant elongation. As such, we parametrically modeled the sources' shape.

We tried a variety of models, including bivariate Gaussian, Lorentz, Moffat, and sinc distributions. Additionally, we tried two-component models, including combinations (e.g., Gaussian + Moffat). For each model, the goodness of fit was quantified with the fraction of variance unexplained:

Equation (1)

This value was calculated in a box centered on the star with a side length of about 4 times the FWHM. Using this quantity to compare different models, we found that for AO-off images the best model was a single-component elliptical Moffat profile. We had predicted that for the AO-on images a two-component elliptical Moffat would be ideal: a narrower, brighter component representing the corrected portion of the final image, and a dimmer component with a size similar to that of the AO-off image, representing the uncorrected portion of the PSF. However, as even a carefully constrained double-component model showed no improvement in the FVU, we ultimately chose a single-component Moffat for AO-on images as well.

The model for a 2D elliptical Moffat with rotation is defined as

Equation (2)

Equation (3)

Equation (4)

where the star's centroid is given by xo and yo, the amplitude is a, β describes the slope of the PSF, αx and αy describe its width, and ϕ is the rotation of the major axis from horizontal. The data were fit with a Levenberg–Marquardt algorithm and least-squares statistic, with 3σ outliers rejected iteratively over two passes. The corresponding FWHM θ is calculated as

Equation (5)

Note that unless otherwise indicated, the Moffat minor FWHM will be used to describe PSF size in further analyses in order to remove the contribution of telescope jitter apparent in the AO-off images.

The quality of the model fit is illustrated in Figure 4, which shows a radial profile of a AO-off and AO-on PSF and the best-fit Moffat profile along the minor axis. There are small discrepancies between the observed and model PSF, particularly in the 2D residuals (Figure 5). The distinct high-order structure evident in the residuals is likely due to the Moffat fitting with a single exponent in the presence of jitter, since the PSF profile follows a different power law along the narrow axis than the elongated one. Static aberrations are calibrated out by optimizing the image quality on artificial sources and recording the centroid offsets on the wave-front sensors, so they are likely not the cause of this residual structure in the PSF. However, the telescope environment may introduce differential aberrations on the various wave-front sensors, or some poorly controlled mirror modes could introduce such a pattern once the loop is closed and noise is injected into the system. Table 4 compares the result of the Moffat fit, specifically, the rms of the minor and major FWHM to the previously described metrics.

Figure 4.

Figure 4. Radial profiles along the minor axis of PSFs in AO-off (blue) and AO-on (red) images, shown with linear (top) and logarithmic (bottom) y-axes. In each case, the image data are represented by circles, and the best-fit model is shown as a solid line. Both PSFs came from the median-sized star in stacked images from 2017 May 20 UT and are representative of most of our data.

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Figure 5.

Figure 5. Best-fit PSF model composed of a single-component, elliptical Moffat for the AO-off (left column) and AO-on (right column) data. The original image (top), the best-fit model (middle), and the residuals (bottom) are shown over the fitting box of 2farcs56 × 2farcs56. Color-bar units are in ADU. Image samples were taken from stacked images on 2017 May 20 UT, a night with typical seeing conditions and performance. Note that the color scale is different between AO-off and AO-on to highlight PSF structure, so the differences in S/N between AO-off and AO-on are not represented here.

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Table 4.  PSF Size Improvement

Metric AO-off AO-on Change
  (arcsec) (arcsec)  
  R Band (658 nm)    
Moffat FWHM (min) 0.857 ± 0.014 0.589 ± 0.012 37%
Moffat FWHM (maj) 1.097 ± 0.016 0.639 ± 0.013 53%
Empirical FWHM 1.008 ± 0.015 0.666 ± 0.013 41%
NEA width 1.000 ± 0.014 0.736 ± 0.015 30%
50% EE diameter 1.221 ± 0.030 0.899 ± 0.031 30%
80% EE diameter 2.101 ± 0.026 1.790 ± 0.032 16%
  I Band (806 nm)
Moffat FWHM (min) 0.761 ± 0.059 0.450 ± 0.007 51%
Moffat FWHM (maj) 1.089 ± 0.070 0.499 ± 0.008 74%
Empirical FWHM 0.845 ± 0.012 0.498 ± 0.008 52%
NEA width 0.822 ± 0.011 0.565 ± 0.008 37%
50% EE diameter 1.255 ± 0.020 0.985 ± 0.023 24%
80% EE diameter 1.799 ± 0.020 1.435 ± 0.014 22%
  1000 nm
Moffat FWHM (min) 0.663 ± 0.037 0.377 ± 0.025 55%
Moffat FWHM (maj) 0.868 ± 0.047 0.416 ± 0.023 70%
Empirical FWHM 0.796 ± 0.036 0.456 ± 0.023 54%
NEA width 0.715 ± 0.038 0.516 ± 0.028 32%
50% EE diameter 0.849 ± 0.020 0.682 ± 0.027 22%
80% EE diameter 1.468 ± 0.031 1.304 ± 0.035 12%

Note. Mean PSF sizes by several different metrics, in the AO-off and AO-on. All values are give in arcseconds. Reported errors are the uncertainty in the mean. The data have been divided between observation filters.

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The seeing-limited AO-off images are well described by a Moffat profile with a median β ≃ 4.8, which is slightly above the β of roughly 3–4 typically measured in astronomical images (Saglia et al. 1993). Additionally, they show relatively little dependence on conditions or FWHM, as expected (Figure 6). For the AO-on images, there is a correlation between β and FWHM.

Figure 6.

Figure 6. Comparisons of the slope parameter β in the Moffat profile to the minor FWHM of the same source. The data show each night of Run 3 in a different color, with each data point representing the median value PSF for a single frame. Points without error bars have uncertainties smaller than the marker size. Left: AO-off (median β = 4.82). Right: AO-on (median β = 2.27).

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5.3. Wavelength Conversion

As previously stated in Section 3, the data comprising our observations were taken through three different filters (details in Table 3). For ease of comparison, the MASS/DIMM data (which are observed at 500 nm) are converted to the wavelength of the corresponding ʻImaka science images. The telemetry data have been similarly converted. The data are converted in the following way.

For a given wavelength λ, the Fried parameter describing the amount of wave-front distortion due to atmospheric turbulence scales as

Equation (6)

To scale a given seeing measurement θobs observed at a wavelength, λobs, we assume an infinite outer scale and that the seeing measurement is proportional to the ratio of the imaging wavelength and the Fried parameter, which gives

Equation (7)

Equation (8)

where θconv is the seeing scaled to a wavelength λconv.

6. Results

6.1. GLAO Performance

The simplest analysis that can be done to characterize the GLAO performance is to compare the FWHM in AO-off images to that in AO-on images, as shown in Figure 7. The FWHM along the minor axis decreases from 0farcs76 in the AO-off case to 0farcs45 with AO correction in I band, a change of 51%. Changes in all other PSF size metrics at all observed wavelengths are given in Table 4 and show roughly consistent improvements.

Figure 7.

Figure 7. Comparison of the FWHM in AO-off (blue) and AO-on (red) images. Minor FWHM is shown with solid lines, and major FWHM with dashed lines. Data are divided between I band (left) and R band (right).

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Though already showing a fair amount of correction, this comparison does not capture the full impact of the instrument. As was visible in Figure 5, a change occurs not only in the PSF size but in its shape as well. Static and dynamic aberrations within the telescope and instrument are also corrected by the GLAO system. As noted above, the static aberrations are removed in the AO-off images by applying average voltages to the DM during AO-off images. The correction of the PSF elongation, caused predominately by telescope jitter, is readily seen in the images in Figure 5. AO-off images show elongation in one direction by a factor of ∼1.3. We attribute this elongation to telescope jitter, as it is generally oriented along the east–west direction (i.e., R.A. drive of the telescope). The elongation could be caused by a combination of astigmatism and focus if the DM voltages used for AO-off images were not averaged for a sufficiently long period. However, this effect would give rise to a random direction and amplitude to the image elongation. Since the direction of the PSF elongation is constant over many hours, its unlikely that a static aberration from the DM shape during AO-off images is not the dominant source of elongation. Regardless, elongation is well corrected by the AO system and is nearly nonexistent in the AO-on images. This stark difference can be seen in Figure 8, which shows the elongation parameter:

Equation (9)

The median value of the elongation decreases from 1.34 to 1.08. This residual elongation of 8% is consistent with the plate-scale variation in the ʻImaka design, which is roughly 8% in the east–west direction. Even more, the AO-on elongation values demonstrate substantially less spread than the AO-off values, with standard deviations of 0.28 and 0.35, respectively.

Figure 8.

Figure 8. Comparison of the elongation (derived from the Moffat fit and defined by Equation (9)) of PSFs in AO-off (blue) and AO-on (red) images. The median value of each distribution is indicated by the vertical dashed line in the corresponding color: 1.34 for AO-off and 1.08 in AO-on. The elongation in the closed-loop images is consistent with the 8% plate-scale variation in the optical design.

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In addition to changes in FWHM, we can use our other PSF metrics to quantify ʻImaka's gains. As seen in Table 4, the AO-on/AO-off change in the 50% EE diameter is greater than the same change in the 80% diameter (e.g., in R band, the improvements in 50% EE and 80% EE are 24% and 16%, respectively). The relatively low change in the 80% diameter is indicative of the less substantial correction the system makes to the extended halo. The radius in which any correction of the PSF is possible for a given AO system is set by the number of actuators in the DM. ʻImaka's current DM has 36 actuators; increasing this number could potentially increase the radius of its AO correction, and subsequently increase this amount of correction for the higher encircled energies.

The improvement in our final metric, NEA, is shown in Figure 9. Note that unlike other metrics and the representation of NEA previously, this figure reports NEA as an area; this representation is useful in addition to the NEA width because photometric precision scales with NEA, while astrometric precision scales with NEA1/2. The NEA decreases from 1.96 square arcseconds to 0.89 in I band, a change of over a factor of two.

Figure 9.

Figure 9. Change in NEA between AO-off (blue) and AO-on (red) images across all nights, shown as normalized probability distribution functions. Median values of both distributions are designated by vertical dashed lines. The data are divided into I band (left) and R band (right).

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Besides improvements in individual PSFs, AO-on images demonstrate higher stability throughout each night of observing. The spread of minor FWHM for each night in both AO-off and AO-on images can be seen in Figure 10. Regardless of seeing conditions for a given night, there is noticeably more variation in the size of AO-off PSFs than those of the AO-on images. This effect is particularly apparent when the free atmosphere is weak. This is well illustrated in the May run, where the night-averaged standard deviation of FWHM decreases from 0farcs59 to 0farcs05, a change of more than an order of magnitude. In contrast, when the total seeing is dominated by poor free-atmosphere seeing (e.g., Run 1), the PSF variability even in GLAO mode is more pronounced. This trend can also be seen with more detail in Figure 16, where the same data are shown with MASS/DIMM data over time for each night. Generally, even when the ground-layer seeing has more variation over the course of the night than the free atmosphere, the AO-on FWHM remains more stable than in the AO-off case.

Figure 10.

Figure 10. Comparison of the PSF stability between AO-off (blue) and AO-on (red) across all nights. For each data point, the median value of the empirical FWHM is represented by the center line, with a box surrounding it and spanning the second and third quartiles of the data. The full range of data is shown by the extended lines. Shaded regions refer to the observation wavelength: R band in gray, 1000 nm in yellow, and I band is unshaded.

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6.2. Comparisons to Seeing

The comparison between AO-off and AO-on images already begins to characterize the gains from GLAO. However, a more objective indicator of success would be to compare the GLAO PSFs to the seeing above the ground layer using MASS/DIMM measurements described in Section 3.3. First, we compare the FWHM of the focal plane images to the contemporaneous MASS/DIMM seeing in Figure 11, where the top and bottom panels show the correlations between AO-off images and DIMM and between AO-on images and MASS, respectively.

Figure 11.

Figure 11. Correlations between focal plane data and MASS/DIMM. Top: correlation between AO-off images and DIMM seeing, matched by observation time. Bottom: correlation between AO-on images and MASS. In each panel, data points are shown with a line of best fit in the same color, with the corresponding correlation coefficient C reported. A dashed black line in each panel shows a 1:1 correlation. The AO-on/AO-off data are separated by filter, with I band on the left and R band on the right. The MASS/DIMM data are converted to match the wavelength of the ʻImaka image data using Equation (8). Note that the I-band and R-band data sets were taken on different sets of nights with different seeing conditions.

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Assuming accurate measurements by the MASS/DIMM instruments and no error in our correction, the DIMM should show some correspondence with the AO-off image FWHM, and similarly the MASS should correspond to the AO-on data. To examine this relationship, we looked at the correlation between the focal plane data, telemetry, and MASS/DIMM seeing. Across all nights, we calculated the correlation coefficient for six combinations: three in the total atmosphere regime (AO-off vs. free-atmosphere telemetry, AO-off vs. DIMM, integrated seeing telemetry vs. DIMM) and three in the free-atmosphere regime (AO-on vs. integrated seeing telemetry, AO-on vs. MASS, free-atmosphere seeing telemetry vs. MASS). In the case of AO-on images, we see good correlation with the MASS, with a correlation coefficient of 0.46 in I band and 0.52 in R band. These correlations are shown in Figure 11. The image data are similarly well correlated with ʻImaka's telemetry in I and R band, though some discrepancies occur at 1000 nm. We note that the amount of data taken in this filter is small, so the lack of correlations here may not be significant. A full list of correlation coefficients is presented in Table 5.

Table 5.  Correlations Coefficients between Data and Seeing

  Total Atmosphere Free Atmosphere
  (AO-off/DIMM) (AO-on/MASS)
  R Band (658 nm)
Focal plane versus telemetry 0.68 0.70
Focal plane versus MASS/DIMM 0.45 0.52
Telemetry versus MASS/DIMM 0.35 0.47
  I Band (806 nm)
Focal plane versus telemetry 0.33 0.36
Focal plane versus MASS/DIMM 0.32 0.46
Telemetry versus MASS/DIMM −0.10 0.23
  1000 nm
Focal plane versus telemetry 0.15 0.43
Focal plane versus MASS/DIMM −0.02 0.14
Telemetry versus MASS/DIMM −0.23 0.27

Note. Correlation coefficients for 'Imaka image data, 'Imaka telemetry, and MASS/DIMM seeing in both the total and free-atmosphere cases. Telemetry and MASS/DIMM data have been converted to the matching observation wavelength with Equation (8).

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Although the AO-on images are correlated with the MASS seeing, there is a distinct offset between their cumulative distributions, with the MASS seeing being smaller than the AO-on FWHM. One limiting factor in the agreement is the apparent floor in the AO-on images at approximately 0farcs3. Across all analyses, our GLAO PSF sizes generally do not go below this minimum even when the seeing predicted by the MASS does drop below 0farcs3. This limitation is likely due to systematic effects (e.g., static aberrations, internal seeing), which the low-order system (due to a relative lack of DM actuators and the low bandwidth of our wave-front sensor cameras) cannot correct.

As mentioned in Section 3.3, comparisons to MASS/DIMM are also limited by the fact that they are not observing along the same lines of sight through the atmosphere. To compensate for this, we compare the image quality to our estimates of the integrated and free-atmosphere seeing derived from our telemetry measurements. These have the advantage that these data are synchronized with the images. Figure 12 compares the science image PSF FWHM to both the telemetry measured by ʻImaka and the seeing measured by the MASS/DIMM. Median values and standard deviations are given for all these data sets in Table 6.

Figure 12.

Figure 12. Cumulative distribution functions comparing image plane, telemetry, and MASS/DIMM data. The top panels show values associated with the total atmosphere: telemetry and DIMM seeing; these are compared to the AO-off image plane PSF size. The bottom panels show the free-atmosphere case: the telemetry case is for all turbulence above ∼600 m, along with MASS and AO-on image plane PSF size. The AO-on/AO-off data are separated by filter, with I band on the left and R band on the right. The MASS/DIMM and telemetry, taken from nights that corresponded to each set of observation data, are converted to match the wavelength of the ʻImaka image data using Equation (8). Note that the I-band and R-band data sets were taken on different sets of nights with different seeing conditions.

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Table 6.  Comparison of Image Quality with Seeing Estimates

  Total Atm. Free Atm. Change
  or AO-off or AO-on  
  (arcsec) (arcsec)  
  R Band (658 nm)    
'Imaka images 0.857 ± 0.014 0.589 ± 0.012 37%
'Imaka telemetry 0.854 ± 0.014 0.665 ± 0.012 25%
MASS/DIMM 0.728 ± 0.011 0.616 ± 0.013 17%
  I Band (806 nm)    
'Imaka images 0.761 ± 0.059 0.45 ± 0.007 51%
'Imaka telemetry 0.572 ± 0.012 0.401 ± 0.009 35%
MASS/DIMM 0.567 ± 0.007 0.253 ± 0.006 76%
  1000 nm    
'Imaka images 0.663 ± 0.037 0.377 ± 0.025 55%
'Imaka telemetry 0.563 ± 0.023 0.453 ± 0.023 22%
MASS/DIMM 0.445 ± 0.011 0.297 ± 0.021 40%

Note. Mean PSF sizes by three different measurements, observing the total integrated atmosphere (from top to bottom: AO-off images, AO-off telemetry, MASS integrals) and the free atmosphere (AO-on images, AO-on telemetry, DIMM integrals). All values are given in arcseconds. Reported uncertainties are the error on the mean. The data are separated by observation wavelength of the 'Imaka images, but all data are shown at their original wavelengths.

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Figure 12 shows the cumulative distributions for the image FWHM and the seeing from the MASS/DIMM and the ʻImaka telemetry. There is a mix of agreement and disagreement between the distributions of seeing and image FWHM. During the nights when we observed in I band, both the AO-on and AO-off images' FWHM distributions were shifted to values larger than the I-band-converted MASS/DIMM seeing and telemetry-derived seeing. In these cases the distribution of MASS seeing values is significantly lower than either the telemetry-derived free-atmosphere seeing or the AO-on image FWHM. On the other hand, on nights when we observed in R band, the AO-off image FWHMs are smaller than the telemetry seeing but worse than the MASS/DIMM seeing, but the AO-on image FWHMs are comparable or better than the MASS or telemetry-derived free-atmosphere seeing.

Some of this difference could come from the fact that the I-band and R-band nights had quite different seeing conditions. During most of the nights when we observed in I band, the free-atmosphere seeing was weak, and both the MASS seeing and DIMM seeing are better than their corresponding image FWHMs. During the R-band nights, the total seeing was dominated by large free-atmosphere seeing. Here, the MASS seeing cumulative distribution function (CDF) and AO-on image CDF are similar for the better free-atmosphere seeing but skewed to values larger than the AO-on image FWHM CDF in the poorer free-atmosphere seeing conditions. Together, the I-band and R-band AO-on data suggest that we have an instrumental floor that prevents GLAO images of better than about 0farcs3. Alternatively, the data may be indicating that the MASS underestimates the free-atmosphere seeing under good seeing conditions, as seen in Lombardi & Sarazin (2015).

For the telemetry data the shapes of the distribution functions are similar in all cases to the distributions for the image FWHM, but with fixed offsets between them. One possibility is that the effective wavelength of the wave-front sensors changes between the observed fields. All of the R-band data were taken on the Pleiades field, where the guide stars are generally bluer than the guide stars in the other fields. Since we assume a wavelength of 0.7 μm for the WFSs, we may be overestimating our seeing estimates in the Pleiades field (e.g., R-band data). Alternative explanations could be an effect that happens on longer timescales, such that it is seen in the 30–45 s science camera exposures but not in the 15 s telemetry exposures. Additionally, if the dome seeing consists of mostly high frequencies (which the AO system cannot correct for), these residual wave-front aberrations could contribute to a broadening of the wings of the PSF, in turn slightly enlarging the FWHM.

6.3. Wavelength Dependence

We can examine the wavelength dependence of GLAO correction by plotting the raw FWHM values at different wavelengths, as shown in Figure 13. Ideally, we would simply look at how FWHM varies with wavelength. However, because the observations in the different filters were done over different nights and over a wide range of observing conditions, direct comparisons cannot be made from night to night. For this reason, we present each data set with the MASS/DIMM seeing measurements for the corresponding times, converted from 500 nm to the relevant wavelength. As in previous figures, we see an offset between AO-off and DIMM, as well as between AO-on and MASS. Despite this discrepancy, at each wavelength there is a clear improvement between AO-off and AO-on, sometimes larger than the difference between DIMM and MASS. Though we do not yet have enough data in consistent seeing conditions to conclude anything about the specific dependence of GLAO correction on wavelength, we can already see that ʻImaka achieves substantial correction at all currently observed wavelengths.

Figure 13.

Figure 13. Wavelength dependence of PSF size shown here as a minor Moffat FWHM for AO-off (blue) and AO-on (red) images for all nights, with no wavelength conversion applied. Each set is shown next to the MASS (orange) and DIMM (purple) seeing measurements for the same observation times. As the MASS/DIMM data are initially measured at 500 nm, their values are presented here scaled to the wavelength of the corresponding ʻImaka data points. Each box represents the mean value with a solid line and the second and third quartiles with a shaded region. We note that the R-band and I-band points are from an average of ≥5 nights, while the 1 μm point is from only one night (refer to Table 3 for observation details).

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6.4. Field Variability

From simulations the GLAO PSF is predicted to be quite uniform across the field. However, as GLAO is deployed over wider and wider fields, it is important to ensure that the instrumental PSF quality does not suffer with increasing field size. The left panel of Figure 14 shows the FWHM of each star as a function of position in the stacked AO-on image from 2017 May 19 UT (chosen because its seeing conditions were typical of the run), with the location of guide stars marked in green. To better view any global trends across the field, these data had outliers removed through an iterative sigma-clipping routine, rejecting points more discrepant than 3σ from the median, with five iterations.

Figure 14.

Figure 14. FWHM of individual stars in a stacked image of all AO-on frames from 2017 May 18 UT. Left: original data, showing the variability of the PSF across the science field. Right: same data as in the left panel, but after subtraction of the best-fit plane, with the median data point from the left (0farcs40) added to all points for comparison purposes. Wave-front sensors' positions relative to the science frame are marked in green, and WFS1 is the brightest guide star. The data were taken at I band with no wavelength conversion applied. By visual inspection, the field on the left shows more structure in its variability, with a strong gradient in FWHM increasing to the bottom left. This global pattern in the variability is largely removed in the right panel. Between the two figures, the range of FWHM decreases from 0farcs201 on the left to 0farcs110 on the right.

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The dominant field variation is a gradient in FWHM, with PSFs increasing in size toward the east side of the field. In single guide star AO, the expectation is for the PSF quality to improve closer to the guide star. The trend visible here is not well correlated to the distance to the field center or to any single guide star. The trend is repeated over multiple nights and appears fixed to the sky, as we describe in more detail below.

We used several methods of quantifying the global variation. First, the data shown in the left panel of Figure 14 were fit in three dimensions (x, y, and FWHM) to a plane. The best-fit plane is defined by two quantities. The first, ϕ, is the position angle of the plane's normal vector projected onto the focal plane and measured east of north in degrees. The second is the gradient, which measures the spatial change of FWHM in arcseconds per arcminute. The right panel of Figure 14 shows the residual FWHM after subtraction of the best-fit plane for the stacked image on 2017 May 19 UT, with an offset of 0farcs44 added for the purpose of comparison. In addition to these parameters, we calculated the range of FWHM values before and after the plane removal (${\rm{\Delta }}{\mathrm{FWHM}}_{i}$ and ${\rm{\Delta }}{\mathrm{FWHM}}_{f}$).

Figure 15.

Figure 15. PSF FWHM vs. airmass for each night. Each data point (black) represents the median value of all sources in a frame (AO-on minor FWHM). The data were fit to two models: a constant FWHM (red solid line) and a 3/5 power law (blue dashed line). The corresponding reduced χ2 for both fits are reported in matching colors.

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As seen in Figure 14, though some faint, high-order structure appears to remain, the variation decreases from the left to the right panels substantially. Averaged over the five nights of the May run, the range decreases from 0farcs145 to 0farcs082. Finally, the average variation of FWHM across the best-fit planes in the direction of greatest change is 0farcs0086 per arcminute of the field.

To justify the removal of the fitted plane, the variability would have to be attributed to an instrumental effect, such as a tilt in the CCD relative to the incoming beam. To check whether the planar variability could be due to an atmospheric effect, similar plane fits were generated for each individual frame on the same night. On a frame-by-frame basis for all images taken on 2017 May 18 UT, neither the direction nor the gradient showed significant correlation to time, ground-layer seeing, wind speed or direction, or zenith angle of the telescope (a potential cause of flexure in the instrument). Based on the lack of any trends in these analyses, we conclude that the field variability of the FWHM is dependent on an instrumental effect such as misalignment, which will be addressed in the future.

Further evidence for an instrumental origin of the PSF field variability comes from the stability of the plane over multiple nights. The stacked AO-on images from each night of the 2017 May run were fit with a plane in the same manner as above, and results are listed in Table 7. The plane parameters ϕ and gradient are given, along with ΔFWHMi and ΔFWHMf. The uncertainties in angles were generated using a full sample bootstrap with replacement routine in the fit. In order to generalize this effect, we report 4.5% as the typical variation in FWHM across the field, calculated as the mean of each night's percent change from the median to the minimum point. As such, we can tentatively apply a correction of 4.5% to any focal plane PSF size measurements owing to field variability.

Table 7.  Nightly Variability Plane Fit for Run 3

Date ${\rm{\Delta }}{\mathrm{FWHM}}_{i}$ ${\rm{\Delta }}{\mathrm{FWHM}}_{f}$ Direction ϕ Gradient
(UT) (arcsec) (arcsec) (deg) (arcsec/arcmin)
2017 May 17 0.128 0.032 153.4 ± 6.0 (16.6 ± 0.2) × 10−3
2017 May 18 0.201 0.110 97.0 ± 9.7 (8.8 ± 0.1) × 10−3
2017 May 19 0.104 0.091 95.8 ± 9.7 (8.2 ± 0.1) × 10−3
2017 May 20 0.115 0.086 86.0 ± 14.5 (5.0 ± 0.1) × 10−3
2017 May 21 0.178 0.092 92.3 ± 31.3 (4.2 ± 0.1) × 10−3

Note. For each night of the May run, the mean range of FWHM values of all stars in AO-on images is given for both before (${\rm{\Delta }}{\mathrm{FWHM}}_{i}$) and after (ΔFWHMf) the removal of a best-fit plane. The value ϕ represents the direction of the best-fit plane (in degrees, east of north with respect to the detector), while the gradient describes the variation in arcseconds per arcminute of the plane.

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The variation in the data of Table 7 may be explained by adjustments made to the instrument between nights. For example, the science camera was removed and rotated by 45° between 2017 May 17 UT and 2017 May 18 UT, corresponding to the large change in the direction of variation. Also, between 2017 May 19 and 20, the camera was taken off and returned to the same position. The constant direction with different inclination suggests that after remounting the camera, we modified the camera tilt slightly. Though not all the changes between nights can be explained with camera changes, these data do present us with potential experiments we can conduct in the future in order to understand the source of this aberration.

It should be noted that the entirety of this variability analysis comprises only AO-on images. The gradient apparent in these images is not seen in AO-off frames, as the image quality is too poor to detect the small change in the FWHM over the FOV. Any attempts at fitting the variability had uncertainties too large to provide valuable insight, so they were omitted from this analysis.

7. Discussion

The results of our three commissioning runs already show the value of ʻImaka and GLAO and the science cases it makes possible. From the size of the field alone, the potential to obtain sharp images of extended sources or large, crowded fields is apparent. Across all nights, our science images display an improvement in FWHM of up to a factor of 1.8, depending on the metric used (summarized in Table 4). The median (I-band) minor FWHM across all nights of 0farcs45 ± 0farcs03 is consistent with Monte Carlo simulations for ʻImaka, which predicted FWHM in the same band of approximately 0farcs45–0farcs50 within the central 6farcm5 (Chun et al. 2014). The range in improvement comes from the difference in how each metric quantifies the shape of the PSF and can be most simply summarized by looking at the change in minor and major FWHM of the Moffat profile (0farcs72–0farcs49 and 1farcs00–0farcs52, respectively). The differences along the two axes in AO-off images are indicative of significant elongation, likely due to telescope jitter, which is almost entirely removed in AO-on images, where the median ratio of major to minor FWHM decreases from 1.34 to 1.08. This highlights the value of a GLAO system in cleaning up telescope and instrumental artifacts that would otherwise reduce image quality in "seeing-limited" data.

As an alternative metric, the radius of 50% EE decreased from 1farcs26 to 0farcs99 in I band. The decrease of 50% EE radius by a factor of 1.3 corresponds to increasing the depth of observable stars by approximately 0.9 mag at a given exposure time, yielding larger samples of stars in a given field. This is particularly advantageous for high-precision astrometry and photometry, where the precision of a measurement scales with the square root of the number of reference stars used.

Besides the increased number of observable objects, the improvement in individual PSFs allows for other opportunities. Photometric precision, for example, scales with NEA, which ʻImaka has improved from 1.96 to 0.89 arcsec2 (I band), a change of more than a factor of 2. Astrometric precision is also improved by a more concentrated PSF, scaling with the square root of NEA (or what we term the NEA width).

In addition to improving individual PSFs, AO-on images from ʻImaka demonstrate improved stability in the FWHM over time and through varying seeing conditions. This effect is most clearly seen in the five nights of the May run, where the nightly standard deviation of FWHM went down from 0farcs59 in AO-off images to 0farcs05 in AO-on images, a change of nearly an order of magnitude. These improvements greatly aid spectroscopic observation. Besides the fact that increased EE yields a higher S/N for a given exposure time, the stability of the PSF size allows for optimized slit width selection. This optimization in turn allows for maximum spectral resolution in an observing run. Assume, for example, that the ratio of maximum FWHM in a night with AO-off and AO-on is ʻImaka's average of 1.6, as previously reported. A decrease in the slit width by this amount would improve the spectral resolution by nearly a factor of 1.6. In addition, since the GLAO PSF is more stable spatially and temporally, there is the possibility to decrease the slit width further.

Furthermore, ʻImaka has demonstrated an amount of correction that could be the difference between an unusable night of observing and a usable night. This is a major benefit of GLAO observing; Andersen et al. (2006) demonstrated in simulations that at the Cerro Pachon site in Chile, a GLAO system would improve an observatory's efficiency by up to 40% by increasing the percentage of the "best seeing-limited image quality nights" from 20% to about 70%. As is visible in Figure 16, sporadic changes in seeing are minimized by ʻImaka, in addition to the seeing being significantly decreased. Eliminating nights unusable because of bad seeing would increase the science output of any facility, an advantage for all types of observing.

Figure 16.

Figure 16. Nightly performance summaries. In each plot, AO-off and AO-on image FWHMs (blue and red circles, respectively) are compared over time with the MASS/DIMM seeing (red and blue solid lines, respectively). The MASS/DIMM values are converted to the corresponding observation wavelength with Equation (8). The observation wavelength is reported with the date and indicated by each figure's background color: gray for R band, yellow for 1000 nm, and no shading for I band. The image FWHM data points each represent the median value of all sources in a single frame. Each panel's caption gives the UT date of observation.

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Considering the fact that ʻImaka has thus far only been run in natural guide star (NGS) mode, its gains are already comparable to GLAO systems using laser guide stars (LGSs). For example, the previously mentioned ARGOS instrument and the GLAO system on the MMT telescope both achieved improvement in FWHM of roughly a factor of two in LGS mode (Hart et al. 2010; Orban de Xivry et al. 2016). We have come close to this improvement in larger fields while still using NGSs, which, for GLAO, inject noise from atmospheric profiles unrelated to the corrected field. The initial success of ʻImaka compared to such instruments makes the prospect of adding LGS capability in the future particularly promising.

In that vein, ʻImaka was constructed on a low budget, as it is meant primarily as a demonstrator for GLAO on Maunakea. As such, it exhibits limitations that the high-quality optics and system engineering commonly used in large-telescope instrumentation projects could easily address.

Despite the clear gains ʻImaka has achieved, there are distinct differences between the distributions of FWHM we observe in our science images and the seeing (both integrated and free atmosphere) estimated from the ʻImaka wave-front sensors and Maunakea MASS/DIMM. Though the median MASS measurement of free-atmosphere seeing was 0farcs25 across all nights of observing in I band, the image quality of AO-on images on those nights was reduced to only 0farcs45, while ʻImaka's telemetry measured 0farcs40 seeing for what is ostensibly the same atmospheric profile experienced by the science camera. Despite this offset, the focal plane images are typically correlated to the telemetry and MASS/DIMM. The offset in the cumulative probability distribution (Figure 12) between the telemetry and the focal plane images indicates an instrumental error; it is nearly constant with image FWHM, suggesting that it is not a fixed noncommon path aberration since its contribution to the image degradation would decrease as the seeing degrades. There is some indication that the tomographic reconstruction error (e.g., our ability to separate ground-layer turbulence from high-altitude turbulence) may be larger than expected, but this is left to a later paper to quantify. There could also be a floor in the ʻImaka image quality of FWHMmin ∼ 0farcs3 that the AO-on images cannot go below. Potential causes for this limitation will also be explored in relation to ʻImaka's error budget in a later paper.

The initial characterization of AO-on images in relation to wavelength and field position in this paper reveals that we have not yet reached the atmospheric limits with ʻImaka and we may be able to improve instrument calibration and performance in the future. Though very preliminary, we can already see a weak trend in FWHM as a function of observation wavelength. Because of the limited amount of multiwavelength data and constraints on seeing conditions, it is currently difficult to conclude more about the wavelength dependence. However, we plan to extend this analysis in the future by observing at both shorter and longer wavelengths over a wider range of seeing conditions. As AO correction is substantially more difficult to achieve with shorter wavelengths, we will test how far this limitation can be pushed.

We will also test larger fields in order to better understand the variability of the GLAO correction across images. Initial analysis of the five nights of the May run shows an average range of 0farcs145. This variation is reduced to a range of 0farcs082 when the planar structure is removed. The plane itself varies on average by 0farcs0082 per arcminute across the field, which corresponds to a typical variation (percent change between minimum and median) of 4.5%. We will continue to examine this effect in future runs, with both larger fields and different asterisms. The data presented in this paper represent one configuration of wave-front sensors and control matrices per night on relatively small science fields; in reality, we collected data with a range of asterisms, which we are currently analyzing in more detail.

This paper has only looked at a narrow range of commissioning results. It serves as a complement to M. Chun (2018, in preparation), the main results paper of ʻImaka's commissioning, and will be followed by additional papers specifically on ʻImaka's PSF and ʻImaka's photometric and astrometric precision. We will also be continuing regular ʻImaka runs with new experiments. In order to better address some of the unanswered questions in performance thus far, one new component of the coming runs will be the use of larger science cameras, with plans for an 11' optical camera and a 7' infrared camera. This will allow us to further examine the GLAO correction over large areas and at longer wavelengths.

Collectively, the results of ʻImaka demonstrate the potential for a GLAO system on telescopes on Maunakea. The improvements we see in image quality across large fields could yield a significant boost in sensitivity for multiobject spectrographs, potential for high-precision astrometry, and high spatial resolution of large sources, all of which can be valuable to a wide variety of science cases. Though the delivered image quality of ʻImaka on the UH 2.2 m may not be identical to expectations for larger telescopes, our image quality improvement by a factor of 1.4–1.9 is comparable to the gains made by GLAO systems deployed on larger telescopes, such as the factor of 2 improvement in FWHM achieved by ARGOS on each of LBT's 8.4 m telescopes (Orban de Xivry et al. 2016) and the improvement of 1.5–2 in FWHM on the VLT's 8.2 m UT4 telescope (Arsenault et al. 2017). Furthermore, many instruments on Keck, such as LRIS and DEIMOS, are impacted by effects (e.g., focus changes, telescope jitter) that we have shown ʻImaka can correct (Faber et al. 2003; Rockosi et al. 2010).

8. Conclusion

We have demonstrated the potential of GLAO with guide stars distributed over fields of about 16' over 15 nights of observing. These initial findings are showing promising results.

Between AO-off and AO-on modes, ʻImaka's focal plane images demonstrate a decrease in PSF size by up to a factor of 1.8, depending on the metric used. The AO-on PSF also shows an elongation of 1:1.1, which is consistent with no elongation given the design variation of the plate scale of 8% in the north–south and east–west directions. This represents a substantial reduction from the AO-off value of 1:1.4. The median minor FWHM derived from a Moffat profile for AO-on images was 0farcs56 in R band and 0farcs43 in I band, and 0farcs82 for AO-off images in R band and 0farcs72 in I band (including a 4.5% correction for field variability). These quantities are typically correlated with ʻImaka's telemetry measurements of the free-atmosphere and integrated seeing, with correlation coefficients in R band of 0.68 and 0.70, respectively. Despite variation in the seeing over the course of a night, AO-on images demonstrate significantly more temporal stability than AO-off images, with the standard deviation of minor FWHM decreasing from 0farcs59 to 0farcs05, averaged across the five nights of the final run. The variation in FWHM across the field is also minimized in AO-on images, with FWHM varying on average by 0farcs0082 per arcminute and an average percent variation of 10.3%. Overall, these early results from ʻImaka suggest that a facility-class GLAO system on Maunakea would deliver valuable gains over seeing-limited images and spectroscopy.

ʻImaka is supported by the National Science Foundation under grant no. AST-1310706 and by the Mount Cuba Astronomical Foundation. C.B. acknowledges support from the Alfred P. Sloan Foundation. We would like to acknowledge the UH 2.2 m day crew for assistance with installation and observing setup. In addition, significant contributions to the design and construction of ʻImaka were made by Quartus Engineering, RockWest Composites, and Dream Telescopes.

The authors also wish to recognize and acknowledge the very significant cultural role and reverence that the summit of Maunakea has always had within the indigenous Hawaiian community. We are most fortunate to have the opportunity to conduct observations from this mountain.

Facility: UH:2.2 m (ʻImaka). -

Appendix:

The following figures show various results on a night-by-night basis. Figure 15 shows the dependence of image FWHM on airmass. Figure 16 shows image FWHM as well as MASS/DIMM seeing, both as a function of time over the course of each night.

Footnotes

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10.3847/1538-3881/aad1f2