${\mathcal{T}}$-REx. II. RETRIEVAL OF EMISSION SPECTRA

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Published 2015 October 22 © 2015. The American Astronomical Society. All rights reserved.
, , Citation I. P. Waldmann et al 2015 ApJ 813 13 DOI 10.1088/0004-637X/813/1/13

0004-637X/813/1/13

ABSTRACT

${\mathcal{T}}$-REx (Tau Retrieval of Exoplanets) is a novel, fully Bayesian atmospheric retrieval code custom built for extrasolar atmospheres. In Waldmann et al., the transmission spectroscopic case was introduced, and here we present the emission spectroscopy spectral retrieval for the ${\mathcal{T}}$-REx framework. Compared to transmission spectroscopy, the emission case is often significantly more degenerate due to the need to retrieve the full atmospheric temperature–pressure (TP) profile. This is particularly true in the case of current measurements of exoplanetary atmospheres, which are either of low signal-to-noise, low spectral resolution, or both. We present a new way of combining two existing approaches to the modeling of the said TP profile: (1) the parametric profile, where the atmospheric TP structure is analytically approximated by a few model parameters, (2) the layer-by-layer approach, where individual atmospheric layers are modeled. Both of these approaches have distinct advantages and disadvantages in terms of convergence properties and potential model biases. The ${\mathcal{T}}$-REx hybrid model presented here is a new two-stage TP profile retrieval, which combines the robustness of the analytic solution with the accuracy of the layer-by-layer approach. The retrieval process is demonstrated using simulations of the hot-Jupiter WASP-76b and the hot-super-Earth 55 Cnc e as well as the secondary eclipse measurements of HD 189733b.

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1. INTRODUCTION

The characterization of extrasolar planets through the spectroscopic measurements of their atmospheres has become a well established field today (Tinetti et al. 2013). In Waldmann et al. (2015), we presented the ${\mathcal{T}}$-REx (Tau Retrieval of Exoplanets) suite for transmission spectroscopic measurements. In this paper, we introduce the corresponding retrieval for emission spectroscopic data.

Transmission and emission spectroscopy carry highly complementary aspects. Whereas transmission spectroscopy is less sensitive to thermal gradients, the emission spectroscopy case probes the full temperature–pressure profile (TP-profile hereafter) of the atmosphere. This makes the emission case significantly harder to constrain without the luxury of in situ measurements. King (1958) was the first to suggest remote sensing of the planetary atmospheric temperature structure through the infra-red, thermal radiance of the planet. Kaplan (1959) expanded on this pioneering work by laying the foundations of retrieving exact TP-profiles from emission spectroscopic measurements. Remote sensing of planetary atmospheres in our solar system has been a long story of success (e.g., Wark & Hilleary 1969; Conrath et al. 1970; Hanel et al. 1972, 1981; Conrath et al. 1973; Rodgers 1976; Fletcher et al. 2007; Irwin et al. 2008; as well as Hanel et al. 2003, and references therein). More recently, emission spectroscopy remote sensing has been expanded to exoplanetary atmospheres (Madhusudhan & Seager 2009; Lee et al. 2011; Line et al. 2012; Griffith 2014). Line et al. (2013) provides a comparison of existing exoplanetary emission spectroscopy retrieval codes.

1.1.  ${\mathcal{T}}$-REx

${\mathcal{T}}$-REx is a novel, Bayesian atmospheric spectroscopy retrieval suite designed for extrasolar planets. In Waldmann et al. (2015, hereafter W15), we introduce the overall architecture, data handling, minimization/sampling routines, handling of molecular line lists, Bayesian model selection and the transmission spectroscopy forward model. In this publication, we present the emission spectroscopy forward model as well as the atmospheric TP profile retrieval implemented.

Figure 1 shows a schematic diagram of the ${\mathcal{T}}$-REx architecture for the emission retrieval. The program can be subdivided into five sections.

  • 1.  
    Inputs: program inputs such as parameter files, molecular line-lists (ExoMol Tennyson & Yurchenko 2012), (HITEMP Rothman et al. 2010), stellar spectra (PHOENIX, Allard et al. 2012), and spectroscopic observations to be analyzed.
  • 2.  
    Model and Data handling: the Central Data Module manages all calls to the TP-Profile and Forward Model Modules and provides a standardized, common interface to different sampling routines implemented.
  • 3.  
    Sampling: ${\mathcal{T}}$-REx features three independent sampling routines: Maximum Likelihood estimation (MLE, based on the LM-BFGS minimization in W15), Markov Chain Monte Carlo (MCMC), and Nested Sampling (NS). We refer the reader to W15 for implementation details.
  • 4.  
    Post analysis and refinement: This stage differs from W15 by providing two iteration stages for the determination of the TP-Profile, see Section 3.
  • 5.  
    Output: the final posterior distributions are analyzed and the final model spectrum, TP-Profile, and mixing ratios are returned.

Figure 1.

Figure 1. Flowchart illustrating the modular design of ${\mathcal{T}}$-REx. This flowchart is an update from Waldmann et al. (2015), reflecting the differing architecture of the emission spectroscopy code.

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2. FORWARD MODEL

We briefly describe the radiative transfer forward model; for a more exhaustive discussion, we refer the reader to the standard literature (e.g., Chandrasekar 1960; Goody & Yung 1989; Liou 2002; Hanel et al. 2003; Mihalas & Mihalas 2013). In what follows, we closely follow the nomenclature of Liou (2002). For non-scattering atmospheres in local thermodynamic equilibrium, the basic equation describing the thermal radiation of an atmosphere is given by the Schwartzschild equation:

Equation (1)

where ${I}_{\lambda }$ is the intensity per wavelength, λ, ${B}_{\lambda }$ is the Planck function at temperature T, $\mu =\mathrm{cos}\theta $ is the upward inclination, and τ is the overall optical depth, given as function of altitude (z) by

Equation (2)

where ${\tau }_{\lambda ,m}$ denotes the optical depth per absorbing species, m, given by

Equation (3)

Here ${\varsigma }_{\lambda ,m}$ is the absorption cross section, χm is the column density, and ${\rho }_{{\rm{N}}}$ is the number density. We can now express the upward welling radiance as

Equation (4)

where the first right-hand side term is the radiation at the planetary surface (or defined surface pressure for gaseous planets), and the second term denotes the integrated emission contributions for individual plane-parallel layers. The monochromatic transmittance and its derivative (weighting function) can be defined as

Equation (5)

Hence we express the total integrated radiation at the top of the atmosphere (TOA, $\tau =0,z=\infty $) as

Equation (6)

where τs and Ts are the optical depth and temperature at the planetary surface. The final exoplanetary emission spectrum is now given by

Equation (7)

where I* is the stellar intensity. By default ${\mathcal{T}}$-REx interpolates the stellar flux from a library of Phoenix 1 stellar spectra, gridded at 100 K intervals. Alternatively, ${\mathcal{T}}$-REx can approximate the stellar intensity using a blackbody at the stellar temperature.

3. TP PROFILE

The determination of the vertical atmospheric temperature profile (also referred to as the temperature–pressure profile or TP-profile for short) is one of the key challenges in the retrieval of atmospheric emission spectra. Typically, two approaches exist in the retrieval of the TP-profile: (1) layer-by-layer retrieval and (2) analytic parameterization.

(1) The layer-by-layer approach consists of modeling the temperature of each plane-parallel atmospheric layer independently. This approach is usually adopted for retrieval work of the Earth's atmosphere and solar system planets (Rodgers 2000; Hanel et al. 2003). The advantage of such an approach is its non-parametric nature, i.e., no prior knowledge is imposed on the temperature retrieval nor is the solution limited by potential restrictions and biases of an analytic TP-profile. The obvious disadvantage lies in the potentially poor convergence properties of such an approach in low signal-to-noise ratio (S/N) scenarios. Often, data quality or sparse spectral sampling do not allow for a pure layer-by-layer retrieval due to the large number of free parameters incurred. This is particularly true for current exoplanet spectroscopy data, which is either of relatively low S/N, low spectral resolution, or both. A common approach adopted is to impose a "regularization" of the TP-profile based on the physical reality that adjacent atmosphere layers should exhibit some correlation in temperature.

(2) The second approach to the TP-profile retrieval is to adopt an analytic (here also referred to as "parametric") model. Such models analytically approximate the mean underlying physics of the atmospheric thermal structure. Such models have the advantage of containing far fewer free parameters compared to the layer-by-layer approach, hence they converge faster. However, the solution is constrained within the bounds of the model assumed.

In summary, the layer-by-layer methodology is most objective but features poor convergence properties, while the parametric model is less objective, but converges more robustly. For a review of existing implementations of both approaches in the field of exoplanet atmospheric retrieval, we refer the reader to Line et al. (2013).

As described in Section 3.2, ${\mathcal{T}}$-REx employs a hybrid model combining both parametric and layer-by-layer approaches in a two stage retrieval process. In Section 3.1, we briefly describe the parametric models implemented in ${\mathcal{T}}$-REx as part of the ${\mathcal{T}}$-REx retrieval framework.

3.1. Parametric Models in the Literature

Analytical global-average TP-profiles exist in various flavors ranging from two-stream purely radiative to radiative-convective approximations and global circulation models (GCMs). We refer the reader to the relevant literature for a more in-depth discussion on the various analytic approaches (e.g., Liou 2002; Hubeny et al. 2003; Burrows et al. 2008; Hansen 2008; Madhusudhan & Seager 2009; Showman et al. 2009; Guillot 2010; Pierrehumbert 2010; Heng et al. 2012, 2014; Robinson & Catling 2012). For the Stage 1 approach, ${\mathcal{T}}$-REx features a purely radiative two-stream model as well as a choice of simpler TP-profiles based on purely geometric considerations (see 3.1.1). As described in Section 3.2, the exact form of the TP-profile is less relevant in our case because  the results will be refined in a second stage fitting.

Following Guillot (2010), the mean global temperature profile for a simple radiative downstream–upstream approximation can be expressed as

Equation (8)

where Tint is the planet internal heat flux, Tirr is the solar flux at the top of the atmosphere, and

Equation (9)

where ${\gamma }_{1}={\kappa }_{\nu }/{\kappa }_{\mathrm{IR}}$ is the ratio of mean opacities in the optical (${\kappa }_{\nu }$) and infra-red (${\kappa }_{\mathrm{IR}}$) and E2 is the second-order exponential integral given by

Equation (10)

We note that similar parameterizations exist in the literature (e.g., Equation (18), Robinson & Catling 2012; Pierrehumbert 2010). We also include the variation by Line et al. (2012) and Parmentier & Guillot (2014) including two optical opacity sources ${\kappa }_{{\nu }_{1}}$ and ${\kappa }_{{\nu }_{2}}$ and a weighting factor between optical opacities (left as a free parameter) α,

Equation (11)

The temperature as a function of opacity τ can be mapped to a pressure grid by assuming the following relation

Equation (12)

3.1.1. Other TP-profiles

In addition to the above TP-profiles, we include an isothermal profile as well as a "3-point" and "4-point" profile. The 3-point profile is purely geometric and keeps the top of atmosphere temperature, TTOA, the tropopause temperature and pressure, T1, P1, and the surface (or 10 bar pressure) temperature ${T}_{10\mathrm{bar}}$ as free variables. The TP-profile is then linearly interpolated in ln $(P)$. The 4-point profile adds an extra variable TP point to the profile.

3.2. The ${\mathcal{T}}$-REx Hybrid Model

In ${\mathcal{T}}$-REx, we have worked toward a hybrid solution of the above mentioned approaches in which the final solution is not bound by a parametric model, but does not inherit the potentially poor convergence properties (and susceptibility to noise) of a layer-by-layer approach. Here we proceed in two stages: (1) we perform a parametric model retrieval and (2) we take the retrieval solution to "guide" a second layer-by-layer retrieval, relaxing the parametric model constraint and thereby fine-tuning the TP-profile.

3.2.1. Stage 1

In Stage 1, we adopt a classical parametric model retrieval using one of the TP-profile parameterizations implemented in ${\mathcal{T}}$-REx. The idea is to constrain an initial best-fit of the model and while a realistic model (i.e., one well suited to describe the underlying TP-profile) is preferable, it is not a hard requirement. We now fit the solution using either of ${\mathcal{T}}$-REx's sampling routines (MLE, MCMC, NS). The error on the sampled parametric model parameters is converted to one σ lower and upper temperature bounds for a layer-by-layer model. This is done using a numerical model permutation analysis of the Stage 1 parameters.

We then calculate the following distance matrix

Equation (13)

where $\hat{T}$ is the maximum likelihood temperature estimator of the parametric model fit for the ith and jth atmospheric layer and σ is the respective error. Equation (13) captures the layer to layer temperature variations in the TP-profile and is hence conceptually similar to the Jacobian of the profile. We normalize Δij in terms of the minimal and maximal temperature variations found in the TP-profile,

Equation (14)

which can be understood as a positively defined temperature correlation matrix with layers most similar in temperature featuring the highest correlation and layers most dissimilar resulting in a very low correlation. An example of ${\mathcal{C}}$ for a given TP-profile can be found in Figure 2.

Figure 2.

Figure 2. Left: a given Temperature–Pressure Profile without inversion. Right: correlation matrix ${\mathcal{C}},$ Equation (14), of the TP-profile on the left. Atmospheric layers with similar temperatures feature a high layer–layer correlation while layers with temperature differences feature lower correlations.

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3.2.2. Stage 2

In the second stage of our TP-profile retrieval, we relax the original solution found in Stage 1 and, by that, "fine-tune" the TP-profile. We construct a second correlation matrix imposing an exponential correlation length across pressure levels (Rodgers 1976, 2000)

Equation (15)

where c is the correlation length in terms of atmospheric scale heights. We set c = 3.0 by default, but it can otherwise be user defined. Rodgers (2000) gives an advisable range between 1.0 and 8.0, with Irwin et al. (2008) using a default of c = 1.5 and Line et al. (2013) c = 7.0. Larger values of c correspond to a stronger regularization of the TP-profile (i.e., smoothing). A stronger regularization can be useful in poorly constrained data sets (either low S/N, sparsely sampled, or both). Equation (15) is identical to that used in the layer-by-layer approach by Irwin et al. (2008). We now construct a hybrid correlation matrix by combining Equations (14) and (15)

Equation (16)

where α is a scaling factor ranging from zero to one. Figure 3 shows instances of ${\mathcal{D}}(\alpha )$ at varying values of α. We now correlate our layer-by-layer TP-profile with ${\mathcal{D}}(\alpha )$ whereby leaving α as free parameter to be fitted. By allowing α to vary, we can dynamically relax the parametric model solution from Stage 1, $\alpha =1.0$, to an unconstrained solution, $\alpha =0.0$. The advantage of such an approach is twofold: (1) since the Stage 1 fitting should have already achieved a solution close to the real maximum likelihood, convergence in the second stage toward the volume of lowest χ2 is significantly faster and (2) ${\mathcal{T}}$-REx can freely decide to relax the Stage 1 solution should this be favored by the data. Practically, this happens frequently at later stages of the fitting. Whereas ${\mathcal{T}}$-REx initially converges toward the Stage 1 solution (i.e., $\alpha \to 1$), at later stages of the fitting the code begins to reject the parametric model (i.e., $\alpha \to 0$) as it "fine-tunes" the original solution. This "tuning" can achieve significantly higher maximum likelihoods than the Stage 1 fitting alone.

Figure 3.

Figure 3. Hybrid correlation matrix ${\mathcal{D}},$ Equation (16), at different values of α. The left most is the pure Stage 1 correlation matrix, ${\mathcal{C}},$ whereas the right plot is the pure correlation-length-only matrix S, Equation (15). Over-plotted are contours of ${\mathcal{D}}(\alpha ).$ The middle panel shows an intermediate state of left (60%) and right (40%).

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3.3. Nonlinear Sampling

In the approach explained in Section 3.2, we keep an even sampling of atmospheric layers in log(P) for Stage 2. For well sampled and high S/N data, this approach is adequate. However, for coarsely sampled and/or poor S/N data, it is often advisable to reduce the number of free parameters to a minimum to aid convergence. In these cases, we can utilize the sparsity of the Stage 1 TP-profile solution to devise a nonlinear sampling of the exoplanetary atmosphere. We base our compression algorithm on the fact that only changes in the TP gradient need to be modeled, i.e., an isothermal TP-profile can be perfectly described by a single temperature parameter whereas areas of non-isothermal structure need more parameters to capture variation. The compression algorithm uses the Stage 1 correlation matrix ${\mathcal{C}}$ to only retain TP-profile layers corresponding to a $\gt 2\%$ change in the TP gradient with respect to the previously retained layer. We graphically depict this in Figure 4. In addition to TP-profile layers sampled this way, we also include an extra sampling layer whenever no change in thermal gradient was detected for $\gt 10$ layers. The majority of the TP-profile variations should be captured by the Stage 1 retrieval and Stage 2 is "fine-tuning" this solution. The inclusion of a coarse sampling in isothermal regimes does allow the Stage 2 retrieval to deviate from any Stage 1 solution, should this be supported by a higher global likelihood. Using the nonlinear sampling, we can reduce a 100 layer atmospheric model to typically 15–25 free parameters.

Figure 4.

Figure 4. Nonlinear TP-profile sampling on correlation matrix ${\mathcal{C}}$ (same as in the right hand plot in Figure 2). Starting at the top of the atmosphere (red dot), we retain all layers in the TP-profile that correspond to a change in gradient $\gt 2\%$ with respect to the previously retained layer until the bottom layer (green dot) is reached. The selected layers are denoted by white dots and arrows represent the path of the compression algorithm across the correlation matrix ${\mathcal{C}}.$ Should no gradient change be detected for $\gt 10$ layers, an extra sampling point is introduced (black dots).

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4. VALIDATION OF ${\mathcal{T}}$-REX

We demonstrate the emission spectroscopy retrieval with two simulations and the secondary eclipse spectrum of HD 189733b. The simulations are as follows: (1) high S/N observation simulation of a hot-Jupiter similar to WASP-76b and (2) observations of the hot-super-Earth 55 Cnc e, simulated for a 1 m class spectroscopic space mission. In our simulations, we opt for two oxidized atmospheres at high temperatures (>1500 K).

For each retrieval stage, we calculate the global Bayesian Evidence of the solution set. Here the Bayesian Evidence (E, or simply Evidence hereafter) is given as the integral of the product of the global likelihood and the prior space

Equation (17)

where $P({\boldsymbol{\theta }}| {\mathcal{M}})$ is the prior over the parameter space ${\boldsymbol{\theta }}$, for retrieval model ${\mathcal{M}}$. $P({\boldsymbol{x}}| {\boldsymbol{\theta }})$ is the likelihood for the observed data vector ${\boldsymbol{x}}$ given the parameter space and retrieval model. Retrieval Evidences are reported in Tables 1 and 2.

Table 1.  Retrieved Abundances for Hot-Jupiter WASP-76b

  Input Model Stage 1 Retrieval Stage 2 Retrieval
log(E) NA −43.92 36.20
log(H2O) −4.0 −3.458 ± 0.104 −3.660 ± 0.107
log(CO) −4.69 −4.352 ± 0.143 −4.548 ± 0.113
log(CO2) −6.0 −5.374 ± 0.120 −5.428 ± 0.114

Note. Top row: log Bayesian Evidence for Stage 1 and Stage 2 models. Differences above $| {\rm{\Delta }}\mathrm{log}(E)=5| $ are very significant. Here ${\rm{\Delta }}\mathrm{log}(E)=+80.12$, indicating a significantly improved fit in Stage 2.

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Table 2.  Retrieved Abundances for Hot-super-Earth 55 Cnc e

  Input Model Stage 1 Retrieval Stage 2 Retrieval
log(E) NA 75.40 168.90
log(H2O) −4.0 −4.168 ± 0.795 −4.055 ± 0.571
log(CO) −5.0 −5.764 ± 1.248 −5.613 ± 1.172
log(CO2) −5.0 −5.236 ± 1.112 −5.136 ± 1.019

Note. Top row: log Bayesian Evidence for Stage 1 and Stage 2 models.

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4.1. WASP-76b

WASP-76b (West et al. 2013) is a very hot-Jupiter orbiting a late F7 star. It is highly inflated at ${1.83}_{-0.04}^{+0.06}$ RJup, $0.92\pm $0.03 MJup, and ${T}_{\mathrm{equ}}\sim 2200$ K. We take its bulk and orbital properties and generate a simulated observation at a resolution of 300, a spectral range of 0.5–20 μm, and 100 ppm errors. We set the atmospheric composition to $1\times {10}^{-4}$ H2O, $1\times {10}^{-5}$ CO, and $1\times {10}^{-5}$ CO2. The input TP-profile is shown in Figure 7 (black line). It is important to note that here (as well as in Section 4.2) the input TP-profile was generated using a script external to ${\mathcal{T}}$-REx with no relation to either Stage 1 parametrization. This provides an adequate test-bed for the Stage 1 fitting to accurately retrieve an arbitrary atmospheric profile.

Figure 5.

Figure 5. Correlation matrix, ${\mathcal{C}},$ derived from Stage 1 TP-profile shown in Figure 7. The input model TP-profile is shown as a black continuous line. Otherwise identical to Figure 3.

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As described in Section 3.2, we retrieve the TP-profile and abundances in two stages. For computational efficiency reasons, here we only compute the NS solutions (which are also the most accurate, see W15). Tests were run with both maximum-likelihood retrievals and MCMC retrievals and solutions between all sets of solutions are in good agreement.

The NS Stage 1 solution returns four local likelihood maxima of which the global maximum was selected. Figures 6 (top), 7 (left), and Table 1 show the retrieved spectrum, TP-profile, and retrieved abundances respectively. The Stage 1 TP-profile mostly captures the input TP-profile but shows unrealistic bumps and wiggles as well as unrealistic distributions of the one sigma error bar. These are artefacts of the parameterization in Section 3.1. The three local maxima TP-profiles shown in Figure 7 underestimate the bulk temperature of the planet, driving the retrieval to assume unrealistically low abundances of molecular trace gases. In this example, this is found to be a numerical effect that disappears by increasing the sampling grid density of the NS. Nonetheless, the potential degeneracy between TP-profile and molecular abundances in atmospheric retrievals is worth noting.

Figure 6.

Figure 6. Showing the input spectrum of a WASP-76b-type hot-Jupiter, gray, and Stage 1 and 2 fitting on the top and bottom respectively. Both fits converged but the Stage 2 fit reached a higher maximum likelihood.

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Figure 7.

Figure 7. TP-profiles for Stage 1 and 2 results for WASP-76b in Figure 6. Solid lines represent the mean and shaded regions the one sigma error bars. Solid black lines are the input TP-profile. Stage 2 takes the initial parametric TP-profile fit of Stage 1 and relaxes the solution. Four solutions were obtained for Stage 1, the highest maximum likelihood solution (blue) traces the input TP-profile well, while local maxima underestimate the bulk temperature, see the text. The Stage 2 solution feature a significantly lower χ2 (or higher global Evidence) than all Stage 1 solutions.

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As described earlier, we computed the TP-profile covariance, ${\mathcal{C}}$ (Figure 5), and tuned the Stage 1 retrieval by relaxing the parametric solution. Figures 6 (bottom), 7 (right), and Table 1 show the Stage 2 retrieval results. Inspecting Figure 6, both Stage 1 and Stage 2 retrievals fit the input spectrum sufficiently well but Stage 2 comes significantly closer to the "true" TP-profile and trace gas abundances. Figure 8 shows the normalized emission contribution functions of both retrievals and their difference. This shows the planetary emission mainly emanating in the non-isothermal regions (up to the tropopause) of the TP-profile, as expected. However, Stage 2 emissions originate significantly lower (by nearly an order of magnitude) in the atmosphere (blue band in the bottom panel).

Figure 8.

Figure 8. Left: retrieved TP-profile, right: contribution functions for WASP-76b. First and second rows: best-fit TP-profiles and corresponding emission contribution functions as function of pressure and wavelength for Stage 1 and Stage 2 respectively. Bottom row: difference between both stages. Contribution difference is given as normalized fraction.

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4.2. 55 Cnc e

We simulated an emission spectrum of the hot-super-Earth 55 Cnc e (Fischer et al. 2008). We use trace gas compositions of $1\times {10}^{-4}$ H2O, $1\times {10}^{-5}$ CO, and $1\times {10}^{-5}$ CO2 and a sharp TP-profile shown in Figure 10. Because the previous WASP-76 example is currently unrealistically optimistic, given the combination of high S/N, moderate resolution (R ∼ 300) and a very broad wavelength coverage, we opt for a more realistic example here. We calculated the expected resolution and S/N for 100 co-added eclipses obtained by a one-meter-class transiting spectroscopy space-mission (e.g., the ESA M4 proposal ARIEL) over a wavelength range spanning 2–8 μm. Using EChOSim, an end-to-end simulator for transit spectroscopy space-missions (Pascale et al. 2014; Waldmann & Pascale 2014) developed for the ESA M3 EChO proposal (Tinetti et al. 2012), we calculated realistic error bars for this hot super-Earth, shown in Figure 9.

Figure 9.

Figure 9. Input spectrum of a 55 Cnc e-type atmosphere, gray, and Stage 1 and 2 fitting on the top and bottom respectively. Both fits converged but the Stage 2 fit reached a higher global Evidence.

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Similarly to Section 4.1, Figures 911 show the Stage 1 and 2 retrieved spectra, TP-profiles, and Stage 1 TP-profile covariance respectively. Table 2 shows that Stage 2 retrieval converges at a significantly higher global Evidence and presents an improvement in the accuracy of abundances retrieved as well as the TP-profile retrieved. Figure 12 shows the absolute difference between the Stage 1 and Stage 2 model fits at a spectral resolution of 1000. Here the discrepancies between both spectral fits are of the order of $2\times {10}^{-5}$ or less. This is not very significant in terms of a naive χ2 fit to relatively low S/N data, but does significantly drive the retrieval of the TP-profile and trace gas abundances. This is reflected in the Bayesian Evidence measured for Stage 1 and Stage 2 models. Figure 13 shows the contribution functions for both retrievals. Here we have positive and negative temperature differences (see bottom left plot), resulting in a more complex contribution differential (bottom left plot) than for WASP-76b. It should be noted that this contribution differential is highly wavelength dependent and illustrates the sensitivity of varying wavelength ranges on the TP-profile retrievability.

Figure 10.

Figure 10. TP-profiles for Stage 1 and 2 results for 55 Cnc e in Figure 9. Both solutions converge within the calculated error bar. Stage 2 features a significant improvement in maximum likelihood achieved.

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Figure 11.

Figure 11. Correlation matrix, ${\mathcal{C}},$ derived from Stage 1 TP-profile shown in Figure 10. Otherwise identical to Figure 5.

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Figure 12.

Figure 12. Showing the model fit difference between Stage 1 and Stage 2 at spectral resolution of 1000. Model fit difference are of the order of $2\times {10}^{-5}$ or less.

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Figure 13.

Figure 13. Contribution functions for 55Cnc e, otherwise the same as Figure 8.

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4.3. HD 189733b

Finally, we test ${\mathcal{T}}$-REx on the emission spectrum of the hot-Jupiter HD 189733b. Its emission spectrum is among the most complete and best studied (e.g., Madhusudhan & Seager 2009; Swain et al. 2009; Lee et al. 2011; Line et al. 2012, 2014). We have compiled data sets ranging from the NIR (1.4 μm) to the MIR (24μm), namely: Hubble Space Telescope/NICMOS (Swain et al. 2009), Spitzer/IRAC 3.6, 4.5 μm (Knutson et al. 2012), 8.0 μm (Agol et al. 2010), Spitzer/IRS spectroscopy (Grillmair et al. 2008), Spitzer/IRS 16 and 24 μm photometry (Charbonneau et al. 2008). As in previous studies, we consider the active trace gasses H2O, CH4, CO, and CO2 and otherwise assume a hydrogen dominated atmosphere.

Figure 14 shows the retrieved emission models with retrieved abundances and log(Evidence) reported in Table 3. Figures 15 and 16 report the retrieved Stage 1 and Stage 2 TP-profiles and associated Stage 1 TP-covariance, respectively. Figures 17 and 18 are the marginalized and conditional posteriors for the active trace gasses considered. Figure 19 illustrates the difference between Stage 1 and Stage 2 emission spectra.

Figure 14.

Figure 14. Emission spectrum of a HD 189733b, black circles, and Stage 1 and 2 fitting on the top and bottom respectively; blue: the fitted emission spectrum at R = 1000; red squares: spectrum fit binned to data resolution; gray: photometric passbands for Spitzer/IRAC and MIPS. Both fits converged, but the Stage 2 fit reached a higher global Evidence.

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Figure 15.

Figure 15. TP-profiles for Stage 1 and 2 results for HD 189733b in Figure 14. Both solutions converge within the calculated error bar. Stage 2 features a significant improvement in maximum likelihood achieved.

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Figure 16.

Figure 16. Correlation matrix, ${\mathcal{C}}$, derived from Stage 1 TP-profile shown in Figure 15. Most of the atmosphere is found to be best fit with an isothermal profile, but the lowest ∼20 atmospheric layers (∼0.1 bar). Otherwise identical to Figure 5.

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Figure 17.

Figure 17. Marginalized and conditional posterior distributions of the trace gasses of HD 189733b for Stage 1 fitting. All trace gases are well constrained but only an upper limit to methane can be found.

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Figure 18.

Figure 18. Marginalized and conditional posterior distributions of the trace gasses of HD 189733b for Stage 2 fitting. All trace gases are well constrained.

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Figure 19.

Figure 19. Model fit difference between Stage 1 and Stage 2 at a spectral resolution of 1000. Differences between either retrievals are of the order of 5–8 × 10−4 in most wavelengths.

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Table 3.  Retrieved Abundances for Hot-Jupiter HD 189733b

  Stage 1 Retrieval Stage 2 Retrieval
log(E) −43.23 78.52
log(H2O) −3.918 ± 0.207 −4.978 ± 0.602
log(CH4) −6.732 ± 0.719 −6.768 ± 0.487
log(CO2) −3.722 ± 0.482 −4.204 ± 0.488
log(CO) −2.671 ± 1.387 −2.689 ± 0.769

Note. Top row: log Bayesian Evidence for Stage 1 and Stage 2 models. ${\rm{\Delta }}\mathrm{log}(E)=+121.75$ indicating a very significant improvement in the Stage 2 fit compared to Stage 1.

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As described above, the Stage 1 retrieval was first performed using the parmetric TP-profile by Guillot (2010) with the additional optical opacity terms proposed by Line et al. (2012). Here, all parameters of the TP model were allowed to vary. We modeled the atmosphere over 25 scale heights sampled onto a 150 pressure-layer grid. Following this initial retrieval, the TP-covariance was computed resulting in a predominantly isothermal atmosphere down to the lowest ∼20 layers (∼0.1 bar pressure). The obtained TP-profile is well constrained but shows systematics (e.g., at 5×10−4 bar) typical of this type of parametrization. The posterior distributions of the active trace gases, Figure 17 shows good constrains on abundances. From Figure 17, we can see the retrieved values for methane to only constitute an upper limit.

The Stage 2 hybrid model contained 22 free parameters on its nonlinearly sampled TP-profile grid. All parameters were allowed to vary freely between fully constrained ($\alpha =1.0$ in Equation (16)) and unconstrained scenarios. Figure 15 (right) shows the Stage 2 TP-profile with $\alpha =0.54$, indicating a significant shift away from the parametric solution of ${\text{}}{Stage}\;1$. The Stage 2 model features a lower tropopause pressure along with reduced water and carbon-dioxide abundances to achieve a very significant increase in Bayesian Evidence, see Table 3 and the discussion in Section 5. The Stage 2 TP-profile error bounds are slightly larger. Given a significantly higher Evidence for Stage 2, it is indicative of Stage 1 TP-profile errors to be underestimated by the parameterization used. The posteriors distributions of Stage 2 now show a convergence of methane beyond the upper-bound constrained of Stage 1.

Compared to Table 3 in Line et al. (2014), we obtain lower abundances of CH4 and CO2, but higher values for CO. Whereas these values differ from previous analyses, we find them significantly closer to the chemical model predictions of HD 189733b (e.g., Line et al. 2010; Venot et al. 2012; Moses et al. 2013). Note also that Stage 1 results exhibit the same trend of lower CH4 and CO2 abundances. We find two aspects by which our analysis differs from others in the literature: (1) a finer and complete sampling of correlated likelihoods, in particular, compared to maximum likelihood methods that are often less efficient with sparsely sampled data; (2) the completeness of molecular line-lists used. This is particularly true for the C/O ratio determination using CH4 and CO/CO2 as tracers. In this work, we use the new YT10to10 CH4 line-list (Yurchenko & Tennyson 2014).

5. DISCUSSION

In Section 4, we have demonstrated the efficiency of the ${\mathcal{T}}$-REx retrieval suite for emission spectroscopy using a simulated hot-Jupiter, a hot-Super-Earth, as well as secondary eclipse observations of HD 189733b, as examples.

In all three cases the Bayesian Evidence of the Stage 2 retrieval is significantly higher, log(E) = 36.20 compared to — 43.92, log(E) = 168.9 to 75.40 log(E) = −43.23 to 78.52 for WASP-76b, 55 Cnc e and HD 189733b, respectively. This is clearly indicative of Stage 2 results being more robust statistically. Following the adaptation of the Jeffrey's scale of model evidence (Jeffreys & Kendall 1948) by Kass & Raftery (2012), we can define a strong preference for the Stage 2 model as ${\rm{\Delta }}\mathrm{log}(E)\gt 5$ and equally, a strong preference of the Stage 1 model to be ${\rm{\Delta }}\mathrm{log}(E)\lt -5$. Evidence differences ranging from −5 to 5 indicate a lesser significance. In the case of WASP-76b, we find ${\rm{\Delta }}\mathrm{log}(E)=+80.12$, ${\rm{\Delta }}\mathrm{log}(E)=+132.70$ for 55 Cnc e and ${\rm{\Delta }}\mathrm{log}(E)=+121.75$ for HD 189733b. Furthermore, the improved Stage 2 fit is illustrated by the better retrieval of the trace gas abundances (Tables 13). This illustrates the importance of accurate TP-profile retrievals and the advantage of a two-staged approach, especially in cases of low resolution and/or low S/N data.

6. CONCLUSION

In this paper, we introduced the emission spectroscopy retrieval approach for the ${\mathcal{T}}$-REx retrieval suite framework. Given a common code basis for transmission and emission retrieval, allows us to benefit from computational efficiencies and the high accuracy of molecular line-list handling introduced in W15. To suite the needs of the TP profile retrieval, we implemented an extra loop unique to the emission side of ${\mathcal{T}}$-REx, which allows a two-staged retrieval. We show that such a staged retrieval of the emission spectrum (and TP-profile) allows us to dynamically scale the complexity of the retrieval problem (from a fully parameterized to a fully unconstrained model) and has significant advantages in accuracy and robustness over previously available methods. Future publications will extend the sensitivity analyses presented here to include present and future ground and space instrumentation and a wider range of planets observable in emission spectroscopy.

We thank the referee for providing useful comments. This work was supported by STFC (ST/K502406/1) and the ERC projects ExoLights (617119) and ExoMol (267219)

Footnotes

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10.1088/0004-637X/813/1/13