Simulating Systematic Errors in Exoplanetary Transits for the James Webb Space Telescope

University of Central Florida Honors Undergraduate Thesis

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David Wright
April 9, 2021

Overview

  1. Motivation
  2. Literature Review and Relevant Work
  3. Methodology & Results - Adding JWST Features to ExoSim, Validation, and Comparisons
  4. Future Work and Closing Remarks

Motivation

Background Information

The upcoming™ James Webb Space Telescope (JWST) offers multiple observation modes tailored specifically for transit observation

webb_render.jpg

Figure 1: Artist render of JWST

Need

The community needs simulation tools that create realistic simulations including instrument systematic errors and noise

Literature Review and Relevant Work

Exoplanet Transits

In 1999, HD 209458 b was discovered via photometric transit observations [CH00]

hot-jups.jpg

Figure 2: Hot Jupiters. Image Credit: ESA

Exoplanet Transits

transitgif.gif

Figure 3: Animation of exoplanet transit. Animation credit: NASA

  • Total flux of the star+planet system has a fractional decrease of \(\approx \left(\frac{R_P}{R_S}\right)^2 \), often called the transit depth

Exoplanet Transits

transitgif.gif

Figure 4: Animation of exoplanet transit. Animation credit: NASA

  • The planet’s radius is \(R_P = R_S \sqrt{\textrm{Depth}}\)
  • This is a small ratio, usually ~1-2% for a typical hot Jupiter

Exoplanet Transits

hd209bs28-lc.png

Figure 5: HD 209458 b light curve fit with a Mandel and Agol model. Image Credit: Kathleen McIntyre

  • In practice, this ratio is found by fitting model light curves to the data, such as the model described by Mandel and Agol [MA02]

Exoplanet Transits

Spectroscopic observations yield more information on exoplanet atmospheres

spec-lc.png

Figure 6: HD 209458 b light curves from \(0.29-1.04 \mu\textrm{m}\). Image Credit: Heather Knutson

Exoplanet Transits

The \(\left(\frac{R_P}{R_S}\right)^2 \) ratio at different wavelengths, \(\left(\frac{R_P(\lambda)}{R_S}\right)^2 \), is coined the “transmission spectrum”

w39-lc.png

Figure 7: WASP-39b light curves from \(0.3-5.0 \mu\textrm{m}\). Image Credit: Wakeford et al. 2017 [WA17]

Exoplanet Transits

Transiting planets on circular orbits also pass behind their host star, known as an eclipse or secondary transit

phase-curve.png

Figure 8: Exoplanet phase curve. Image Credit: Deming & Knutson 2020 [DK20]

Exoplanet Transits

As the planet passes behind its star, the observed flux decreased by \( \left(\frac{R_P}{R_S}\right)^2 \frac{ F_{\lambda,P} }{ F_{\lambda,S} } \) with \(F_\lambda\) being the emergent flux density of the planet or star

w39-lc.png

Figure 9: WASP-39b light curves from \(0.3-5.0 \mu\textrm{m}\). Image Credit: Wakeford et al. 2017 [WA17]

The James Webb Space Telescope (JWST)

The James Webb Space Telescope (JWST)

  • JWST has exoplanet science as one of its main goals
  • JWST will observe the 0.6–28\(\mu \textrm{m}\) range with detectors that are capable of greater than 100 parts per million (ppm) precision over time periods from hours to days [BE14]

webb_render.jpg

Figure 10: Artist render of JWST

webb_wl_range.png

Figure 11: JWST wavelength coverage compared to Hubble and Spitzer

The James Webb Space Telescope (JWST)

  • JWST has a 25\(\textrm{m}^2\) primary mirror, the largest of any space telescope to date
  • It will orbit the Earth-Sun L2 point, providing extremely stable observations over long time periods

l2.jpg

Figure 12: JWST orbit at Earth-Sun L2 point. Image credit: NASA

The James Webb Space Telescope (JWST)

  • Webb carries four instruments on board:
    • The Near-InfraRed Camera (NIRCam, [BE12])
    • The Near-InfraRed Spectrograph (NIRSpec, [FE12])
    • The Near Infrared Imager and Slitless Spectrograph (NIRISS, [DO12])
    • The Mid-Infrared Instrument (MIRI, [KE15])

webb_wl_instruments.png

JWST Simulation Tools

Instrument Specific

General JWST

Methodology & Results

A Brief Overview of ExoSim

exosim-pic-jh.jpg

Figure 14: Overview of ExoSim Algorithm. Image credit: Enzo Pascale

Adding New Features to ExoSim

  • In order to simulate JWST, ExoSim requires the following additional capabilities
    1. Simulation of curved spectral traces
    2. Simulation of multiple-ordered spectral traces
    3. Use instrument specific PSFs
    4. Support JWST detector readout patterns
    5. Parallelization

Curved Spectral Traces

Allow a 2D wavelength-pixel relation, \(\lambda(x,y)\)

soss.png

Figure 15: NIRISS SOSS. Three orders cover a wavelength range of \(0.6-2.8\mu\textrm{m}\). Image Credit: STScI

Multiple-Ordered Spectral Traces

Simulate a focal plane for each spectral order and coadd

soss.png

Figure 16: NIRISS SOSS. Three orders cover a wavelength range of \(0.6-2.8\mu\textrm{m}\). Image Credit: STScI

JWST Readout Patterns

ramp_fig.png

Figure 17: General structure of detector readout scheme used by all JWST detectors. Image Credit: STScI

Readout N\(_{frames}\) N\(_{skip}\)
NISRAPID 1 0
NIS 4 0
NRSRAPIDD1 2 1
SHALLOW4 5 1

Instrument Specific PSFs

fig_instrument_comparison.png

Figure 18: Example PSFs from each JWST instrument and the fine guidance sensor.

Parallelization

Parallelization gives nearly an exact proportional decrease in run time for number of parallel processes

exosim-dask-noise.png

Figure 19: Dask parallel computing library task graph built during ExoSim execution.

Example NIRISS SOSS Simulation

niriss-soss-s256.png

Figure 20: NIRISS SOSS simulation from ExoSim.

Validation

Validating the Focal Plane Signal

A simulated black body was compared to an analytic expression

sim-predict-compare-normal-1.png

Figure 21: Flat spectral trace

sim-predict-compare-curved-1.png

Figure 22: Curved spectral trace

Comparison to Original ExoSim

To ensure no unforeseen changes were made to the noise models, I ran identical simulations in my modified version of ExoSim and the original version.

Comparison to PandExo

Table 1: Configuration for each instrument simulated (cont. next slide)
Parameter NIRSpec BOTS NIRCam F444W/Grism-R
Subarray SUB512 SUBGRISM64
Size \(32\ \times\ 512\) \(64\ \times\ 2048\)
W\(_{slit}\)(pix)(pix) 16 N/A
\(\Delta_{pix}(\mu\textrm{m})\) 18 18
PS\((^\circ \times10^{-5}/\Delta_{pix})\) 2.78 1.75
T(K) 40 40

Comparison to PandExo

Table 2: Configuration for each instrument simulated
Parameter NIRISS SOSS MIRI LRS
Subarray SUBSTRIP256 SLITLESSPRISM
Size \(256\ \times\ 2048\) \(72\ \times\ 416\)
W\(_{slit}\)(pix) N/A N/A
\(\Delta_{pix}(\mu\textrm{m})\) 18 25
PS\((^\circ \times10^{-5}/\Delta_{pix})\) 1.81 3.06
T(K) 40 7

Comparisons to PandExo - NIRSpec

flux-comp.png

Figure 23: Comparison of PandExo and ExoSim simulation of NIRSpec. Average percent difference of \(+1.53 \pm 1.63\)%.

Comparisons to PandExo - NIRCam

flux-comp-nircam.png

Figure 24: Comparison of PandExo and ExoSim simulation of NIRCam. Average percent difference of \(+2.18 \pm 1.08\)%.

Comparisons to PandExo - MIRI

flux-comp-miri.png

Figure 25: Comparison of PandExo and ExoSim simulation of MIRI. Average percent difference of \(+3.0 \pm 2.2\)%.

Comparisons to PandExo - NIRISS

flux-comp-niriss.png

Figure 26: Comparison of PandExo and ExoSim simulation of NIRISS. Average percent difference of \(+4.54 \pm 1.37\)%.

Future Work and Closing Remarks

Future Work

  • Write bridge between ExoSim and Pandeia
  • Find cause of discrepancy between simulations
  • Combine ExoSim, Py-JOSE, and BART for an end-to-end simulation and retrieval

Closing Remarks

In summary, I’ve described the development and validation of a time-domain simulator of exoplanet transits and systematic errors JWST.

This tool is open-source and available to the community with the hope that it is used to further our understanding of the effects of systematic noise on exoplanet transits and to prepare for observations of exoplanet transits with the James Webb Space Telescope.

Acknowledgements

Thanks to Dr. Joseph Harrington, Dr. Enzo Pascale, Dr. Ryan Challener, and Kathleen McIntyre for their support and guidance

Links

Bibliography