Elsevier

Planetary and Space Science

Volume 218, 1 September 2022, 105399
Planetary and Space Science

Calibration of NOMAD on ExoMars Trace Gas Orbiter: Part 3 - LNO validation and instrument stability

https://doi.org/10.1016/j.pss.2021.105399Get rights and content

Highlights

  • The LNO channel is 1 of 3 spectrometers in NOMAD on ExoMars Trace Gas Orbiter.

  • The LNO channel observes Mars in limb, nadir and solar occultation modes.

  • This article describes an alternative method of calibration for the LNO channel data.

  • The method is ​based on a comparison between observation of the sun by the LNO channel and a synthetic solar spectrum.

  • Temperature and time dependence of the instrumental responsivity were tested. Nadir observations can be calibrated radiometrically.

Abstract

The LNO channel is one of the 3 instruments of the NOMAD suite of spectrometers onboard the ExoMars Trace Gas Orbiter currently orbiting Mars. Designed to operate primarily at nadir at very high spectral resolution in the 2.3 ​μm–3.8 ​μm spectral region, the instrument observes the martian atmosphere and surface daily since March 2018. To perform an accurate calibration of the instrument, in-flight measurement needs to be integrated to account for potential change during the cruise phase and later during the mission. In a companion article, Thomas et al. this issue, PSS, 2021 proposed a method based on the use of 6 observation sequences of the sun by LNO to derive a self-consistent approach, assuming temporal stability. Here we report an alternative concept of calibration, model the instrument using basic principle, based on the comparison between each solar spectrum observed and a reference solar spectrum. The method has the advantages to allows testing of the temporal stability but also instrumental effects such as temperature. It encompasses the main transfer functions of the instrument related to the grating and the AOTF and the instrument line shape using 9 free parameters which, once inverted, allow the observations to be fitted with an acceptable Root Mean Square Error (RMSE) around 0.5%. We propose to perform a continuum removal step to reduce the spurious instrumental effect, allowing to directly analyze the atmospheric lines. This methodology allows quantifying the instrumental sensitivity and its dependence on temperature and time. Once the temperature dependence was estimated and corrected, we found no sign of aging of the detector. Finally, the parameters are used to propose an efficient calibration procedure to convert the LNO-NOMAD data from ADU to radiances with spectral calibration and the instrument line shape. A comparison with the method reported in Thomas et al. this issue, PSS, 2021 showed that both calibrations are in agreement mostly within 3%.

Introduction

The ExoMars program consists of two missions designed to study the trace gases of the martian atmosphere but also to acquire information on potential ongoing geological and biological processes on the surface of Mars (Vago et al., 2015). Since April 2018, the four instruments aboard the ESA/Roscosmos ExoMars Trace Gas Orbiter mission has acquired observations of both the atmosphere and surface of Mars. Among them the NOMAD instrument (Nadir and Occultation for MArs Discover), led by the Belgian Institute for Space Aeronomy (BIRA-IASB), is a suite of three spectrometers spanning the UV and IR spectral range: SO (Solar occultation), LNO (limb, nadir, and occultation) and UVIS (ultraviolet–visible). The three channels work separately but are all controlled via a single main electronic interface (Neefs et al., 2015). The two first channels are infrared spectrometers based upon the SOIR (Solar Occultation in the InfraRed) instrument aboard the Venus Express mission (Nevejans et al., 2006).

The LNO channel is a compact high-resolution echelle grating spectrometer with an acousto-optic tunable filter (AOTF) working in the infrared domain from 2.3 ​μm to 3.8 ​μm (4250-2630 ​cm−1) with a resolving power (λλ) of around 10 000, specially designed for nadir observation. With such high resolving power combined with the near-circular orbit of TGO permitting 12 orbits in one sol, promoting a global coverage of the planet, the NOMAD-LNO instrument is perfectly suited to study the martian surface and atmosphere.

The main objective of this article is to propose an original calibration procedure, adaptable for the full dataset of NOMAD-LNO. This calibration is complementary to the one proposed by Thomas et al. (2021) who developed a fully empricial method using in-flight data. In their paper the LNO ground calibration, occultation and nadir boresight pointing vectors, detector characterisation and illumination pattern are covered. A combination of several observation of the sun is used to derive instrument temperature effects such as the shape and intensity of a LNO spectrum. The radiometric calibration is done by assuming temporal stability of the instrument and directly using solar observation to calibrate nadir observation.

In this paper we will not assume temporal stability of the instrument. Our approach is thus able to investigate the temporal evolution of the instrumental sensitivity, which is expected to vary due to degradation by energetic particles. This approach will be based on an empirical continuum removal to take into account the departure between actual blaze function and its theoretical form. By construction, our approach is thus more robust but may fail to model some instrumental effect such as the temperature dependence of the blaze and AOTF transfer function on the raw continuum of an LNO spectrum. The main calibration of NOMAD-LNO is well described in Thomas et al. (2021). This complementary work aims to validate the calibration of LNO but also to give additional information about instrumental transfer function and instrumental line shape.

Section snippets

NOMAD LNO instrument

The optical design of the LNO spectrometer is identical to that of SO and therefore very similar to SOIR (Nevejans et al., 2006; Vandaele et al., 2013), it is a combination of a high-dispersion echelle grating along with an AOTF and a cooled detector. The main advantage of using an echelle grating is that the full height of the detector can be used to register spectral lines (Neefs et al., 2015), which greatly improves the SNR after column binning. In the spatial direction, the detector

Solar fullscan

The NOMAD-LNO fullscans are solar observation made for calibration purposes. The instrument, normally in nadir position, is pointing toward the sun. The choice of using solar fullscans was made for two reasons. First, there are not enough miniscans to cover all diffraction orders with a significant amount of data while fullscans always cover the whole spectral range which allows testing the time dependence of the calibration. Second, it is important to estimate the instrumental sensitivity over

Method

The calibration aim was to build a model to estimate the spectral conversion (wavenumbers in cm−1 for each spectels of the detector) and the photometric sensitivity (conversion factor from ADU to spectral radiance). The model must be versatile enough to face the uncertainties of some instrumental functions, such as the AOTF transfer function and the grating blaze function.

The method used here is based on the usual comparison between a real solar observation and a simulated solar spectrum. The

Justification of the continuum removal

All modeled effects are not able to perfectly fit both the overall shape of the spectra and the absorption lines of the observation as shown in Fig. 5. In this figure, we applied the calibration procedure with/without the continuum removal (Fig. 5 A and B). One can see that without the continuum removal, the fitting procedure is dominated by the large-scale feature and unfortunately not coherent with detailed solar line shape. Such results imply that in the present state of instrument

Results

Fit of order 189. An interesting way to check the validity of the model is to compare observations and simulations at the spectrum scale. Fig. 6 shows such comparison for order 189 on the whole of a fullscan (here 14/03/2 019), as an example. Here the spectra are flat due to the continuum removal step which allows apprehending only the level of the spectrum and the position of the bands. The 13 observation sequences are shown in a shade of gray while the optimized simulation after the inversion

Calibration pipeline

With such an approach any nadir observation can be calibrated to spectral radiance, the pipeline to calibrate a raw nadir spectrum is as follows: first, the raw spectrum is normalized following equation (1) with the spectral resolution (eq. (15)). Second, we remove the continuum using eq. (18) to get a flat spectrum. Then, knowing the temperature at the time of the measurement from housekeeping and using coefficients a and b from eq. (24), we apply the sensitivity factor to convert the

Conclusion

We propose an alternative calibration method for the LNO data using reference solar spectra with the advantage of being able to investigate the correlations between the instrumental sensitivity and the temperature of the instrument. By having done this, we can understand the potential temporal variations of the instrument due to its aging. The method is based on the adjustment of a synthetic spectrum to the solar data acquired with NOMAD-LNO fullscan operation mode, which allows a calibration

Author statement

Guillaume. Cruz Mermy: Methodology, Investigation, Software, Validation, Writing. Frédéric Schmidt: Methodology, Investigation, Software, Validation, Supervision. Ian R. Thomas: Investigation, Software, Validation, Supervision. Frank Daerden: Validation, Supervision. Bojan Ristic: Validation, Supervision. Manish R. Patel: Validation, Supervision. Jose Juan Lopez-Moreno: Validation, Supervision. Giancarlo Belluci: Validation, Supervision. Ann Carine Vandaele: Validation, Supervision.

Declaration of competing interest

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

Acknowledgements

The NOMAD experiment is led by the Royal Belgian Institute for Space Aeronomy (IASB-BIRA), assisted by Co-PI teams from Spain (IAA-CSIC), Italy (INAF-IAPS), and the United Kingdom (Open University). We would like to thank everyone involved in the ExoMars project. Funding: This project acknowledges funding by the Belgian Science Policy Office (BELSPO), with the financial and contractual coordination by the ESA Prodex Office (PEA 4000 103 401, 4000 121 493), by Spanish Ministry of Science and

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