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1.NANOCARB GHG SENSORGlobal and frequent (intraday) monitoring of greenhouse gases (GHG) is increasingly required to better model climate changes, especially to discriminate sources and sinks of GHG, and to help public policies of GHG reduction. Space measurement can provide such a global and frequent coverage, a constellation of about 25 satellites ensuring a revisit of half-a-day. However, due to budget constraints, such a mission should rely on small satellites and hence very compact payloads. These payloads consists in an instrument directly sensitive to GHG concentration, completed with an instrument dedicated to aerosol measurement, since it is recognized that aerosol estimation is a key element to improve the quality of GHG concentration retrieval from space optical measures [1]. During the H2020 Scarbo project [2][3], two such compact payloads were studied, the one for aerosol being SpexOne, from SRON [4] and the one focusing on GHG being Nanocarb. Nanocarb is a very compact imaging spectrometer, developed by Grenoble-Alpes University (UGA) and Onera in France [5]. Nanocarb has three key features (summed up on Figure 1 from [6]).
2.PERFORMANCE ESTIMATION OF A SPACE MISSION BASED ON A FIRST NANOCARB DESIGNDuring the Scarbo project, a first design of Nanocarb for a space mission was proposed, with an associated performance model on the radiometrically calibrated interferograms (L1 products). These outputs, with their counterparts from Spex, were merged by LMD (Laboratoire de Météorologie Dynamique, Palaiseau, France) to assess the quality of the estimated total GHG column (CO2 and CH4), called L2 product. These results were then used by Noveltis (France), SRON and the University of Bremen (Germany) to model the quality of the fluxes are local and regional scales (L4 products), but this is out the scope of this proceeding. We briefly recall in the next subsections this first Nanocarb design for a space mission, and the main results of the L2 performance estimation. More details can be found in [10][11][12]. 2.1First Nanocarb designThe Nanocarb payload consists in 4 cameras, each one dedicated to a specific spectral band where the targeted gas presents quasi-periodic lines: B1 for O2, B2 for CO2, B3 for CH4, and B4 also for CO2. The choice of these four spectral bands based on published design of other instruments, like CarbonSat ([13] table 5.3) or CO2M ([14]), but with a spectral range reduced to fit with the periodicity of the lines. From these spectral bands, relevant OPDs were selected, with a simple radiometric model [10], and with the requirements to maximize signal dependency to CO2 while minimizing dependency to H2O, and taking into account spectral shift of the narrow band filter and of the Fabry-Perot interferometer with incidence angle. The resulting spectral bands and OPD intervals are given in Table 1. Table 1.The four spectral bands of Nanocarb (first design): spectral ranges and OPDs
2.2Main results from the L2 performance estimationL2 performance estimation was performed in a simplified way [11], as it was evaluated on 324 scenarios corresponding to different values for 5 observation parameters: scene albedo (ALB), solar zenithal angle (SZA), height (CLH) and optical depth (COD) of a coarse aerosol layer, and optical depth of a fine aerosol layer (FOD). Interferograms from the 4 spectral bands were simulated thanks to an instrumental model of Nanocarb, and retrieval was performed jointly on the four spectral bands. In other words, what we call interferogram is actually the concatenation of the four interferograms provided by each Nanocarb camera. Retrieval was done according to the optimal estimation approach [15], with only 10 variables in the state vector: 3 scaling factors of H2O, CO2 and CH4 vertical profiles, surface pressure, 4 albedos (one for each spectral band), and 2 aerosol optical depths (for the coarse and fine modes). SpexOne data were used through an a-priori estimation of the aerosol parameters and the associated uncertainties. An important point is that the errors were calculated not for a single Nanocarb frame, but taking into account the numerous frames where a ground point appear: indeed, as Nanocarb is a 2D snapshot imager, a ground point is seen by successive frames, while it goes across the field-of-view. This significantly increases the amount of data available and thus reduces random error. The main results of this L2 performance estimation is summed-up on Figure 2, reproduced from [12]1: it shows that with the current Nanocarb design, precision better than 1 ppm for XCO2 and 6 ppb for CH4 are attainable. Obviously, this conclusion has to be slightly qualified. On one hand, the performance evaluation was done with simplifying hypothesis, for instance on the vertical profiles (including temperature), on the spectral variation of albedos, on measure noises, and so on. On the other hand, the Nanocarb design will be improved from the results of this L2 performance evaluation, especially by refining the selection of the spectral bands and of the OPDs. However, this L2 product study also emphasized another point to be improved, which is the correlation between gas concentration and albedo estimations. This is the topic we will discuss in the next of this proceeding. 3.CORRELATION BETWEEN ALBEDO AND GAS CONCENTRATION ON THE INTERFEROGRAM3.1Preliminary remarkThe illustrations below are made with simulated spectra calculated with 4AOP radiative transfer code [16]. Main simulation parameters are listed in Table 2. Some of these parameters differ from the ones used in [11] or [12], that is why a direct comparison with the numerical results that can be found in these references has to be done caustiously: especially, the nominal CO2 concentration is different, we do not consider aerosol, integration time is reduced, and in this proceeding we focus only on band B2. Our goal is indeed to describe tracks to reduce the correlation between albedo and XCO2 estimation, not to provide a thorough analysis of the system performance. 3.2MethodologyThe very common approach to retrieve the geophysical parameters from the measured interferograms is to minimize a merit function with two terms: a data fidelity term, and a regularization term, to take into account a-priori knowledge on these parameters. Here, we will neglect this latter term, since we focus on the instrumental model. Thus, under common simplifying assumptions on the noise (normal distribution), the merit function is the square of the Malahanobis distance between the measured interferogram and the simulated one. Furthermore, we assume that noise is decorrelated with the same standard deviation & for each OPD, so that the merit function χ2 to minimize is merely: with p the parameter vector, J(p, δi) the simulated interferogram at OPD δi and Imes (δi) the measured (and noisy) interferogram. If we note K the Jacobian matrix, that is then it can be shown that the covariance matrix on the retrieved parameters is given by: with K being calculated at the a-posteriori value for p, but we assume that is identical to K calculated at the true position. The square-root of diagonal elements of give the standard-deviation on the estimation of the parameters, and the nondiagonal elements give the correlation between these parameters. Table 2.Main parameters used for the simulation
Another (but equivalent) way to obtain this result is to compare χ′(p, ptrue) the distance between J(p, δ) and J(ptrue, δi) – ptrue being the true set parameters − with &, the “blur” radius due to noise around J(ptrue, δi). When J(p, δ) is closer to J(ptrue, δi) than &, p would become a likely parameter. In the vicinity of ptrue, χ′2(p, Ptrue) is the quadratic form of matrix Kt · K: the orientation of its eigenvectors indicate the correlation between the parameters. With only two parameters in the state vector, it is thus very easy to visualize the correlation between these two parameters. This is our case, since to focus on correlation between albedo and CO2 scale factor, we restrict our state vector to albedo and a scale factor on the CO2 vertical profile. 3.3Correlation between albedo and CO2 scale factor for the first Nanocarb design in band B2Let us take the example of the first Nanocarb design, with the filter and the OPDs defined in [11] (but limited to band B2). On Figure 3 we plotted χ′2(p, ptrue) normalized by , the variance of the noise level improved by the M multiple observations. We clearly see the correlation between albedo and CO2 concentration: the axes of the quadratic form are slanted with respect to the parameters (albedo, CO2 scale factor) axes: if we choose state vectors on the major axis of the ellipse, they may produce very similar interferograms, roughly indiscernible compared to the noise, up to a CO2 scale factor of 1.0048, or 2 ppm2 (see Figure 4, bottom, green plot). This is far larger than the width of the χ′2 function taken at constant albedo: if the albedo were known, the random error on CO2 scale factor would be greatly reduced (see Figure 4, bottom, red plot: if the albedo were known, this interferogram would not be likely copared with the noise level). It is thus desirable to reduce this correlation between albedo and CO2 concentration, either to reach better precision on CO2 estimation, or, at constant precision, to simplify the payload. In the next section, we propose possible solutions to this problem. 4.PROPOSITIONS TO REDUCE CORRELATION BETWEEN ALBEDO AND GAS CONCENTRATIONTo deal with this difficulty of the correlation between albedo and gas concentration, we could consider solutions based on pure processing of Nanocarb images. It could be for instance a joint retrieval of the whole pixels of the image3, with regularization conditions on albedo and CO2 spatial texture, like Total Variation (TV) regularization on the albedo image (to deal with edges), and smoother regularization function on CO2. However, we will not consider such solutions, to focus on hardware improvement. We listed two approaches: the first one is to add an imager dedicated to albedo estimation. This is a similar solution to the one brought to the problem of aerosol, with the presence of SpexOne, the output of which (aerosol information) being an input for Nanocarb retrieval. The second approach is to modify the Nanocarb interferometer, to reduce correlation at the very interferogram level. 4.1Panchromatic or hyperspectral ancillary imagerThe goal here is to estimate albedo with more information than the one provided by Nanocarb, which means that a panchromatic imager in exactly the same spectral band than Nanocarb would be of no use4. On the contrary, an hyperspectral imager would bring information at other wavelengths. It would thus allow to estimate the spectral slope of albedo to interpolate it in Nanocarb spectral bands. Furthermore, a visible and shortwave infrared (SWIR) hyperspectral camera would also improve Spex aerosol estimation at 1.6 μm. The main difficulty is the precision (and probably accuracy) required on the estimated albedo: for instance, with the scenario described at Section 3.3, precision on albedo has to be better than 0.1%. Another difficulty is that adding an hyperspectral camera compliant with this requirement would probably make the payload considerably heavier, and we would therefore lose one of the main asset of Nanocarb, its compacity. A panchromatic camera would be more adapted as a compact payload, but the limit is that a very narrow spectral band, to be out of the CO2 signature, will lead to a very low signal-to-noise ratio (SNR), while a broader spectral band would not bring more information than Nanocarb. Thus, a multispectral camera may be a good trade-off, to estimate the spectral slope of surface reflectance around the Nanocarb spectral band, while maintaining a high SNR and a low dependency to CO2 or other trace gas content. 4.2Multiple harmonics and higher finesse interferometerRather than relying on an additional camera, we can also try to reduce intrinsic sensitivity of Nanocarb to albedo. In this first analysis, we choose not to change neither the spectral band nor the number of OPDs (i.e. the number of micro-lenses of the Nanocarb camera), to focus only on the interferometer level. There are thus two free parameters: the plate thickness (i.e. the OPDs), and the surface reflectivity (i.e. the interferometer finesse). About the choice of OPDs, we could dedicate some of them to higher harmonics of the gas signature: they are still sensitive on CO2 and to albedo, but the ratio of dependency to these parameters may be different from the OPDs at the fundamental frequency, which could lead to a better separation of the parameters. Nevertheless, fringe contrast decreases as the harmonics increases, and the whole performance of the system is worse. For instance, if the twenty last OPDs are around 11.2 mm rather than 5.6 mm, the standard deviation on the CO2 scale factor increases to 0.006, instead of 0.005 for the initial set of OPDs. Changing the surface reflectivity seems more promising. Indeed, if we increase the surface reflectivity (i.e. the finesse of the interferometer), the baseline of the spectral transmission of the Fabry-Perot interferometer tends to zero. Consequently, the signal at the OPDs where the peaks of the Fabry-Perot spectral transmission do not coincide with the CO2 spectral lines does not depend (or only slightly) on CO2 concentration, but only on albedo. On the contrary, at OPDs where the peaks of the Fabry-Perot spectral transmission do coincide with the CO2 spectral lines, the signal contain as much information as with low finesse interferometer5. The limit is that the total measured signal decreases as the finesse increases. There is thus an optimal finesse, as it appears on Figure 5. In the studied configuration, with a finesse about 5, the standard deviation on the CO2 scale factor decreases to 0.004, but this exact optimal finesse may depend on the scenario (scene and system). 5.CONCLUSIONCurrent performance of Nanocarb is limited by the correlation between albedo and CO2 concentration. To overcome this limitation, a solution would be to use an ancillary camera, either hyperspectral (if we also want to increase aerosol correction) or multispectral (if we focus only on albedo estimation). The drawback of such a solution is to make a payload more cumbersome. Thus, another way would be to change the parameters of the Fabry-Perot interferometer at the heart of Nanocarb, and especially by increasing its finesse. In this current study, restricted to the spectral band around 1.6 μm, we showed that with a finesse equal to 5 rather than 2.5, the error on CO2 scale factor is decreased by 20%. A more thorough study will be conducted, both to confirm these results on more scenarios and to optimize Nanocarb spectral band and OPD definition. Notes[1] For sake of clarity, we discarded from this figure the sensitivity to uncertainties of SpexOne product (see p. 4850 from [12] for more details on this aspect). 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