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ORIGINAL RESEARCH article

Front. Remote Sens., 10 August 2021
Sec. Atmospheric Remote Sensing
This article is part of the Research Topic Polarization of Light as a Tool for Characterizing Different Facets of the Atmosphere-Ocean System View all 9 articles

Simultaneous Aerosol and Ocean Properties From the PolCube CubeSat Polarimeter

Snorre Stamnes
Snorre Stamnes1*Rosemary BaizeRosemary Baize1Paula BontempiPaula Bontempi2Brian CairnsBrian Cairns3Eduard Chemyakin,Eduard Chemyakin1,4Young-Jun Choi,Young-Jun Choi5,6Jacek Chowdhary,Jacek Chowdhary3,7Yongxiang HuYongxiang Hu1Minsup JeongMinsup Jeong5Kyung-In KangKyung-In Kang8Sungsoo S. Kim,Sungsoo S. Kim9,10Xu LiuXu Liu1Robert LoughmanRobert Loughman11Dave MacDonnellDave MacDonnell1M. Patrick McCormickM. Patrick McCormick11Bongkon MoonBongkon Moon5Ali OmarAli Omar1Carlos M. RoithmayrCarlos M. Roithmayr1Chae Kyung SimChae Kyung Sim5Wenbo Sun,Wenbo Sun1,10Bastiaan van Diedenhoven,,Bastiaan van Diedenhoven3,12,13Gorden Videen,,Gorden Videen10,14,15Andrzej Wasilewski,Andrzej Wasilewski3,16
  • 1NASA Langley Research Center (LaRC), Hampton, VA, United States
  • 2University of Rhode Island, Graduate School of Oceanography, Narragansett, RI, United States
  • 3NASA Goddard Institute for Space Studies (GISS), New York, NY, United States
  • 4Science Systems and Applications, Inc., Hampton, VA, United States
  • 5Korea Astronomy and Space Science Institute (KASI), Daejeon, South Korea
  • 6Department of Lunar and Planetary Science, University of Science and Technology, Daejeon, South Korea
  • 7Department of Applied Physics and Applied Mathematics, Columbia University, Broadway, NY, United States
  • 8Korea Advanced Institute of Science and Technology, Daejeon, South Korea
  • 9Department of Astronomy and Space Science, Kyung Hee University, Yongin, South Korea
  • 10Humanitas College, KHU, Yongin, South Korea
  • 11Department of Atmospheric and Planetary Sciences, Hampton University, Hampton, VA, United States
  • 12Center for Climate Systems Research, Columbia University, New York, NY, United States
  • 13Now at SRON Netherlands Institute for Space Research, Leiden, Netherlands
  • 14US Army Research Laboratory, Adelphi, MD, United States
  • 15Space Science Institute, Boulder, CO, United States
  • 16SciSpace LLC, Bethesda, MD, United States

We quantify the performance of aerosol and ocean remote sensing products from the PolCube instrument using a previously developed polarimeter retrieval algorithm based on optimal estimation. PolCube is a modified version of the PolCam lunar instrument on the Korea Pathfinder Lunar Orbiter that has been optimized for Earth-Science observations of aerosol, ocean, and thin cloud optical properties. The objective of the PolCube instrument is to retrieve detailed fine-mode (pollution and smoke) and coarse-mode (sea-salt and dust) aerosol properties over the ocean for a range of light to heavy aerosol loadings using its polarimetric-imaging capability at multiple angles and wavelengths from 410865 nm. An additional objective is to discriminate aerosols from thin clouds. PolCube’s retrieval performance of aerosol optical and microphysical properties and ocean products is quantitatively assessed. We estimate that PolCube can retrieve total aerosol optical depth at 555 nm (AOD555) within ±0.068, fine-mode AOD555 within ±0.078, and fine-mode single-scattering albedo within ±0.036, where all uncertainties are expressed as one standard deviation (1σ). PolCube’s accurate and high-resolution aerosol-retrieval products will provide unique spatial and temporal coverage of the Earth that can be used synergistically with other instruments, such as the Geostationary Environmental Monitoring Spectrometer to improve air-quality forecasting.

1 Introduction

The 2017 Decadal Survey for Earth Science and Applications from Space identifies aerosol absorption as one of the key geophysical variables to address as part of the Aerosols Designated Observable (National Academies of Sciences and Medicine, 2018), which is now part of the future NASA Aerosols, Clouds, Convection and Precipitation (ACCP) mission (Braun et al., 2019). Aerosol absorption or SSA is one of the most difficult aerosol properties to retrieve from remote-sensing measurements. Retrieval of aerosol absorption requires simultaneous retrieval of aerosol height; currently, aerosol location represents one of the largest uncertainties of aerosol-absorption retrievals (Buchard et al., 2015). Improved quantification of aerosol absorption is critical for applications including aerosol direct radiative forcing, actinic flux for photochemistry applications, aerosol speciation, aerosol transport, aerosol processes such as aging, and the retrieval of ocean color properties (Stamnes et al., 2018). Aerosol absorption is critical for calculating aerosol direct radiative forcing, the uncertainty of which is still large even over clear-sky ocean (±1.25 W/m2) (Thorsen et al., 2020). Aerosol absorption is needed for atmospheric-chemistry applications to quantify accurately the actinic flux, which controls photolysis rates (Tian et al., 2019) and particle formation that create cloud-condensation nuclei (Zheng et al., 2021). Aerosol absorption is important for aerosol speciation since aerosols produced by biomass burning and combustion processes from industry and automobiles can be highly absorbing.

Aerosol absorption is critical for accurate retrieval of water-leaving radiances in coastal zones where the presence of multiple aerosol types above complex waters creates tremendous challenges for single-angle multi-wavelength instruments (Kahn et al., 2016). Yet the coastal zones are where a majority of people live and these zones support activities such as tourism, recreation, agriculture, transportation, and fisheries. Moreover, these estuarine environments are where the greatest concentrations of organic and inorganic nutrients are found and transformed. Complex aerosol situations can arise in coastal zones where the continental outflows of pollution, smoke and dust mix together in layers, become processed by clouds, and absorb water, change shape, bleach, and undergo photochemical transformations. Retrieval of aerosol properties in coastal zones is complicated by the complexity of ocean water because of terrestrial river outflows, sewer discharges, plankton blooms, and resuspension of unconsolidated bottom sediments (Loisel et al., 2013).

Aerosol speciation is significantly improved by knowledge of absorption, size, and real refractive index. Aerosol size and real refractive index are linked to relative humidity since hygroscopic aerosols grow in size and approach the real refractive index of water as they collect moisture (Schuster et al., 2009). Accurate quantification of aerosol size and real refractive index can improve our understanding of the Earth’s water cycle and aerosol-cloud interactions. In turn, improved aerosol speciation allows for improved aerosol air quality forecasts and monitoring (Lin et al., 2005; Dubovik et al., 2019), aerosol transport (Chin et al., 2007) and chemical transformations (Tian et al., 2019).

Thus, accurate and reliable remote sensing of aerosol microphysical properties, such as absorption and size, is necessary to address critical unanswered questions in Earth Science from aerosols’ impact on climate change to the health of the oceans. Single-angle multi-wavelength total radiance (intensity) measurements such as from the Moderate Resolution Imaging Spectroradiometer (MODIS) or the Visible Infrared Imaging Radiometer Suite (VIIRS) are unable to retrieve aerosol absorption, and aerosol absorption is difficult to characterize from multi-angle intensity measurements such as from the Multi-angle Imaging SpectroRadiometer (MISR). Multi-angle multi-channel total and polarized radiance measurements are necessary to determine aerosol absorption reliably. The only currently known and practical method to characterize column-averaged aerosol optical and microphysical properties from space is through multi-angle multi-wavelength polarimeter measurements (Cairns et al., 1999; Mishchenko et al., 2004; Mishchenko et al., 2007; Knobelspiesse et al., 2012; Stamnes et al., 2018; Chowdhary et al., 2019; Dubovik et al., 2019). Collocated multi-channel UV-VIS-NIR lidar measurements, particularly high-spectral-resolution lidar measurements are synergistic with polarimeter measurements and can enable the retrieval of vertically-resolved aerosol optical and microphysical properties (Liu et al., 2016). For that reason the NASA ACCP mission calls for a high-spectral resolution lidar together with a multi-angle multi-channel polarimeter to resolve vertical aerosol properties, such as absorption in the free troposphere and planetary boundary layer. Unfortunately, ACCP is not expected to launch until 2027 or later. Nonetheless, the outlook for polarimetry is promising with four set to launch in the 2023–2024 timeframe (3MI/MetOp-SG, SPEXone/PACE, HARP2/PACE, MAIA). Despite this promising outlook, currently there is a lack of satellite polarimetric measurements meaning aerosol absorption is poorly quantified. Polarimeters with finer spatial resolutions of ∼1 km and better allow for neighborhood-resolved air quality monitoring, enhanced water quality monitoring in heterogeneous coastal zones, improved cloud screening, and the retrieval of small, broken cumuliform cloud microphysical properties. Enhanced polarimetric accuracy enables improved measurements of aerosol properties such as absorption. Crucially, dramatically reduced instrument costs are needed to enable constellations of small satellite polarimeters that collect measurements at multiple times each day to resolve hourly variations in aerosol and cloud properties. An example of this dramatic reduction price without sacrifice in capability is the HARP polarimeter that deployed from ISS in 2020 (Martins et al., 2018).

To further the goal of high capability and low cost, we consider a modification to the Wide-Angle Polarimetric Camera (PolCam) (Jeong et al., 2018) that can reliably and accurately retrieve aerosol optical and microphysical properties across the VIS-NIR. PolCam was developed for the KPLO mission and will make lunar polarimetric observations beginning in 2023 (Ju, 2017; Jeong et al., 2018; Sim et al., 2019). The PolCam instrument was designed to measure the lunar bidirectional reflectance and polarized reflectance distribution functions (BRDF and BPDF) and to retrieve lunar grain size. In this paper we introduce a modified version of this polarimeter instrument for Earth-Science applications called PolCube. PolCube will provide improved characterization of the absorption and scattering by small particles (aerosols) in the Earth’s atmosphere, which requires total radiance and polarized radiance measurements from multiple angles and at multiple wavelengths. We quantify PolCube’s ability to characterize aerosols by analyzing the retrieval capability of detailed aerosol optical and microphysical properties including aerosol absorption, effective radius and refractive index using the Microphysical Aerosol Properties from Polarimetry (MAPP) retrieval algorithm (Stamnes et al., 2018). Another target of observation for PolCube is the detection of thin liquid water and cirrus clouds using polarized reflectance measurements near backscattering viewing geometries (Sun et al., 2014) and the characterization of ice cloud crystal shape and scattering properties (van Diedenhoven et al., 2012). The miniature and cost-effective design of new CubeSat polarimeters such as PolCube and HARP (Martins et al., 2018) are poised to provide greatly enhanced spatial (1 km) and temporal coverage of aerosol and cloud optical and microphysical properties. PolCube is a joint international and educational outreach mission between NASA Langley Research Center (LaRC), NASA Goddard Institute for Space Studies (GISS), the Korea Astronomy and Space Science Institute (KASI), Kyung Hee University, Hampton University, University of Rhode Island, Army Research Lab and the city of Busan, Republic of Korea. PolCube is expected to launch in 2023.

The PolCube design, modified for Earth observations, is based on a rich dataset of aircraft polarimeter measurements (Cairns et al., 1999). PolCube has two cameras whose wavelengths and viewing angles are optimized for remote sensing of aerosols in the Earth’s atmosphere. The PolCube instrument is outlined in Section 2. The aerosol and ocean remote-sensing retrieval capability of PolCube is analyzed starting from Section 2.1. PolCube’s measurement capabilities are described in Section 2.2, and the aerosol model is described in Section 2.3. PolCube’s products and their uncertainties are listed in Section 2.4. A desired orbit for PolCube and collocation of PolCube data with GEMS, TEMPO and Sentinel-4 is discussed in Section 2.5. A conclusion is provided in Section 3.

2 PolCube Instrument Design

The PolCube concept and design, based on PolCam (Jeong et al., 2018; Sim et al., 2019), is described in Figure 1 and Table 1. PolCube consumes approximately 10 W, weighs 4 kg, occupies a volume of 8 U, and will launch as a 19 U CubeSat upon integration with the spacecraft bus. The two optical heads (cameras) of PolCube will be separated by 50° as depicted in Figure 1. In the default operating attitude, PolCube will have one camera pointing backward at 25° and one camera pointing forward at +25°. However, the spacecraft’s attitude control system will allow four regions per day to be observed with PolCube pitched up by 25° such that one camera points at nadir, and one camera points forward at 50° (as depicted in Figure 1). The results of aerosol and ocean properties for this forward-looking mode are discussed in this paper, but the results for both modes are provided in Section 2.4. To simulate performance of this forward-looking attitude, two viewing zenith angles (VZA) are selected from the range of viewing zenith angles afforded by each camera after correcting for Earth curvature. The two viewing zenith angles for the forward-looking attitude are approximately {+57°,+52°} for the forward-viewing camera and {0°,5°} for the nadir-viewing camera. For the default operating attitude, the VZA are approximately {+30°,+25°} and {25°,30°}. PolCube has four spectral channels across the spectrum of the visible (VIS) to near infrared (NIR): 410,555,670,865nm. Since PolCube has four spectral channels with four viewing angles that each construct two observables (the total radiance I and the degree of linear polarization DoLP), PolCube collects 32 measurements of each Earth ground pixel.

FIGURE 1
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FIGURE 1. The PolCube CubeSat polarimeter mission will study aerosols and complement current GEMS, TEMPO and Sentinel-4 satellite observations, and future PACE, 3MI/MetOp-SG and ACCP missions. SSAI/Tim Marvel.

TABLE 1
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TABLE 1. Summary of PolCube CubeSat instrument capabilities and spacecraft specifications.

Each PolCube camera is a pushbroom imager as depicted in Figure 1. The cameras have a 10° FOV imaged onto a Teledyne e2v Onyx EV76C664 CMOS focal plane with 1,024 by 1,280 pixels. To increase SNR, each set of 4×4 pixels are averaged into a super-pixel. The cross-track set of 1,024 pixels is used to measure swath ±5°. The along-track set of 1,280 pixels is used to achieve spectral and polarization measurements via the use of bandpass spectral filters and wire-grid polarizers. With an approximate orbit altitude of 567 km the corresponding swath is approximately ±50km and the nadir-facing super-pixel ground resolution is 0.39×0.31km (cross-track × along-track). The super-pixel viewing a target at which VZA =57° has a ground resolution of 0.65×0.96km after taking into account Earth curvature, and represents PolCube’s effective multi-angle super-pixel ground resolution.

The detector wavelengths and bandwidths for PolCube are based on the airborne NASA GISS Research Scanning Polarimeter (RSP) (Cairns et al., 1999) design that was optimized for aerosol observations. The center wavelengths and the full width half maximum (FWHM) bandwidths in parentheses are 410(20),555(20),670(20),865(20)nm. The bandwidth for the 865 nm channel is broad enough to collect sufficient signal, and not too broad as to overlap with absorption by the surrounding water vapor bands.

There is a tradeoff between swath and the number of viewing angles. The goal is to achieve a swath of 100 km in the cross-track while ensuring enough viewing angles in order to retrieve aerosol optical and microphysical properties to within the desired uncertainties. A study was performed to trade the number of cameras (23) and the number of viewing angles. Different sets of viewing angles for the PolCube cameras were investigated: three angles, four angles, six angles, and either 20 or 30 degrees FOV with hyperangular viewing angle resolution (1°resolution). In order to anchor our results against a best-case scenario in terms of aerosol performance, RSP was used to represent a state-of-the-art polarimeter design. RSP has seven window channels (410,469,555,670,865,1594,2264nm) with 100+ angles between ±55°. Based on this trade study our performance objectives were met with a design that called for two cameras with four spectral channels (410,555,670 and 865 nm) with four viewing angles per channel. Inclusion of the 865 nm channel was needed for coarse-mode aerosol properties. Table 1 summarizes the PolCube instrument.

2.1 PolCube Aerosol and Ocean Performance Analysis

The objective is to perform an aerosol and ocean property-retrieval performance study of aerosol optical and microphysical properties from the PolCube polarimeter satellite instrument. The performance of PolCube is assessed by performing retrievals on synthetic PolCube data for aerosol and ocean properties that were randomly generated by Monte Carlo as by Stamnes et al. (2018). These randomly varying input parameters are subsequently used by a vector radiative transfer (RT) code (Hansen and Travis, 1974; Cairns et al., 1999) to generate synthetic PolCube data for a wide range of scenarios with different aerosol properties, ocean windspeeds and sub-surface inherent optical properties (IOP)s and viewing geometries (Stamnes et al., 2018; Hasekamp et al., 2019).

The inversion of PolCube synthetic data is carried out using the MAPP algorithm. The state vector of PolCube MAPP retrieval parameters is defined as

x=xaerosolxocean(1)

where xaerosol is the aerosol state vector defined in Section 2.3 and  xocean is the ocean state vector. The ocean model is described by chlorophyll-a and windspeed (Chowdhary et al., 2012; Stamnes et al., 2018) so that the ocean state vector is given by

xocean=v[Chla](2)

where v is the windspeed in m/s and [Chla] is the chlorophyll-a concentration in mg/m3.

2.2 Synthetic PolCube Data and Measurement Error Model

PolCube measures the TOA total radiance and the degree of linear polarization RI, RDoLP at four channels: 410,555,670, and 865 nm. The VZA are 57°,52°,0°,5°. The measurement errors are assumed to be normally distributed. Based on PolCube’s instrument performance specifications, synthetic PolCube data are created by applying a simple Gaussian measurement error model that assigns 2% error to the total and polarized reflectances RI, RQ, RU, and where the DoLP error is propagated from the reflectances. For each synthetic-data simulation, the solar zenith angle is randomized between 0°60° and the solar-instrument relative azimuth angle is randomized between 0°180°. The random set of Monte Carlo generated state vectors defined in Eq. 1 represents ground truth, while the corresponding forward-modeled measurements with random Gaussian noise are the PolCube synthetic data.

2.3 Aerosol Model

To simulate aerosol retrieval performance by PolCube, we use three types of distinct aerosols externally mixed together: a fine-mode aerosol component, a sea-salt aerosol component, and a dust aerosol component. The fine-mode aerosol component (used to denote aerosol particles that have effective radii <1 μm (Hansen and Travis, 1974)) is also known as the accumulation mode, and the vast majority by number concentration of aerosols with radii greater than 50 nm are typically contained within this mode. The fine-mode aerosol is made up of both natural and anthropogenic aerosols such as biomass burning aerosol (smoke) and pollution, so its optical and microphysical properties, such as size and absorption, can be highly variable. By contrast, coarse-mode aerosols (which have effective radii >1 μm) such as sea-salt and dust tend to have natural sources. As a result, the fine-mode is of particular importance to a wide range of aerosol applications from air quality to speciation, transport, and the direct aerosol radiative effect. In our study we try to capture this significant variability of the fine-mode aerosol properties, since these aerosol applications are a particular focus of PolCube. The marine planetary boundary layer is fixed to 01 km and contains fine-mode aerosol mixed together with sea-salt aerosol. Above that, a free tropospheric layer contains fine-mode aerosol mixed with dust aerosol. The aerosol height of this upper aerosol layer is allowed to vary between 1.1 and 5 km.

The following aerosol parameters and ranges are investigated for these three aerosol components (see the first three columns in Table 2). In terms of amount, the fine-mode AOD555 varies from 0 to 0.5, the sea-salt AOD555 varies from 0 to 0.2, and the dust AOD555 varies from 0 to 0.2. In terms of size, the fine-mode effective radius varies from 0.1 to 0.4 μm (in mode radius, 0.063–0.254 μm), the sea-salt effective radius from 1.0 to 3.5 μm (in mode radius, 0.308–1.079 μm), and the dust effective radius from 1.0 to 4.0 μm (in mode radius, 0.176–0.706 μm). In terms of composition, the fine-mode real part of the refractive index varies from 1.36 to 1.65 and the fine-mode imaginary part of the refractive index varies from 0 to 0.03 (resulting in a range of SSA from 0.8 to 1.0). In addition, the following two ocean surface parameters are varied: windspeed from 0.02 to 11.5 m/s and chlorophyll-a concentration from 0.025 to 9.9 mg/m3.

TABLE 2
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TABLE 2. PolCube aerosol and ocean products. The ranges used in the Monte Carlo simulations are listed in the third column. The fourth column lists desired uncertainties, and the corresponding PolCube simulated retrieval performance is in the fifth column (forward-looking attitude) and sixth column (default attitude). All uncertainties are given as 1σ uncertainties, and the RMSD is used to estimate the 1σ retrieval performance of the PolCube instrument.

The following assumptions for the aerosol and ocean surface parameters are made, or assumed, to be known a priori. It is assumed that the aerosol particles can be approximated by spherical particles with lognormal size distributions. The fine-mode effective variance is assumed to be 0.2 (in mode width, 0.427). The fine-mode real and imaginary parts of the complex refractive index can vary, but are assumed to be constant with wavelength, which is generally considered to be a reasonable assumption in the VIS-NIR. The sea-salt complex refractive index is fixed to 1.01 times that of water (1.35 + 0i in the VIS). The sea-salt effective variance is fixed to 0.6 (in mode width, 0.686). The dust complex refractive index is assumed to be fixed, and is set equal to the mean dust properties found at the Bahrain-Persia AERONET site (Dubovik et al., 2002) so that the dust real refractive index is equal to 1.55 and the dust imaginary refractive index is equal to 0.0025 at 355 and 410 nm, and 0.001 at 670 nm. The dust effective variance is fixed to 1.0 (in mode width, 0.833). We sought to balance realism with simplicity by employing an ocean model that varies with windspeed and chlorophyll-a concentration (Chowdhary et al., 2012; Stamnes et al., 2018). We are assuming that a realistic ocean bio-optical model can be constructed for a given region of interest that co-varies with chlorophyll-a (and/or other suitable parameters) for the purpose of retrieving accurate aerosol properties at the PolCube channels.

The aerosol state vector is therefore defined as

xaerosol=τfτcτdreff,freff,creff,dnrfnifhf(3)

where nif is the imaginary refractive index of the fine-mode aerosol, and is the main parameter that determines fine-mode SSA. The other symbols are defined in the second column of Table 2.

2.4 PolCube Aerosol and Ocean Products

The PolCube retrieval performance of the forward-looking mode for several aerosol and ocean properties are given in Figure 2. The total AOD555 is depicted in Figure 2A. Using RMSD as a measure of retrieval performance, such that we expect to be within 2σ for 95% of successfully converged retrievals, the 1σ total AOD555 performance is 0.068, and the R-correlation coefficient is 0.95. The mean absolute deviation (MAD) is also listed and tends to be significantly smaller than the RMSD since it comparatively places less weight on the larger deviations and more weight on the smaller deviations. The choice of RMSD rather than MAD to estimate retrieval performance is two-fold: 1) based on prior empirical studies where RMSD from synthetic retrievals resulted in realistic values (Stamnes et al., 2018; Hasekamp et al., 2019), and 2) since RMSD values are larger than other metrics such as MAD, it naturally leads to more conservative uncertainty estimates. We prefer to err on the side of caution and underestimate performance rather than overestimate it, but will attempt to achieve the uncertainties suggested by the MAD metrics in practice on real data. The listed standard deviation (SD) measures the spread of the deviations from the mean deviation. A total of 1,024 retrievals were performed, and a χ normalized cost function threshold was used to discriminate between successful and failed retrievals. Using χ<0.7 results in 771 successful retrievals for a convergence rate of 75.2%. The normalized cost function is defined by

χ=1m12(fy)TSϵ1(fy).(4)

where m=32 is the number of PolCube measurements from Table 1, x is the state vector from Eq. 1, f is the forward-modeled I and DoLP at the four channels and viewing angles, and y is the corresponding synthetic PolCube measurements for I and DoLP. Sϵ is the measurement error covariance which is defined using covariances CIsim=(0.02I)2, CQsim=(0.02Q)2, CUsim=(0.02U)2, that are propagated to the degree of linear polarization, DoLP=Q2+U2I such that. Sϵ=diag(CIsim,CDoLPsim).

FIGURE 2
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FIGURE 2. PolCube retrieval performance of aerosol optical and microphysical properties of the forward-looking mode. The root-mean-square deviation (RMSD) is used to estimate 1σ retrieval uncertainty, and the results are defined in Table 2. The dashed black lines represents the desired ±1σ uncertainty in the same table. (A–D) Display AOD555 performance referenced to 555 nm. PolCube AOD555 uncertainties are 0.068 (total), 0.078 (fine-mode), 0.039 (sea-salt), and 0.038 (dust). (E) PolCube’s fine-mode effective radius (size) uncertainty is 0.059 μm. (F) PolCube’s fine-mode SSA uncertainty, which is directly proportional to absorption, is 0.036 at 555 nm.

The PolCube retrieval performance of the AOD555 for each of the three aerosol species separately is depicted in Figures 2B–D. The 1σ uncertainty is 0.078 for the fine-mode AOD555, 0.039 for sea-salt AOD555, and 0.038 for dust AOD555. The corresponding R correlation coefficients are 0.91, 0.75, and 0.79, respectively. Figures 2E,F depict the retrieval performance of two important fine-mode aerosol microphysical products: the effective radius and single-scattering albedo, which quantify size and absorption, respectively. The fine-mode effective radius is retrieved to 0.059 μm with an R correlation coefficient of 0.73. The fine-mode SSA is retrieved to ±0.036 with an R correlation coefficient of 0.64. For the ocean properties, we used a criteria of AOD555<0.3. For this criteria, windspeed is retrieved to ±1.1 m/s with an R correlation coefficient of 0.94. We note that chlorophyll-a concentration [Chla] is difficult to retrieve during high aerosol loading, but for cases of low-to-moderate aerosol loading, we can use PolCube’s aerosol retrieval products to improve [Chla] estimates from collocated ocean color measurements. [Chla] is retrieved to ±2.4 mg/m3 with an R correlation coefficient of 0.62.

A summary of PolCube retrieval performance for all aerosol and ocean products is given in Table 2. The desired uncertainty targets are listed in the fourth column. The performance of PolCube’s forward-looking mode, which can be used to target four regions per day, is given in the fifth column. By comparison, the default observation attitude leads to increased uncertainties by single digit percentages for all properties except total and fine-mode AOD, which have increased uncertainties of 43 and 33%, respectively. All of the aerosol and ocean products meet the desired uncertainties under the forward-looking mode. And all products except AOD meet or nearly meet the desired uncertainties under the default operating attitude. On this last point, we note that for global observations using Polcube’s default observing attitude, the presence of three aerosol modes is probably overly complex and may underestimate performance: we would expect improved total and fine-mode AOD performance when the aerosol is only a mixture of two species, e.g. fine mode and sea-salt only.

2.5 PolCube Orbit and GEMS, TEMPO and Sentinel-4 Collocated Data

GEMS (Kim et al., 2020) is a geostationary mission designed to monitor trans-boundary pollution events for the Korean peninsula and the Asia-Pacific region using a scanning ultraviolet-visible spectrometer (300–500 nm) with hyperspectral resolution (0.6 nm). GEMS will contribute to the understanding of pollution events, source/sink identification, and long-range transport of pollutants and SLCFs (Short-Lived Climate Forcers) as a part of the activities of the Atmospheric Composition Constellation under CEOS (Committee on Earth Observation Satellites). GEMS, which obtains observations of the Asia Pacific region, is part of a constellation that includes other geostationary pollution monitoring satellites: TEMPO (Tropospheric Emissions: Monitoring Pollution, North America) and Sentinel-4 (Europe and North Africa). GEMS has been designed to provide hourly measurements of aerosols and ozone at high spatial resolution over Asia and to monitor regional transport events of transboundary pollution and Asian dust. GEMS is also designed to improve our understanding of the interactions between atmospheric chemistry and meteorology, and interhemispheric transport of Asian pollution across the Pacific.

A proposed orbit that would maximize synergies between PolCube and GEMS (and TEMPO and Sentinel-4) is depicted in Figure 3. This particular sun-synchronous orbit has a ground-track repeat of one day, which means the ground tracks would not shift. The spacecraft is moving approximately northward when it passes over the ground tracks directed from southeast to northwest; each point at which the spacecraft passes northbound through the equatorial plane is known as an ascending node, and the time of each such crossing is local solar noon. The subsatellite point is in daylight in the sections of ground track shown with a black curve. After the spacecraft reaches its northernmost latitude, it moves approximately southward over tracks (not shown) directed from northeast to southwest and each southbound pass through the equatorial plane occurs at local solar midnight. A non-shifting ground track together with PolCube’s pointing capabilities can maximize collocation of PolCube VIS-NIR data with GEMS for a target region. Collocated PolCube data will improve GEMS aerosol retrievals by simultaneously measuring multi-angular total and polarized radiances across a wavelength range of 400–865 nm. In particular, PolCube’s longer wavelength observations will help GEMS to improve retrieval of the coarse-mode AOD555 (sea-salt and dust aerosol) and aerosol speciation via separation of the total AOD555 into fine- and coarse-mode AOD555. Critically, it is expected that PolCube will be able to improve GEMS estimates of aerosol absorption, aerosol height, and surface reflectance, which represent the largest uncertainties in retrievals of ozone and trace gases. PolCube’s polarized radiance measurements at 410 nm are particularly useful for constraining aerosol height compared to radiance-only measurements (Wu et al., 2015), and can also assist GEMS to correct for intensity polarization sensitivity effects.

FIGURE 3
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FIGURE 3. A proposed orbit for the PolCube instrument chosen for synergy with the GEMS, TEMPO and Sentinel-4. This unique sun-synchronous orbit has an altitude of 566.90 km with an inclination of 97.66° resulting in an orbit with a ground-track repeat of one day. The local time of the ascending node is noon, but the orbit altitude and crossing time are subject to change based on ride share availability. The epoch for this simulation was set to the first day of fall in the Northern hemisphere: September 23, 2018. PolCube will be capable of collecting global measurements. Several important study regions include the Yellow Sea that borders China to the West and South Korea to the East; the Gulf Coast, Great Plains and Western United States including Texas and California; Hawaii and the Pacific Ocean; the North slope of Alaska; Northern Norway, the United Kingdom, Ireland, and coastal Western Australia. This orbit also provides coverage of the NASA Earth Venture Suborbital study domains West of Africa (ORACLES), the North Atlantic (NAAMES), and the Eastern seaboard (ACTIVATE).

PolCube will help address GEMS objectives related to aerosol transport and air quality, including outflows from the Asian continent, and can contribute to atmospheric-chemistry studies by improving retrievals of the actinic flux that is required for photochemistry applications and is a function of AOD555, height and SSA (absorption). PolCube is also expected to improve estimates of particulate composition through the retrieval of aerosol effective radius (size) and refractive index (chemical composition). PolCube will make measurements in the Yellow Sea of trans-Pacific fine-mode pollution transport, separate from sea-salt and dust aerosol, providing critically needed data for regional air-quality studies (Shin et al., 2015; Noh et al., 2016). PolCube can help GEMS provide enhanced retrievals of spatial and temporal variations of aerosol properties, facilitate studies of aerosol-cloud interactions and meteorological impacts, and improve air quality forecasts.

3 Conclusion and Future Work

Accurate and reliable retrieval of aerosol microphysical and optical properties such as SSA (absorption) is a difficult problem. However, solving this aerosol problem becomes possible using a multi-channel, multi-angle polarimeter together with retrieval algorithms that correctly treat the atmosphere and ocean as a coupled system and that can optimize total and polarization measurements from multiple channels simultaneously. We have used an accurate, coupled vector radiative-transfer model with optimal estimation to investigate the performance of the future PolCube CubeSat polarimeter which takes its heritage from the PolCam lunar polarimeter on KPLO. PolCube significantly improves upon current aerosol satellite measurements with its capability to retrieve aerosol microphysical properties such as speciated AOD, effective radius and SSA.

The real-world is rich in diversity and cannot be easily replicated via simulations, but we outline a simple yet robust performance analysis that uses Monte Carlo-style simulations to randomly vary aerosol and ocean conditions. By combining this Monte Carlo-style aerosol and ocean model with accurate vector radiative-transfer calculations of the coupled atmosphere and ocean system, together with reasonable estimates for the PolCube instrument measurement uncertainties, we can provide a reasonable estimate of real-world aerosol-retrieval performance. The validity assumes that the ranges and assumptions that we made reasonably cover the actual range of observations. The assumption that all the aerosol and ocean parameters are essentially uncorrelated, when in fact they may be correlated, may cause performance to be underestimated. This underestimation is to some extent balanced by a potential overestimate of performance because variability in aerosol and ocean properties that are not captured completely by our simplified Monte Carlo simulations will also need to be retrieved or constrained by adding a priori information. Furthermore, proper cloud screening is needed to perform aerosol retrievals. The multi-angle polarization measurements provide sensitivity to detect clouds, including thin cirrus (Sun et al., 2014; Stap et al., 2015).

Overall, the aerosol retrieval of PolCube with four channels 410, 555, 670, and 865 nm and four viewing zenith angles from two cameras centered at nadir and approximately 50° meets or exceeds our desired aerosol performance requirements listed in Table 2 although some parameters, like fine-mode AOD555, SSA, and sea-salt effective radius are more difficult to retrieve. An additional channel in the UV at 355 or 380 nm would help provide additional information about UV aerosol properties and the impacts of brown carbon on the actinic flux as well as oceanic color dissolved organic matter absorption. Thanks to PolCube’s flexible and scalable design, which has no moving parts, future versions of PolCube can be readily modified to include additional wavelengths, a wide field of view using lenses for increased swath and viewing angles, and to incorporate new detector technologies to improve SNR of the Stokes components. PolCube could be placed in a different orbit than the one suggested here. The rapid advances of CubeSat bus capabilities in pointing and attitude control enable dynamic missions that can target wildfires, dust storms, and volcanic eruptions, enabling applications such as improvements to air quality and severe-weather forecasting.

Future work involves analyzing and applying PolCube for additional applications. These include air quality, atmospheric chemistry, water quality, and terrestrial biogeophysical properties, including cryosphere properties, such as snow grain impurity, size and shape, in addition to exploring the use of combined PolCube measurements and retrieval products with other satellite measurements such as from GEMS, TEMPO and Sentinel-4.

Data Availability Statement

The raw data supporting the conclusion of this article will be made available by the authors, without undue reservation.

Author Contributions

PolCube design: SS, RB, PB, BC, Y-JC, YH, MJ, K-IK, SK, DM, BM, AO, CS, WS, and GV. PolCube hardware: Y-JC, MJ, K-IK, and BM. Orbit and viewing geometry considerations: SS, BC, Y-JC, JC, YH, BD, JC, YH, MJ, SK, AO, CR, CS, WS, BD, GV, and AW. Algorithm development and quality control: SS, BC, EC, JC, YH, SK, XL, RL, PM, AO, CS, and GV. Text: All authors.

Funding

The work by authors SS, RB, EC, YH, DM, AO, CR and WS was funded by NASA Langley Research Center. The work by SK was supported by the National Research and ICT (2019R1A2C1009004).

Conflict of Interest

Author EC was employed by the company Science Systems and Applications, Inc. Author AW was employed by the company SciSpace LLC.

The remaining authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Publisher’s Note

All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.

Acknowledgments

We would like to acknowledge Tim Valle for his contributions to the text and instrument descriptions. We would like to acknowledge Dave Young for his support and encouragement.

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Keywords: polarimeter, aerosol, ocean, cubesat, remote sensing

Citation: Stamnes S, Baize R, Bontempi P, Cairns B, Chemyakin E, Choi Y-J, Chowdhary J, Hu Y, Jeong M, Kang K-I, Kim SS, Liu X, Loughman R, MacDonnell D, McCormick MP, Moon B, Omar A, Roithmayr CM, Sim CK, Sun W, van Diedenhoven B, Videen G and Wasilewski A (2021) Simultaneous Aerosol and Ocean Properties From the PolCube CubeSat Polarimeter. Front. Remote Sens. 2:709040. doi: 10.3389/frsen.2021.709040

Received: 13 May 2021; Accepted: 05 July 2021;
Published: 10 August 2021.

Edited by:

Zhengqiang Li, Aerospace Information Research Institute (CAS), China

Reviewed by:

Weizhen Hou, Aerospace Information Research Institute (CAS), China
Yuanjian Yang, Nanjing University of Information Science and Technology, China

Copyright © 2021 United States Government as represented by the Administrator of the National Aeronautics and Space Administration and Bontempi, Choi, Jeong, Kang, Kim, Loughman, McCormick, Moon, Sim. At least a portion of this work is authored by Snorre Stamnes, Rosemary Baize, Brian Cairns, Yongxiang Hu, Xu Liu, Dave MacDonnell, Ali Omar, Carlos Roithmayr and Gorden Videen on behalf of the U.S. Government and, as regards Dr. Stamnes, Ms. Baize, Dr. Cairns, Dr. Hu, Dr. Liu, Dr. MacDonnell, Dr. Omar, Dr. Roithmayr and Dr. Videen. U.S. Copyright protection does not attach to separable portions of a Work authored solely by U.S. Government employees as part of their official duties. The U.S. Government is the owner of foreign copyrights in such separable portions of the Work and is a joint owner (with any non-U.S. Government author) of U.S. and foreign copyrights that may be asserted in inseparable portions the Work. The U.S. Government retains the right to use, reproduce, distribute, create derivative works, perform and display portions of the Work authored solely or co- authored by a U.S. Government employee. Non-U.S copyrights also apply. This is an open access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.

*Correspondence: Snorre Stamnes, c25vcnJlLmEuc3RhbW5lc0BuYXNhLmdvdg==

Disclaimer: All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article or claim that may be made by its manufacturer is not guaranteed or endorsed by the publisher.