The NASA/NOAA Visible Infrared Imaging Radiometer Suite (VIIRS) is a key instrument in the JPSS missions (SNPP, JPSS-1-4). Being part of the calibration and validation process, JPSS-4 VIIRS prelaunch geometric performance assessment focuses on the sensor’s spatial response, band-to-band co-registration (BBR), and pointing knowledge. In general, JPSS-4 VIIRS’ prelaunch geometric performance is very good, and consistent with SNPP and JPSS-1-2-3 VIIRS. This paper highlights some specific key findings from the JPSS-4 VIIRS’ prelaunch tests. We first show that with timing adjustments, JPSS-4 VIIRS scan BBR error between VisNIR and SMWIR and LWIR bands has been reduced from 0.11/0.04 M-band sampling intervals to around 0.01 M-band sampling intervals, respectively. Focal Plane Assembly (FPA) rotations are about 0.03 degree in VisVIR, 0.08 degree in SMWIR and LWIR. Another finding from the prelaunch test is that JPSS-4 VIIRS track direction band-to-band co-registration errors between VisNIR and SMWIR and LWIR bands have been improved when compared to JPSS-3. This BBR mis-registration increases when aft‐optics assembly (AOA) temperature decreases. During TVAC cold performance test (AOA temperature is 253K), the track BBR mis-registration is about 0.04 M-band sampling intervals between VisNIR and SMWIR bands, and 0.03 M-band sampling intervals between VisNIR and LWIR bands. By comparison, the track BBR mis-registration in JPSS-3 is 0.10/0.08 M sampling intervals between VisNIR and SMWIR/LWIR bands, respectively. The unsymmetrical Day Night Band (DNB) scan-direction Line Spread Function (LSF) of JPSS-2 VIIRS at different gain stages and aggregation modes have been corrected in J4 VIIRS. Lastly, to correct the scan-to-scan underlaps in J1/J2, the scan rate of J4 VIIRS is increased to 3.546 rad/sec, compared to 3.510 rad/sec of J2. As a result, NOAA IDPS will reduce from 85.35 sec to 85.00 secs in each 48-scan granule, and NASA LSIPS will increase the number of scans from 202 scans in J2 to 204 scans in J4 in each 6-minute granule.
The second NOAA/NASA Join Polar Satellite System (JPSS-2) satellite was successfully launched on November 10, 2022, becoming NOAA-21. Instruments on-board the NOAA-21 satellite include the Visible Infrared Imaging Radiometer Suite (VIIRS). This instrument is the third build of VIIRS, with the first and second flight instruments onboard NASA/NOAA Suomi National Polar-orbiting Partnership (SNPP) and NOAA-20 satellites operating since October 2011 and November 2017, respectively. The purpose of these VIIRS instruments is to continue the long-term measurements of biogeophysical variables for multiple applications including weather forecasting, rapid response, and climate research. The geometric performance of VIIRS is essential to retrieving accurate biogeophysical variables. This paper describes the early on-orbit geometric performance of the JPSS-2/NOAA-21 VIIRS. It first discusses the on-orbit position and attitude performance, a key input needed for accurate geolocation. It then discusses the on-orbit geometric characterization and calibration of VIIRS and an initial assessment of the geometric accuracy. It follows with a discussion of correcting the scan angle dependent geolocation biases across the scan. Finally, this paper discusses onorbit measurements of the band-to-band co-registration, focal length and the impact of this on the scan-to-scan underlap/overlap.
The NASA/NOAA Visible Infrared Imaging Radiometer Suite (VIIRS) is a key instrument in the JPSS missions (SNPP, JPSS-1-4). Being part of the calibration and validation process, JPSS-3 VIIRS prelaunch geometric performance assessment focuses on the sensor’s spatial response, band-to-band co-registration(BBR), and pointing knowledge. In general, JPSS-3 VIIRS’ prelaunch geometric performance is very good, and consistent with SNPP and JPSS-1-2 VIIRS sensors. This paper highlights some specific key findings from the JPSS-3 VIIRS’ prelaunch tests. We firs t s how that with timing adjustments, JPSS-3 VIIRS scan BBR error between VisNIR and S/M/LWIR bands has been reduced from 0.12/0.03 M sampling intervals to 0.005/0.002 M sampling intervals, respectively. Focal Plane Assembly (FPA) rotations have beenchangedfrom0.1 degree to 0.04 degree in VisVIR, from 0.18 degree to 0.09 degree in S/MWIR, and 0.16 degree to 0.08 degree in LWIR. Another finding from the pre launch test is that JPSS-3 VIIRS has relatively large band-to-band co-registration errors between VisNIR and S/M/LWIR bands in the track direction. This BBR mis - registration increases when aft‐optics assembly (AOA) temperature decreases. The BBRmis-registration is about 0.10 M sampling intervals between VisNIR and S/MWIR bands, and 0.08 M sampling intervals between Vis NIR and LW IR bands. By comparison, the track BBR offset in JPSS-2 is less than 0.02 M sampling intervals between VisNIR and S/M/LWIR bands. We also notice that the unsymmetrical Day Night Band (DNB) scan-direction Line Spread Function (LSF) of JPSS-2 VIIRS at different gain stages and aggregation modes have been corrected in J3 VIIRS.
The Control Point Matching(CPM) program and a set of over 1200 globally distributed ground control points (GCPs ) have been successfully used to develop more than 20 years of MODIS geolocation products. In this research, we refresh current GCP library with more than 2500 new GCPs using the latest Landsat 8 Collection 2 images. The refreshed GCPs are distributedfrom56 S to 80 N latitude, with more than 2000 shoreline and 500 inland GCP chips. The size of these GCPs are extended from 800*800 to 1400*1400 Landsat pixels and the CPM program correspondingly increases the searching distance from0.8 pixels to 2.5 pixels, which also extends the geolocation error measurement from+/-45 to the edge of scan at +/-55 degree in scan angle. This will allow the algorithm to catch geolocation errors that are larger than one MODIS pixel. The geolocation errors measured with the refreshed GCP library are comparable to the previous results, yet with 2-3 more times of matched GCPs. The daytime Aqua ascending orbits and Terra descending orbits enable us to identify a few GCP outliers which might be due to the quality of the original Landsat images. Most importantly, the refreshed GCP library will include images from both Landsat band 4 to match with VII RS I1, and Landsat band 6 to match with VIIRS I3. This will allow us to measure and correct on orbit band-to-band registration at both track and scan directions, which will help understanding and improving future JPSS mission’s prelaunch geometric performance.
Two Visible Infrared Imaging Radiometer Suite (VIIRS) sensors have been in operations for more than 8.5 and 2.5 years since they were launched in October 2011 on SNPP satellite and in November 2017 on NOAA-20 satellite, respectively. These are two satellites in the Join Polar Satellite System (JPSS) constellation, of which Suomi National Polar-orbiting Partnership (SNPP) is a risk reduction satellite and NOAA-20 is the first of four JPSS satellites (JPSS-1 became NOAA- 20 after launch). Accurate geolocation is a critical element in data calibration for accurate retrieval of global biogeophysical parameters. In this paper, we describe the latest trends in the continuously improved geolocation accuracy in VIIRS Collection-1 (C1) and C2 re-processing. We implemented a VIIRS instrument geometric model update (VIGMU) for both sensors that correct for geolocation error oscilations in the scan direction. We borrowed code from Moderate Resolution Imaging Spectroradiometer (MODIS) geolocation software to correct for time-dependent pointing variations, that are particularly acute in NOAA-20 VIIRS, and some pointing anomalies in SNPP VIIRS. We developed a Kalman Filter using gyro data to correct for attitude errors due to the degradation of the star trackers performance from the SNPP satellite. We also present an improved ground control point matching (CPM) tool, in which the ground control point (GCP) chips library is refreshed using recently launched Landsat-8 images.
Two Moderate Resolution Imaging Spectroradiometer (MODIS) sensors have been in operations for more than 19 and 17 years (thus 36 combined years) as part of NASA's Earth Observing System (EOS) on the Terra platform that was launched in December 1999 and on the Aqua platform that was launched in May 2002, respectively. Accurate geolocation is a critical element needed for accurate retrieval of global biogeophysical parameters. In this paper, we describe the latest trends in the continuously improved MODIS geolocation accuracy in Collection-5 (C5), C6 and C6.1 re-processing and forward-processing data streams. We improved geolocation accuracy in the re-processed data and corrected for geolocation biases found in forward-processed data, including those caused by operations such as the stop-go-stop status of the Advanced Microwave Scanning Radiometer for EOS (AMSR-E) instrument on the Aqua platform. We discuss scan-toscan underlaps near nadir over the equator regions that was discovered in checking the non-underlapping requirement in the Visible Infrared Imaging Radiometer Suite (VIIRS) based on trending parameters from the actual Suomi National Polar-orbiting Partnership (S-NPP) satellite orbit. The underlaps are closely tied to instrument effective focal length that is measured from on-orbit data using a technique we recently developed. We also discuss potential improvements for the upcoming C7 re-processing.
The first NOAA/NASA Join Polar Satellite System (JPSS-1) satellite was successfully launched on November 18, 2017, becoming NOAA-20. Instruments on-board NOAA-20 satellite include the Visible Infrared Imaging Radiometer Suite (VIIRS). This instrument is the second build of VIIRS, with the first flight instrument on-board NASA/NOAA Suomi National Polar-orbiting Partnership (SNPP) satellite operating since October 2011. The purpose of these VIIRS instruments is to continue the long-term measurements of biogeophysical variables for multiple applications including weather forecasting, rapid response and climate research. The geometric performance of VIIRS is essential to retrieving accurate biogeophysical variables. This paper describes the early on-orbit geometric performance of the JPSS-1/NOAA-20 VIIRS. It first discusses the on-orbit orbit and attitude performance, a key input needed for accurate geolocation. It then discusses the on-orbit geometric characterization and calibration of VIIRS geometry and an initial assessment of the geometric accuracy. This section includes a discussion of an improvement in the geometric model that corrects small geometrical artifacts that appear in the along-scan direction. Finally, this paper discusses on-orbit measurements of the focal length and the impact of this on the scan-to-scan underlap/overlap.
This paper describes trends in the Suomi National Polar‐orbiting Partnership (SNPP) spacecraft ephemeris data over the four and half years of on-orbit operations. It then discusses the implications of these trends on the geometric performance of the Visible Infrared Imaging Radiometer Suite (VIIRS), one of the instruments onboard SNPP. The SNPP ephemeris data includes time stamped spacecraft positions and velocities that are used to calculate the spacecraft altitude and sub-satellite locations. Through drag make-up maneuvers (DMUs) the orbital mean altitude (spacecraft altitude averaged over an orbit) has been maintained at 838.8 km to within +/- 0.2 km and the orbital period at 101.5 minutes to within +/- 0.2 seconds. The corresponding orbital mean velocity in the terrestrial frame of reference has been maintained at 7524 m/s to within +/- 0.5 m/s. Within an orbit, the altitude varies from 828 km near 15° N to 856 km near the South Pole. Inclination adjust maneuvers (IAMs) have maintained the orbit inclination angle at 98.67° to with +/- 0.07° and the sun-synchronous local time at ascending node (LTAN) at 13:28 to within +/- 5 minutes. Besides these trends, it is interesting to observe that the orbit’s elliptic shape has its major axis linking the perigee and apogee shorter than the line linking the ascending node and the descending node. This effect is caused by the Earth’s oblate spheroid shape and deviates from a Keplerian orbit theory in which the two orbiting bodies are point masses. VIIRS has 5 imagery resolution bands, 16 moderate resolution bands and a day-night band, with 32, 16 and 16 detectors, respectively, aligned in the spacecraft flight (aka. track) direction. For each band’s sample within a scan, the detectors sample the Earth’s surface simultaneously in the track direction in the Earth Centered Inertial frame of reference. The distance between the center of the area sensed by the trailing detectors of one scan and the leading detectors of the next includes a component caused by earth rotation. This earth rotation component is relatively small (~70 m/s) for an orbit like SNPP, but must be taken into account in the design of low-Earth orbit scanning sensors similar to VIIRS to ensure contiguous coverage at nadir.
Following the successful operations of the first Visible Infrared Imaging Radiometer Suite (VIIRS) instrument on-board the Suomi National Polar‐orbiting Partnership (SNPP) spacecraft since launch in October 2011, a second VIIRS instrument to be on-board the first Joint Polar Satellite System (JPSS-1) satellite has been fabricated, tested and integrated onto the spacecraft, readying for launch in 2017. The ground testing, including geometric functional performance testing and characterization, at the sensor level was completed in December 2014. Testing at the spacecraft level is on-going. The instrument geometric performance includes sensor (detector) spatial response, band-to-band coregistration (BBR), scan plane and pointing stability. The parameters have been calibrated and characterized through ground testing under ambient and thermal vacuum conditions, and numerical modeling and analysis. VIIRS sensor spatial response is measured by line spread functions (LSFs) in the scan and track directions for every detector. We parameterize the LSFs by: 1) dynamic field of view (DFOV) in the scan direction and instantaneous FOV (IFOV) in the track direction; and 2) modulation transfer function (MTF) for the 17 moderate resolution bands (M-bands) and for the five imagery bands (I-bands). We define VIIRS BBR for M-bands and I-bands as the overlapped fractional area of angular pixel sizes from the corresponding detectors in a band pair, including nested I-bands within the M-bands. The ground tests result in static BBR matrices. VIIRS pointing measurements include scan plane tilt and instrument-to-spacecraft mounting coefficients. This paper summarizes the pre-launch test results along with anomaly investigations. The pre-launch performance parameters will be tracked or corrected for as needed in on-orbit operations.
The Visible Infrared Imager Radiometer Suite (VIIRS) instrument onboard the Suomi National Polar‐orbiting Partnership (SNPP) satellite was launched on 28 October 2011. The VIIRS has 5 imagery spectral bands (I-bands), 16 moderate resolution spectral bands (M-bands) and a panchromatic day/night band (DNB). Performance of the VIIRS spatial response and band-to-band co-registration (BBR) was measured through intensive pre-launch tests. These measurements were made in the non-aggregated zones near the start (or end) of scan for the I-bands and M-bands and for a limited number of aggregation modes for the DNB in order to test requirement compliance. This paper presents results based on a recently re-processed pre-launch test data. Sensor (detector) spatial impulse responses in the scan direction are parameterized in terms of ground dynamic field of view (GDFOV), horizontal spatial resolution (HSR), modulation transfer function (MTF), ensquared energy (EE) and integrated out-of-pixel (IOOP) spatial response. Results are presented for the non-aggregation, 2-sample and 3-sample aggregation zones for the I-bands and M-bands, and for a limited number of aggregation modes for the DNB. On-orbit GDFOVs measured for the 5 I-bands in the scan direction using a straight bridge are also presented. Band-to-band co-registration (BBR) is quantified using the prelaunch measured band-to-band offsets. These offsets may be expressed as fractions of horizontal sampling intervals (HSIs), detector spatial response parameters GDFOV or HSR. BBR bases on HSIs in the non-aggregation, 2-sample and 3-sample aggregation zones are presented. BBR matrices based on scan direction GDFOV and HSR are compared to the BBR matrix based on HSI in the non-aggregation zone. We demonstrate that BBR based on GDFOV is a better representation of footprint overlap and so this definition should be used in BBR requirement specifications. We propose that HSR not be used as the primary image quality indicator, since we show that it is neither an adequate representation of the size of sensor spatial response nor an adequate measure of imaging quality.
The NASA/NOAA Visible Infrared Imager Radiometer Suite (VIIRS) instrument on‐board the Suomi National
Polar‐orbiting Partnership satellite was launched in October 2011. Assessment of VIIRS’ geometric performance
includes measurements of the sensor’s spatial response, band‐to‐band co‐registration (BBR), and geolocation accuracy
and precision.
The instrument sensor (detector) spatial response is estimated by line spread functions (LSFs) in the scan and track
directions. The LSFs are parameterized by dynamic field of view in the scan direction and instantaneous FOV in the
track direction, modulation transfer function for the 16 moderate resolution bands (M‐bands), and horizontal spatial
resolution for the five imagery bands (I‐bands). VIIRS BBR for the M and I bands is defined as the overlapped fractional
area of angular pixel sizes from the corresponding detectors in a band pair, including nested I‐bands into M‐bands, and
measured on-orbit using lunar and earth data. VIIRS geolocation accuracy and precision are affected by instrument
parameters, ancillary data (i.e., ephemeris and attitude), and thermally induced pointing variations with respect to orbital
position. These are being tracked by a ground control point matching program and corrected in geolocation parameter
lookup tables in the ground data processing software.
This on-orbit geometric performance assessment is an important aspect of the VIIRS sensor data record calibration and
validation process. In this paper, we will discuss VIIRS’ geometric performance based on the first seven‐month of
VIIRS' on-orbit earth and lunar data, and compare these results with the at‐launch performance based on ground test data
and numerical modeling results. Overall, VIIRS’ on-orbit geometric performance is very good and matches the prelaunch
performance, and is thus expected to meet the needs of both the long-term monitoring and operational
communities.
Visible Infrared Imager Radiometer Suite (VIIRS) instrument on-board the National Polar-orbiting Operational
Environmental Satellite System (NPOESS) Preparatory Project (NPP) satellite is scheduled for launch in October, 2011.
It is to provide satellite measured radiance/reflectance data for both weather and climate applications. Along with
radiometric calibration, geometric characterization and calibration of Sensor Data Records (SDRs) are crucial to the
VIIRS Environmental Data Record (EDR) algorithms and products which are used in numerical weather prediction
(NWP). The instrument geometric performance includes: 1) sensor (detector) spatial response, parameterized by the
dynamic field of view (DFOV) in the scan direction and instantaneous FOV (IFOV) in the track direction, modulation
transfer function (MTF) for the 17 moderate resolution bands (M-bands), and horizontal spatial resolution (HSR) for the
five imagery bands (I-bands); 2) matrices of band-to-band co-registration (BBR) from the corresponding detectors in all
band pairs; and 3) pointing knowledge and stability characteristics that includes scan plane tilt, scan rate and scan start
position variations, and thermally induced variations in pointing with respect to orbital position. They have been
calibrated and characterized through ground testing under ambient and thermal vacuum conditions, numerical modeling
and analysis. This paper summarizes the results, which are in general compliance with specifications, along with
anomaly investigations, and describes paths forward for characterizing on-orbit BBR and spatial response, and for
improving instrument on-orbit performance in pointing and geolocation.
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