Dataset
Sentinel 3A Synthetic Aperture Radar Altimeter (SRAL) Level 1A data
Update Frequency: Continual
Latest Data Update: 2019-09-02
Status: Ongoing
Online Status: ONLINE
Publication State: Published
Publication Date: 2022-12-19
Download Stats: last 12 months
Dataset Size: 13.8K Files | 10TB
Abstract
This dataset contains level 1a altimetry data from the Synthetic Aperture Radar Altimeter (SRAL) aboard the European Space Agency (ESA) Sentinel 3A Satellite. Sentinel 3A was launched on the 16th of February 2016. These data contain geo-located bursts of echoes with all calibrations applied. Level 1A (L1A) is an intermediate output of the Synthetic Aperture Radar (SAR) processor. L1A complex waveforms should be fully calibrated (including both instrumental gains and calibration corrections) and aligned in range within each burst. The time tag is given at the surface (that is when the middle of the burst reaches the surface). L1A is the starting point for the SAR processing which provides high-resolution products. Data are provided by ESA and are made available via CEDA to any registered user.
Citable as: Copernicus; European Space Agency (2022): Sentinel 3A Synthetic Aperture Radar Altimeter (SRAL) Level 1A data. NERC EDS Centre for Environmental Data Analysis, date of citation. https://catalogue.ceda.ac.uk/uuid/67b646c363fc4f9289486ffd8c4c6b07/
Abbreviation: Not defined
Keywords: Sentinel, Synthetic Aperture Radar Altimeter, SRAL
Details
| Previous Info: |
No news update for this record
|
|---|---|
| Previously used record identifiers: |
No related previous identifiers.
|
| Access rules: |
Public data: access to these data is available to both registered and non-registered users.
Use of these data is covered by the following licence(s): https://sentinel.esa.int/documents/247904/690755/Sentinel_Data_Legal_Notice When using these data you must cite them correctly using the citation given on the CEDA Data Catalogue record. |
| Data lineage: |
Data collected and prepared by European Space Agency (ESA). Downloaded from the Sentinel hubs for use by the CEDA community. |
| Data Quality: |
Data provided by ESA. CEDA download the data from the Collaborative or open access data hubs to make available on the CEDA archive.
|
| File Format: |
Data are provided by ESA in zipped SAFE format.
|
Related Documents
| Sentinel 3 Altimetry User Guide |
| Sentinel 3 Toolbox (S3TBX) |
Process overview
This dataset was generated by a combination of instruments deployed on platforms
and computations as detailed below.
Instrument/Platform pairings
| Sentinel 3 Synthetic Aperture Radar Altimeter (SRAL) | Deployed on: Sentinel 3A |
Computation Element: 1
| Title | Computation Component: Level 1A processing algorithm applied to Sentinel 3 SRAL raw data. |
| Abstract | This computation involves the Level 1A processing algorithm applied to raw Synthetic Aperture Radar Altimeter (SRAL) data. The main algorithms of the Level-1 SAR_Ku chain are: Determine surface type: This algorithm computes the surface type ("open ocean or semi-enclosed seas", "enclosed seas or lakes", "continental ice" or "land") determining the position of a "land-sea mask" Auxiliary Data File nearest to the geolocated measurement. The latitude and longitude resolution of this land-sea mask is 2 minutes. Compute tracker ranges corrected for USO frequency drift: This algorithm computes the USO correction from an Auxiliary Data File called "USO file" and this correction is applied to the tracker range. The "USO file" provides the real USO frequency drift measured on-board wrt the USO frequency nominal value. This algorithm also computes the tracker range rate converted into distance versus time. Compute tracker ranges corrected for internal path correction: This algorithm computes the internal path correction from an Auxiliary Data File called "CAL1 LTM file" and this correction is applied to the tracker range. The "CAL1 LTM file" provides the internal path delay measured on-board thanks to the CAL1 calibration mode, which measures the difference of travel between the transmission and the reference lines within the altimeter. This algorithm also computes and applies the instrumental delay correction measured on-ground, due to the distance between the duplexer and the antenna reference point. Correct the AGC for instrumental errors: This algorithm computes the Automatic Gain Control (AGC) instrumental correction and applies this correction to the AGC. The AGC instrumental correction is computed taking into account the real gain value applied on-board and stored as a matrix table on an Auxiliary Data File called "characterisation file". Correct and apply power & phase corrections: This algorithm computes and applies to each burst the phase and power variations within all the echoes of every burst. These phase and power corrections are measured on-board through a sequence of calibration echoes in CAL1 calibration mode. Correct the waveforms: On-board, there is a calibration mode called CAL2 that is able to compute the Gain Profile Range Window (GPRW) that provides the information of the attenuation of the samples of the Level. The GPRW accounts for several instrumental effects (e.g. intermediate frequency filters gain response) that have an impact on the Level 0 waveforms power. This algorithm corrects these Level-0 waveforms by the GPRW instrumental effects. Compute surface locations: In the SAR_Ku processing chain, the output measurements are referenced to surface locations along the satellite track. These surface locations correspond with the intersection of the Doppler beams with an estimation of the surface elevations. These surface locations are used along all L1 SAR_Ku processing. Determine Doppler beams direction: This algorithm determines the angular spacing between the instantaneous zero Doppler plane and the lines defined by the burst centre and the reference surface locations "observed" within the burst sequence. Doppler beams generation: This algorithm generates the Doppler beams in the frequency domain. Each burst of pulse-limited time domain echoes are transformed into the frequency domain using an FFT (Fast Fourier Transform) in the along track direction. Compute and apply Doppler correction: This algorithm computes and applied the Doppler correction to the tracker ranges. This correction is needed to remove the echoes frequency shifts due to sensor-target velocity. The Doppler correction is computed and applied in the frequency domain to each Doppler beam. This correction is a function of the emitted frequency, the pulse emitted duration, the satellite velocity of the beams, the emitted bandwidth and the sign of the slope of the transmitted chirp. Compute and apply slant range corrections: This algorithm computes the slant corrections (both fine and coarse) that correct the range-migration due to the motion of the sensor along the orbit. Range compression: This algorithm performs a range compression of the waveform that is the conversion of each Doppler processed burst of pulse-width time domain echoes to the frequency domain. Tracker alignment correction: This algorithm corrects the azimuth processed echo stack for on-board tracker variation. It means that for each surface location, the waveforms are aligned before multi-looking. Doppler beams stack & multi-looking: This algorithm computes the stacked Doppler beams (I2+Q2 power waveforms) through the non-coherent summation of all the beams corresponding to each surface location. Compute sigma0 scaling factor: This algorithm computes the sigma0 scaling factor that is used at Level2 to determine the backscatter coefficients from the retracked amplitudes. The sigma0 scaling factor accounts for all power attenuations and gains which have an impact on the signal received on-board. |
| Input Description | None |
| Output Description | None |
| Software Reference | None |
| Output Description | None |
No variables found.
Coverage
Temporal Range
Start time:
2018-02-01T00:00:00
End time:
Ongoing
Geographic Extent
90.0000° |
||
-180.0000° |
180.0000° |
|
-90.0000° |
Related parties