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Concept

Principle
Instrument

 

Principle

ASAR Stripmap modes
ASAR ScanSAR modes

ASAR consists of a coherent, active phased array SAR (i.e., distributed transmitter and receiver elements) which is mounted with the long axis of the antenna aligned with the satellite's flight direction (i.e., Y-axis). The SAR antenna with its two-dimensional beam pattern images a strip of ground to the right side of the flight path which has potentially unlimited content in the direction of motion (i.e., the azimuth direction) but is bounded in the orthogonal direction (i.e., the range direction) by the antenna elevation beamwidth. The objective of the SAR system is to produce a two-dimensional representation of the scene reflectivity at high resolution, with axes defined in the range and azimuth direction.

satellite's flight configuration
A coherent, active phased array SAR, is mounted with the antenna long axis aligned with the satellite's flight direction (i.e. Y-axis)

 

The range resolution of a pulsed radar system is limited fundamentally by the bandwidth of the transmitted pulse (the wider the bandwidth, the better the range resolution). A wide bandwidth can be achieved by a short duration pulse. However, the shorter the pulse, the lower the transmitted energy (for a fixed-peak power limitation), and the poorer the signal to noise ratio, hence the radiometric resolution. To preserve the radiometric resolution, the technique adopted by ASAR is to generate a long pulse with a linear frequency modulation (or chirp). The length of the pulse is defined to be consistent with the requirement for the signal to-noise ratio. The chirp bandwidth is defined by the required range resolution. After the received signal has been compressed the range resolution is optimised without loss of radiometric resolution.

The azimuth resolution of a real aperture radar system is a function of the antenna length (the larger the antenna, the better the azimuth resolution). It can be shown that a spaceborne real aperture radar, giving a useful azimuth resolution for points on the Earth's surface, would require an impractically large antenna. Aperture synthesis, therefore, offers a means of greatly improving the azimuth resolution.

The measurement principle of ASAR depends on the use of coherent radiation, together with precise knowledge of the transmit and receive point of the radar pulse. For a given target, as the platform moves, the distance from the radar to the target (i.e., the slant range) changes continuously, hence the phase of the reflected signal changes according to a law given by the geometry of observation. As this law is deterministic, it is therefore possible to correctly phase the return signals with respect to each other so that the net effect is equivalent to them all having been received simultaneously by an antenna of length equal to the path length over which the radar signals were collected (i.e., the synthetic aperture). In this way, the synthesized antenna can be thought of as a number of independently radiating elements (i.e., the real aperture), whose separation is established by the pulse repetition frequency (PRF) and the platform velocity. The change of the phase with respect to time is the Doppler angular frequency. The azimuth resolution is determined by the Doppler bandwidth of the received signal. For ASAR, the bandwidth of target returns, in azimuth, is defined by the Doppler bandwidth covered between the half-power points of the one-way azimuth pattern. This implies that pulses must be transmitted with a repetition frequency greater than the azimuth bandwidth in order to satisfy the Nyquist sampling criterion.

There is an upper limit on the PRF, imposed by the geometry. If the PRF is so high that return signals from two consecutively transmitted pulses arrive simultaneously at the receiver, there would be ambiguities in the response. This would therefore define a set of unambiguous intervals for a given geometry and PRF, which corresponds to constraining the ground range extent of the region illuminated within the elevation beamwidth of the antenna footprint (i.e., the swath width).

As a consequence of the ASAR antenna being used for pulse transmission and echo reception, there are echoes that are not received due to periods when the antenna is transmitting pulses and hence not receiving echo returns. For a given geometry and PRF, these 'blind' intervals lie at constant ground range positions.

The return from nadir (the ground point vertically below the satellite) are significantly larger than the returns from the required swath, because of its close range and high reflectivity. To avoid this unwanted signal saturating any other returns arriving at the same time, the PRFs for ASAR are chosen such that the nadir returns do not occur in the imaging window.

The significant feature of the ASAR instrument is the active phase array antenna, which allows independent control of the phase and amplitude of the transmitted radiators from different regions of the antenna surface. It also provides independent weighting of the received signal to each of these regions. This offers great flexibility in the generation and control of the radar beam, giving the ASAR instrument the capability to operate in a number of different modes. These modes use two principal methods of taking measurements; the ASAR instrument may operate as a conventional stripmap SAR or as a ScanSAR.

ASAR Stripmap Modes
(Image, Wave)

When operating as a Stripmap SAR, the phased array antenna gives ASAR the flexibility to select an imaging swath by changing the beam incidence angle and the elevation beamwidth. In addition, the appropriate PRF required to ensure acceptable ambiguity performance and to suppress unwanted nadir returns is selected.

In the image mode, ASAR operates in one of seven predetermined swaths with either vertically or horizontally polarised radiation; the same polarisation is used for transmit and receive (i.e., HH or VV).

The wave mode uses the same swaths and polarisations as image mode. However, a continuous strip of data is not required. Instead, small areas of the ocean are imaged at regular intervals along the swath. This intermittent operation provides a low data rate, such that the data can be stored on board the satellite, rather than being downlinked immediately to the ground station.

image mode
Image Mode

[wave mode]
Wave Mode

ASAR ScanSAR Modes: Wide swath, global monitoring, and alternating polarisation

While operating as a stripmap SAR, ASAR is limited to a narrow swath which is imposed by the ambiguity limitation. This constraint can be overcome by utilising the ScanSAR principle, which achieves swath widening by the use of an antenna beam which is electronically steerable in elevation.

Radar images can then be synthesized by scanning the incidence angle and sequentially synthesizing images for the different beam positions. The area imaged from each particular beam is said to form a sub-swath. The principle of the ScanSAR is to share the radar operation time between two or more separate sub-swaths in such a way as to obtain full image coverage of each.

The system transmits pulses to and receives echoes from a sub-swath for a period long enough to synthesize a radar image of the area within the beam footprint at the required resolution. It then switches beams to illuminate a different sub-swath and continues in this manner until the full-wide swath is covered at which point it returns to the original sub-swath and the scanning cycle is repeated.

The imaging operation is, therefore, split into a series of blocks of pulses, each block providing returns from one of the sub-swaths. Each block is processed to provide an image of a section of the corresponding sub-swath. The imaging operations must therefore be such that it cycles around the full set of sub-swaths sufficiently rapidly for the imaged sections in any one sub-swath to be adjoining or overlapping.

ASAR operates according to the ScanSAR principle, as described above, in two measurement modes: the wide swath mode and global monitoring mode. These use five predetermined overlapping antenna beams which cover the wide swath.

An additional ASAR measurement mode, called alternating polarisation mode, which employs a modified ScanSAR technique, has also been defined. Instead of scanning between different elevation sub-swaths, the alternating polarization mode (co-polar) scans between two polarisations, HH and VV, within a single swath (which is preselected, as for image and wave modes). In addition, there are two cross-polar modes, where the transmit pulses are all H or all V polarisation, with the receive chain operating alternatively in H and V, as in the co-polar mode.

mode_ws.gif (7447 bytes)
Wide Swath Mode

mode_gm.gif (6912 bytes)
Global Monitoring Mode

 mode_ap.gif (7018 bytes)
Alternating Polarisation
Mode
 

 

Instrument

The ASAR, operated at C-band (5.331 GHz), can be regarded as an advanced version of the SAR flying on ERS-1/2. It can be operated continuously for 30 minutes in a high-resolution mode for each orbit. Its application covers observations of land and sea characteristics under all weather conditions.


The ASAR, operated at C-band (5.331 GHz)

In order to provide the possibility to adapt to various observing requirements, ASAR incorporates the capabilities to steer the beam to image different swath positions. Additionally, imaging can be performed in horizontal and vertical polarization. These features provided by the active array antenna requires a dedicated calibration scheme. The table summarizes the ASAR capabilities.

Instrument Parameters Image Mode Alternating Polarisation Wide Swath Global Monitoring Wave Mode
Swath width up to 100 km up to 100 km > 400 km > 400 km 5 km vignette
Operation time up to 30 min per orbit rest of orbit
Data Rate up to 100 Mbit/s 0.9 Mbit/s
Power 1365 W 1395 W 1200 W 713 W 647 W

The use of the ASAR generic processor for near real time and off-line processing in the processing and archiving centres (PACs) and national stations offering ESA services is a simplification for processing and product validation. This allows full product compatibility between the different processing centres.

Keywords: ESA European Space Agency - Agence spatiale europeenne, observation de la terre, earth observation, satellite remote sensing, teledetection, geophysique, altimetrie, radar, chimique atmospherique, geophysics, altimetry, radar, atmospheric chemistry