PHased ARray Universal Sar (PHARUS): a polarimetric C-band airborne SAR
PHARUS (PHased ARray Universal Sar) was a full polarimetric C-band (5.3 GHz) aircraft Synthetic Aperture Radar (SAR) that was used to image the earth’s surface. It was designed and built by TNO-FEL in The Hague, NLR in Amsterdam and the Delft University of Technology under program management of the Netherlands Agency for Aerospace Programs (NIVR) in Delft. TNO-FEL was the main contractor and was responsible for project management. Financial support for the project was provided by the Ministry of Defence and by the Netherlands Remote Sensing Board (BCRS).
SAR systems are distinguished by their high azimuth resolution capability, achieved through signal processing of the Doppler shifts generated by the forward motion of the radar and aircraft. The azimuth resolution in such a system is theoretically independent of the operating distance with the highest obtainable resolution in the order of several meters. SAR systems like PHARUS can generate radar images day and night and in all weather conditions. More on the Principle of SAR and polarimetry can be read at the bottom of this page.
The PHARUS system was divided into three subsystems:
the radar in the pod outside the aircraft,
the onboard data processing and recording inside the aircraft,
the ground-based SAR processing.
The PHARUS system had a modular architecture, enabling easy adaptation to specific requirements and a user-oriented configuration. The use of a modular phased array enabled a fixed mounting of the radar to the aircraft and avoids gimbaling systems making this SAR concept also suited for small aircraft, which considerably reduced operating costs. The system was capable of operating under turbulent conditions. PHARUS was fully programmable, featuring single and multi-polarisation modes and the selection of resolution and range. Even pulse-to-pulse beam steering was supported, enabling advanced features like spotlight mode, active nulling and multi-target tracking.
Some key features of the PHARUS system were:
Modern solid-state radar technology
Modular system architecture
A modular active phased array antenna
Programmable radar characteristics
Programmable recording and data-processing
Internal calibration
Supports satellite-simulating modes (ASAR)
Key specifications of the PHARUS system were:
Frequency: 5.3 GHz (C-band)
Transmit power: 2OW/module
Resolution: 3.75 m in range, up to 1 m azimuth
Range up to 30 km
Swath width up to 20 km
Before the construction of PHARUS started, experience in the field of SAR had been gained through the development of a prototype system with limited capabilities, called PHARS. This small but powerful system was successfully tested in November 1990 and provided good SAR imagery. PHARS also successfully participated in the ERS-l CAL/VAL campaign in Norway.
Flights with PHARS and PHARUS
(The table below was captured from the year 2000 Pharus project’s webpage and extended with the later flights;
most images can be enlarged by clicking on them)
FLIGHT NO.
DATE
LOCATION
REMARKS
August 25, 1992
–
PHARS trial above Amsterdam
Recording date
August 25, 1992
Track angle
0 N
Altitude
4,877 m
Centre incidence angle
35 Left
Processing mode
12 looks, 50% overlap
Resolution
6 m * 6 m
Number of pixels
768 * 768
February 11, 1994
–
Langeoog, Germany by PHARS
Recording date
February 11, 1994
Track angle
179 N
Altitude
4,877 m
Centre incidence angle
35 Left
Processing mode
12 looks, 50% overlap
Resolution
6m * 6m
Number of pixels
768 * 768
February 1, 1995
–
PHARS was flown over some of the flooded areas in the Netherlands. The image shows an area on the border between Belgium and the Netherlands, near Maaseik, showing the river Maas and the flooded areas surrounding it. The image was recorded at an altitude of 4300 m, imaging a swath of 6 km, starting at 5700 m range. The image was processed to a 6-metre resolution using six independent looks.