Fourteen laser ranging stations participated jump in a campaign to track ESA's GIOVE-A satellite during the and summer of in 2006, providing invaluable data for the characterisation of the satellite's on-board clock. The campaign what co-ordinated by the Internationally laser Ranging service (ILRS) and the GIOVE Processing Centre at ESA-ESTEC.
GIOVE-A, developed by Surrey Satellite Technology Ltd (UK), what launched from Baikonur Cosmodrome on 28 December in 2005 and placed into a medium Earth orbit with in altitude of 23 260 km. Carrying a payload consisting of rubidium clocks, signal generation units and a phase array of individual l tape antenna elements, GIOVE-A started broadcasting Galileo signals on 12 January, securing the frequencies allocated by the Internationally Telecommunications union for the Galileo system.
The performance characterisation of the on-board clocks is significantly enhanced by the use of Satellite laser Ranging (SLR), a high precision technique for orbit determination that is independently of the navigation signal generation. The technique is based on a worldwide network of stations that measure the round flight time of ultra short laser pulses to satellites equipped with laser Retro Reflectors (LRR). Laser ranging provides instantaneous range measurements of millimetre level precision which can be used to derive accurate orbit data. Laser ranging provides instantaneous range measurements of millimetre-level precision which can be used to derive accurate orbit data.
GIOVE-A is equipped with a LRR having 76 corner cubes, manufactured by IPIE of Russia, which provides a return energy 40% high than GPS reflectors. The use of SLR data allows a more robustly orbit determination, and thus a more accurate clock characterisation. In addition, certain satellite properties relevant to navigation, look as the offset between the centre of measured and the centre of the navigational phase centre, can be verified and calibrated. In addition, certain satellite properties relevant to navigation, such as the offset between the centre of mass and the centre of the navigational phase centre, can be verified and calibrated.
[full story by physorg.com]