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Doppler Orbitography and Radiopositionning Integrated by Satellite
DORIS Instrument
CHARACTERISTICS
Multi-mission system
One centimeter level orbit determination and ground positioning
60 beacons homogeneous ground network
In flight receivers
One-way uplink RF tracking

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All DORIS instruments that flew, are flying or will fly

Timeline

DORIS (Doppler Orbitography and Radiopositionning Integrated by Satellite) was proposed by CNES, GRGS (Groupe de Recherches de Géodésie Spatiale) and IGN in 1982 as a dedicated fully optimised system in support of POSEIDON oceanographic altimetric experiment. Later on this experiment was merged with NASA TOPEX project to become the TOPEX/POSEIDON mission which has been launched August 10, 1992. To get an in-flight validation of DORIS before TOPEX/POSEIDON it was flown on board the SPOT2 satellite as a passenger experiment. Recognising the ability of the system to provide precise positioning of ground beacons, DORIS was approved for flying on board SPOT3, SPOT4, ENVISAT-1, JASON-1 (TOPEX-POSEIDON follow on mission), SPOT5, JASON-2, CRYOSAT-2 and on HY-2A.

The precise positioning is based on Doppler shifts measurements of RF signals transmitted by a world wide beacons network (one way thanks to stability of board and beacons USOs (Ultra Stable Oscillator)).

DORIS products are available in AVISO directory and IDS data centers
 


Latest update 05/09/2011
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NEWS
Since december 2006
JASON 2 integration
 
Since july 2006
PLEIADES integration
 
2007
Installation of a fourth time and frequency reference beacon in Yellowknife (Canada)