Independent generation of Earth Orientation Parameter
Programme Reference
T710-503GN
Status
Closed
Country
Germany
Start Date
2017
End Date
2020
Programme: TDE Prime Contractor: Technische Universitaet Muenchen
Subcontractors:
Bundesamt f?r Kartographie und Geod?sie • Germany
HELMHOLTZ-ZENTRUM POTSDAM - DEUTSCHGEOFORSCHUNGSZENTRUM • Germany
TU Wien • Austria
Objectives
Development of ESA capability for the estimation and prediction of Earth Orientation Parameter (EOP) to become independent of the International Earth Orientation and Reference Service (IERS).
Description
Earth Orientation Parameters (EOP) are of fundamental importance for all ESA missions. Currently, the EOPs are obtained from an external entity the Earth Orientation and Reference Service (IERS). The goal of this activity is the development of ESA capability for the estimation and prediction of Earth Orientation Parameter in order to become independent of external services. Several aspects related to this subject topic need to be investigated and further developed. Of particular concern are the following topics: - The estimation of EOPs based on the combination of different complementary observation types such as SLR, VLBI and GNSS. The study shall analyse the difficulties resulting from the combined processing of different observation types and their contribution to the individual global parameters. Different concept shall be proposed, implemented, prototyped and tested. - The prediction of EOPs based on empirical and also physical modelling. The prediction of EOP is a very difficult area, which need fundamental development in order to obtain reliable results. In the frame of this activity, different concepts for the prediction of EOPs shall be developed, prototyped and tested.
• Application domain: Generic Technologies
•
Technology Domain:
10 - Flight Dynamics and GNSS
10 - Flight Dynamics and GNSS
•
Competence Domain:
10-Astrodynamics, Space Debris and Space Environment
10-Astrodynamics, Space Debris and Space Environment
• Initial TRL: TRL 1
• Target TRL: TRL 3
• Achieved TRL: TRL 4
•HarmoRoadMap: N/A
•IPC Document: ESA/IPC(2016)3
•Public Document: