Development of a tool that predicts the orbital parameters of a satellite from an initial state vector for a specified time interval is addressed. The elements used in the algorithm are presented. The prediction performance of the algorithm is demonstrated by using the two line elements of a GPS satellite and the CHAMP scientific satellite.
Development of a Tool for Prediction of the Orbital Parameters of Earth Observation Satellites
2007-06-01
2515927 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Orbital elements, trajectory simulation, and prediction for earth satellites
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