Autonomous orbit propagation system and method

G - Physics – 01 – S

Patent

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G01S 5/14 (2006.01)

Patent

CA 2705027

A method of predicting a location of a satellite is provided wherein the GPS device, based on previously received information about the position of a satellite, such as an ephemeris, generates a correction acceleration of the satellite that can be used to predict the position of the satellite outside of the time frame in which the previously received information was valid. The calculations can be performed entirely on the GPS device, and do not require assistance from a server. However, if assistance from a server is available to the GPS device, the assistance information can be used to increase the accuracy of the predicted position.

L'invention propose un procédé permettant de prédire la position d'un satellite, le dispositif GPS, à partir d'informations précédemment reçues sur la position d'un satellite, telle qu'une éphéméride, générant une accélération de correction du satellite qui peut être utilisée pour prédire la position de ce satellite en dehors de l'intervalle de temps dans lequel les informations précédemment reçues étaient valides. Les calculs peuvent être effectués entièrement sur le dispositif GPS, sans l'aide d'un serveur. Cependant, si l'aide d'un serveur est disponible pour le dispositif de GPS, les informations d'aide peuvent être utilisées pour affiner la prédiction de position.

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