METHOD OF MANAGING ADDITIONAL FILTERS IN A SATELLITE NAVIGATION SYSTEM

The method involves determining a theoretical constellation of satellites (2-6), located above a horizon of an aircraft (1), from an aircraft position supplied by a main filter. Additional filters excluding the satellites are created and maintained. The satellites are incorporated in the additional...

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Bibliographische Detailangaben
Hauptverfasser:	VACHER, CHARLIE, GOUDON, JEAN-CLAUDE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING
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Beschreibung
Zusammenfassung:	The method involves determining a theoretical constellation of satellites (2-6), located above a horizon of an aircraft (1), from an aircraft position supplied by a main filter. Additional filters excluding the satellites are created and maintained. The satellites are incorporated in the additional filters as long as the satellites are present in the theoretical satellite constellation.