Reverse-ephemeris lunar navigation system for long-distance route determination

The disclosed system and method transmit a signal from the surface (or surroundings) of a celestial object to a satellite (for which you know the orbital elements) that re-transmits the signal back to a transceiver on the surface of the celestial object from which a time delay to obtain a range meas...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Mcbeth, Michael S, Moses, Robert W
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:The disclosed system and method transmit a signal from the surface (or surroundings) of a celestial object to a satellite (for which you know the orbital elements) that re-transmits the signal back to a transceiver on the surface of the celestial object from which a time delay to obtain a range measurement and a Doppler shift to obtain the range-rate can be measured. With knowledge of the satellite's orbital elements and the range and range-rate, a location of the transceiver can be determined.