Satellite navigation method, especially using Global Satellite Navigation system

摘要

The method involves deriving suitable measurement parameters for satellite navigation from the signals from navigation satellites using at least two satellite receiver antennas at different predefinable positions on the object. The geometry between satellites, receiving antennas and a predefined reference point on the object being navigated is derived from the measurement parameters of the satellite navigation system or another navigation system. Several antennae are arranged near the reference point to enable at least the distances between the antennas and from these to the reference point to be determined. Measurement parameters such as pseudorange or phase-Doppler shifts for each receiver antenna are transformed to the navigated object and a mean value is computed taking anomalies into account.