Phase Ambiguity Resolution Method for a Satellite Based Positioning System
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Abstract
The invention relates to a satellite-based positioning system in which a transmitter (2) emits electromagnetic radiation at least at N≧3 carrier frequencies (3, 4, 5). In order to resolve the phase ambiguity for said satellite-based positioning system, the electromagnetic radiation is received by a receiver (1), and K pseudo paths (3a, 4a, 5a, 6a) and L carrier phases (3b, 4b, 5b, 6b), especially at least two pseudo paths (3a, 5a) and at least two carrier phases (3b, 4b), are derived from the received radiation as M pieces of distance data, wherein M=K+L. In order to determine the position, the integer phase ambiguity is derived from the linear combination of a maximum of M≦2N−1 pieces of distance data.
62 Citations
25 Claims
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1-11. -11. (canceled)
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12. A phase ambiguity resolution method for a satellite-based positioning system, the method comprising the following acts:
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transmitting electromagnetic radiation by a transmitting unit, the electromagnetic radiation having N carrier frequencies with at least one first carrier frequency, one second carrier frequency, and one third carrier frequency, where N≧
3;receiving the electromagnetic radiation by a receiving unit; deriving K pseudo-paths and L carrier phases as M distance data, where M=K+L, from the received radiation; and determining an integral phase ambiguity from a linear combination of the carrier phases and the pseudo-paths for the position determination, wherein not more than M≦
2N−
1 distance data are used for the derivation. - View Dependent Claims (13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25)
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Specification