Conveying orbit information via ambiguous position information
First Claim
1. A method of conveying information regarding an orbit used at a Global Navigation Satellite System (GNSS) base station to a GNSS receiver, said method comprising:
- determining a satellite position for a particular time from an orbit of a GNSS satellite;
extracting an ambiguity value from said satellite position, said extracting based upon a satellite position determination margin of error of a GNSS receiver;
encoding said ambiguity value into an encoded ambiguity value;
assembling a message including said encoded ambiguity value and a time tag representing said time; and
transmitting said message from said GNSS base station, whereby said encoded ambiguity value and said time tag convey information regarding said orbit to a GNSS receiver in receipt of said message.
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Accused Products
Abstract
In a method of conveying information regarding an orbit used at a Global Navigation Satellite System (GNSS) base station to a GNSS receiver, a satellite position is determined for a particular time from an orbit of a GNSS satellite. An ambiguity value is extracted from the satellite position. The ambiguity value is extracted based upon a satellite position determination margin of error of a GNSS receiver. The ambiguity value is encoded into an encoded ambiguity value which is assembled into a message. The message also includes a time tag representing the particular time. The message is transmitted from the GNSS base station. The encoded ambiguity value and the time tag convey information regarding the orbit to a GNSS receiver in receipt of the message.
23 Citations
25 Claims
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1. A method of conveying information regarding an orbit used at a Global Navigation Satellite System (GNSS) base station to a GNSS receiver, said method comprising:
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determining a satellite position for a particular time from an orbit of a GNSS satellite; extracting an ambiguity value from said satellite position, said extracting based upon a satellite position determination margin of error of a GNSS receiver; encoding said ambiguity value into an encoded ambiguity value; assembling a message including said encoded ambiguity value and a time tag representing said time; and transmitting said message from said GNSS base station, whereby said encoded ambiguity value and said time tag convey information regarding said orbit to a GNSS receiver in receipt of said message. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A Global Navigation Satellite System (GNSS) base station comprising:
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an orbit processor configured for executing a GNSS orbit algorithm in association with an orbit of a GNSS satellite and a time, such that a satellite position is determined for said time; an ambiguity value extractor configured for extracting an ambiguity value from said satellite position based upon a satellite position determination margin of error of a GNSS receiver; an ambiguity value encoder configured for encoding said ambiguity value as an encoded ambiguity value; and a message assembler configured for assembling a message comprising said encoded ambiguity value and a time tag representing said time. - View Dependent Claims (9, 10, 11)
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12. A method of synchronizing orbits used at a Global Navigation Satellite System (GNSS) receiver and at a GNSS base station, said method comprising:
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receiving a message from said GNSS base station, said message comprising a time tag and an encoded ambiguity value derived from a satellite position of a GNSS satellite, said satellite position calculated by said GNSS base station utilizing a first orbit for said GNSS satellite and a time represented by said time tag; calculating a second satellite position for said GNSS satellite utilizing said time represented by said time tag and a broadcast orbit received at said GNSS receiver from said GNSS satellite; resolving a third satellite position for said GNSS satellite using said encoded ambiguity value and an ambiguous portion of said second satellite position; and determining that orbits used at said GNSS base station and said GNSS receiver are synchronized when said third satellite position and said second satellite position are in agreement. - View Dependent Claims (13, 14, 15, 16, 17, 18, 19, 20, 21)
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22. A Global Navigation Satellite System (GNSS) receiver comprising:
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a message receiver configured for receiving a message broadcast from a GNSS base station, said message comprising a time tag associated with a satellite position and an encoded ambiguity value derived from said satellite position; an orbit processor configured for utilizing a broadcast orbit from said GNSS satellite to determine a second satellite position of said GNSS satellite, said satellite position and said second satellite position both being for a time represented by said time tag; and an orbit determiner configured for resolving a third satellite position from said encoded ambiguity value and said second satellite position, said third satellite position comprising an approximation of said satellite position. - View Dependent Claims (23, 24, 25)
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Specification