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US Patent 12105211 Systems and methods for high-integrity satellite positioning

Patent 12105211 was granted and assigned to Swift Navigation on October, 2024 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent
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Patent attributes

Patent Applicant
Swift Navigation
Swift Navigation
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Current Assignee
Swift Navigation
Swift Navigation
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
121052110
Patent Inventor Names
Sebastien Carcanague0
Fergus MacPherson Noble0
Date of Patent
October 1, 2024
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Patent Application Number
183741280
Date Filed
September 28, 2023
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Patent Citations
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US Patent 7292183 GPS reference system providing synthetic reference phases for controlling accuracy of high integrity positions
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US Patent 7298325 Technique for accurate estimate of large antenna inertial two dimensional orientation using relative GPS spatial phase
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US Patent 7382313 Method for absolute calibration of global navigation satellite system antennas
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US Patent 7409289 Device for monitoring the integrity of information delivered by a hybrid INS/GNSS system
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US Patent 7538721 GNSS signal processing with partial fixing of ambiguities
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US Patent 7692578 GNSS signal processing with clock difference modeling
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US Patent 7696922 Method and apparatus for geolocation determination
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US Patent 8089402 System and method for correcting global navigation satellite system carrier phase measurements in receivers having controlled reception pattern antennas
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Patent Primary Examiner
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Harry K Liu
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CPC Code
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G01S 19/49
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G01S 19/52
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G01S 19/07
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G01S 19/20
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G01S 19/252
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G01S 19/44
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Patent abstract

A system for estimating a receiver position with high integrity can include a reference station observation monitor configured to: receive a set of reference station observations associated with a set of reference stations, detect a predetermined event, and mitigate an effect of the predetermined event; a modeling engine configured to generate corrections; a reliability engine configured to validate the corrections; an observation monitor configured to: receive a set of satellite observations from a set of global navigation satellites corresponding to at least one satellite constellation; detect a predetermined event; and mitigate an effect of the predetermined event; a carrier phase determination module configured to determine a carrier phase ambiguity of the set of satellite observations; and a position filter configured to estimate a position of the receiver.

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