System, method, and apparatus for compensating for ionospheric delay in a multi constellation single radio frequency path GNSS receiver
First Claim
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1. A method for a single Radio Frequency (RF) path receiver to compensate for ionospheric delay in multi constellation Global Navigation Satellite Systems (GNSSs), the method comprising:
- identifying that a first satellite in a first GNSS constellation and a second satellite in a second GNSS constellation are within a predetermined distance from each other;
receiving a first signal at a first frequency from the first satellite;
receiving a second signal at a second frequency from the second satellite; and
calculating the ionospheric delay using the received first signal and the received second signal,wherein identifying that the first satellite and the second satellite are within the predetermined distance from each other comprises identifying that the first satellite and the second satellite are positioned within a same sector among a plurality of sectors in an azimuth plane.
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Abstract
Systems, methods, and apparatuses are provided for compensating for ionospheric delay in multi constellation Global Navigation Satellite Systems (GNSSs). In one method, a single Radio Frequency (RF) path receiver receives a first signal at a first frequency from a first satellite in a first GNSS constellation, receives a second signal at a second frequency from a second satellite in a second GNSS constellation, and calculates the ionospheric delay using the received first signal and the received second signal.
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Citations
14 Claims
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1. A method for a single Radio Frequency (RF) path receiver to compensate for ionospheric delay in multi constellation Global Navigation Satellite Systems (GNSSs), the method comprising:
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identifying that a first satellite in a first GNSS constellation and a second satellite in a second GNSS constellation are within a predetermined distance from each other; receiving a first signal at a first frequency from the first satellite; receiving a second signal at a second frequency from the second satellite; and calculating the ionospheric delay using the received first signal and the received second signal, wherein identifying that the first satellite and the second satellite are within the predetermined distance from each other comprises identifying that the first satellite and the second satellite are positioned within a same sector among a plurality of sectors in an azimuth plane. - View Dependent Claims (2, 3, 4, 5, 6)
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7. A single Radio Frequency (RF) path receiver that compensates for ionospheric delay in multi constellation Global Navigation Satellite Systems (GNSSs), the receiver comprising:
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an antenna configured to receive a first signal at a first frequency from a first satellite in a first GNSS constellation, and to receive a second signal at a second frequency from a second satellite in a second GNSS constellation; a processor; and a non-transitory computer-readable medium having program instructions recorded thereon, the program instructions configured for the processor to identify that the first satellite and the second satellite are within a predetermined distance from each other; and calculate the ionospheric delay using the received first signal and the received second signal, wherein the processor identifies that the first satellite and the second satellite are within the predetermined distance from each other by identifying that the first satellite and the second satellite are positioned within a same sector among a plurality of sectors in an azimuth plane. - View Dependent Claims (8, 9, 10, 11, 12)
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13. A navigation system, comprising:
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a first satellite in a first Global Navigation Satellite Systems (GNSS) constellation; a second satellite in a second GNSS constellation; and a single Radio Frequency (RF) path receiver configured to receive a first signal at a first frequency from the first satellite, receive a second signal at a second frequency from the second satellite, and calculate ionospheric delay using the received first signal and the received second signal, wherein the receiver identifies that the first satellite and the second satellite are within a predetermined distance from each other, when the first satellite and the second satellite are positioned within a same sector among a plurality of sectors in an azimuth plane. - View Dependent Claims (14)
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Specification