Using space based augmentation system (sbas) ephemeris sigma information to reduce ground based augmentation systems (gbas) ephemeris decorrelation parameter
US-2017212241-A1 · Jul 27, 2017 · US
US9989644B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9989644-B2 |
| Application number | US-201615019840-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 9, 2016 |
| Priority date | Feb 9, 2016 |
| Publication date | Jun 5, 2018 |
| Grant date | Jun 5, 2018 |
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A system to mitigate errors in GPS corrections and ephemeris uncertainty data broadcast to a vehicle is presented. The system includes reference receivers in a first ground subsystem and a processor. The processor: receives, from reference receivers in a wide area network of reference receivers, satellite measurement data for a first plurality of satellites and receives, from the reference receivers in the first ground subsystem, satellite measurement data and ephemeris data from a second plurality of satellites; evaluate the satellite measurement data to determine if the GPS corrections are degraded by a current ionosphere disturbance activity; determine a current quality metric of the ionosphere; adjust a Vertical Ionosphere Gradient standard deviation sigma-vig; evaluate the ephemeris data to determine if the GPS corrections provided to the vehicle are degraded by ephemeris errors; and establish ephemeris uncertainty to protect integrity based on the evaluation of the ephemeris data.
Opening claim text (preview).
What is claimed is: 1. A system to mitigate errors in global position system (GPS) corrections and ephemeris uncertainty data broadcast to a vehicle consuming the GPS corrections and the ephemeris uncertainty data, the system comprising: at least two reference receivers, in a first ground subsystem at a first ground site, configured to receive satellite measurement data and ephemeris uncertainty data from a second plurality of satellites in view of the first ground subsystem; at least one processor communicatively coupled to the at least two reference receivers, the at least one processor configured to: receive, from a plurality of reference receivers in a wide area network of reference receivers positioned at other ground sites, satellite measurement data for a first plurality of satellites in view of the plurality of reference receivers; and receive, from the at least two reference receivers in the first ground subsystem, the satellite measurement data and the ephemeris data, wherein the first ground site is different from the other ground sites and wherein the second plurality of satellites is a subset of the first plurality of satellites; execute algorithms to: evaluate the satellite measurement data received from the at least two reference receivers in the first ground subsystem and the satellite measurement data received from the plurality of reference receivers in the wide area network of reference receivers to determine if the GPS corrections broadcast to the vehicle are degraded by a current ionosphere disturbance activity; determine a current quality metric of the ionosphere based on the evaluation of the satellite measurement data adjust a Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) based on the determined quality metric of the ionosphere; evaluate the ephemeris data associated with the second plurality of satellites in view of the first ground subsystem and evaluate the satellite measurement data for the first plurality of satellites in view of the plurality of reference receivers to determine if the GPS corrections provided to the vehicle are degraded by ephemeris errors; and establish ephemeris uncertainty to protect integrity based on the evaluation of the ephemeris data. 2. The system of claim 1 , wherein the at least one processor is further configured to: determine if the ephemeris uncertainty for one or more of the second plurality of satellites in view of the first ground subsystem is less than a preselected threshold; and if the ephemeris uncertainty for a satellite in view of the first ground subsystem is less than the preselected threshold, broadcast the adjusted Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) and the ephemeris uncertainty data from the first ground subsystem. 3. The system of claim 1 , further comprising: at least one transmitter in the first ground subsystem, wherein the at least one processor is further configured to: determine if the ephemeris uncertainty for one or more of the second plurality of satellites in view of the first ground subsystem is less than a preselected threshold, and if the ephemeris uncertainty for a satellite in view of the first ground subsystem is less than the preselected threshold, broadcast the adjusted Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) and the ephemeris uncertainty data from the at least one transmitter in the first ground subsystem. 4. The system of claim 1 , wherein the at least one processor is further configured to: determine if the ephemeris uncertainty for one or more of the second plurality of satellites in view of the first ground subsystem exceeds a preselected threshold; and if the ephemeris uncertainty for a satellite in view of the first ground subsystem exceeds the preselected threshold, ceasing broadcast, from the first ground subsystem, of the correction data for the effected satellite. 5. The system of claim 1 , further comprising: the plurality of reference receivers positioned at the other ground sites. 6. The system of claim 5 , wherein the wide area network of reference receivers positioned at other ground sites, includes a wide area network of reference receivers in other ground subsystems positioned at respective other ground sites. 7. The system of claim 6 , further comprising: at least one processor in the other ground subsystems positioned at respective other ground sites. 8. The system of claim 7 , wherein the at least one processor in the other ground subsystems positioned at the respective other ground sites is configured to: receive satellite measurement data and ephemeris data from at least two reference receivers in the other ground subsystem in which the respective at least one processor is located, and receive, from the at least two reference receivers in the first ground subsystem, satellite measurement data from the second plurality of satellites in view of the first ground subsystem. 9. The system of claim 6 , wherein the at least two reference receivers in the first ground subsystem include at least one transmitter. 10. The system of claim 1 , further comprising: a receiver in the first ground subsystem to input and compile the satellite measurement data from the plurality of reference receivers for output to the at least one processor. 11. The system of claim 1 , further comprising: a modem in the first ground subsystem to input and compile the satellite measurement data from the plurality of reference receivers for output to the at least one processor. 12. A method of mitigating errors in global position system (GPS) corrections and ephemeris uncertainty data broadcast to a vehicle consuming the GPS corrections and the ephemeris uncertainty data, the method comprising; receiving at a first ground subsystem positioned at a first ground site, from a plurality of reference receivers in a wide area network of reference receivers positioned at other ground sites, satellite measurement data for a first plurality of satellites in view of the plurality of reference receivers, wherein the other ground sites are different from the first ground site; receiving, from at least two reference receivers in the first ground subsystem, satellite measurement data and ephemeris data from a second plurality of satellites in view of the first ground subsystem, wherein the second plurality of satellites is a subset of the first plurality of satellites; evaluating the satellite measurement data received from the at least two reference receivers in the first ground subsystem and the satellite measurement data received from the plurality of reference receivers in the wide area network of reference receivers to determine if the GPS corrections broadcast to the vehicle are degraded by a current ionosphere disturbance activity; determining a current quality metric of the ionosphere based on the evaluation of the satellite measurement data; adjusting a Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) based on the determined quality metric of the ionosphere; evaluating the ephemeris data associated with the second plurality of satellites in view of the first ground subsystem and evaluating the satellite measurement data for the first plurality of satellites in view of the plurality of reference receivers to determine if the GPS corrections provided to the vehicle are degraded by ephemeris errors; and establish ephemeris uncertainty to protect integrity based on the evaluation of the ephemeris data. 13. The method of claim 12 , further comprising: determining if the ephemeris uncertainty for one or more of the second plurality of satellites in view
providing integrity data, e.g. WAAS · CPC title
Ionosphere corrections · CPC title
DGPS corrections · CPC title
providing integrity information, e.g. health of satellites or quality of ephemeris data · CPC title
providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections · CPC title
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