Using space-based augmentation system (SBAS) grid ionosphere vertical error (GIVE) information to mitigate ionosphere errors for ground based augmentation systems (GBAS)

Patent metadata

Field	Value
Publication number	US-9945954-B2
Application number	US-201414549382-A
Country	US
Kind code	B2
Filing date	Nov 20, 2014
Priority date	Nov 20, 2014
Publication date	Apr 17, 2018
Grant date	Apr 17, 2018

Abstract

GBAS includes reference receivers, processing module, and communication device. Processing module checks GNSS satellite measurements to determine proximity of GNSS satellite measurement's IPP to IGPs derived from SBAS geostationary satellites. Processing module determines that GNSS satellite measurement is safe for mitigation using overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) when IGPs possess acceptable GIVE values. Processing module determines whether number of GNSS satellite measurements determined safe for mitigation using σ vig are able to produce VPL that meets VAL required for precision approach. Communication device communicates overbounded σ vig along with differential corrections and indication of which GNSS satellite measurements that are safe for mitigation using at least one overbounded σ vig are able to produce VPL that meets VAL required for precision approach to GNSS receiver when number of GNSS satellite measurements determined safe for mitigation using overbounded σ vig are able to produce VPL that meets VAL required for precision approach.

First claim

What is claimed is:

1. A Ground Based Augmentation System (GBAS) comprising:
a plurality of reference receivers having known positions;
at least one processing module communicatively coupled to the plurality of reference receivers;
at least one aircraft communication device communicatively coupled to the at least one processing module;
wherein the at least one processing module is configured to check a Global Navigation Satellite System (GNSS) satellite measurement for each of a plurality of Global Navigation Satellite System (GNSS) satellites to determine a proximity of each Global Navigation Satellite System (GNSS) satellite measurement's Ionosphere Pierce Point (IPP) to a plurality of Ionosphere Grid Points (IGPs) derived from at least one Space-Based Augmentation System (SBAS) geostationary satellite;
wherein the at least one processing module is further configured to determine that the Global Navigation Satellite System (GNSS) satellite measurement for each of the plurality of Global Navigation Satellite System (GNSS) satellites is safe for mitigation using at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) when the Ionosphere Grid Points (IGPs) possess acceptable Grid Ionosphere Vertical Error (GIVE) values;
wherein the at least one processing module is further configured to determine whether a number of Global Navigation Satellite System (GNSS) satellite measurements determined safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) are able to produce a Vertical Protection Limit (VPL) that meets a Vertical Alert Limit (VAL) required for a precision approach; and
wherein the at least one processing module is configured to cause the at least one aircraft communication device to communicate the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) along with differential corrections for at least one of the plurality of GNSS satellites and an indication of which Global Navigation Satellite System (GNSS) satellite measurements that are safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) are able to produce the Vertical Protection Limit (VPL) that meets the Vertical Alert Limit (VAL) required for the precision approach to an aircraft GNSS receiver when the number of Global Navigation Satellite System (GNSS) satellite measurements determined safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) are able to produce a Vertical Protection Limit (VPL) that meets a Vertical Alert Limit (VAL) required for the precision approach.

2. The Ground Based Augmentation System (GBAS) of claim 1 , wherein the plurality of reference receivers includes four reference receivers.

3. The Ground Based Augmentation System (GBAS) of claim 1 , wherein the number of Global Navigation Satellite System (GNSS) satellite measurements determined safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) are able to produce the Vertical Protection Limit (VPL) that meets the Vertical Alert Limit (VAL) required for the precision approach when the Vertical Protection Limit (VPL) is less than the Vertical Alert Limit (VAL).

4. The Ground Based Augmentation System (GBAS) of claim 1 , wherein the at least one processing module is configured to wait a timeout period before resuming operation when the number of Global Navigation Satellite System (GNSS) satellite measurements determined safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) are not able to produce the Vertical Protection Limit (VPL) that meets the Vertical Alert Limit (VAL) required for the precision approach.

5. The Ground Based Augmentation System (GBAS) of claim 1 , wherein the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) includes a separate overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) for each of the plurality of Global Navigation Satellite System (GNSS) satellites.

6. The Ground Based Augmentation System (GBAS) of claim 1 , wherein the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) includes a single overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) which covers a worst case Global Navigation Satellite System (GNSS) satellite measurement from the plurality of Global Navigation Satellite System (GNSS) satellites.

7. The Ground Based Augmentation System (GBAS) of claim 1 , further comprising:
wherein the at least one processing module is further configured to determine a Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) based on a real-time screen of all possible Global Navigation Satellite System (GNSS) satellite geometries when there is not the number of Global Navigation Satellite System (GNSS) satellite measurements determined safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) that are able to produce a Vertical Protection Limit (VPL) that meets a Vertical Alert Limit (VAL) required for a precision approach.

8. The Ground Based Augmentation System (GBAS) of claim 1 , wherein the overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) corresponds to Grid Ionosphere Vertical Error (GIVE) values around each of the plurality of Global Navigation Satellite System (GNSS) satellite's Ionosphere Pierce Point (IPP).

9. A method of using a Space-Based Augmentation System (SBAS) to mitigate error induced by an ionosphere for a Ground Based Augmentation System (GBAS) used with a Global Navigation Satellite System (GNSS), the method comprising:
checking a plurality of Global Navigation Satellite System (GNSS) satellite measurements observable to a Ground Based Augmentation System (GBAS) to determine a proximity of each Ionosphere Pierce Point (IPP) for the plurality of Global Navigation Satellite System (GNSS) satellite measurements to a plurality of Ionosphere Grid Points (IGPs) derived from at least one Space-Based Augmentation System (SBAS) geostationary satellite;
when the Ionosphere Grid Points (IGPs) possess acceptable Grid Ionosphere Vertical Error (GIVE) values, considering the Global Navigation Satellite System (GNSS) satellite measurement safe for mitigation using an overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig );
determining if a number of Global Navigation Satellite System (GNSS) satellite measurements meeting the overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) will be able to produce a vertical protection limit (VPL) that meets a Vertical Alert Limit (VAL) required for a precision approach; and
communicating the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) along with differential corrections for at least one of the plurality of GNSS satellites and an indication of which Global Navigation Satellite System (GNSS) satellite measurements that are safe for mitigation using the at least one overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) will produce the Vertical Protection Limit (VPL) that meets the Vertical Alert Limit (VAL) required for the precision approach to an aircraft Global Navigation Satellite System (GNSS) receiver when the number of Global Navigation Satellite System (GNSS) satellite measurements meeting the overbounded Vertical Ionosphere Gradient standard deviation sigma-vig (σ vig ) are able to prod

Assignees

• Honeywell Int Inc

Inventors

• Mcdonald James Arthur
• Jakel Tom
• Class Kim A

Classifications

• G01S19/072 Primary

  Ionosphere corrections · CPC title

• G01S19/071

  DGPS corrections · CPC title

• G01S19/074 Primary

  providing integrity data, e.g. WAAS · CPC title

• G01S19/03

  Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers · CPC title

• G01S19/40

  Correcting position, velocity or attitude · CPC title