Differential satellite positioning system ground station with integrity monitoring

• US 5,600,329 A
• Filed: 06/30/1995
• Issued: 02/04/1997
• Est. Priority Date: 06/30/1995
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Brenner, Mats A.
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/497,995
• Time in Patent Office: 585 Days
• Field of Search: 342/357, 342/33, 342/407, 364/424.06, 340/979
• US Class Current: 342/357.44
• CPC Class Codes: G01S 19/071 DGPS corrections
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/41 Differential correction, e.g. DGPS [differential GPS]
• CPC Class Codes: G01S 5/009 Transmission of differential positioning data to mobile

Abstract

In the present invention, a plurality of DGPS receivers are employed to determine receiver-satellite-specific differential correction values. In turn, satellite-specific differential correction values are determined as an average of the individual receiver-satellite-specific differential correction values for each of the tracked satellites. A discriminator is employed for determining a receiver-satellite-specific discriminant which may be sampled and subsequent determination of a receiver-satellite-specific statistical value thereof. The receiver-satellite-specific statistical values may then be employed for determination of a Detection Threshold value and other integrity information associated with each of the satellite-specific differential correction values. The ground station further includes a means for communicating the satellite-specific differential correction values and integrity information associated therewith to a DGPS airborne receiver.

An DGPS airborne system in accordance with the present invention is configured to include a mechanization for receiving the satellite-specific differential correction values and integrity information associated therewith. An airborne integrity monitoring system may then be employed to derive particular integrity limit values associated with the DGPS derived position for pilot awareness as to whether or not the pilot should rely upon the DGPS solution for a precision landing.

Claims

1. A differential satellite positioning system ground station for determining GPS differential correction information with integrity monitoring, said differential satellite positioning system ground station comprising:

a plurality of GPS signal receivers, each at a known geocentric position, each operative for receiving a satellite-specific information signal transmitted from each of selected ones of a plurality of satellite vehicles, and each operative for deriving, from each of said received satellite-specific information signals from said satellite vehicles, receiver-satellite-specific GPS signal information;

first differential correction processing means for deriving receiver-satellite-specific GPS differential correction information associated with each of said satellite-specific information signals, where said receiver-satellite specific differential correction information is a function of said receiver-satellite-specific GPS signal information determined by a specific one of said GPS signal receivers and said known position of said GPS signal receivers for the same one of said GPS signal receivers;

second differential correction processing means operative for determining satellite-specific GPS differential correction information, associated with each of said satellite-specific information signals, as a function of said receiver-satellite-specific GPS differential correction information determined by more than one of said plurality of GPS signal receivers and associated with the same one of said satellite-specific information signals;

ground station integrity monitoring means for determining satellite-specific integrity information associated with each of said satellite-specific information signals, as a function of said receiver-satellite-specific GPS differential correction information and said satellite-specific GPS differential correction information, where said satellite-specific integrity information is descriptive of the integrity of said satellite-specific GPS differential correction information.

2. The differential satellite positioning system ground station of claim 1 wherein:

said first differential correction processing means is operative for determining a receiver-satellite-specific GPS differential correction value, associated with each of said satellite-specific information signals and each of said plurality GPS signal receivers, as a function of said receiver-satellite-specific GPS signal information, and said known position of the corresponding one of said plurality of GPS signal receivers;

said second differential correction processing means includes means for providing a satellite-specific statistical GPS differential correction value, associated with each of said received satellite-specific information signals, as an average of said receiver-satellite-specific differential correction values associated with the same satellite information signal and derived from said receiver-satellite-specific GPS signal information from more than one of said plurality of GPS signal receivers; and

said ground station integrity monitoring means includes,

discriminator means operative for determining, for each of said receiver-satellite-specific GPS differential correction values, a receiver-satellite-specific integrity discriminant value as a selected function of corresponding ones of said satellite-specific statistical GPS differential correction values and said receiver-satellite-specific differential correction values associated with the same satellite-specific information signal and corresponding one of said plurality of GPS signal receivers,

a statistical value processing means operative for determining a receiver-satellite-specific statistical value associated with each of said receiver-satellite-specific integrity discriminant values, as a function of corresponding ones of said receiver-satellite-specific integrity discriminant values, and which is descriptive of the behavior of said receiver-satellite-specific integrity discriminant values sampled over a selected time period.

3. The differential satellite positioning system ground station of claim 2 wherein said ground station integrity monitoring means determines said satellite-specific integrity information as a function of said receiver-satellite-specific statistical integrity discriminant values associated with more than one of said plurality of GPS signal receivers and associated with the same one of said satellite-specific information signals.

4. The differential satellite positioning system ground station of claim 2 wherein said integrity monitoring means further includes deselecting means for identifying those of said receiver-satellite-specific integrity discriminant values which exceed a selected detection threshold.

5. The differential satellite positioning system ground station of claim 4 wherein said deselecting monitoring means includes:

means for determining a detection threshold value as a function of said receiver-satellite-specific statistical integrity discriminate values; and

comparator means for comparing each of said integrity discriminate values with said detection threshold value, and providing an identification of which receive-satellite-specific ones of said receiver-satellite-specific discriminant values exceeds said detection threshold value.

6. The differential satellite positioning system ground station of claim 1 further comprising means for communicating said satellite-specific differential correction information and corresponding satellite-specific integrity information to a remote differential satellite positioning system user.

7. The differential satellite positioning system ground station of claim 1 wherein said differential correction processing means includes means for determining said receiver-satellite-specific differential correction values synchronized to a common measurement time and with receiver-specific clock bias removed.

8. The differential satellite positioning system ground station of claim 5 wherein each of said satellite-specific differential correction values is a function of said receiver-satellite-specific differential correction values excluding those receiver-satellite-specific ones having corresponding receiver-satellite-specific discriminant values which were identified by said comparator means.

9. A differential satellite positioning system comprising:

ground station for determining GPS differential correction information, with integrity monitoring including,

a plurality of GPS signal receivers, each at a known geocentric position, each operative for receiving a satellite-specific information signal transmitted from each of selected ones of a plurality of satellite vehicles, and each operative for deriving, from each of said received satellite-specific information signals from said satellite vehicles, receiver-satellite-specific GPS signal information;

first differential correction processing means for deriving receiver-satellite-specific GPS differential correction information associated with each of said satellite-specific information signals, where said receiver-satellite specific differential correction information is a function of said receiver-satellite-specific GPS signal information determined by a specific one of said GPS signal receivers and said known position of said GPS signal receivers for the same one of said GPS signal receivers;

second differential correction processing means operative for determining satellite-specific GPS differential correction information, associated with each of said satellite-specific information signals, as a function of said receiver-satellite-specific GPS differential correction information determined by more than one of said plurality of GPS signal receivers and associated with the same one of said satellite-specific information signals;

ground station integrity monitoring means for determining satellite-specific integrity information associated with each of said satellite-specific information signals, as a function of said receiver-satellite-specific GPS differential correction information and said satellite-specific GPS differential correction information, where said satellite-specific integrity information is descriptive of the integrity of said satellite-specific GPS differential correction information

means for transmitting said satellite-specific differential correction information and said satellite-specific integrity information to a remote differential satellite positioning system; and

a remote differential satellite positioning system including,

means for receiving said satellite-specific differential correction information and said satellite-specific integrity information,

GPS signal receiver operative for (i) receiving a satellite-specific information signal transmitted from each of selected ones of a plurality of satellite vehicles, and operative for deriving from each of said satellite-specific information signals from said satellite vehicles user-satellite-specific GPS signal information,(ii) deriving the user-position of said remote GPS signal receiver as a function of said user-satellite-specific GPS signal information corrected by said satellite-specific GPS differential correction information, and (iii) determining a position solution matrix representative of the line of sight vectors between the derived user-position and each of said satellite vehicles, and

integrity monitoring means for determining the integrity of said user position as a function of said position solution matrix and said satellite-specific integrity information.

10. A differential satellite positioning system ground station for determining satellite-specific GPS differential correction information with corresponding satellite-specific integrity information, said differential satellite positioning system ground station comprising:

a plurality of GPS signal receivers, each at a known geocentric position, each operative for receiving a satellite-specific information signal transmitted from each of selected ones of a plurality of satellite vehicles, and each operative for deriving, from each of said received satellite-specific information signals from said satellite vehicles, receiver-satellite-specific GPS signal information;

differential correction processing means for separately deriving a receiver-satellite-specific GPS differential correction value for each GPS signal receiver, and associated with each of said satellite-specific information signals, as a function of said receiver-satellite-specific GPS signal information determined by each of said plurality of GPS signal receivers;

means for determining a satellite-specific GPS differential correction value, associated with each of said satellite-specific information signals, as an averaging function of said receiver-satellite-specific GPS differential correction values determined by more than one of said plurality of GPS signal receivers and associated with the same one of said satellite-specific information signals;

discriminator means for determining a receiver-satellite-specific discriminant value associated with each satellite-specific information signal and specific one of said GPS signal receivers, where each receiver-satellite-specific discriminant value is a function of the difference between corresponding ones of said receiver-satellite-specific GPS differential correction value and said satellite-specific GPS differential correction value associated with the same one of said satellite-specific information signals and specific one of said GPS signal receivers

statistical value processing means for determining a receiver-satellite-specific statistical value descriptive of the corresponding behavior of each of said receiver-satellite-specific discriminant values

detection threshold processing means operative for calculating at least a satellite-specific detection threshold value as a function of a selected false detection probability and corresponding receiver-satellite-specific statistical value; and

ground station integrity monitoring means for determining satellite-specific integrity information, associated with each of said satellite-specific information signals and corresponding satellite-specific GPS differential correction values, as a function of said receiver-satellite-specific statistical value, said satellite-specific detection threshold value, and the number of operating GPS signal receivers.

11. The differential satellite positioning system ground station of claim 10 where said receiver-satellite-specific statistical value is descriptive of the behavior of said receiver-satellite-specific integrity discriminant values sampled over a selected time period.

12. A differential satellite positioning system ground station for determining GPS differential correction information with integrity monitoring, said differential satellite positioning system ground station comprising:

a plurality of GPS signal receivers, each at a known geocentric position, each operative for receiving a satellite-specific information signal transmitted from each of selected ones of a plurality of satellite vehicles, and each operative for deriving from each of said received satellite-specific information signals from said satellite vehicles receiver-satellite-specific GPS signal information;

differential correction processing means for determining a receiver-satellite-specific differential correction value associated with each of said selected satellite information signals;

averaging means for determining a satellite-specific average value of said receiver-satellite-specific differential correction values associated with a mutually exclusive one of said satellite information signals;

discriminator means responsive to receiver-satellite-specific differential correction values and said satellite-specific differential correction average values for determining a receiver-satellite-specific discriminant value;

means for determining a statistical value representative of the behavior of said discriminant values; and

integrity monitoring means responsive to said discriminant values and said statistical values for deriving selected integrity information as one or more selected functions thereof.