Satellite integrity monitor and alert

• US 6,603,426 B1
• Filed: 03/22/2001
• Issued: 08/05/2003
• Est. Priority Date: 03/22/2001
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Clark, Ronald H.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US09/813,813
• Time in Patent Office: 866 Days
• Field of Search: 342/357.06, 701/213, 455/12.1, 455/427, 455/428
• US Class Current: 342/357.64
• CPC Class Codes: G01S 19/10 providing dedicated supplementary positioning signals
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/32 Multimode operation in a single same satellite system, e.g. GPS L1/L2

Abstract

The present invention is a system for providing GPS users with a high level of confidence in the integrity and accuracy of received GPS signals. The system provides a means for each GPS satellite itself to verify the accuracy and/or integrity of its own operations by calculations and processing internal to the GPS satellite and by crosslink communications with other GPS satellites in the GPS constellation. After a GPS satellite verifies the accuracy and/or integrity of its own signals, the GPS satellite transmits an integrity message to all GPS users in view of the satellite. The integrity message can alert GPS users to a loss of integrity or accuracy in the GPS signals. Alternatively, the integrity message can contain information to correct errors in the GPS signals. The integrity message can be incorporated into the existing GPS navigation message transmitted by GPS satellites, or the integrity message can be transmitted over a separate channel such as the planned L5 band channel.

Claims

1. A method for verifying the integrity of a navigation message transmitted from a Global Positioning System (GPS) satellite, comprising:

monitoring the integrity of a GPS navigation message produced by a first GPS satellite, the monitoring performed by the first GPS satellite or a second GPS satellite; and

broadcasting a GPS integrity message from the first GPS satellite to GPS users in-view of the satellite, wherein the GPS integrity message indicates the integrity of the GPS navigation message produced by the first GPS satellite.

2. The method of claim 1, wherein the GPS integrity message is incorporated into the GPS navigation message transmitted to GPS users.

3. A method for verifying the integrity of a signal transmitted from a space vehicle, comprising:

monitoring the integrity of a transmission signal produced by a first space vehicle, the monitoring performed by the first space vehicle or a second space vehicle; and

transmitting a first integrity signal from the first space vehicle to a user, wherein the first integrity signal indicates the integrity of the transmission signal produced by the first space vehicle.

4. The method of claim 3, wherein the first and second space vehicles are GPS satellites.

5. The method of claim 3, wherein the first integrity signal is incorporated as a message into the transmission signal.