Spacecraft position monitoring and control

• US 20070085735A1
• Filed: 10/19/2005
• Published: 04/19/2007
• Est. Priority Date: 10/19/2005
• Status: Abandoned Application

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Bay, Fm
• Application Number:
  US11/253,369
• Publication Number:
  US 20070085735A1
• Time in Patent Office: Days
• US Class Current: 342/357.330
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/50 whereby the position solution is constrained to lie upon a particular curve or surface, e.g. for locomotives on railway tracks
• CPC Class Codes: G01S 5/14 Determining absolute distances from a plurality of spaced points of known location

Abstract

A method and system for providing integrity information from a spacecraft in a non-geostationary constellation of spacecraft. According to one aspect of the present invention, a terrestrial source is provided for generating and providing a position message to a spacecraft in the non-geostationary constellation. The position message causes the spacecraft to generate and provide a response message to the terrestrial source. The response message is processed in the terrestrial source to determine spacecraft position data. The spacecraft position data is then provided to the spacecraft and utilized by the spacecraft and other spacecraft in the constellation to provided integrity information to a navigational aid.

Claims

1. A method for updating position data in a non-geostationary constellation of spacecraft, the method comprising:

generating a position message in a terrestrial source;

providing the position message to a first spacecraft to cause the first spacecraft to generate and provide a response message to the terrestrial source;

processing the response message in the terrestrial source to determine spacecraft position data;

sending the spacecraft position data to the first spacecraft;

determining a location of a second spacecraft relative to the first spacecraft; and

providing a navigation message to a navigational aid from the second spacecraft, wherein the navigation message includes an integrity indication based on the location of the second spacecraft relative to the first spacecraft when the navigation message is provided.

2. The method of claim 1 further comprising:

repeating the steps of generating and providing position messages a predetermined number of times to cause the spacecraft to generate and provide a corresponding number of response messages; and

processing the corresponding number of response messages in the terrestrial source to determine the spacecraft position data.

3. The method of claim 1 wherein the step of providing the position message includes:

including a time tag in the position message to cause the spacecraft to include a time tag in the response message.

4. The method of claim 1 wherein the step of providing the position message comprises:

providing the position message from at least one ground station to a spacecraft known to be in view of the at least one ground station.

5. The method of claim 1 wherein the step of providing the position message includes:

providing the position message from at least one ground station to a spacecraft known to be in view of a plurality of ground stations including the at least one ground station.

6. The method of claim 1 wherein the spacecraft position data includes:

ephemeris data relating to the spacecraft.

7. The method of claim 1 further comprising:

updating position data stored in the spacecraft using the spacecraft position data.

8. The method of claim 1 further comprising:

updating position data stored in at least one other spacecraft in the constellation using the spacecraft position data.

9. The method of claim 1 further comprising:

updating position data stored in a plurality of other spacecraft in the constellation using the spacecraft position data.

10. The method of claim 1 wherein the spacecraft position data includes clock synchronization information for the spacecraft.

11. The method of claim I wherein the step of providing the position message includes:

providing the position message over a first set of predetermined frequencies.

12. The method of claim 11 further comprising:

generating the response message in the spacecraft and transmitting the response message over a second set of predetermined frequencies different from the first set of predetermined frequencies.

13. A system for updating position data in a non-geostationary constellation of spacecraft, the station comprising:

a processing system operable to generate a position message for a spacecraft in the constellation, receive a response message from the spacecraft, and process the response message to generate spacecraft position data for the spacecraft; and

an interface system in communication with the processing system and operable to provide the position message to the spacecraft, receive the response message from the spacecraft and provide the spacecraft position data to the spacecraft.

14. The system of claim 13 wherein the processing system is configured to generate a plurality of position messages for the spacecraft and process a corresponding plurality of response messages from the spacecraft to generate the spacecraft position data.

15. The system of claim 13 wherein the position message and corresponding response message include a time tag.

16. The system of claim 13 wherein the spacecraft position data includes ephemeris information relating to the spacecraft.

17. The system of claim 13 wherein the spacecraft position data includes clock synchronization information for the spacecraft.

18. The system of claim 13 wherein the interface system is configured to provide the position message over a first set of predetermined frequencies and receive the response message over a second set of predetermined frequencies different from the first set of predetermined frequencies.

19. A method for providing navigation information from a spacecraft in a non-geostationary constellation of spacecraft, the method comprising:

receiving first updated position data in a first spacecraft of the non-geostationary constellation of spacecraft;

determining in a second spacecraft of the non-geostationary constellation of spacecraft, second updated position data based on the first updated position data received in the first spacecraft; and

providing a navigation message to a navigation aid from the second spacecraft, wherein the navigation message includes a first integrity indication based on the location of the second spacecraft relative to the first spacecraft when the navigation message is provided.

20. The method of claim 19, wherein the receiving step comprises:

receiving the first updated position data in the first spacecraft from a terrestrial source.

21. The method of claim 19 further comprising:

receiving, from the terrestrial source, third updated position data in a third spacecraft of the non-geostationary constellation.

22. The method of claim 21 further comprising:

determining in the second spacecraft, the second updated position data based on the third updated position data received in the third spacecraft and determining in the first spacecraft, the first updated position data based on the third updated position data received in the third spacecraft.

23. The method of claim 22 further comprising:

providing a navigation message to the navigation aid from the second spacecraft, wherein the navigation message includes a second integrity indication based on the location of the second spacecraft relative to the third spacecraft when the navigation message is provided.