Satellite navigation using long-term navigation information

• US 8,676,501 B2
• Filed: 12/22/2006
• Issued: 03/18/2014
• Est. Priority Date: 12/22/2006
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Tekawy, Jonathan A., DiEsposti, Raymond S., Kelley, Clifford W.
• Primary Examiner(s): Tran, Khoi
• Assistant Examiner(s): Sample, Jonathan L
• Application Number:
  US11/615,259
• Publication Number:
  US 20080154502A1
• Time in Patent Office: 2,643 Days
• Field of Search: None
• US Class Current: 701/469
• CPC Class Codes: G01S 19/02 Details of the space or ground control segments
• CPC Class Codes: G01S 19/05 providing aiding data

Abstract

An improved approach to satellite-based navigation (e.g., GPS) is provided. In one embodiment, a method includes receiving a first set of tracking information. A nominal orbital path for the navigation satellite is determined using the first set of tracking information. Ephemeris data corresponding to the nominal orbital path is computed and uploaded to the navigation satellite. Long-term navigation information corresponding to the nominal orbital path is transmitted to a communication system for broadcast to a plurality of navigation devices. A second set of tracking information is received, an orbital path of the navigation satellite using the second set of tracking information is predicted, and a difference between the predicted orbital path and the nominal orbital path is determined. Commands configured to instruct the navigation satellite to adjust an actual orbital path of the navigation satellite to substantially conform to the nominal orbital path are uploaded to the navigation satellite.

Claims

1. A method of providing satellite-based navigation at a navigation device, the method comprising:

receiving long-term navigation information at the navigation device from a communication system, wherein the long-term navigation information is associated with a nominal orbital path of a navigation satellite for a time period longer than approximately 24 hours, wherein the navigation satellite has an actual orbital path that is repeatedly adjusted to substantially conform to the nominal orbital path;

estimating at the navigation device a position of the navigation satellite using the long-term navigation information;

repeating at the navigation device the receiving and the estimating operations for a plurality of additional navigation satellites using long-term navigation information associated with each of the additional navigation satellites;

determining at the navigation device a position of the navigation device based on the estimated positions of the navigation satellite and the additional navigation satellites; and

wherein the actual orbital path adjustment and the long-term navigation information permit the estimating, repeating, and determining to be performed during the time period without requiring updated navigation information.

2. The method of claim 1, wherein the long-term navigation information is ephemeris data corresponding to the nominal orbital path.

3. The method of claim 1, wherein the long-term navigation information is state vector data.

4. The method of claim 3, wherein the state vector data comprises models of earth gravity, earth harmonics, earth tides, moon gravity, sun gravity, solar radiation pressure, and predicted satellite trajectory effects based on application of translational control forces.

5. The method of claim 1, further comprising:

receiving ephemeris data from the navigation satellite, wherein the ephemeris data corresponds to the nominal orbital path of the navigation satellite;

selecting the long-term navigation information received from the communication system or the ephemeris data received from the navigation satellite; and

estimating the position of the navigation satellite based on the selected long-term navigation information or the selected ephemeris data.

6. The method of claim 5, further comprising:

repeating the second receiving, the selecting, and the second estimating operations for the plurality of navigation satellites and long-term navigation information or ephemeris data associated with the plurality of navigation satellites; and

determining the position of the navigation device based on the estimated positions of the navigation satellites.

7. The method of claim 1, wherein the communication system is the Internet.

8. The method of claim 1, wherein the communication system is a wireless communication system.

9. The method of claim 1, wherein the method is performed by the navigation device pursuant to a fee-based service agreement.

15. The method of claim 1, wherein the time period is up to several months.

10. A navigation device comprising:

means for receiving long-term navigation information from a communication system, wherein the long-term navigation information is associated with nominal orbital paths of a plurality of navigation satellites for a time period longer than approximately 24 hours, wherein the navigation satellites have actual orbital paths that are repeatedly adjusted to substantially conform to the nominal orbital paths; and

a processor adapted to;

estimate positions of the navigation satellites using the long-term navigation information,

determine a position of the navigation device based on the estimated positions of the navigation satellites, and

wherein the actual orbital path adjustments and the long-term navigation information permit the estimate and determine operations to be performed during the time period without requiring updated navigation information.

11. The navigation device of claim 10, further comprising:

means for receiving ephemeris data from the navigation satellites, wherein the ephemeris data corresponds to nominal orbital paths of the navigation satellites, wherein the processor is further adapted to;

compare the long-term navigation information received from the communication system to the ephemeris data received from the navigation satellites as a consistency check,

select the long-term navigation information received from the communication system or the ephemeris data received from the navigation satellites, and

estimate the positions of the navigation satellites based on the selected long-term navigation information or the selected ephemeris data.

12. The navigation device of claim 10, wherein the long-term navigation information is ephemeris data corresponding to the nominal orbital paths of the navigation satellites.

13. The navigation device of claim 10, wherein the long-term navigation information is state vector data.

14. The navigation device of claim 10, wherein the state vector data comprises models of earth gravity, earth harmonics, earth tides, moon gravity, sun gravity, solar radiation pressure, and predicted satellite trajectory effects based on application of translational control forces.

16. The navigation device of claim 10, wherein the time period is up to several months.