Controlled access satellite navigation receiver

• US 20130176168A1
• Filed: 11/28/2012
• Published: 07/11/2013
• Est. Priority Date: 01/05/2012
• Status: Abandoned Application

• Current Assignee: Clipper Street Systems, LLC
• Original Assignee: Clipper Street Systems, LLC
• Inventors: Lo, Sherman C., De Lorenzo, David S., Jennings, Chad
• Application Number:
  US13/687,875
• Publication Number:
  US 20130176168A1
• Time in Patent Office: Days
• US Class Current: 342/357.3
• CPC Class Codes: G01S 19/18 Military applications
• CPC Class Codes: G01S 19/215 issues related to spoofing
• CPC Class Codes: G01S 19/42 Determining position
• CPC Class Codes: G01S 19/426 by combining or switching between position solutions or signals derived from different modes of operation in a single system
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial

Abstract

A controlled access satellite navigation receiver has only incomplete knowledge of secret codes transmitted by satellites. This incomplete knowledge allows only intermittent position determination. Incomplete secret codes and the intermittent positions they provide are useful for authenticating navigation signals or controlling access to secret satellite services.

Claims

1. A controlled access satellite navigation receiver comprising:

a secret code segment memory that stores segments of a secret code to be transmitted by a satellite in the future;

a correlator that correlates signals received from the satellite with secret code segments retrieved from the memory; and

,

a position filter that estimates position intermittently based on pseudoranges computed from secret code segment correlations.

2. The receiver of claim 1, the secret code segments generated by a secret code generator in the receiver.

3. The receiver of claim 1, the receiver obtaining secret code segments over the air in encrypted form.

4. The receiver of claim 1, further comprising a public code GNSS receiver that generates public code position estimates, and the position filter further comparing public and secret code position estimates.

5. The receiver of claim 4, the position filter indicating that the public code position estimate is authentic if it is consistent with the secret code position estimate.

6. The receiver of claim 1, further comprising an INS that generates position estimates, and the position filter further correcting INS drift whenever a secret code position estimate is available.

7. The receiver of claim 6, the INS including an IMU and a clock.

8. The receiver of claim 6, the INS being a clock.

9. The receiver of claim 1, the secret code being a memory code.

10. The receiver of claim 1, the secret code segments having a duty cycle of no more than 50% of the secret code.

11. A method for operating a controlled access satellite navigation receiver comprising:

receiving a signal from a satellite;

demodulating and sampling the signal to convert it to digital form;

correlating the signal against a secret code segment; and

,

computing secret pseudoranges from the secret code segment correlation.

12. The method of claim 11 further comprising:

estimating position based on the secret pseudoranges.

13. The method of claim 12 further comprising:

correcting drift in an INS with the estimated position.

14. The method of claim 13, the INS including an IMU and a clock.

15. The method of claim 13, the INS being a clock.

16. The method of claim 11 further comprising:

estimating position based on the secret pseudoranges and INS measurements.

17. The method of claim 11 further comprising:

correlating the signal against a public code;

computing public pseudoranges from the public code correlation; and

,

estimating position based on the public and secret pseudoranges.

18. The method of claim 11 further comprising:

estimating a first position based on the secret pseudoranges;

correlating the signal against a public code;

computing public pseudoranges from the public code correlation;

estimating a second position based on pseudoranges obtained with public code; and

,

authenticating the second position estimate if it is consistent with the first position estimate.

19. The method of claim 11 further comprising:

correlating the signal against a public code;

computing public pseudoranges from the public code correlation;

estimating a position based on pseudoranges obtained with public code; and

,

authenticating the position estimate if the secret and public pseudoranges are consistent.