Assimilating GNSS Signals to Improve Accuracy, Robustness, and Resistance to Signal Interference

• US 20110068973A1
• Filed: 09/23/2010
• Published: 03/24/2011
• Est. Priority Date: 09/24/2009
• Status: Abandoned Application

• Current Assignee: Apple Inc.
• Original Assignee: Coherent Navigation, Inc. (Apple Inc.)
• Inventors: Galusha, Bryan T., Ledvina, Brent M., Cohen, Clark E., Bencze, William J., Humphreys, Todd E.
• Application Number:
  US12/889,242
• Publication Number:
  US 20110068973A1
• Time in Patent Office: Days
• US Class Current: 342/357.3
• CPC Class Codes: G01S 19/215 issues related to spoofing

Abstract

A method for upgrading GNSS equipment to improve position, velocity and time (PVT) accuracy, increase PVT robustness in weak-signal or jammed environments and protect against counterfeit GNSS signals (spoofing). A GNSS Assimilator couples to an RF input of existing GNSS equipment, e.g., a GPS receiver, and extracts navigation and timing information from available RF signals, including non-GNSS signals, or direct baseband aiding, e.g., from an inertial navigation system, frequency reference, or GNSS user. The Assimilator fuses the diverse navigation and timing information to embed a PVT solution in synthesized GNSS signals provided to a GNSS receiver RF input. The code and carrier phases of the synthesized GNSS signals are aligned with those of actual GNSS signals to appear the same at the target receiver input. The Assimilator protects against spoofing by continuously scanning incoming GNSS signals for signs of spoofing, and mitigating spoofing effects in the synthesized GNSS signals.

Claims

1. A method for generating a set of radio-frequency (RF) GNSS signals, the method comprising:

receiving a plurality of RF signals, each signal bearing one or more navigation or timing usable observables;

estimating a first navigation solution based on the observables from the plurality of signals; and

generating a plurality of simulated radio-frequency GNSS signals defining a second navigation solution substantially consistent with the first navigation solution.

2. The method of claim 1, wherein the one or more observables comprises at least one of a code phase, carrier phase, carrier frequency, navigation data bit sequence phase, and correlation function profile.

3. The method of claim 1, wherein at least one of the plurality of signals is a non-GNSS signal.

4. The method of claim 3, wherein the one or more observables includes at least one of signal time-of-arrival, signal angle-of-arrival, carrier frequency, and data bit sequence phase.

5. The method of claim 1, further comprising receiving at least one of position, velocity, and acceleration observables from a local inertial measurement unit for use in at least one of the estimating and the generating.

6. The method of claim 1, wherein the second navigation solution is obtained using an estimator routine to fuse at least one of the one or more GNSS observables and one or more non-GNSS observables.

7. The method of claim 1, further comprising relating an antenna position, velocity and receiver time to at least one of a GNSS observable and a non-GNSS observable.

8. The method of claim 1, further comprising inputting the simulated GNSS signal into a GNSS receiver.

9. The method of claim 1, wherein the plurality of signals includes exclusively non-GNSS signals.

10. The method of claim 1, further comprising aligning at least one of a carrier phase and a code phase of the synthesized GNSS signal with a respective one of a carrier phase and a code phase of one or more ambient radio-frequency GNSS signals at a predetermined three-dimensional position offset and a predetermined velocity offset relative to a predetermined antenna reference location.

11. The method of claim 1, further comprising compensating, with the synthesized GNSS signals, for at least one of a jammed GNSS signal, a weak GNSS signal, a counterfeit GNSS signal, and a compromised GNSS signal.

12. The method of claim 1, further comprising receiving a baseband signal bearing at least one of time, position and velocity data wherein the baseband signal comprises one of an inertial navigation system signal, a time reference signal, a frequency reference signal, and a user input.

13. The method of claim 1, wherein an output signal is compliant with a target dedicated GNSS receiver.

14. The method of claim 1, wherein the assimilator is integrated into a GNSS receiver.

15. A GNSS signal assimilator comprising:

a signal receiver configured to receive a plurality of RF signals and extract at least one code observable corresponding to each of the plurality of signals;

a navigation and timing fusing module configured to render, from the code observables, time and position data, and to calculate a first navigation solution based on the rendered data; and

a signal simulator module configured to synthesize a plurality of GNSS signals that collectively define a second navigation solution substantially consistent with the first navigation solution.

16. The GNSS signal assimilator of claim 15, wherein the GNSS signal receiver is a multi-system receiver module configured to receive a non-GNSS signal and wherein the navigation and timing fusion module is configured to render time, position, or velocity data from the non-GNSS signal.

17. The GNSS signal assimilator of claim 15, wherein the navigation and timing fusion module is configured to render a navigation solution using time, position or velocity data rendered exclusively from one or more non-GNSS signals.

18. The GNSS signal assimilator of claim 15, wherein the one or more non-GNSS signals includes at least one of a television signal, communications network signal, HDTV signal, LORAN signal, ELORAN signal, Radar signal, and IRIDIUM™

signal.

19. The GNSS signal assimilator of claim 15, further comprising an RF output and wherein the synthesizing module is configured to output the second navigation solution as an RF GNSS signal.

20. The GNSS signal assimilator of claim 19, further configured to align at least one of a carrier phase and a code phase of the synthesized GNSS signal with a respective carrier phase and code phase of one or more ambient radio-frequency GNSS signals at a predetermined three-dimensional position offset and a predetermined velocity offset relative to a predetermined assimilator reference location.

21. The GNSS signal assimilator of claim 19, further comprising an anti-spoofing module operable to continuously analyze data received at the GNSS signal receiver to detect potential spoofing via one of a data bit latency, a vestigial signal, a signal angle-of-arrival, a signal angle-of-arrival measured by multiple antennae, RAIM outlier data, signal quality deterioration, and a cryptographic signature.