Radionavigation signal tracking device

• US 20140191903A1
• Filed: 01/10/2014
• Published: 07/10/2014
• Est. Priority Date: 01/10/2013
• Status: Active Grant

• Current Assignee: Centre National D'Etudes Spatiales, M3Systems Co.
• Original Assignee: Centre National D'Etudes Spatiales, M3Systems Co.
• Inventors: VIGNEAU, Willy, JARDAK, Nabil, PAIMBLANC, Philippe, PUENGNIM, Anchalee, RIES, Lionel
• Granted Patent: US 9,529,070 B2
• Time in Patent Office: Days
• US Class Current: 342/357.68
• CPC Class Codes: G01S 1/02 using radio waves G01S19/00 takes precedence
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A radionavigation signal tracking device comprises a first and a second tracking stage for radionavigation signals. The first tracking stage comprises a first carrier phase-locked loop. The latter produces a first error signal arising from a phase difference between the first carrier and its replica. The phase of the replica of the first carrier is adjusted with the first error signal. The second tracking stage comprises a second carrier phase-locked loop. The latter produces a second error signal arising from a difference between the first phase difference and a phase difference between the second carrier and the replica thereof. The phase of the replica of the second carrier is adjusted with the first and second error signals.

Claims

1. A radionavigation signal tracking device comprising a first tracking stage of a first radionavigation signal contained in an incoming signal to be applied to the device, the first radionavigation signal comprising a first carrier at a first frequency modulated by a first spreading waveform, said first tracking stage comprising a first carrier phase-locked loop with a mixer configured to multiply the incoming signal with a local replica of the first carrier, the first carrier phase-locked loop comprising a phase discriminator of the first carrier configured to produce a first error signal arising from a first phase difference between the first carrier and the local replica of the first carrier, the first carrier phase-locked loop being configured to adjust the phase of the local replica of the first carrier on the basis of the first error signal;

a second tracking stage of a second radionavigation signal contained in the incoming signal, the second radionavigation signal comprising a second carrier at a second frequency, different from the first frequency, modulated by a second spreading waveform, the second tracking stage comprising a second carrier phase-locked loop with a mixer configured to multiply the incoming signal with a local replica of the second carrier,

wherein the second carrier phase-locked loop comprises a phase discriminator of a beat between the first carrier and the second carrier configured to produce a second error signal arising from a difference between the first phase difference and a second phase difference between the second carrier and the local replica of the second carrier; and

wherein the second phase-locked loop is configured to adjust the phase of the local replica of the second carrier on the basis of the first and second error signals.

2. The device according to claim 1, in which the first phase-locked loop comprises a numerically controlled oscillator controlled by a first filter receiving the first error signal as input.

3. The device according to claim 2, in which the second phase-locked loop comprises a numerically controlled oscillator controlled by the first filter and a second filter receiving the second error signal as input.

4. The device according to claim 3, in which the second filter comprises a Kalman filter, an extended Kalman filter or a particle filter.

5. The device according to claim 1, in which the first and second radionavigation signals are selected from among Galileo E1, E5 and E6 signals or among GPS L5, L2C and L1 signals or among GLONASS L3, G2 and G1 signals.

6. The device according to claim 1, in which the first radionavigation signal is a Galileo E5 signal and in which the second radionavigation signal is a Galileo E1 signal or Galileo E6 signal.

7. The device according to claim 1, in which the first tracking stage comprises a first correlator configured to correlate a local replica of the first spreading waveform with the incoming signal multiplied by the local replica of the first carrier, and in which the phase discriminator of the first carrier determines the first error signal on the basis of a correlation result produced by the first correlator.

8. The device according to claim 7, in which the second tracking stage comprises a second correlator configured to correlate a local replica of the second spreading waveform with the incoming signal multiplied by the local replica of the second carrier, and in which the phase discriminator of the beat between the first carrier and the second carrier determines the second error signal on the basis of the correlation result produced by the first correlator and a correlation result produced by the second correlator.

9. The device according to claim 8, in which the phase discriminator of the beat between the first carrier and the second carrier is configured to use the product of the correlation result produced by the first correlator and of the complex conjugate of the correlation result produced by the second correlator or the product of the complex conjugate of the correlation result produced by the first correlator and of the correlation result produced by the second correlator to produce the second error signal.

10. The device according to claim 9, comprising a third tracking stage of a third radionavigation signal contained in the incoming signal, the third radionavigation signal comprising a third carrier at a third frequency, different from the first and second frequencies, modulated by a third spreading waveform, the third tracking stage comprising a third carrier phase-locked loop with a mixer configured to multiply the incoming signal with a local replica of the third carrier,

the third carrier phase-locked loop comprising a phase discriminator of a beat between the first carrier and the third carrier configured to produce a third error signal arising from a difference between the first phase difference and a third phase difference between the third carrier and the local replica of the third carrier;

and the third phase-locked loop being configured to adjust the phase of the local replica of the third carrier on the basis of the first and third error signals.

11. The device according to claim 10, in which the third phase-locked loop comprises a numerically controlled oscillator controlled by the first filter and a third filter receiving the third error signal as input.

12. The device according to claim 10, in which the second filter comprises a Kalman filter, an extended Kalman filter or a particle filter;

and in which the third phase-locked loop comprises a numerically controlled oscillator controlled by the Kalman filter, the extended Kalman filter or the particle filter.

13. The device according claim 10, in which the third tracking stage comprises a third correlator configured to correlate a local replica of the third spreading waveform with the incoming signal multiplied by the local replica of the third carrier, and in which the phase discriminator of the beat between the first carrier and the third carrier determines the third error signal on the basis of the correlation result produced by the first correlator and of a correlation result produced by the third correlator.

14. The device according to claim 13, in which the phase discriminator of the beat between the first carrier and the third carrier is configured to use the product of the correlation result produced by the first correlator and of the complex conjugate of the correlation result produced by the third correlator or the product of the complex conjugate of the correlation result produced by the first correlator and of the correlation result produced by the third correlator to produce the third error signal.

15. The device according to claim 1 embodied by a digital signal processor.

16. A GNSS receiver comprising one or more radionavigation signal tracking devices according to claim 1.

17. A positioning and/or dating device including a GNSS receiver according to claim 16.

18. The device according to claim 1, comprising a third tracking stage of a third radionavigation signal contained in the incoming signal, the third radionavigation signal comprising a third carrier at a third frequency, different from the first and second frequencies, modulated by a third spreading waveform, the third tracking stage comprising a third carrier phase-locked loop with a mixer configured to multiply the incoming signal with a local replica of the third carrier,

the third carrier phase-locked loop comprising a phase discriminator of a beat between the first carrier and the third carrier configured to produce a third error signal arising from a difference between the first phase difference and a third phase difference between the third carrier and the local replica of the third carrier;

and the third phase-locked loop being configured to adjust the phase of the local replica of the third carrier on the basis of the first and third error signals.